1967 Beech D55

replacementRemoved and replaced ELT battery in Artex ELT 345 with new battery P/N A3-06-2883 Rev F, S/N 1033547-030. New battery expiration 08/2033 marked on ELT exterior per FAR 91.207(c). Performed ELT self-test per manufacturer's instructions; test satisfactory.

replacementRemoved and replaced right engine fuel flow transducer with new JPI P/N 700900-1, S/N 254856. Set right engine fuel flow K-factor to 29.67 in JPI EDM 790 and the right side of the Shadin Digiflow. Leak and function check good.

ad complianceLubricated uplock rollers per AD 2007-08-08. Next due Hobbs 2635.3. Inspected left and right engine mounts per AD 91-15-20; no cracks noted. Next due Hobbs 2635.3. Complied with AD 76-07-12 by visual verification of ignition switch part number label and function test of both ignition switches; key removable in OFF position only. Next due Hobbs 2635.3. Nothing follows.

annualAnnual inspection this date. Installed new 131553-4M and 131553L-4M rod ends on both aileron actuating tubes. Installed new 45-135039-3 aileron tab actuating arm and new attach hardware. Installed new 131553-6M rod ends on both elevator actuating tubes. Fuel strainers cleaned and reinstalled. Installed new left aux tank CCA1550 quick drain valve. Cleaned bug debris from right main tank flush vent and anti-siphon vent. Set left side of Shadin fuel flow indicator to 29.13 K-factor to match new left engine transducer. Installed new Michelin Air 6.50-8-8 PR main wheel tires. Bearings cleaned and repacked. Resealed both brake calipers and right master cylinder. System bled. Adjusted main gear up stops. Adjusted left engine gear warning horn switch to actuate. Installed new BA6205 induction air filter elements. Installed new M-111 EGT probe left engine #2 cylinder. Installed used serviceable OEM CHT probe #2 right engine cylinder. Removed both instrument air pumps and associated plumbing from engine compartments. W&B revised. C/W AD 76-07-12 (Mag Switches) by test. Next due HM 2583. C/W AD 91-15-20 (Engine Mounts) by inspection. Next due 2583. C/W AD 2007-08-08 (Uplock Rollers) by inspection and lube. Next due 2583. C/W FAR 91.207 (d) on ELT. Next due 04/27. I certify that this Aircraft has been inspected in accordance with the requirements of FAR 43, App. D and Maintenance Manual for an Annual inspection and determined to be in an airworthy condition.

ad complianceComplied with AD 07-08-08 Lubricated main landing gear uplock rollers and ensured freedom of movement. Complied with AD 91-15-20 engine mount visual inspections per SB 2362, No defects noted. Installed customer supplied FF transducer on left engine. P/N: 700900-1 S/N: 241643. Leak and function check good. Installed serviceable drain valve on the left aft induction tube on the left engine. Leak and function check good. Maintenance Release: The aircraft and/or component(s) on 18MD was repaired and inspected in accordance with current rules of the Code of Federal Regulations and was found Airworthy for return to service. Pertinent details of the repair are on file at this repair station under Work Order No. 11676-08-2025, Dated 08-21-2025.

repairCentury ID 395 autopilot computer was repaired by Autopilots Central. Ground Ops check satisfactory.---ENO------ The component identified above was repaired, installed and inspected IAW Federal Aviation Regulations and was found to be in an airworthy condition for return to service. Dated: 04/17/2025 N18MD Beech D55 S/N TE-455. For more info see w/o #39341A

annualComplied with AD91-15-20 and SB NO 2362, rev 1, by cleaning the engine mount frames and visually inspecting, performed dye penetrant inspection on a few suspect areas, no defects noted, next due 2466.9 Hobbs. Complied with AD76-07-12 by visual verification of ignition switch part number label and function test of both switches, due 2466.9 Hobbs. Remarked right fuel gage with yellow arc in accordance with AD72-11-02, verified the other placarding required in the AD are still installed. Complied with AD2008-12-17 by visual verification that each breaker switch is not listed by part number in this AD, no further action required. Repaired nose gear light bracket by welding, epoxy primed and painted white, reinstalled and verified operation. Replaced the two lower pilots instrument panel shock mounts, 150-PL-8. Sandblasted corrosion in battery box and painted with acid proof paint. Re-rigged left inboard gear door to fair to lower wing skin. Converted rear seats from premium recline to base model recline, used a combination of new and used parts as needed to conform to applicable IPC. Converted copilots seat to premium recline using a combination of used and new parts as needed to conform to the IPC, repaired pilots seat reline system as needed. Removed Janitrol heater and blower assembly, heater overhauled by Aircraft Heating and Electrical of Redding California, see 8130-3, they also installed a new motor in the blower housing, test ran and verified operation, this heater has no applicable AD's at this time. Both trim tab actuators overhauled by Crusieair, replaced trim tab components as needed and verified rigging. Stop drilled crack in left wing tip trailing edge. Stop drilled crack in lower left aileron skin. Removed both elevators to facilitate replacement of the outboard hinges (PN:35-650121-4), the old hinges were incorrectly riveted with oversized holes, disassembled left elevator tip weight assemble so that the elevator could be used to jig the hinges on both sides, reassembled left elevator and verified balance to be within limits. Replaced both throttle warning switch's, they still need rigged to manifold pressure determined during test flight. Replaced Vacuum garter and nacelle canister filters. Performed battery capacitance test, passed, next due 1-2026. Replaced brake discs, caliper shims and linings. Replaced 2 flexible brake lines on the right gear and one on the left gear with new, replaced o-rings in both brake calipers with new and bled brakes. Replaced brake disks, linings and shims. Rekeyed the baggage door and main cabin door to match main power switch. Lubricated internal components of both the baggage and main cabin door. Replaced Tail nav light bulb GE305. Replaced tab on one wing bolt cover. Replaced ships CHT probes on both engines and verified correct operation. Removed entrance step, welded cracks as needed, treated corrosion on skin under step and reinstalled. Tightened EGT probes as needed and verified they are all installed at the same depth. Replaced serval loose rivets in the trailing edge of the left nacelle with cherry rivets. Performed routine service and lubrication. Checked all controls for proper travel and cable tensions all operations normal through 3 retraction and extension cycles and one emergency extension. Complied with FAR 91.207d, no defects found, next due 2-2026. ELT battery due 10-2026. Cleaned, inspected and replaced wheel bearings. Replaced missing storm window placard. Corrected discrepancies in weight and balance report and added report to aircraft records. All operations normal on test run. I certify this aircraft has been inspected in accordance with FAR 43 app. D, Annual/100 Inspection criteria and determined Airworthy.

inspectionPerformed conformity inspection of the following STC's, found to conform and completed form 337: Rosen sun visors, STC SA3599NM. Brackett Aero filters, STC SA71GL. D'Shannon cooling baffles, left engine, SA09220SC. Saden fuel flow system, SA486GL. JPI EDM 830, SA2586NM

alteration1) Removed the existing compass system and HSI, GPSS interface and attitude gyro including all hoses, fittings and brackets/racks/mounting assemblies, wiring and mounting racks as needed. 2) Installed dual Garmin GI275 Multifunction Instruments, S/N 5MZ204562 and 5MZ204322 configured as a primary ADI and an HSI IAW STC SA02658SE dated 13 January 2020 & Garmin GI 275 Part 23 AML STC Installation Manual (IM) P/N 190-02246-10, Rev 17 dated August 2023. These were mounted in the pilots' instrument panel. The HSI has a back-up battery installed. A new GMU 11 magnetometer S/N 56J122523 mounted in the empennage, provides heading information to the system, and a GTP 59, S/N 47995607 provides outside air temperature to the system. A Garmin GSB15 USB charger assembly S/N: 63M261196 provides data transfer interface. The ADI/HSI interfaces to the existing Century III autopilot, GNS 530W and the audio system. See FAA Form 337 dated January 30 2025, for Installation Details, Data and Approval. 3) The existing GNS 530W, S/N 23802879 was removed to Garmin for Com repair. Received repaired unit, installed and ops checked satisfactory. Garmin 8130-3 #RMA1913115657 dated 11 October 2024 refers. 4) Removed the existing DME system including the receiver, coax cable, wiring and display. Removed the existing Argus 5000 GPS. 5) Carried out a compass swing and provided a new correction card. 6) Performed data correspondence testing per 91.217, and Performed FAR 91.411 Altimeter static system and altitude reporting equipment test and inspection per FAR 43 appendix E and F to 20,000 feet. GI275 S/N's 5MZ204562 and 5MZ204322 provide primary altimeter information. United instrument S/N 433119 provides standby altimeter information. Transponder GTX 330ES S/N 84100336 and SSD120 encoder S/N 15406. a. A new Weight and Balance document was prepared. Equipment list is updated. The aircraft, or appliance(s) identified above was repaired and inspected in accordance with the current maintenance rules of the Federal Aviation Regulations and is approved for return to service. Pertinent details of the work performed are on file at this repair station under Work Order #1914.

ad complianceLubricated uplock rollers per AD 2007-08-08. Next due Hobbs 2411.5. Inspected Left and Right engine mounts per AD 91-15-20, no cracks noted. Next due Hobbs 2411.5. ~~~ Nothing follows ~~~

repairReplaced LH fuel boost pump. Repaired LH oil temperature cannon plug. Repaired RH Tach Generator cannon plug. Replaced RH vacuum pump. Repaired LH & RH lower eng cowl bug. Replaced brake linings. Repaired & sealed both brake calipers. Changed oil LH & RH eng & replaced filters. Engines run and checked OK.

annualCompleted annual inspection per service manual and FAR 43 appendix D. ELT was inspected IAW FAR 91.207(d) (1-4), battery due 10/2026. C/W AD 2007-08-08 effective 5/25/2007 lubrication of up lock rollers, next due tach: 2315. C/W AD 91-15-20 effective 9/3/1991 engine mount inspection, no defects noted, next inspection due at tach: 2315. C/W AD 2023-09-09 effective 7/17/2023 DNA by part not installed. C/W AD 2023-10-02 effective 5/26/2023, DNA by part not installed. C/W AD 2022-03-15 effective 3/21/2022 DNA by part not installed. Replaced the RH engine mounts with new. Replaced the landing gear motor with overhauled P/N: 58-380090 S/N: AA14091 (see respective release certificate near this date). Replaced the landing gear spur and pinion with new P/N: 35-810135. Removed the RH brake cylinder, clean, inspect, replace o-rings, reinstall and bleed. Replaced the rear seat cabin heat SCAT tubing. Secured the LH landing gear door actuator rod end bearing. Replaced the LH landing gear uplock cable with new P/N: 35-815109. Secured the LH oil temp probe. Secure the LH exhaust hanger. Installed alternator exhaust tubes. I certify this aircraft was inspected IAW an annual inspection and was determined to be in airworthy condition.

repairRemoved left engine cowlings. Cleaned cowlings. Installed new hose clamp on breather hose to overboard exit tube. Installed new hose clamp at fuel control blast hose. Installed new terminal ends on alternator field wires. Removed induction balance tube. Adjusted position of balance tube support bracket. Reinstalled balance tube. Checked clearance of propeller governor control arm, checks good. Removed starter 646275-1 serial number T01CA066R. Installed overhauled starter 646275-1 serial number H-P-272009. Installed new baffle attach screws as needed. Installed new vacuum pump inlet filter B3-5-1. Removed alternator and reinstalled with new gasket.

repairRemoved engine IO-550-C serial number 684240 for repairs. Removed propeller PHC-C3YF-2UF/FC7663B-2R for repairs. Installed repaired engine IO-550-C serial number 684240. Reinstalled original engine shock mounts, engine mount bolts, exhaust and baffles. Serviced engine with Aeroshell 100 mineral oil. Installed overhauled propeller PHC-C3YF-2UF/FC7663B-2R serial number EB8411A. Installed 2 new nut plates on spinner bulkhead. Ground run, leak and operational checks good. Checked idle speed, mixture, magneto drops. Performed full power ground run and checked RPM, MAP and fuel flow.

replacementReplaced weak avionics master breaker-switch with new 35A TE W31-X2M1G-35. Operation check successful. ~~~ Nothing follows ~~~

other1. Removed left alcohol discharge tube and installed AN4 cap on elbow. 2. Labeled prop anti-ice switch INOP. This aircraft is determined to be airworthy with respect to the maintenance performed as described above.

replacementRemoved LH MLG tire assembly. Installed new tube P/N 092-337-0 and tire P/N 301-036-006 S/N 160929. Cleaned, inspected, and repacked wheel bearings. Installed new oxygen charging valve P/N 268?5-48 -- no leaks detected. This aircraft is approved for return to service with respect to the above work performed. W.O. 9677

ad compliance1. Complied with AD 91-15-20. No abnormalities noted. 2. Complied with AD 2007-08-08. Examined and lubricated lockup roller bearings with Mobile SHC 100. No abnormalities noted. All maintenance completed AIW Beechcraft Service Instruction No. 0488-211, Rev. 1 and Beechcraft Mandatory Service Bulletin No. 2362, Rev 1. Next required inspection and service to be performed at or before Hobbs: 2230.8 and/or TTAF 5198.5. This aircraft is determined to be airworthy with respect to the maintenance performed as described above.

ad complianceComplied with AD 90-08-14 and Raytheon MSB 53-2269 rev. 2 via instructions incorporated therein. No cracks noted in spar web faces from visual or NDT inspection. Next inspection due 2594.2. Repaired minor leak at emergency landing gear crank flange seal. ~~~ Nothing follows ~~~

repairT/S RH engine #2 CHT intermittent operation. Found insulation had been melted off. Repaired and secured away from exhaust pipe. Adjusted LH oil pressure in one full turn. Cleaned LH alternator wire connections. Tightened connections as necessary. Inspected manual gear extension handle for overservicing -- no defects noted. This aircraft is approved for return to service with respect to the above work performed. W.O. 9623

annualCompleted annual inspection per service manual and FAR 43 appendix D. ELT was inspected IAW FAR 91.207(d) (1-4), battery due 10/2026. C/W AD 2007-08-08 effective 5/25/2007 lubrication of up lock rollers, next due tach: 2134. C/W AD 91-15-20 effective 9/3/1991 engine mount inspection, no defects noted, next inspection due at tach: 2134. Secured the LH engine controls. Minor sheet metal repair to the RH #6 cylinder baffling. I certify this aircraft was inspected IAW an annual inspection and was determined to be in airworthy condition.

replacementRemoved GEM 1200 engine analyzer, wiring, and probes. Installed new JPI790 engine analyzer, wiring, and probes for both engines using JPI Installation manual 8-1-14 Rev. B. W/B change is negligible. Removed left engine due to time. Installed zero-time exchange engine from Western Skyways. Installed overhauled propeller from Johnson Propeller. Test run satisfactory. ~~~ Nothing follows ~~~

replacementWork Performed: Replaced right main tire and tube with owner provided parts. Tire is Goodyear Flight Custom 301-035-006 6.50-8 tire. Replaced outboard wheel bearing with 13889 and race with 13836. Wheel bearings packed with SHC 100.

annualCompleted annual inspection per service manual and FAR 43 appendix D. ELT was inspected IAW FAR 91.207(d) (1-4), battery due 10/2026. C/W AD 2007-08-08 effective 5/25/2007 lubrication of up lock rollers, next due tach: 2030. C/W AD 91-15-20 effective 9/3/1991 engine mount inspection, no defects noted, next inspection due at tach: 2030. Secured the LH prop control rod end. Secured the engine controls. Secured the LH vacuum pump outlet hose. Secured the RH engine tach generator plug. Secured the RH engine fuel control blast tube. Secured the RH engine ground. Re-worked both spinners forward nutplates. Replaced brake linings. Removed the nose landing gear assembly, cleaned, inspected, replaced parts as required, overhauled the strut assembly and reinstalled (P/N's: 130909B102, 60-820032-3, 60-820032-1, 60-820032-5, 60-820039, nose strut overhaul kit). I certify this aircraft was inspected IAW an annual inspection and was determined to be in airworthy condition.

repairTroubleshoot out of tolerance leak in static system and found multiple bad fittings aft of pilots panel, and a case leak in the Airspeed Indicator. Removed Airspeed Indicator for overhaul and sent in to Airtech under PO 21-PCA-2700. Reinstalled repaired unit and replaced fittings aft of pilot panel. Work performed IAW Beech D55 maintenance manual to meet the requirements of 14 CFR 23.1325. NDN. Interfaced Shadin Fuel Flow Indicator to Garmin GNS 530W IAW G530W installation manual 190-00357-06 Rev D, dated Mar 2002. NDN. Performed 14 CFR 91.411 certification of the altimetry system. The altimeter, static system, and altitude reporting system have been tested and found to meet the requirements of 14 CFR Part 43 Appendix E to a pressure altitude of 20,000 feet. Performed 14 CFR 91.413 certification of the Garmin GTX 330ES Transponder s/n 84100336 and found the transponder to meet the requirements of 14 CFR Part 43 Appendix F. This aircraft has been inspected in accordance with current federal aviation regulations and found to be airworthy with respect to the work performed. Details will be on file at Pacific Coast Avionics under Mike Brannigan, work order 21-4379. CRS OPXR455L

otherWeight and Balance, N18MD, Beech D55 TE-455. Aircraft Former Empty Weight 3419.65, arm 78.85, moment 270076.30. Remove 4 x Hoses for Factory Fuel Gauge -2.34 (arm 37.00, moment -86.58). Remove Dual Contol Arm -10.60 (arm 68.00, moment -720.80). Remove Factory Fuel Pressure Gauge -1.20 (arm 58.50, moment -70.20). Install Single Control Arm 3.90 (arm 68.00, moment 265.20). Install Shadin Fuel Flow Gauge 1.00 (arm 58.50, moment 58.50). New Aircraft Empty Weight 3410.41, arm 79.03, moment 269522.42. Configuration Two (five seats, full alcohol) Empty Weight 3398.21, arm 78.77, moment 267668.02. Configuration Three (four seats, full alcohol) Empty Weight 3385.01, arm 78.48, moment 265661.62. Configuration Four (six seats, no alcohol) Empty Weight 3389.41, arm 79.44, moment 269244.17. Configuration Five (five seats, no alcohol) Empty Weight 3389.41, arm 78.89, moment 267389.77 s. Configuration Six (four seats, no alcohol) Empty Weight 3364.01, arm 78.89, moment 265383.37. Gross weight and useful load: not shown.

alterationRemoved factory fuel pressure gauge p/n United Instruments 6221 serial number K12240. Installed Shadin Avionics Digiflo-L Fuel computer p/n 910532P s/n 9626 in accordance with SA486GL and Shadin Company Report 4023. Drained factory fuel pressure lines and sealed with caplugs and AN929-4 fittings. Dual control arm and copilot yoke removed and replaced with single Beech control arm. AD 71-24-10R1 N/A by control yoke part number. New weight and balance generated by computation. Ground checked, ground run, and test flown, all found satisfactory. ~~~ Nothing follows. ~~~

alterationReplaced 2 x Concorde RG25 ship batteries with 2 x Concorde RG25XC batteries. Installed BM-AIK2 Battery Minder charge port in nose baggage compartment avionics shelf area. Fabricated & installed 2-wire battery charger connection harness using MIL-W-22759/16 wire with 10A inline circuit protection fuse. Attached to battery relay and airframe ground with ring terminals. Terminated opposite end with Anderson SB50 plug with protective cover. All work IAW AC43.13/1B. Verified continuity, polarity, tested with charger and for proper aircraft electrical system operation. Ground function check, test flown, all found satisfactory. ~~~ Nothing follows. ~~~

alterationUpdated Garmin GNS 530W s/n 23802879 to main software version 5.4 IAW with Garmin Service Bulletin 1766 Rev A. NDN. Unit installed on top of copilots glovebox and receives power from an inline 1A fuse. NDN. Installed Flight Stream 210 p/n 011-03257-40 s/n 3RE008869 IAW Garmin manual 190-01700-00 Rev G. This aircraft has been inspected in accordance with current federal aviation regulations and found to be airworthy with respect to the work performed. Details will be on file at Pacific Coast Avionics under John Brannigan, work order 20-907. CRS OPXR455L

annuali certify this airframe identified above was inspected in accordance with an Annual inspection and was found to be in an airworthy condition. Ran electrical check, cleaned fuel strainer, lubricated all points and repacked wheel bearings. Complied with FAR 91.207 paragraph (C) & (D) on ELT. Replaced (2) BA-6205 Air filters. Replaced (8) APS066-04400 Brake linings on left and right main gear. Replaced (2) RA-B3-5-1 Tempest garter air filter. Serviced propeller accumulators with Nitrogen. Removed and reinstalled oxygen bottle after hydro static inspection by A to Z cylinders. Removed and resealed brake calipers. Replaced o-rings P/N MS28775-222. Removed and reinstalled nose landing gear strut after overhaul. Replaced o-rings included in reseal kit P/N NG58SS-K1, serviced with Nitrogen and 5606H hydraulic fluid. Adjusted landing gear tensions to specification. Adjusted knee to skin clearance on landing gear to specification. Adjusted uplock and downlock tensions to specification. Replaced (2) 45-815091-3 Springs on landing gear retract rod, installed with (2) MS20392-3C33 Pins. Serviced landing gear box with Mobile 636 oil. Removed and reinstalled right inner gear door after adjustment, replaced mounting hardware. Replaced (1) 35-810122-1 Bushing on right main gear knee. Replaced (1) ADNEL6-317 Rod end and (1) ADNE5-323 Rod End on forward nose gear retract rod. Replaced (1) 104-820050-3 Arm on nose gear aft retract rod, installed with (1) AN26-28 Bolt & (1) MS16624-1131 Retaining Ring. Replaced (1) 35-825188 Spring on nose gear downlock, replaced (1) MS20392-2C29 Clevis Pin. Adjusted nose gear uplock tensions

replacementRemoved defective Artex ELT45 and replaced with new Artex 345 serial number 317-01340 and new ELT Battery p/n A3-06-2883 serial number 382910-045 Revision E. NEW ELT BATTERY EXPIRATION OCT 2026. Performed ELT check, 91.207 check, and test flown, all found satisfactory. ~~~ Nothing follows. ~~~

replacementRemoved defective Artex ELT45 and replaced with new Artex 345 serial number 317-01340 and new ELT Battery p/n A3-06-2883 serial number 382910-045 Revision E. NEW ELT BATTERY EXPIRATION OCT 2026. Performed ELT check, 91.207 check, and test flown, all found satisfactory. ~~~ Nothing follows. ~~~

otherSeptember 16, 2019 N18MD Hobbs 1807.0 Airframe. Installed new I/B exhaust, RH engine: K96-950002-57, S/N 271200; K96-950002-7, S/N 268013; K96-950002-9, S/N 268027. Replaced RH throttle position switch, flight check required. Cleaned and lubricated stall warning switch, flight check required. CWCR, checked nose gear door rigging, sat. Installed BAS shoulder harnesses in front row, see form FAA-337 & weight & balance / equipment list amendment, both this date. Operational inspection of affected systems sat.

annual01/07/2019 HOBBS: 1776.1 TTAF: 4743.8 Ser# TE-455 N18MD. Annual Inspection completed this date with reference to Beechcraft Service Manual. Lubricated control surfaces and pulleys. Performed landing gear retract test and alignment checks. ELT inspection and 91.207 test performed; battery due 10/2023. C/W AD 07-08-08 MLG uplock rollers. C/W AD 91-15-20 Engine Mount Inspection. C/W AD 76-07-12R1 Ignition Switches. See AD Compliance Listing dated 12/21/18. I certify that this airframe has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition. Douglas Durning A&P-IA 3275089

annual12/16/2017 HOBBS: 1749.6 TTAF: 4717.3 Ser# TE-455 N18MD. Annual Inspection competed this date with reference to Beechcraft Service Manual. Lubricated control surfaces and pulleys. Performed landing gear retract test and alignment checks. ELT inspection and 91.207 test performed; battery due 10/2023. C/W AD 07-08-08 MLG uplock rollers. C/W AD 91-15-20 Engine Mount Inspection. C/W AD 76-07-12R1 Ignition Switches. See AD Compliance Listing dated 12/16/17. I certify that this airframe has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition. Douglas Durning A&P-IA 3275089

replacementReplaced L/H Auxiliary fuel pump with O/H unit P/M 4404-00-7NV. See aircraft records for 8130. Ops check good.

replacementReplaced MLG & NG tires with new Goodyear Flight III. Replaced caliper seals & brake linings with new parts. Douglas Durning A&P-IA 3275089

replacementReplaced R/H auxilary fuel pump with O/H unit P/M 4404-00-7NV. See aircraft records for 8130. Ops check good. Douglas Durning A&P-IA 3275089

annual12/2/2016 HOBBS: 1726.8 TTAF: 4694.5 Ser# TE-455 N18MD. Annual Inspection competed this date IAW Beechcraft Service Manual. Lubricated control surfaces and pulleys. Performed landing gear retract test and alignment checks. Replaced ELT with new Artex 345 406 MHZ unit. Installed remote cockpit switch IAW Manufacturer instructions. ELT inspection and 91.207 test performed; battery due 10/2023. C/W AD 07-08-08 MLG uplock rollers. Replaced L&R fuel strainer seals. C/W AD 91-15-20 Engine Mount Inspection. C/W AD 76-07-12R1 Ignition Switches. See AD Compliance Listing dated 12/02/16. I certify that this airframe has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition. Douglas Durning A&P-IA 3275089

alterationLOG ENTRY, N18MD, BEECH D55, S/N TE-455, TACH: 1700.8. REMOVED KING KT-76 TRANSPONDER, INSTALLED CUSTOMER FURNISHED, GARMIN GTX-330ES, (ADSB OUT) TRANSPONDER, AS PER FAA STC # SA01714WI, DATED MAY 1 2013, SEE FAA FORM 337 THIS DATE FOR DETAILS, WEIGHT CHANGE NEGLIGABLE. REPAIR AND INSPECTION PREFORMED IN ACCORDANCE WITH CURRENT FAA REGULATIONS AND WAS FOUND AIRWORTHY FOR RETURN TO SERVICE. DETAILS OF THIS REPAIR ARE ON FILE AT THIS AGENCY UNDER W.O.#, 16289. AVIONICS SERVICES INC., CRSAT2R702K, NORMAN OKLAHOMA. PHILIP STEELE DATE 7/18/16

inspectionTHIS TRANSPONDER SERIAL NUMBER 84100336 HAS BEEN TESTED IN ACCORDANCE WITH F.A.R. PART 43, APPENDIX F, AND MEETS THE REQUIREMENTS OF F.A.R.91.413. DATE: 7/18/2016 SIG. [signature] CRS AT2R702K AVIONICS SERVICES INC. NORMAN, OKLAHOMA

inspectionThis transponder serial number 37134/KT-76 has been tested in accordance with F.A.R. Part 43, Appendix F, and meets the requirements of F.A.R. 91.413.

inspectionINSTALLED ALTIMETER, MODEL 5934P-3, S/N 433119, CERTIFIED UNDER PART 43, APPENDIX E, AND TESTED AS PER 91.411 TO 20,000 FEET ON 3/21/2016 BY AT2R702K W.O. 16237. I CERTIFY THE STATIC SYSTEM TEST REQUIRED BY F.A.R. PART 91.411, HAVE BEEN PREFORMED. THIS DATE 3/21/16 SIG [signature] AVIONICS SERVICES INC. CRS AT2R702K

inspectionTHIS TRANSPONDER SERIAL NUMBER 37134/KT-76 HAS BEEN TESTED IN ACCORDANCE WITH F.A.R. PART 43, APPENDIX F, AND MEETS THE REQUIREMENTS OF F.A.R.91.413. DATE: 3/21/2016 SIG. [signature] CRS AT2R702K AVIONICS SERVICES INC. NORMAN, OKLAHOMA

annualAnnual Inspection competed this date IAW Beechcraft Service Manual. Lubricated control surfaces and pulleys. Replaced Aileron Rod End Bearings. R&R MLG Gear Doors for Painting. Performed landing gear retract test and alignment checks. ELT inspection and 91.207 test performed; battery replaced due 01/2017. C/W AD 07-08-08 MLG uplock rollers. C/W AD 91-15-20 Engine Mount Inspection. C/W AD 76-07-12R1 Ignition Switches. See AD Compliance Listing dated 10/28/15. I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

replacementREPLACED A/C BATTERIES WITH NEW CONCORDE 25AMP

otherCV1J4 Filter Installation Record (Include with A/C Maintenance Records). A/C "N" No. 18MD. Engine: L/H. Date Installed: 4/16/2015. Installed By: D Durning. FAA-PMA Ser No. 011686.

otherCV1J4 Filter Installation Record (Include with A/C Maintenance Records). A/C "N" No. 18MD. Engine: R/H. Date Installed: 4/16/2015. Installed By: D Durning. FAA-PMA Ser No. 011692.

replacementREMOVED ARTIFICIAL HORIZON. REPLACED WITH O/H 52D67 PART FROM AIRCRAFT QUALITY INSTRUMENTS, INC. SERIAL # 574SBX. OPS CHECK GOOD.

replacementREPLACED AIRCRAFT BATTERIES WITH NEW GILL G255

annualAnnual Inspection competed this date IAW Beechcraft Service Manual. Lubricated control surfaces and pulleys. Adjusted control cable tensions per service manual. Performed landing gear retract test and alignment checks. ELT inspection and 91.207 test performed; battery replaced due 01/2017. Installed new seals L/H MLG Strut. C/W AD 07-08-08 MLG uplock rollers. C/W AD 91-15-20 Engine Mount Inspection. C/W AD 76-07-12R1 Ignition Switches. C/W AD 90-08-14 Wing Spar Structure. See AD Compliance Listing dated 11/04/14. I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

inspectionALTIMETER INDICATOR CALIBRATION. Serial No. 433119, W/O 15785, 3/11/14. Test setting / Inst. reading: -1000 / -1020; 0 / -10; 500 / 490; 1000 / 1000; 1500 / 1500; 2000 / 2000; 3000 / 3000; 4000 / 4000; 6000 / 6010; 8000 / 8015; 10000 / 10,020; 12000 / 12,040; 14000 / 14050; 16000 / 16060; 18000 / 18105; 20000 / 20110. Altimeter Mod. 5934P-3 certified under Part 43, tested as per 91.411 to 20K feet on 3/11/14, W.O. No. 15785. I certify the static system tests required by F.A.R. Part 91.411 have been performed this date 3/11/14. CRS AT2R702K. Mechanic and inspector signatures present, names not legible.

inspectionINSTALLED ALTIMETER, MOD. 5934P-3, S/N 433119, CERTIFIED UNDER PART 43, APPENDIX E AND TESTED AS PER 91.411 TO 20K FEET ON 3/11/14, BY AT2R702K, W.O. NO. 15785. I CERTIFY THE STATIC SYSTEM TESTS REQUIRED BY F.A.R. PART 91.411 HAVE BEEN PERFORMED THIS DATE: 3/11/14 SIG. CRS AT2R702K. TRANSPONDER SERIAL NUMBER 37134 / KT76A HAS BEEN TESTED IN ACCORDANCE WITH F.A.R. PART 43, APPENDIX F, AND MEETS THE REQUIREMENTS OF F.A.R. 91.413. DATE: 3/11/14. CRS AT2R702K, AVIONICS SERVICES INC., NORMAN, OKLAHOMA.

replacementReplaced MLG brake rotors with new RAPCO P/N BA1164-027DL & new brake linings P/N RAKE-44. Lubricated all wheel bearings. Doug Durning A&P-IA 3275089

annualAnnual Inspection competed this date IAW Beechcraft Service Manual. Lubricated control surfaces and pulleys. Performed landing gear retract test and alignment checks. ELT inspection and 91.207 test performed; battery due 01/2015. Replaced elevator bearings and hardware. C/W AD 07-08-08 MLG uplock rollers. C/W AD 91-15-20 Engine Mount Inspection. C/W AD 76-07-12R1 Ignition Switches. See AD Compliance Listing dated 11/09/13. I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

annualAnnual Inspection competed this date IAW Beechcraft Service Manual. Lubricated control surfaces and pulleys. Performed landing gear retract test and alignment checks. ELT inspection and 91.207 test performed; New BP-1010 battery installed; due 01/2015. Replaced brake linings with new P/N 66-044. C/W AD 07-08-08 MLG uplock rollers. C/W AD 91-15-20 Engine Mount Inspection. C/W AD 76-07-12R1 Ignition Switches. See AD Compliance Listing dated 11/02/12. I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

otherREMOVED O2 BOTTLE FOR RECERTIFICATION HYDROSTATIC TEST PERFORMED BY CITY CARBONICS. SEE A/C DOCUMENTS FOR INVOICE. REINSTALLED & RECHARGED O2 SYSTEM. NO LEAKS DETECTED. RECERTIFICATION NEXT DUE 5/2017. Doug Durning A&P-IA 3275089

replacementREPLACED AIRCRAFT BATTERIES WITH NEW GILL G-355. CLEANED BATTERY BOX.

inspectionTransponder #1 Mfg by King, Model No. KT-76, S/N 37134 has been tested, inspected, and found to comply with FAR 91.413. Reference W.O. 87815 by Nick Knight. Date 2-16-12. Altimeter #1 Mfg by United Instr., Model No. 5934P-3, S/N 43319 has been certified by Nick Knight on 2.20.12 to an altitude of 20 thousand feet. Static/Encoding system inspected, tested, and found to comply with FAR 91.411. Reference W.O. 87815 by Nick Knight. Date 2.20.12. Altimeter Indicator Calibration table, Serial No. 43319, signed by Mechanic and Inspector Nick Knight, dated 2/20/12.

replacementREPLACED MAIN GEAR & NOSE WHEEL TIRES WITH NEW GOODYEAR FC III TIRES. HUBS CLEANED & REPAINTED. BEARINGS LUBRICATED. Dany Durning A&P-IA 3275089

annualAnnual Inspection competed this date IAW Beechcraft Service Manual. Lubricated control surfaces and pulleys. Performed landing gear retract test and alignment checks. Serviced oleo struts. ELT inspection and 91.207 test performed; battery due 12/2012. C/W AD 07-08-08 MLG uplock rollers. C/W AD 91-15-20 Engine Mount Inspection. C/W AD 76-07-12R1 Ignition Switches. See AD Compliance Listing dated 11/11/11. I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

alterationREMOVED DUAL PHASE ALCOR EGT GAUGE. INSTALLED NEW INSIGHT GEM 1200 ENGINE MONITOR. WORK PERFORMED I/A/W MANUFACTURERS INSTALLATION MANUAL. NO CHANGE TO W&B.

annualPerformed Annual Inspection this date IAW Aircraft Service Manual. Replaced Landing Gear Motor with overhauled P/N 58-380090-1 see A/C records for 8130-3. Replaced seals in L/H MLG strut and serviced strut. Cleaned Battery Box and Serviced Batteries. Lubricated control surfaces and pulleys. Lubricated landing gear and performed a retract test. ELT Inspection C/W, Battery due 12/2012. C/W AD 72-22-01 MLG uplock rollers, next due at 4382 TTAF. C/W AD 91-15-20 Engine Mount Insp; No cracks found, next due at 4382 TTAF. C/W AD 76-07-12R1 Ignition Switches, next due at 4382 TTAF. I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

replacementREPLACED ELT BATTERY WITH NEW BP-1010. PERFORMED 91.207 TEST. BATTERY DUE 12/2012.

inspectionTransponder #1 Mfg by King, Model No. KT-76, S/N 37134 has been tested, inspected, and found to comply with FAR 91.413. Reference W.O. 87742 by Nick Knight. Date 2-2-10. Altimeter #1 Mfg by United Instr., Model No. 59348-3, S/N 43319 has been certified by Nick Knight on 2-12-10 to an altitude of 20 thousand feet. Static/Encoding system inspected, tested, and found to comply with FAR 91.411. Reference W.O. 87742 by Nick Knight. Date 2-12-10. Altimeter Indicator Calibration table, Serial No. 43319, signed by Mechanic and Inspector Nick Knight.

annualAnnual Inspection complied with this date. All AD's comply at this time. I certify that this A/c was inspected IAW an ANNUAL Inspection and was determined to be in Airworthy Condition. A&P 2596106 IA

100 hourPerformed 100hr. Inspection this date IAW Aircraft Service Manual. Replaced left and right brake caliper seals and installed new RA66-44 Brakes; Bled brakes. Repaired surface corrosion under access step. Cleaned Battery Box and Serviced Batteries. Repaired Deice Fluid Qty Sender. Installed O/H Rapco Vacuum Pumps. Lubricated control surfaces and pulleys. Lubricated landing gear and performed a retract test. ELT Inspection C/W, Battery due 9/2010. C/W AD 72-22-01 MLG uplock rollers, next due at 4324 TTAF. C/W AD 91-15-20 Engine Mount Insp; No cracks found, next due at 4324 TTAF. C/W AD 76-07-12R1 Ignition Switches, next due at 4324 TTAF. I certify that this aircraft has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

ad complianceC/W AD 2008-13-17 CIRCUIT BREAKER SWITCHES.

100 hourPerformed 100hr. Inspection this date IAW Aircraft Service Manual. Replaced left and right flap rod end bushings with new P/N 100801S5-0500. Repaired cracked RH landing gear door clamp with weld. Lubricated control surfaces and pulleys. Lubricated landing gear and performed a retract test. ELT Inspection C/W, Battery due 9/2010. C/W AD 72-22-01 MLG uplock rollers, next due at 4275 TTAF. C/W AD 91-15-20 Engine Mount Insp; No cracks found, next due at 4275 TTAF. C/W AD 76-07-12R1 Ignition Switches, next due at 4275 TTAF. I certify that this aircraft has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

annualAnnual Inspection Completed this date. All ADs in compliance @ this time. I certify that this Aircraft was inspected IAW an ANNUAL Inspection and was Determined to be in Airworthy Condition. [signature and certificate number appear struck through]

replacementREPLACED ELT BATTERY WITH NEW BP-1010. OPS CHECK GOOD. NEXT DUE SEP 2010

replacementREPLACED L/H & R/H PNEUMATIC FILTERS WITH NEW P/N 254-7. REPLACED R/H OUTBOARD ELEVATOR HINGE BUSHING WITH NEW

repairR&R LEFT AUX FUEL BLADDER. TESTED & CERTIFIED BY AERO-TECH SERVICES. 8130-3 ISSUED. NO LEAKS-OPS CHECK GOOD

inspectionTRANSPONDER SERIAL # 37134 HAS BEEN TESTED IN ACCORDANCE WITH F.A.R. PART 43, APPENDIX F, AND MEETS THE REQUIREMENTS OF F.A.R. 91.413. DATE 1/28/08 SIG. [signature]

inspectionTHIS TRANSPONDER SERIAL # 37134 HAS BEEN TESTED IN ACCORDANCE WITH F.A.R. PART 43, APPENDIX F, AND MEETS REQUIREMENTS OF F.A.R. 91.413. I CERTIFY THE STATIC SYSTEM TESTS REQUIRED BY F.A.R. PART 91.411 HAVE BEEN PERFORMED THIS DATE 1/28/08

alterationHobbs 1160.5 Removed Avionics #1 N/C ADF R-Nav. and Northstar GPS Installed New Garmin GNS-530 W with GA 56W Antenna, and Mid-continent MD41 Annunciator as per STC # SA01932LA Installed DAC GDC 31 Roll Steering as per STC # SA1023CSC see FAA forms 337 this date for details. Equipment list and Weight and balance Data revised Airplane Flight Manual Supplements for GNS-530W and GDC 31. Must remain in Aircraft at all times

inspectionALTIMETER SCALE CORRECTION CARD, Altimeter S/N 433119. Standard altitude vs altimeter reading recorded from -1000 ft through 53000 ft (readings written at each standard altitude). Tested by J. Bush, date 01-09-08.

inspectionINSTALLED ALTIMETER, MOD. 5934P-3 S/N 433119 CERTIFIED UNDER PART 43, APPENDIX AND TESTED AS PER 91.411 TO 20,000 FEET ON 1/9/2008 BY: E12R795K W.O. NO. 93564

100 hourPerformed 100hr. Inspection this date IAW Aircraft Service Manual. Replaced right propeller accumulator with overhauled unit P/N #95-380026A. Replaced right alternate air duct with new. Replaced Tail Strobe Lens with new P/N A402R. Replaced pressure pump intake filters with new P/N B-3-5-1. Lubricated control surfaces and pulleys. Lubricated landing gear and performed a retract test. ELT Inspection C/W, Battery due 8/2008. C/W AD 72-22-01 MLG uplock rollers, next due at 4221 TTAF. C/W AD 91-15-20 Engine Mount Insp; No cracks found, next due at 4221 TTAF. C/W AD 76-07-12R1 Ignition Switches, next due at 4221 TTAF. C/W AD 90-08-14 Wing Spar Carry-Through, No cracks found, next due 4621 TTAF. I certify that this aircraft has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

annualCertifying this Aircraft was inspected IAW an ANNUAL Inspection and was Determined to be in Airworthy Condition.

inspectionTransponder #1 Mfg by KING, Model No. KT-76, S/N 37134 has been tested, inspected, and found to comply with FAR 91.413 Reference W.O. 87649 by [illegible]. Date 3-8-07. Altimeter and static/encoding sections left blank.

annualAnnual Inspection completed this date. Jacked aircraft, performed retraction and extension check in both normal and emergency, All checks and clearances normal. Checked ELT battery, next due 9/2008. Luberacated aircraft IAW Beech service manual. I certify that this aircraft was inspected IAW an ANNUAL inspection and was determined to be in airworthy condition.

annualAnnual Insp. Completed this date. Jacked A/C. Performed Retract & Ext in Normal & Emergency All checks Normal. Replaced All tubes & Tires, Installed New Rotors & Brake Pads. Adjusted Nose Landing Gear doors. Lubed A/C IAW Beech service Manual. Installed New 3/8" Windshield. Installed New PS Engineering PMA6000 Audio Panel. All Functional checks good. Inspected ELT Battery due 9/2006. I certify that this A/C was Inspected IAW an ANNUAL Insp. and was Determined to be in Airworthy Condition.

inspectionTransponder #1 Mfg by KING, Model No. KT-76, S/N 37134 has been tested, inspected, and found to comply with FAR 91.413 Reference W.O. 87599 by [illegible]. Date 3-16-05. Altimeter #1 and #2 and static/encoding system sections left blank.

annualOn this date performed an annual inspection using Beech check list. Inspected all controls, systems, attach points and structures. Lubricated in accordance with Beech manual. Ran gear retract test several times and checked gear warning horn per service manual. Performed the following Maintenance: 1. Replaced Lower Skin of Left Horizontal Stabilizer, see 337 in records. 2. Replaced Left Main Wheel Bearings and Races. 3. Replaced Nose Wheel Bearings and Races. 4. Replaced Batteries. 5. Found Hobbs to have not changed since 6/30/03, inspected and repaired bad ground wire. Complied the following AD's: 72-22-01 up lock rollers, 91-15-20 Engine Mount Inspection, 76-07-12R1 mag. switch check, for a complete listing of all AD's see compliance record attached to aircraft records in folder labeled AD compliance record. For other details of work see WO#8794. I certify that this aircraft has been inspected in accordance with an annual inspection and was determined to be in airworthy condition.

replacementOn this date replaced Narco 10 ELT Battery and tested in accordance with FAR 91.207, next replacement due 9/2006. As per customers request, heater has been placarded inop.

repairREPLACED NOSE TIRE (500X5) FLIGHT CUSTOM II AND TUBE. REPLACED RT. OTBD FUEL TRANSMITTER WITH O/H'D UNIT, P/N 95-380013-3. REPAIRED CEILING HANGER STRAP. RUN-UP BOTH ENGINES AND ADJUSTED HIGH/LOW FUEL FLOWS AND IDLE ADJUSTMENTS PER SID 97-3. REMOVED, WELDED, PAINTED AND REPLACED ENTRY STEP WHICH WAS CRACKED. REMOVED, RESEALED AND REINSTALLED BOTH MAIN GEAR BRAKE CALIPERS. TROUBLESHOOT VACUUM SYSTEM AND FOUND BOTH REGULATORS, P/N 2H30-6 BAD. FOUND REGULATORS FULL OF OIL AND SOOT. REPLACED BOTH REGULATORS, CLEANED OUT THE MANIFOLD, REMOVED LINES TO THE GYRO AND CLEANED OUT VACUUM SYSTEM. RUN-UP ENGINES AND OPS CHECKED VACUUM SYSTEM. RETURN TO SERVICE.

repairRelocate Data plate to E/H wing Root position, Cockpit entrance stair cracked, welded 4130 steel with Heliarc welded per AC 43.13-1B 4-74 d and (5) a through (5) ok for service

inspectioncheck E/H brake for leak, cleaned ops ck good ok for service. Investigate E/H prop [illegible] blade [illegible] ... prop log ok for service

inspectionInspect starter vibrator and switching for intermittent kick back E/H engine. Adjust retard breaker to open at proper crankshaft position - all switching verified. Vibrator suspect if persists o/s ok for service. ops ck good

inspectionoil leak R/H engine oil pump cover is Resealed using silkthread method Ref 10-550 O.M. left oil temp plug resoldered. 4H RPM transmitter R&R with overhauled unit. Lubricate Gear Rollers iaw AD 72-22-01 inspected engine mounts for cracking AD 91-15-20 no defect noted left oil service door repaired AD 76-07-12 Bendix FI/C good. I certify this aircraft inspected IAW annual inspection and determined to be in an airworthy condition and ok for continued service. ELT B&H ops ck 1/2 switch good B&H due 9/05.

ad complianceLube MLG uplock Rollers iaw AD 72-22-01 ok for service @100FH

replacement[001] Removed right engine S/N 271786-R and reinstalled after overhaul. See engine log book for details. Overhauled 24V 50A GD alternator P/N 1100723, S/N A108019 installed with serviceable alternator drive gear S/N 223097-72C supplied by customer.

repair[050] Induction air filter replaced on left engine. New P/N BA6205 installed. Induction air filter replaced on right engine. New P/N BA6205 installed. [051] Replaced left engine outboard exhaust stack assembly P/N 96-950002-9, stack P/N 96-950002-7 and exhaust system brace P/N 96-950002-85. [053] Replaced left alternate air duct, installed a new P/N 111716AX6XX30. [054] Pressure pump intake filter P/N B-3-5-1 replaced. [055] Replaced left engine induction crossover drain line, installed a new P/N 96-910001-98.

repair[060] Removed cowling, cleaned, and inspected. Removed broken components. Installed the following new components. Cowl former P/N 58-910011-107, cowl former P/N 58-910011-3, cowl skin P/N 58-91011-122U, cowl reinforcement P/N 96-9100011-205, cowl strips P/N 96-91001-193 and P/N 96-91001-194. Installed the following new exhaust items. Exhaust weld assembly P/N 96-950002-55 and exhaust stack P/N 96-950002-47.

repair[100] Replaced right engine alternate air box door spring, installed a new P/N 35-910288. [200] Replaced o-rings in left and right brake master cylinders. [250] Replaced tail navigation light bulb, installed a new P/N 305. [251] Replaced 1 static wick on the rudder and 1 static wick on the left elevator, installed new P/N 35-5010-3. [275] Replaced bushing and bolt on aileron trim tab. [276] Replaced upper and lower bulbs in right navigation light, installed new P/N MS25309-7512. [278] Static wicks on left and right wings replaced, installed new P/N 35-5010-3.

repair[352] Fabricated, primed, painted and installed nose door actuator bracket. Operationally checked good. [354] Nose gear torque link bushings, bolts and pins replaced.

annualANNUAL INSPECTION - complied with in accordance with the Beech Baron 58 Shop Manual inspection guide.

ad compliance[450] FAR 91.207(d) - annual ELT inspection c/w, no defects noted, operational check was good, battery replacement due June 2002. [452] AD 72-22-01 Landing Gear Uplock Rollers by lubrication per paragraph complied with, next due at 3728.3 hours total aircraft time. [453] AD 89-05-02 Elevator Control Fittings, fittings determined to be of aluminum composition, no further action required per para (a) (1). [454] AD 90-08-14 Wing Spar Structure inspection complied with per para (a), no cracks found, next due at 4128.3 hours total aircraft time. [455] AD 91-15-20 Cracked Engine Mounts inspection c/w per paragraph (a), no cracks found, next due at 3728.3 hours total aircraft time. [456] AD 2000-18-02 Elevator Skin Separation inspection complied with by checking aircraft records per paragraph (d) (1), none of the affected elevator skin assemblies have been installed since December 31, 1998, no further action required. [457] AD 96-20-07 Janitrol Heaters determined to be N/A by heater P/N. [458] AD 2001-17-13 Fuel Regulator Shutoff Valve determined to be N/A by heater P/N and model. [459] Cabin heater pressure test complied with. [461] Left and right fuel selector valve inspection complied with. [462] Landing gear selector switch replaced. New P/N MS25125E3 switch installed. [464] Wing attachment bolts replaced on left and right wings. New bolts, nuts and washers installed. I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in airworthy condition. Pertinent details are on file at this agency under work order PG-01-02872.

inspectionAltimeter test form, N18MD, to 20000 ft. Case leak 0. Altimeter S/N 67H4046, date tested 8-28-01. Scale error readings and friction error recorded at -1000 through 20000 ft; hysteresis up/down readings at 8000 ft (8010/8040) and 10000 ft (9960/9985). Bara scale error block marked O/K. Form notes: static system, altimeter instruments and automatic pressure altitude reporting system tested and inspected to 20000 ft. Transponder KT-76 SN 37134. Alt enc S/N 24566. Pertinent details on file under W/O AG-01-02479. Also shows partial text: 'EL CELL LEAKING... INSTALLED NEW ... -9009 -2S, SERIAL ... SATISFACTORY' (continuation of 1-18-2001 entry).

inspectionI certify that the static pressure system, altimeter instruments, and automatic pressure altitude reporting system have been tested and inspected as required by FAR 91.411, Part 43, Appendix E & F. Static system test date 8/28/01 to 20000 ft. #1 Alt model 22-374-B01 S/N 67H4046. Alt enc model [blank] S/N 24566. This transponder has been tested and inspected and found to comply with FAR 91.413, Part 43, Appendix F. #1 model KT-76 S/N 37134. Pertinent details are on file at this agency under W/O AG-01-02479.

repairPart Name: Engine, MFG: Continental, TSN: UNK, Remarks: Damage crank case, Alt or Gear [as written], Work Order No. PG0102872 [as written], SOK No. C01, Date 7/24/01. Tag marked REPAIRABLE.

replacementFound right main fuel cell leaking. Removed old fuel cell an installed new fuel cell part no. 35-9009-2S, serial no. [illegible]. Leak checked satisfactory.

annualTTAF 3453.3 C/W 100 HR / ANNUAL INSP. REPLACED SLT BATT PACK NEXT DUE -> JUN 02. ADJUSTED R/H INBD GEAR DOOR. INSTALLED NEW ELT ANTENNA P/N 110-324. INSTALLED NEW TAXI LAMP. REPLACED R/H FUEL FUSELAGE QUICK FUEL DRAIN. REMOVED R/H ENG COWL FLAP MOTOR AND INSTALLED NEW POWER WIRES. C/W AD 92-22-01 UP LOCK ROLLER. C/W AD 26-07-12 ENG MOUNT INSP. C/W AD 91-15-20 BINDEX ION SWITCH, C/W AD 90-08-14 WING SPAR INSPECTION. C/W AD 95-03-14 ENG MOUNT INSPECTION. I CERTIFY THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

inspectionThe ATC transponder tests and inspections required by FAR 91.413 were performed this date and found to comply with FAR 43, Appendix F. Transponder #1 KT76 SN 37134. Transponder #2 none. Details of this inspection are on file at this repair station under WO # 9194-1 Date 7-13-99. I certify that each automatic pressure altitude reporting system tests and inspections required by FAR 91.411 have been performed. LH Altimeter S/N [illegible] Tested To 20000 ft. RH Altimeter S/N [illegible] (line overwritten with 'Encoder') Tested To 20000 ft. Details of this test and inspection are on file at this repair station under WO# 9194-1 Date 7-13-99.

annualC/W annual inspection. Replace both main brake linings. Installed new seals R/H brake caliper. Serviced all systems. C/W AD 72-22-01 up lock rollers. AD 91-15-20 eng mount. 96-07-12 ign switch. AD 99-05-13 placard fuel selector. I certify this aircraft has been inspected in accordance with an annual inspection and was determined to be in airworthy condition. Rolfe A&P 266263280 IA.

100 hourC/W Beechcraft Baron 55 100 hr inspection. C/W AD 72-22-01 insp & lube uplock rollers next due 382.0. C/W AD 96-07-12 eng mount insp next due 382.0. C/W AD 91-15-20 func ck Bendix ign switch next due 382.0. Replace R/H elevator outboard bearing P/N 3560000 3-M528975 and center bearing K3LFS160. Installed new ELT batt pack P/N 00-10-009 next due June 2000. Installed new O rings P/N M528725-222 R/H brake caliper. See next page.

annualI certify this aircraft has been inspected in accordance with an annual inspection and was determined to be in airworthy condition. Rolfe A&P 266263280 IA.

replacementInstalled overhauled boost pump R/H side. Inf. Rolfe A&P 266263280

alterationInstalled inflatable door seal kit by Aerocessories STC# 4184WE, complied with AD 97-14-15. Cabin door latch ops ck good. Inf. Rolfe A&P 266263280 IA

inspectionI certify that each automatic pressure altitude reporting system tests and inspections required by FAR 91.411 have been performed. LH Altimeter S/N 674046 tested to 20000 ft. RH Altimeter (encoder) S/N 24566 tested to 20000 ft. Details of this test and inspection are on file at this repair station under WO# 7134-1, date 5-14-97. The ATC transponder tests and inspections required by FAR 91.413 were performed this date and found to comply with FAR 43, Appendix F. Transponder #1 KT76 SN 37134. Transponder #2 entry struck through. Details on file under WO# 7134-1, date 5-14-97.

annualPerformed an annual inspection/service this date per FAR 43 Appendix D and Beech maint manual. Egs Run-up, oil drained, insp panels removed. Acft serviced per Beech manual. Retract test performed per Beech manual. Uplock roller clearance checked & adjusted per manual. Acft lubed per lube chart. AD's checked & c/w to this date. See AD compliance manual dated 5/11/97 for details. See individual engine logs for details of engine insp/service. Engines run & flight test performed. All pressures & indications good. I certify that this aircraft was inspected I.A.W an annual inspection and was found to be in airworthy condition. Clark & Earle 219847102 IA

replacementRemoved L/H engine tri-gauge and installed P/N 22804-08-1 S/N 395139P overhauled gauge overhauled by S.D. Chapdelaine under their WO# 5-5745. Operationally checked - leak tested & found OK.

alteration(1) Removed Northstar Loran, antenna and antenna coupling unit. (2) Installed GPS receiver and GPS antenna. Also 3 key c/b for GPS, also coupled to HSI. (3) Installed Aqeus 5000 - 2 key c/b, remote info + select switches. (4) Hard wired intercom into aircraft. All systems ground checked good.

repair8-1-96 B-55 N 18MD S/N TE-455 H.M. 38.2 REPAIRED #1 GLIDESLOPE, BENCH CHECKED #2 GLIDESLOPE, REPAIRED #2 VOR-LOC-G/S INDICATOR. FUNCTION CHECKED WITH NAV-401. FOR ADDITIONAL INFORMATION SEE W.O. 18185.

otherAircraft striped etched primed and painted. Controls balanced after painting installed new No 2 Rudder hinges & L/H INBD & center elevator bearings all work done in accordance with A/C service manual and appropriate F.A.R.

annualContinued from previous page: Installed a new bearing and bushing, p/n B-55 and 35-600003 in outboard position of L/H elevator. Reinstalled elevator. Installed, customer supplied, reskinned elevator in the R/H position. Installed a new CI-122 antenna. Replaced baffling in both engines. Repaired several instrument post lights. Lubricated heater iris valve. Reinstalled interior, cowlings and all inspection panels. Ground ran aircraft, leak checked, test flew and approved for return to service. I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS FOUND TO BE IN AN AIRWORTHY CONDITION.

100 hourC/W 100 hour inspection requirements iaw Beechcraft and Continental maintenance manuals and inspection checklists. Removed all cowlings, interior and all access panels. C/W AD 72-22-01 lubrication of uplock mechanism iaw SI 0448-211, next due at AFTT 3079.4. C/W AD 91-15-20 engine mount inspection iaw SB2362, found okay, next due at AFTT 3079.4. C/W AD 76-07-12 Bendix ignition switch inspection, found okay, next due at AFTT 3079.4. Check applicability of AD 95-03-14 dye check of engine mount fitting iaw MSB 94-9 and found N/A, subject engine mount fittings previously replaced. Greased all wheel bearings. C/W lubrication requirements. Repaired taxi light wiring. Replaced L/H engine lower L/H engine mount with a new mount, p/n 5-10778-16. Repaired wiring on R/H alternator. Removed surface corrosion at several areas on fuselage. Etched and alodined all bare aluminum surfaces. Primed all areas with polymide epoxy primer. Removed right main landing gear shockstrut from aircraft. Disassembled and installed new seals. Reassembled shockstrut, serviced, leak tested and reinstalled. Replaced several corroded rivets outboard of both engine nacelles on lower surfaces of wings. Replaced landing gear actuator. Installed, customer supplied, actuator gearbox with new seals and serviced. Performed a gear retraction test and several emergency extensions. Adjusted and rigged landing gear system iaw Beechcraft rigging procedures. Installed a new engine nacelle fillet fairing on L/H outboard position. Fabricated and installed several sheet metal repairs to engine cowlings. Installed a new ELT battery, operationally checked okay, next battery change due at June 1998. Installed two new b3-5-1 and two new IJ4-7 instrument filter. Removed L/H elevator, removed paint, removed corrosion, treated and primed using polymide epoxy primer.

inspectionATC TRANSPONDER TEST: I certify the ATC transponder(s) test and inspections required under FAR91.413 have been tested and inspected and found to comply with Appendix F of Part 43. #1 Make KING, Model KT-76, SN 37134. #2 Make N/A, Model N/A, SN N/A. WO# 17800, Date 5-8-96. Recertify 24 mos. from above date. ALTIMETER TESTS: I certify that each static pressure system, each altimeter instrument, and each automatic altitude reporting system has been tested and inspected, and found to comply with FAR 43 Appendix E. Altimeters tested to 20000. MFG LH Weston, PN LH 22-374-B01, SN LH 67H 4046, Date LH 5-8-96, RH N/A. Altitude reporting tested to 20000. WO# 17800, recertify 24 mo. from above date.

inspectionATC TRANSPONDER TEST: I certify the ATC transponder(s) test and inspections required under FAR91.413 have been tested and inspected and found to comply with Appendix F of Part 43. #1 Make KING, Model KT-76, SN 37134. #2 Make N/A, Model N/A, SN N/A. WO# 17800, Date 5-8-96. Recertify 24 mos. from above date. ALTIMETER TESTS: I certify that each static pressure system, each altimeter instrument, and each automatic altitude reporting system has been tested and inspected, and found to comply with FAR 43 Appendix E. Altimeters tested to 20000. MFG LH Weston, PN LH 22-374-B01, SN LH 67H 4046, Date LH 5-8-96, RH N/A. Altitude reporting tested to 20000. WO# 17800, recertify 24 mo. from above date.

annualAnnual inspection completed; all controls checked + lubed; wheels + brakes checked; Replaced Hobbs meter with new; Replaced right vacuum regulator + adjusted; wheels + brake checked; replaced right tire tube with Goodyear FLCII; ELT removed for repair - Reinstalled on panel; Gear retraction checked + emergency extension checked. Landing gear greased - c/w AD 72-22-01 by lubing up locks; c/w AD 91-15-20 by inspection of engine mounts; c/w AD 76-07-12 by inspection of mag switches. For AD status, see separate listing.

annualAll controls checked and lubed; wheels + brakes checked; replaced both brake discs and linings; replaced both lower brake hoses; resealed both master cylinders; brake bleed; replaced left main tire with new FC-II; replaced all four engine cowl door hinges; replaced right up lock cable; system rigged; lights checked + repaired as needed; battery serviced; replaced gear door rods at transmission; repaired shielded wire on right throttle switch; replaced right alternator + drive assy with overhauled units; see yellow tag; c/w A.D. 72-22-01 by greasing up lock rollers; c/w A.D. 90-08-14 by inspection of wing spar; c/w A.D. 91-15-20 by inspection of both engine mounts; c/w A.D. 76-07-12 by inspection of both mag switches. For A.D. status, see separate listing. Paper bottle hydrostatic tested - see yellow tag.

otherHobbs - 2368 Total - 2924 Log book closed - see log book #2. Steve A. Hall AP587786743

replacementReplaced RH starter with O/H starter by electro systems. Ops chk OK.

annualAnnual insp completed. Airframe & control system insp. and lubricated. Loose elevator and aileron cables, re-adjusted as necessary. Replaced both [illegible] push rod bearings, [illegible] push rods. Repaired/replaced elevator bushings and bearings. Replaced left elevator trim tab [illegible] inboard bearings. Engine system insp. and servicing. Gear system inspected & lubricated. Main/nose gear struts and torque links, bushings and bolts repaired as necessary. Struts serviced. Gear retraction check completed. Check ... flap ... lubricated as per AD 72-22-01. Annular fluid system serviced. Electrical system serviced. Battery serviced. Insp. pitot heat/static ... Replaced both [illegible] mounts. Insp. fuel drains as per AD 91-15-20. Vacuum/pressure system filters replaced. (Continued next page)

annual(Annual continued) Both eng cyls compression checked [as read]. Ant. Gel battery with manufacturing date of Nov. 9[illegible] installed. Adj. ALT [illegible] ... Fuel flow and gear up warning horn. Acft test flight & fuel system operation checks. AD 93-23 checked & AD status checked [as read, through 1500 ft]. I certify that this ACFT has been inspected in accordance with a ANNUAL inspection and was determined to be in airworthy condition. 12/9/93.

repairYellow tag: Component Name ALT, Model or Type 374, Mfg. Name Bendix [as read], Serial No. 67H4046. Status SERVICEABLE. Owner: Stanolise Flying Svc. Work Order No. 14899. Date 8-5-93.

inspectionI certify that the transponder test required by FAR 91.413 [remainder obscured by tag]

inspectionI certify that the transponder test required by FAR 91.413 has been performed this date and found to comply. Transponder King KT76, sn 37134, Date 8-3-93. [Preprinted text "FAR 91.413 has been performed this date and" and "found to comply" appear struck through.] I certify that the altimeter, encoding system and static system test required by FAR 91.411 have been performed this date. The altimeter on 67H4046 was tested to 20000 ft. on 8-3-93. Date 8-3-93. Certified Repair Station #YNIR644K.

alterationInstalled Engine Model # 10-550-C, Serial # 271787-R in Lt. hand position and 10-550-C, Serial # 271786-R in Rt. hand position. This Installation performed IAW P'Shannon Products STC # SA38455W Drawings & Instructions. Washed, ground ran + adjusted per TCM Bulletin M89-10. See 337 Form, Wt. + Balance/Equipment List revised this Date. End

alterationForm 337 Major Repair and Alteration. Make: Beech, Model D-55, Serial No. TE-455, Registration B18MD (as written). Alteration checked. Block 6 Certificated Mechanic, certificate AP413176848. Inspection authorization: Michael [illegible] Lloyd, Designation No. 415869827, date of approval 3/25/93. Work description continues on page 4: removed left and right engines IO-520C and propellers, installed IO-550C engines and PHC-C3YF-20F/FC7663-2R propellers per D'Shannon Products Drawing No. DL87001, Revision 4, dated August 24, 1993, STC SA3845SW.

alteration1. Removed left and right engines, Teledyne Continental IO-520C and propellers and installed Teledyne Continental IO-550C engines and Hartzell PHC-C3YF-20F/FC7663-2R propellers in accordance with D'Shannon Products Drawing No. DL87001, Revision 4, dated August 24, 1993, as approved under STC SA3845SW. 2. Revised aircraft logs, weight & balance and equipment list as required. 3. Airplane Flight Manual Supplement attached to Federal Aviation Administration approved Airplane Flight Manual. 4. This alteration does not interfere with other aircraft systems at this time. END

ad complianceAD 90-08-14 (rev 9/3/91) Eng mounts: 'Insp eng mounts thru bolt BE bul 2362'. Next comp 2805.

ad complianceAD 72-22-01 Up lock rollers: 'Clean & lube up lock rollers'. Next comp 2805.

ad complianceAD 77-13-22 Crankcase: 'C/W one (1) inch crack at H 2 cyl thru bolt.' Next comp 2805.

ad complianceAD 77-13-22 Crankcase (second entry): 'C/W no cracks observed.' Next comp 2805.

ad complianceAD 91-17-01 Color code blue trim actuators: 'C/W per B/E Bul 2379 dtd Mar 91'. Next comp 2705.

inspectionTHC 1997 TOTAL ACFT 2553 THIS ACFT INSP IAW BE-D55 INSPECTION CHECK LIST AND ASSOC MAINT TECH DATA. LUBED IAW LUBE CHART. JACKED AIRCRAFT AND PERFORMED NORMAL RETRACTIONS AND NORMAL & EMERGENCY EXTENSIONS. REMOVED DAMAGED NOSE TIRE AND INSTALLED NEW GOODYEAR 301-D15-090 TIRE. INSTALLED NEW AIR (INSTRUMENT) AIR INTAKE FILTERS. INSTALLED New Taxi Lamp. INSTALLED NEW RIGHT OTBD FUEL DRAIN VALVE. REMOVED RIGHT BRAKE INSTALLED NEW SEALS CLEANED REINSTALLED & BLED OPC CHECKED OK. INSTALLED NEW ELT BATTERY W/EXP DATE OCT 93. ELT CHECKED. REPAIRED BROKEN WIRE TO RT THROTTLE GEAR WARNING HORN & OPS CHECKED OK. CW AD 92-22-01 DTD 25 OCT 72 BY LUBING LG UPLOCK ROLLERS AN AD 91-15-20 DTD 3 Sep 91 BY INSPECTING ENG MOUNTS ON BOTH ENGS. BOTH ADS NEXT DUE AT 2653 ACFT CONT.

ad complianceAD 90-08-14 (rev 9/9/90): inspect eng mounts; 'Insp eng mount thru bolt 2362, no cracks noted.' Next comp 2653 hrs. AD 91-15-20 (rev 9/24/91): inspect eng mounts, 'Insp eng mount thru bolt 2362 no cracks noted'. AD 72-22-01 LG uplock rollers: 'Lube up lock rollers', next comp 2653 hrs.

ad complianceAD 77-13-22 Left Eng crankcase cracks: 'C/W one inch crack at #2 cyl thru bolt.' Next comp 2653.

ad complianceAD 77-13-22 RT Eng crankcase cracks: 'C/W no cracks noted.' Next comp 2653.

replacementInstalled New 6.50x8 6ply Tires 2+R New Tube RH Main. Richard [illegible] A&P H[illegible]

replacementReplaced Right main tire & tube with used tire & tube. Replaced nose tire & tube with new tire & tube. R.D. Stark A&P 4[illegible]9465991

inspectionI certify that the altimeter, encoding system, and static system test required by FAR 91.411 have been performed this date. The altimeter sn 67H4046 was tested to 20,000 ft. on 2-25-91. Signature Dickey J Robertson. Date 8-5-91. Certified Repair Station #206-2. I certify that the transponder test required by FAR 91.413 has been performed this date and found to comply. Transponder King KT76, sn 37134, Date [blank]. Signature Dickey J Robertson. Certified Repair Station #206-2.

alterationInstalled LH forward side window P/N 978/188GT in accordance with Beryl D'Shannon Aviation Specialties, Inc. STC No. SA2871WE Drawing list DLB-1301 using D'Shannon installation kit. Replaced LH & RH engine upper and lower cowl bugs and painted to match existing paint scheme. Deloyd Rankin A&P H29642582 1A

inspectionComplied with AD 90-08-14 with AD paragraph (a) and Beechcraft service bulletin No. 2269 Revision 1. Inspection performed using Penetrate inspection method. No cracks noted, due again at 2977.2 total aft time.

ad complianceAD NOTES COMPLIANCE RECORD, Page 1 of 1, Date 04-10-91. Reg # N18MD. A/C Make/Model/Popular Name BEECH [illegible]. S/N TE-1455. AD 77-13-22 crankcase cracks: method of compliance 'C/W by inspection' 3-23-90 (one-time, recurring checkmark), next comp 1832.9 (as written). AD 72-22-01 LH and RH up lock rollers: C/W by lube 3-23-90 at 1839.9; next comp 1923.2 (as written). AD 90-08-14 spar carry-thru web structure: C/W by inspection in accordance with B/E S.B. 2369 Revision 2, 04-10-91 at 1923.2; 'No cracks were noted. Insp by [illegible]. Penetrant inspection.' Left engine AD 77-13-22 crankcase cracks: 'C/W by insp. one inch crack at #2 cyl thru bolt', 04-10-91 at 1923.2, next comp 2023.2. Right engine AD 77-13-22 crankcase cracks: 'C/W by insp 1 MW Farm(?)... No cracks noted', 04-10-91 at 1923.2, next comp 2023.2.

inspectionService tag: Component ENC, Mfg TCI, Model D120P2-I, Serial 24566 [as read]. Owner: Standridge Flying Svc. Work Order No. 12723. Date 2/25/91. Tag marked Serviceable (Repaired/Overhauled/Tested/Inspected boxes not clearly marked). Altimeter correction sheet (Garwin 374, S/N 67H4046) shows altitude pressure and friction test readings, barometric scale error, and encoder serial 84566. Checked by [illegible].

inspectionService tag: Component 374 (altimeter), Mfg Garwin, Model 374, Serial 67H4046. Owner: Standridge Flying Svc. Work Order No. 12723. Date 2/25/91. Tag marked Serviceable (Repaired/Overhauled/Tested/Inspected boxes not clearly marked). Altimeter correction sheet shows pressure and friction test readings, altitude/encoder readings, barometric scale error, and encoder serial 84566. Checked by [illegible].

inspectionAltimeter correction sheet. Customer: Standridge Flying Svc. Make Garwin, Model 374, Part No. 2-374-801, Serial No. 67H4046. Altitude pressure and friction test. Encoder serial no. 84566. Work order no. 12723. Recorded values include altitude/encoder readings from -1010/-1.0 through 10000/10.0 feet, friction test values (20, 25, 30, 35, 45) and barometric scale errors from -1727 to +974 ft across 28.10 to 30.99 in. Hg. Tolerances: case leak 20 rpm, after effect 5, hysteresis 50% 40, hysteresis 40% 40.

annualI certify this aircraft inspected in accordance with an annual inspection and found airworthy this date.

replacementREPLACED LEFT ENGINE GUAGE WITH OVERHAULED UNIT.

repairReplaced all brake linings CLWAD 32-22-01 by cleaning & lubing [illegible] replace [illegible]. CLWAD 76-7-12 [illegible] check mag switch CLWAD 77-13-22 check left [illegible] confirm for crack O.K. CLWAD 27-05-02 and [illegible] 97-414 & elevator [illegible] Injection [illegible] 2242 [illegible] are aluminum O.K. Clean & repaint [illegible] bolt & [illegible] drain. Reseal R.H. [illegible] cyl. Replaced outer [illegible] & bushings left elevator. Replace landing light. Replace left [illegible] accumulator. C/W Beech SB 2269 check continuation [illegible] after attach [illegible] fitting [illegible].

ad compliance77-13-22 Eng Case Insp. | 3-23-90 1898.9 | check visually for cracks | next 100 hrs | Eng 2 Bradley (as written, partly illegible)

ad compliance72-22-01 Uplock Rollers | 3-23-90 1898.9 | Lube + clean | next 100 hrs | Eng 2 Bradley (as written, partly illegible)

ad compliance[illegible] Elevator Check Tube | 3-23-90 1898.9 | [illegible]

ad compliance59-25-8 Eye penetrant spar fitting | 3-23-90 1898.9 | check for cracks at rivets | recurring, next 25 hrs

replacementReplaced left fuel boost pump. Removed and installed [illegible]. Sam [illegible] A&P 2138234

inspectionAll routine maintenance performed this date IAW inspection form. Gear retraction performed IAW service manual. L/H cowl flap actuator O/H. Gel battery due Jul 1990. Shimmy damper O rings. Gill G-25 batteries replaced. Brake linings replaced. Taxi lite bracket replaced. New seal beam.

ad compliance77-13-22 Engine Cases | 15 Dec 88 2226 | Check for cracks | recurring, next 100 hrs

ad compliance72-22-01 Uplock Rollers | 15 Dec 88 2226 | Grease rollers | recurring, next 100 hrs

ad compliance76-7-12 Bendix Switch | 15 Dec 88 2226 | Operational check | recurring, next 100 hrs

replacementmixture control cable assy

annualJack aircraft run retraction test. Ck emergency gear extend system. Remove right landing flap motor and install skin patch. Clean all fuel filters. Drain air induction filters. Repair left top cowling. Replace right top cowling with suitable part. Ck brake [illegible] fittings, servicing battery and lock assembly. Inspect in accordance with Beech inspection data. Replace electric fuel boost pump for left engine with new pump.

repairHR.MTR 1411.8 Replaced oil light brake linings P/N 66-22- test O.K. - Lube nose s[illegible]. Also serviced brake reservoir. Robert H Brooks A&P 1332060

replacementReplace L/H Vacuum pump & filter Hobbs 1315.6 9-26-86 Harry P Hunt

annualGear retraction test done. Changed both main tires. Lubed aircraft. Checked flight controls. I certify that this aircraft/engine has been inspected in accordance with a 100 hr./annual inspection and was determined to be in airworthy condition. Researched A.D's through issue no. 8-25-86. Date 8-28-86 Tach reading [blank]. Hour meter 1286.2. Certificate no. 22/2022 Total time [blank].

replacementRemoved one KN65 DME and replaced it w/ one KN65A DME, no change in weight and balance.

otherHOBBS 1190.4 MAIN TIRES rotated and BEARINGS ["checked" struck through in blue] and repacked

replacementReplaced 52D607 Horizon gyro with same P/N gyro S/N X78270H OPS chkd OK. David Eudy Austin Jet Corp. R.S. # 210-74 XXX

otherLamp Check. VOR/LOC for #2 Nav/Com KX [illegible] ±1°. #2 Nav/Com ±1°.

replacementReplaced Lft & Right main tires and tubes - 6.50x8-4PLY Flight Custom II tires & 6.50x8 new tubes. Replaced nose tire 800 x 5-10 PLY.

annualReplace ELT Battery June 87. The altimeter & Digitizer Repair & checked by Garmin Co. for IFR & certify the static system test required by FAR 91.171 have been performed this date. Replaced [illegible] vac & filter & Gaskets [illegible]. Preform check & calibrate Jack A/C & Nose Gear, New Blade & Bolts [illegible], Replace Rt prop Spinner & hub. I CERTIFY THAT THIS A/C HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

replacementReplaced the right vacuum pump & filter. Replaced the left tach generator. Hobbs 930 Hrs. W.O. 44303 Chaparral Aviation - Tradewind Inc. R.S. 207-525 Lloyd & Nefner

replacementREPLACED ALL PROP ANTI ICE BOOTS, REPLACED THE HEATER FUEL PUMP AND THE HEATER IGNITION UNIT. Work Order 43639.

otherCheck Heater apparatus, Clean Fuel Pump & Screen. Repair Cabin Doors. Hourly.

annualMount Main Wheel Tires & Brake Lines. Repack all wheel Bgs. Reseal wheel cyl & Some. Replace Flap Bumpers RT & LT, Jack A/C Lube & Check Gear. Install Boots on Retract Rods. Tighten Elevator Trim-RT, Tighten & Rework Aileron Trim Tab. Pressure Check Cabin Heater, Replace Press Filter LH eng. Rework Escape Window & Install Placard per SIL 1241 & AD 84-9-1. C/K may 2nd 76-7-12.

ad compliance94-9-1 Emergency Egress | 721 7-10-84 | Initialed & tested (method partly illegible)

alterationInstalled Fuel Quan Gage Kit B/A 55-9019-5-$ S/N 150 in left wing as per BSI 925R3. Work order 42008. T.T. 602.3.

otherCheck Installation of New Belts by owner, Install RH landing light. Work order 41938.

alterationBEECH D55 S/N TE-455 N18MD. Installed Avionics equipment at the location described on the revised Weight and Balance/Equipment list dated 11/16/83. Installation was in accordance with equipment manufacturer's installation data and drawings. Structural mountings for the above installation were in accordance with AC43.13-2A, Chapters 1, 2, 3 and 11. All wiring was in accordance with AC43.13-1A, Chapter 11. Magnetic compass accuracy was checked and/or calibrated as required. New empty weight=3381.2 (lbs). New C.G.=79.1 (inches). New useful load=1918.8 (lbs).

inspectionAll work filed under work order # 37053. Aircraft Tach 433.2. The Altimeter and Static System Test required by F.A.R. 91.171 has been performed. Altimeter Mfg. Weston, Model # 22-314-601, S/N 6971406 (as written), Certified To 20,000 Feet by Garner Instrument, Dated 6/13/83. System meets operational requirements of F.A.R. 91.171. Date: 6/12/83 (as written).

inspectionAll work filed under work order # 37053. Aircraft Tach 433.2. The Blind Encoder and Static System Test required by F.A.R. 91.171 has been performed. Blind Encoder Mfg. Trimble (as written), Model # DIR-0127 (as written), S/N 2456 (as written), Certified to 20,000 Feet by Garner Instr. Dated 6/13/83. System meets operational requirements of F.A.R. 91.171. Date: 6/13/83.

inspectionAll work filed under work order # 37053. Aircraft Tach 433.2. I certify that ATC Transponder Test & Inspection required by F.A.R. 91.172 has been performed. Transponder complies with part 43, Appendix F, Paragraph C. Test has been performed on. Transponder Model # King KT-76 (as written), S/N 37134. Second Transponder Model # [illegible], S/N [illegible]. Date: 6/13/83.

annualInstall New Main Tires, Repack Brg. Replace Brake linings. Reset LT Mount cyl. Replace Vac system Filters. Reseal Fuel Drain as needed. Service Brakes & Batteries. Check O/C Syngen & adj LT up lock. Check Heater for Leaks. Hobbs 366. AD 82-7-3 N.A. model. New ELT Battery Dated "Jan 85", Servo Shimmy Damper.

otherThe aircraft identified above was painted in accordance with current FAR's. All flight controls were balanced in accordance with current [illegible] recommendations and is approved for return to service. Make Beechcraft Model D55 SN TE-455 N N18MD

replacementProp OK & connected to oil filled hubs by Hartzell [illegible]. New S/N hubs LT S/N 815854 RT S/N 815857. Installed Taxi lights on nose gear [illegible] from nosedown [illegible] at close

repairComplied with SB 990 Rev II installation of bulkhead doubler kit, stop drilled crack in bulkhead & replaced forward stab spar. Freed-up stiff elevator trim by lubing actuators & cables

inspectionChk Elevator system & cable tension, Record Request

replacementInstall New nose wheel Tire, Repack nose wheel Brg. Install New LT cond flap actuator

ad complianceSonitrol Heater AD 82-7-3 Off Deice by-pass on Heater Hobbs meter or [illegible] no [illegible]. MC Conley Prop Dye chk OK per AD 77-24-4 - Due in 100 hrs. Replace press system filters Reline Brakes. Reseal Rt master cyl, Replace lower strobe light bulb assy. Ck Gear & Linkage? up lock rollers aileron trim tab bushings tightened, Sewn? Brakes & Batteries Repair RT McCauley prop. Bendix Mag Svc CK OK per AD 76-7-12. Hobbs 227. T. Time 183. I certify that this A/C has been inspected in accordance with a [illegible] and was determined to be in airworthy condition. Denver Pitts

alterationH.W. Reads 172.5 hrs. Packard Panel showing R-Nav Approach for IFR enroute & approach per 337 dated 9-17-81.

otherClean prop alchal pump Filter & orifice at each prop. Remove & manifold [illegible] Denver Pitts A&E 111885. Hobbs 171

repairReseal more studs, install single control fuel assy, chk [illegible] & Tube [illegible] Denver Pitts A&E 111885

replacementReplace all Fuel Cells with Factory New Kit # 35-9009-15, 35905-25, 35909-35, 35909-45 - Buffed Fuel Cells. Lt main S/N W5775 uninstall 35-380135-11 TSO-C80. Rt main S/N W5122 uninst. 926 Oct 80. 35-380135-12 TSO-C80. Lt Aux SN 81-13449 Goodyear BTC-85 P/N 95-920011-13 LH June 81. Rt Aux SN 80-1016Y Goodyear BTC85 P/N 95-920011-14 RH mar 80. AD 78-5-6 no longer applicable. Install new vent system filter in off months. Hobbs 050. Denver Pitts A&E 111885

repairReplace plastic line to vac instrument, Replace Batteries, Lube Elevator Trim system, Replace Gartn? fitting on vac Regs, Replace Brake Linings Denver Pitts A&E 111886. Hobbs 023. Dine & Linings

replacementRemove Hobbs Reading 415 & Install New Hour Meter Unit Reading 00. Replac vac line to DG Horizon [illegible] Denver Pitts A&E 111885. TOTAL Time 556 hrs.

alteration1YR MTR 433 HRS. REMOVE KING KX-160, KS-505, KE-201C, ADF T12B SYSTEM, BEECH B-11 ANTENNA + MISC. WIRING. INSTALL KING KMA-20, KR-86/KA-42B, KX-175B, KE-204, KN-73, NARCO B.B. COMMANT, AND DOME MACOLIN [illegible] N-42-1 NAV. REC. ANTENNA. ADD BOOM MIC JACKS + PRIME MUTING RELAY. REPLACE KX-170A WITH KX-175B. ADD AVIONICS MASTER SWITCH. CORRECTED EQUIPMENT LIST + WT + BAL DATA. NEW E.W. 3361 E.W.C.G. 78.77 USEFUL 1939 MOMENT 264751

replacementChanged the KSG100 Remote DG, Joe McKee #2264487

repairRemoved KSG-100 S/N 1582 and installed original slaved gyro. Repaired KPI-550A S/N 1139 [illegible]

inspectionThe Altimeter and Static System Tests Required by F.A.R. Part 91.170, Appendix E, Have Been Performed. The Altimeter was Tested to 20,000 ft. on 16 April 1981. Signed [signature]. Date 16 April 81. Next Tests Due By: 16 April 83. King KT-76 Transponder tested in accordance with F.A.R. Part 43, Appendix F, and meets the requirements of F.A.R. 91.177. Next test due by 16 April 1983.

repairPres Check Fuel Cells per Beech SI 895 & AD 78-5-6. Tighten Vent Line Fittings. Lt any Fuel Cell. Lube up lock Rollers, Replace ELT Battery (Dates "Dec 82") Install New Battery - 1. PS6-9.5/N 545108 + 1.5-25 Replace all Fuel cap "O-ring" Seals, Replace Seal Lt main Fuel Cell Drain, Repair Fuel Leak Lt main Sumpator [illegible] Beech AD 79-1-1 Tail Fins Screw-NA for "X" marked Screw. Installed AD No. 406. 60-9-11 N.P. make of Heater [illegible]

otherA/C OK for Ferryflight TCC NM to [illegible]

ad compliance78-5-6 Goodyear Fuel Cells | 403 9-21-78 | Press ck ST 595 NA-Never | next 9-21-79

repairCheck Trim Tabs per Beech SI 0846-152 Replace Two Bolts in Aileron Trim tab Rod ends. Re seal Shimmy Damper. Repair opt. Front Nose at RT Gear Door. Pres Check Fuel Cells per SI 895 & AD 78-5-6 (Checked & has BTC-39 cells installed). Mags Switches OK per AD 76-7-12. Service Sd. gear. Replace hose in Vac. system. Replace Flap Rubber Bumpers. E.L.T. Battery Replaced (Mar 1980). Replaced Bulb in upper Stowe Light. #A065-403

ad compliance77-24-4 Dye check | 403 9-21-78

ad compliance76-7-12 Bendix Sw | 403 9-21-78 | Dye check | next 503

ad compliance77-13-22 TCM Case | 403 9-21-78 | Manual / Inspect per [illegible] | next 503

otherRecd OK Ferry Flt TCC to HPD [entry text partly illegible]

otherCheck Airframe. Repair Brake [illegible] & Pressure [illegible]. Install new filter RT & LT pumps. Repair Door latch. Install new nosewheel tire & repair nickel bags [illegible]. Lube & grease nose gear & [illegible] rollers. [Annual inspection certification stamp: 'I certify that this A/C has been inspected in accordance with a ANNUAL inspection and was determined to be in airworthy condition.' AI1118851, signed Dennis Pettit]

alterationRemoved: Legacy control head, RT antenna coupler, cable & harness. Installed: King KT-76 & Transcal Digitizer DI20P3-T. Static system leak checked per FAR 91.170. New Empty Weight (lbs) 3365.55, New Empty Weight (C.G.) 98.56, New Useful Load 1934.45.

ad compliancePer AD-75-16-10 (Par 'A' Install new Rod P# 96-520013-7) (Par 'B' Install more Rivets & Step Pin # MS20435 P3-8 & 96-524032 - Beech Kit # 55-4020-15 S/N 526-) (Par 'C' NA model & S/N) (Par 'D' Install new Tab assy # 96-610006-69 & 70) (Par 'E' NA S-N) (Par 'F' NA model) The above installed per Beech SI 0610-152 Al. Controls Painted & Elevators Re balanced per Beech maint manual. Install Beech Improved Fuel Boost Pump Kit 55-9011-1S S/N 153 per SI 0584-285. (Both RT & LT Pumps new) Reseal RT & LT main gear shock struts & service brakes. A/C jacked & gear lubed & retraction test run OK.

ad compliance75-16-10 Electric Trim Tab | C/a 4-27-76 371 Hobbs

ad compliance76-4-7 Window Emergency | C/a H.S. markings 4-27-76

ad compliance70-15-14 Bendix Switch | 371 4-27-76 | Run up ck manual

alterationE.L.T. Installed. +2.22 Arm 240 +480. New Emp 3373.5. New CG 78.29. New moment 264122.1. (1) [illegible] signed by [illegible].

replacementInstall Main tires Ck & Sub Gear Retraction Altimeter Ck & Certify to 20,000' by Garan [illegible]. I certify that the static system ck per FAR 91.170 have been performed. Install fuel flow per Bd 73-24-2. I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

alterationInstall #1 KN-74 RNav - Placard "VFR Only", KX-170A/KA39/KN-73 KN-65/265 / KPI-550A system per manufacturers instructions & AC 43.13-2 fig 2.9. Gnd ck ok. New Empty Weight 3371.5. New CG 78.2. New Moment 263642.1. New Useful Load 1928.5. 6-14-73 4181 Signature [illegible]

annualChk Controls & Cables. AD 72-11-2 Fuel Cocks & Ptr Scavs C/w & Flt Manual Sup to Date. 72-17-2 Grease Bolts in 3rd Gear Institution C/w this date. 72-22-1 Grease Rollers in 3rd Gear C/w this date. Left aileron Trim Ck & Rep by Garmin Dist. Altimeter Drive to be checked at 400 hr. A/C Jacked & Gear Sucker Ck'd OK. I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

inspectionFiled under Work Order No. R-2786. Inspected as per applicable Beech Inspection guide. Repaired L.H. and fuel cap. Replaced both battery terminal bolts. Replaced static cable. Reseal Skinning dampner. Replaced L/H + R/H flap bumpers. Replaced right main fuel cap seals on filler cap, fuel tank. Lubricated aileron rod ends + cleaned. Rebushed nose sissors. Adjusted left uplock tension. Complied with BSI 0074-395 (inst new circuit breaker). Complied with BSI 0217-393 (instrument panel plumbing insp). Complied with BSI 0257-190 (insp pneumatic press. reg valves + lines). Complied with BSI 0442-324 (rerouting cigarlighter wire). Rebushed L/H + R/H elev. trim tab actuating brackets. Tubed up lock rollers as per BSL 66-13. AD 68-26-6 has been previously complied with. The altimeter was certified for IFR flight by Garmin instruments to 20,000ft & the static system was checked as per FAR 91.170

ad compliance71-18-2 Control Cable | Recheck before 950 hrs P/C/u | 2-1-72 | Engine log

ad complianceFiled under Work Order No. R-1987. Replace the Control wheel Adapter as per AD 71-12-4. Removed D.G. for repair at Garmer Instrument & replace.

alterationInstalled Gyro Pressure Filter Covers Both Engs. - Installed Both Voltage Regulators - Sym operates Normal - AF 160569 Attn the Co [illegible]

annualCheck Controls & Cables. Check Gear Retraction & Func. Service Brakes & Battery. Dir Gyro Removal & O.H. by Garmin Instr. Co. PO 70-15-18 Mitchell auto pilot ... has new static clamps. I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

ad complianceAD 68-26-6 C/a. Bernard Grimm Beaver [illegible]. Install Wheeler 14DT & Grebelite [illegible]. Mt. Clay Mfg. New nose tire Rep. by [illegible]. I certify that this aircraft has been inspected in accordance with a [illegible] inspection and was determined to be in airworthy condition. Dwain Ridings ID 1118851

otherS.B. # 67-37 complied with. 1-6-69 John C Watt #1139697

alterationInstalled Bendix 3046 3 lite markers in accordance with AC 43.13-2. Weight change negligible. Inspected by Robert Cutter. Dated 11-29-68.

inspection11/22/68 hr. meter reads 81 hr. Installed new hour meter. Insp. all cables, pulleys, turnbuckles & control surfaces, repack wheel bearings. Clean fuel screens ser. shimmy dampner, check torque on wing bolts. Insp. per Work Sheet Part No. 118662 Work order no. 7175. A.D. Note 68-10-7 & Beech Craft S/B #67-37 NOT C/W. Parts not in stock at this insp. Parts to fill AD 68-10-7 are on back order from Beech Ckg. Acft must be reinspected when parts are avail for compliance of AD. I certify that this Aircraft has been inspected in accordance with a 100 hr. inspection and was determined to be in airworthy condition. Total time 81. Signed Danny Lucero

other[illegible] local. Checked VORs

inspectionIn accordance with F. A. R. 91.25 Omni directional receivers were found to be accurate to within [illegible] degrees. Pilot or Radio crew chief. Margin note: 11-1667

inspectionI Certify that the altimeter and static system tests required by FAR Part 91.170 have been performed. The altimeter was tested to 20,000 feet on 9-20-67.

annualto specification. Removed and reinstalled left flap actuator after reseal, cleaned and lubricated actuator, replaced (2) MS16625-1112 Snap Rings. Replaced all landing gear servicing placards. Replaced Fuel quantity placards. Removed and resealed shimmy damper, installed new O-Rings, serviced with hydraulic fluid. Removed and reinstalled cabin assist step after repair by T&T Welding. Replaced (1) FCA-25750 Gasket on right AUX fuel sender, performed leak check. Repalced (16) MS27039-08-08 Screw on aileron mounting hardware. Replaced (1) 131765-1F Rod End on right and left propeller governor controls. All airworthiness directives through January 2020 checked for compliance and recurrence. AD 91-15-20 Engine Mount Inspection - Complied with by inspection of engine mounts, no defects noted. Next Due AFTT 4909.0 This airframe identified above was repaired and inspected in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. Details of the work performed are on file with Waypoint Aviation Services under work order 5259.

annual(PN:35-650121-4), the old hinges were incorrectly riveted with oversized holes, disassembled left elevator tip weight assemble so that the elevator could be used to jig the hinges on both sides, reassembled left elevator and verified balance to be within limits. Replaced both throttle warning switch's, they still need rigged to manifold pressure determined during test flight. Replaced Vacuum garter and nacelle canister filters. Performed battery capacitance test, passed, next due 1-2026. Replaced brake discs, caliper shims and linings. Replaced 2 flexible brake lines on the right gear and one on the left gear with new, replaced o-rings in both brake calipers with new and bled brakes. Replaced brake disks, linings and shims. Rekeyed the baggage door and main cabin door to match main power switch. Lubricated internal components of both the baggage and main cabin door. Replaced Tail nav light bulb GE305. Replaced tab on one wing bolt cover. Replaced ships CHT probes on both engines and verified correct operation. Removed entrance step, welded cracks as needed, treated corrosion on skin under step and reinstalled. Tightened EGT probes as needed and verified they are all installed at the same depth. Replaced serval loose rivets in the trailing edge of the left nacelle with cherry rivets. Performed routine service and lubrication. Checked all controls for proper travel and cable tensions all operations normal through 3 retraction and extension cycles and one emergency extension. Complied with FAR 91.207d, no defects found, next due 2-2026. ELT battery due 10-2026. Cleaned, inspected and replaced wheel bearings. Replaced missing storm window placard. Corrected discrepancies in weight and balance report and added report to aircraft records. All operations normal on test run. I certify this aircraft has been inspected in accordance with FAR 43 app. D, Annual/100 Inspection criteria and determined Airworthy.

replacementSupplemental log entry. Replaced main L/S tire w/ new AirHawk 6.50/8 (Owner Supplied). Replaced tube, repaired threads on bolt, insp & greased bearings, greased nose gear.

inspectionI certify that I have conducted a check flight in compliance with 14 CFR Part 91.407. The flight characteristics have not been appreciably changed and operation has not been substantially affected. Pilot Certificate # [blank] Date [blank]

replacementREPLACED ELT BATTERY WITH NEW # BP1010 DUE AUG 2008 Dary Dunn owner

replacementFAA Form 8130-3 Authorized Release. Item: 1. Description: ALTIMETER. Part Number: 5934P-3. Remarks: Test & Certified IAW 43 APP E TO 30,000 [ft]. Block 14 certification boxes not checked. Block 15 Authorized Signature, 16 Approval Authorization No., 17 Name, and 18 Date are blank.

alterationPartial inspection record entry (cropped): "GPS 530 Removed Avionics #1 N/C ADF" and "Installed New Garmin GNS 530".

replacementFAA Form 8130-3 Authorized Release. Item: 2. Description: DIGITIZER [illegible]. Part Number: [illegible]. Remarks: [illegible]. Block 14 certification boxes not checked. Block 15 Authorized Signature, 16 Approval Authorization No., 17 Name, and 18 Date are blank.

inspectionALTIMETER INDICATOR CALIBRATION. Serial No. 433119. Test settings -1000 to 12000 with instrument readings recorded at each step (e.g., 500 test / 490 inst; 4000 test / 4000 inst; 12000 test / 12030 inst). Mechanic initials as written [illegible].

inspectionLOG BOOK ENTRY. Make & Model: Beechcraft D55. Reg#: N18MD. S/N: TE-455. 1. Performed the following FAR 91.411 inspection IAW FAR 43 appendix E. No discrepancies were noted. 2. Performed the following FAR 91.413 inspection IAW FAR 43 appendix F. No discrepancies were noted. Table: #1 ADC, P/N 5934P-3, S/N 433119; #1 XPDR, P/N 011-00455-60, S/N 84100336. Reference Capital Aviation, Inc. Process Specifications CA-300 for work performed. No Flight Manual Supplement required. No 337 Required. Weight and Balance is negligible. All work performed complies with current Federal Aviation Regulations. This aircraft is approved for return to service IAW, 14 CFR 135.411(a)(1) the work performed. Details are on file at this facility under W/O #3178.

alterationCUSTOM PAINTED BY Cimarron Aircraft Corp. Number AF5. EXTERIOR: Base coat 4321 Moondust; Primary 78387 Blue; Secondary 63203 Blue; 99 Black. INTERIOR: Banff Blue 66004. Serial number TE-455.

alterationInstalled King KX-160, KI-211, UDI-2 DME, 505 Transponder, Mitchell AK194 Autopilot and Sky ox oxygen system. See FAA Form 337 this date for details.

other[illegible]

annualContinued from previous page. I certify that this aircraft has been inspected in accordance with a ~~100 hr.~~ Annual inspection and was determined to be in airworthy condition.

replacementInstall more gear retraction rod ends per Beech SI 0600-205, Chk gear retraction & Lube. Install kit per Beech SI 0118-243 Kit # 55-40275 S/N 246 on more copies of engine Manuals & Repair sides of cowling. Chk complete A/C & controls. Clean out ruts next & installation in wings & engine nacelle. Serv Prop accumulator. Install new Brake [illegible] lines in wings & engine nacelle. Install new main gear struts with fluid. [illegible] 40-16-18. AD 75-5-3 Due within 100 hr. I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

annualChecked Mag Gaskets [sic] per AD 76-7-12 Par 'A'. Found to operate satisfactorily. [Annual inspection certification stamp: 'I certify that this A/C has been inspected in accordance with a ANNUAL inspection and was determined to be in airworthy condition.' AI1118851, signed Dennis Pettit]

inspectionFiled under Work Order No. X8022. Operational checks per FAR Part 43 Appendix F, have been performed on King KT-76, serial number [illegible], per 3/134, using IFR-1200 & TIC-33B test equipment. Unit meets operational requirements as stated in above FAR.

repairRear gear check. Replaced nose wheel bearing & races.

alterationInstalled a Northstar M1 Loran C system as per 337 form dated 3-4-91. New EW 3386.08 New CG 79.08 New Mom 267774.44 New UL 1913.92

annualI certify that this aircraft has been inspected IAW ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AN AIRWORTHY CONDITION. HM 2149 TOTAL ACFT TIME 2705 ACFT INSP IAW BE D55 checklist AN ASSOC SERVICE MANUAL LUBED IAW LUBE CHART. ACFT JACKED AND BOTH Normal & Retract INSPECTIONS performed. WARNING HORN ON BOTH THROTTLES INSTALLED NEW INSTRUMENT AIR INTAKE FILTERS. REMOVED WHEELS & RECAITED TIRES. INSTALLED NEW TAXI LAMP & LEFT LOWER NAV LIGHT. CW AD 92-22-01 DTD 25 OCT 72 BY CLEANING & LUBING LG uplock ROLLERS & AD 91-15-20 DTD 3 Sep 91 BY INSPECTING ENG MOUNTS ON EACH ENGINE BOTH ADS NEXT DUE AT 2805 ACFT Hours. CW AD 91-17-01 DTD 25 Nov 91 BY COLOR CODING ELEV TRIM ACTUATORS BLUE/LEFT BLACK RIGHT. CW AD 91-15-04 DTD 7 Aug 91 BY INSP OIL FILLER PLUGS IAW PIPER 'F' NO SIGN OF LEAKAGE. I CERTIFY THAT THIS ACFT HAS BEEN INSPECTED IAW AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AN AIRWORTHY CONDITION. Horace R Furlong 2233193 A&P/IA

alterationInstalled Engine Model # 10-550-C, Serial # 271787-R in Lt. hand position and 10-550-C, Serial # 271786-R in Rt. hand position. This Installation performed IAW P'Shannon Products STC # SA38455W Drawings & Instructions. Washed, ground ran + adjusted per TCM Bulletin M89-10. See 337 Form, Wt. + Balance/Equipment List revised this Date. End

alterationInstalled Engine Model # 10-550-C, Serial # 271787-R in Lt. hand position and 10-550-C, Serial # 271786-R in Rt. hand position. This Installation performed IAW P'Shannon Products STC # SA38455W Drawings & Instructions. Washed, ground ran + adjusted per TCM Bulletin M89-10. See 337 Form, Wt. + Balance/Equipment List revised this Date. End

ad compliance74-12-2 BPT Fairing Seals | N/A

ad compliance74-13-2 Mechanical Fastners | N/A - SN

ad compliance74-24-3 Stroke System | N/A | Not Installed

ad compliance75-13-2 Prop. Blade Vib | N/A | model

ad compliance74-24-13 Alt. United Inst. | N/A

ad compliance20-14-7 Contr. Fuel Pump | P/C/u

ad compliance71-11-4 Cont. SSag 20-3 | [illegible]

ad compliance72-20-3 Oil Filter | N/A

ad compliance68-10-3 Mechanical Hub | N/A SN

ad compliance75-12-7 Mechanical | N/A.

ad compliance74-26-9 Bendix Mags | [illegible]

ad compliance76-7-12 Bendix Switch | N/A | model

ad compliance72-2-6 Mitchel Middlecable clamp - Nos New Style | X | PLC/u

ad compliance73-13-11 Mitchel | N/A model

ad compliance76-19-4 Mechanical Prop | N/A models

ad compliance82-7-3 Tanitrol Heater | NA model of heater

ad compliance72-24-4 MC prop | 227 | Dye ck | next 327

ad compliance79-1-1 Screws in control system | NA. N25 x marked

ad complianceAD 91-15-04: 'Inspect for leaks props.' 'Props are oil filled. Check for leaks I&W. PAR F OK.' Next comp 14 Dec 2705.

ad compliancePD ADS / MEMORANDUM (D-55 / Date 455 as written). 67-29-1 N/A S/N no. 68-10-7 Trim tab rep. C/A 1-6-69. 68-14-1 N/A no boots. 68-26-6 Turn type take off phrased C/A. 71-24-9 N/A S/N no. 71-24-10 Control wheel advt. C/A 7-7-71. 72-1-2 Remove plastic oil drain C/A 2-1-72. 72-11-2 Fuel cells & phrased C/A 2-8-73 DEP. 72-17-2 Grease bolts C/A 2-8-73 DEP. 72-22-1 Grease rollers C/A 2-8-73 DEP. 73-13-3 Fuel hose sent C/A 2-28-74 DEP. 73-14-3 N/A S/N. 73-21-2 Fuel hoses C/A 2-28-74 DEP. 73-26-8 N/A has PK-194 installed. 74-3-2 N/A S/N. 74-24-13 United Inst. Altimeter N/A.

oil changeDrained engine oil. Removed and replaced oil filter with new Champion AA48108. Serviced with 10 qts Phillips X/C 20W-50 and 1 pt CamGuard. Leak check good.

annualN18MD L Eng. IO-550-C Engine S/N: 684240 Date: 04-15-26 Tach/HM: 2483.7 Total Time: 2169.8 Time SOH: 457.4 Work Order: 3507. LOGBOOK ENTRY: Annual inspection this date. Compression check: #1-68, #2-70, #3-68, #4-70, #5-70, #6-70. Spark plugs serviced and reinstalled with new gaskets. Changed oil and filter. Serviced with 10 qts Phillips X/C 20W-50 oil and Camguard. Installed new CH48108 oil filter. Old filter inspected, no visible contamination. I certify that this Engine has been inspected in accordance with the requirements of FAR 43, App. D and Maintenance Manual for an Annual inspection and determined to be in an airworthy condition.

oil changeDate: 6/19/2025, Aircraft: N18MD, Type: D55, S/N: TE-455, Hobbs: 2441.10; Tach: 367.00; Total Time: 2441.10. Shop Order #: 25-39063. ***LH Engine*** Pre-run LH engine with TACH 367.0, drained oil, removed oil filter, cut open oil filter and inspected for containments none found. Installed new filter PN: AA48108-2 torqued and safetied, serviced engine with 10 qt of 20W50. Performed operational / leak check. No discrepancies noted at this time. I certify that this aircraft and/or component has been inspected, repaired, and or overhauled in accordance with current FAA Regulations and was determined to be in airworthy condition and approved for return to service.

annual2-1-2025 N18MD Beech Baron SN: TE-455 Continental IO-550-C SN: 684240 TT: 2053.0 TSOH: 340.6 TTAF: 5334.6 Hobbs: 2366.9. Left Engine Maintenance at Annual: Replaced all 12 spark plugs with new. Drained engine oil, changed spin on filter and cut to inspect for debris, none found, serviced with 10 quarts Phillips CX20W-50 and Camguard. Set up idle, idle mixture, unmetered and metered in reference to SID97-3, rev g and IO-550 permold engine operating limitations 6-3.7.1 dated September, 1, 2014. Cylinder compressions as follows: #1 72/80 #2 73/80 #3 72/80 #4 72/80 #5 74/80 #6 74/80. Removed, cleaned, reinstalled and leak checked GAMI injectors, completed form 337 for installation of GAMI injectors on this SN engine. Fabricated and installed new TKS supply tube at the front of the engine. Replaced various engine hoses as needed with new type D hoses. Cleaned, gapped and tested spark plugs. Removed left magneto to verify compliance with AD2022-16-03, verified previous compliance via star stamp and reinstalled. Washed and test ran engine, no leaks. I certify this engine was inspected in accordance with FAR 43 app. D, Annual/100 hr inspection and determined airworthy.

oil changeMay 9, 2024 N18MD Left Engine TCM IO-550C7F s/n 271786-R (struck through) Hobbs 2311.5 285.2 SMOH. Drained oil. Installed 10 qts new Philips 20/50XC oil and camguard. Installed new Tempest 108-1 filter. Old filter inspected for contaminants, none noted. Operation check successful. ~~~ Nothing follows ~~~

oil changeDec 29, 2023 N18MD Left Engine TCM IO-550C7F s/n 271786-R (struck through) Hobbs 2254.0 227.7 SMOH. Drained oil. Installed 10 qts new Philips 20/50XC oil and camguard. Installed new Tempest 108-1 filter. Old filter inspected for contaminants, none noted. Operation check successful. ~~~ Nothing follows ~~~

annualTwin Oaks Aircraft Maintenance, LLC, Daniel W Stark, danny@twinoaksaircraft.com, Tach: 2215.1 & LETSMOH: 188.8. 8/17/2023 Beech D55 N18MD S/N: TE-455 Continental IO-550-C7F S/N LH: 684240 RH: 271786-R Hartzell PHC-C3YF-2UF S/N LH: EB3411A RH: EB3410A. Completed annual inspection per service manual and FAR 43 appendix D. Compressions: #1- 78/80, #2- 78/80, #3- 78/80, #4- 78/80, #5- 78/80, #6- 78/80. I certify this engine was inspected IAW an annual inspection and was determined to be in airworthy condition.

oil changeApr 21, 2023 N18MD Left Engine TCM IO-550C7F s/n 271786-R (serial struck through and highlighted) Hobbs 2207.0 180.7 SMOH. Drained mineral oil. Installed 10 qts new Philips 20/50XC oil. Installed new Tempest AA48108-2 filter. Operation check successful. ~~~ Nothing follows ~~~

replacementInstalled repaired engine IO-550-C serial number 684240. Reinstalled original engine shock mounts, engine mount bolts, exhaust and baffles. Serviced engine with Aeroshell 100 mineral oil. Ground run, leak and operational checks good. Checked idle speed, mixture, magneto drops. Performed full power ground run and checked RPM, MAP and fuel flow. Work Order Number B001280. Serial Number: 684240.

overhaulEngine Model: IO-550-C Serial Number: 684240 Time: 1879.9 TTE Work Order: W059904 Date: 28 MAR 2023. Disassembled engine. Fluorescent penetrant inspected engine mount legs. Replacement VAR crankshaft serial number N08GA087 was visual, dimensional, magnetic particle inspected and ultrasonic inspected per AD 97-26-17 and MSB96-10B. By Aircraft Specialties Services Inc. Reference their 8130-3, W/O: 275829 dated 28 DEC 2022. Magnetic particle inspected 4 connecting rods, crankshaft gear, camshaft gear, counterweights, governor drive and driven gears, idler gear, starter adapter worm shaft and worm gear, fuel pump coupling, magneto drive gears, oil pump drive and driven gears, thru bolts, tach shaft and gears, and rocker arms. Installed a serviceable crank case, casting # 642001m match # 9B738P certified by DIVCO Inc. Reference their 8130-3, W/O: 136963 dated 18 JAN 2023. Installed a serviceable camshaft, P/N: 654837 certified by Aircraft Specialties Services. Reference their 8130-3, W/O: 277342 dated 21 FEB 2023. Installed overhauled lifters, P/N: 653877 and 653888 certified by Aircraft Specialties Services. Reference their 8130-3, W/O: 277793 dated 02 MAR 2023. Installed two overhauled connecting rods, P/N: 655911, S/N: AE18LA290 in position 5 and S/N: AE18LA286 in position 6. Reference our 8130-3, W/O: W0058645 dated 09 MAY 2021. Installed serviceable oil pump Housing certified under our W/O: W059839 dated 06 MAR 2023. Installed serviceable transfer collar, P/N: 629680 M10 certified under our W/O: W059700 dated12 DEC 2022. Four cylinders P/N: SA52006-A; serial numbers (#1) 526000008347, (#2) 526000008348, (#3) 526000008357, (#4) 526000008358, were honed to STD limits and new ring set, P/N: SA5000-SC5 installed. Installed two NEW cylinders, P/N: SA52006-A23P, S/N: (#5) 526000013580 and (#6) 526000013584. Reference Superior Air Parts 8130-3, W/O: SO-00009610 dated 24 JUN 2022. Installed new pistons, P/N: SA654857 and piston pins, P/N: SA630046. Installed an overhauled Oil Cooler, P/N: 655090, S/N: C02-196-157. Reference Pacific Oil Cooler Service Inc. 8130-3, W/O: 154778 dated 08 MAR 2023. Installed an overhauled Starter, P/N: 646275-1, S/N: T01CA066R. Reference Aerotech of Louisville Inc. 8130-3, W/O: 153345 dated 02 FEB 2023. Magneto, P/N: BL-349350-4, S/N: F21IA065R affected by AD 2022-16-03, effective date, 15 AUG 2022. Inspected magneto per CSB 673, III.B.8.b.1 and III.B.8.b.2 III.B.8.c.1-3. Action complete. Engine was reassembled using new rod and main bearings, new rod bolts and nuts, new crankshaft & counterweight bushings, pins, plates, and snap rings, new gaskets, and seals as necessary. Engine was run in a test cell for leak and operations check. Assembled I/A/W Western Skyways, Inc. Repair Specification WS-100 'Use and Application of Hylomar Sealant' dated 11/10/2010, Continental Motors, Inc. Overhaul Manual M-16 and applicable service publications. The engine and/or component identified above was repaired and inspected I/A/W current FAA Regulations and found Airworthy for return to service. Pertinent details of this repair are on file at Western Skyways, Inc. under the above work order. FORM 201E

otherRemoved engine IO-550-C serial number 684240 for repairs. Work Order Number B001280.

oil changeJan 20, 2023 N18MD Left Engine TCM IO-550C7F s/n 271786-R Hobbs 2188.9 162.6 SMOH. Drained oil. Installed 10 qts new Philips 20/50XC oil and camguard. Installed new Tempest 108-1 filter. Old filter inspected for contaminants, none noted. Operation check successful. ~~~ Nothing follows ~~~

oil changeNovember 17, 2022 Hobbs: 2136.5 N18MD Continental IO-550-C S/N: 684240 LH ENGINE. Drained oil. Removed oil filter. Installed new oil filter P/N AA48109-2. Installed oil quick drain plug P/N S6250. Serviced engine with 1 pint of CamGuard and 12 qts Phillips XC 20W-50 oil. Ops and leak check good. This engine is approved for return to service with respect to the above work performed. W.O. 9677

oil changeAugust 23, 2022 Hobbs: 2048.9 N18MD Continental IO-550-C S/N: 684240 LH ENGINE. Drained oil. Removed oil filter. Cut open and inspected filter – no defects noted. Installed new oil filter P/N AA48109-2. Installed oil drain plug with new MS35769-11 crush gasket. Serviced engine with 1 pint of CamGuard and 12 qts Phillips XC 20W-50 oil. Ops and leak check good. This engine is approved for return to service with respect to the above work performed. W.O. 9623

annualN18MD, Beech D55, Continental IO-550-C7F, Hartzell PHC-C3YF-2UF. S/N TE-455; S/N LH: 684240; RH: 271786-R; S/N LH: EB3411A; RH: EB3410A. Completed annual inspection per service manual and FAR 43 appendix D. Changed oil and filter, checked filter and found clean, service with 10 qts. Phillips 20W-50 check for leaks. Compressions: #1- 78/80, #2- 78/80, #3- 78/80, #4- 78/80, #5- 78/80, #6- 78/80. I certify this engine was inspected IAW an annual inspection and was determined to be in airworthy condition. Daniel W Stark 2708377 IA.

replacementN18MD Left Engine, TCM IO-550C7F s/n 271787-R. Installed IO-550C engine serial 684240 after major overhaul from Western Skyways Inc. Reference Work Order 57748. TTE 1712.4. Engine installed using Baron 55 Maintenance Manual, Baron 55/58 Wiring Diagram Manual, and AC 43.13-1B. Installed D'Shannon improved engine cooling baffles in accordance with STC SA09220SC option C and using installation manual DSP-IM95-4, Rev. E. Installed new CHT and EGT probes from JPI as supplied in JPI790 Kit. Installed new aeroquip AE466 fuel lines. Installed overhauled Delco alternator 1100723 from QAA with new CMI 646655RS elastomeric coupling. Installed new instrument air pump. Installed 10 quarts Aeroshell 100 Mineral Oil. Runup and leak check satisfactory. ~~~ Nothing follows ~~~

overhaulEngine Make: CONTINENTAL, Model: IO-550-C, Serial Number: 684240, W/O No: W057748, Date: 29 NOV 2021, Warranty Number: K21423, Warranty Start Date: DEC 2021, Crankshaft Serial No: H259703N, Cylinder Part Number: SAP SA52006-A23P NEW. This engine and accessories listed below were overhauled to "Factory New Tolerances" per Overhaul Manual No: M-16 and Western Skyways, Inc. Repair Specification WSI-100 "Use and Application of Hylomar Sealant" dated 11/10/2010 on all Teledyne Continental Motor Engines and Lycoming Engines as applicable. See back section for Airworthiness Directives and Service Bulletin compliance. This engine was run in a test cell. Total Previous Time: 1712.4 Hrs. This engine meets requirements of CONTINENTAL M-0 for 1700.0 Hour TBO. Accessories: L/H Mag BL-349350-4 S/N F211A065R; R/H Mag BL-349350-5 S/N F21DA007R; Fuel Pump 646212-19A1 S/N B14IA284R; Inj/Carb 646637A9 S/N A04LA045; Man Valve 646508-14A3 S/N D229704C; Starter MHJ-4003 S/N H-U122246; Turbo N/A; Prop Gov, Wastegate, Alt/Gen, VAPC, Relief Val., Controller, Turbo 2, Pump Vac N/A. Cylinder S/N: #1 526000008347, #2 526000008348, #3 526000008357, #4 526000008358, #5 [illegible], #6 [illegible], #7 N/A, #8 N/A. MAINTENANCE RELEASE: The engine and accessories listed above were overhauled and inspected in accordance with current Federal Aviation Regulations and were found airworthy for return to service. Pertinent details of this repair are on file at this Repair Station on above work order. Form 200. Handwritten sticky note on page reads: "Lavy / Tino fuel pump".

ad complianceAD NOTES COMPLIANCE RECORD, Page 1 of 2, 2021-25. Engine Continental Motors IO-550-C, S/N 684240. Appliance Magnetos TCM (formerly Bendix) S-1200 series, S/N F211A065R and S/N F21DA007R, P/N BL-349350-4 and BL-349350-5, Model S6RN-1225. Appliance Cylinder assembly Superior Air Parts, S/N 526000008347, 526000008348, 526000008357, 526000008358, 526000008360, 526000008363, P/N SA52006-A23P. AD entries: 74-26-08 (one time, N/A per magneto model number); 82-13-01 (recurring, verified green blocks not installed, next comp N/A); 82-20-01 (one time, N/A per magneto serial number); 86-13-04 R3 (recurring, installed NEW Superior cylinders, next comp N/A); 88-03-06 (one time, affected oil filter not installed); 91-19-03 (one time, affected oil filter not installed); 93-08-17 (one time, N/A per engine model); 93-10-02 (one time, installed NEW Superior cylinders); 93-16-15 (one time, installed fuel pump drive coupling P/N 653359); 94-01-03 R2 (one time, N/A per magneto serial number); 94-06-06 (one time, N/A per magneto serial number); 95-03-14 (recurring, engine mount cracks, N/A per engine serial number, next comp N/A); 95-21-15 (one time, engine inspected during overhaul).

ad complianceAD NOTES COMPLIANCE RECORD, Page 2 of 2, 2021-25. PL-98-01-05 (one time, exhaust roller rocker arms, not installed); 96-19-01 (one time, crankshaft failure, not applicable by crankshaft serial number H259703N); 2000-23-21 (one time, fracture of crankshaft connecting rod journal, not applicable by crankshaft serial number H259703N); 2004-08-10 (one time, prevent loss of engine power, installed NEW Superior cylinders); 2007-04-19 (recurring, N/A per cylinder part number); 2007-04-19R1 (recurring, N/A per cylinder part number); 2008-19-07 (recurring, correction to prevent loss of engine power due to cracks in cylinder head, installed NEW Superior cylinders); 2010-11-04 (recurring, prevent excessive hydraulic lifter wear, installed overhauled lifters P/N 653888 and 653877); 2012-03-06 (recurring, fuel injection servo not used on this engine); 2014-05-29 (recurring, superior air parts investment cast cylinder assemblies, N/A per cylinder part number); 2016-16-12 (one time, ECI Class 71 or Class 76 cylinder assembly failures, installed NEW Superior cylinders).

overhaulEngine Model: IO-550-C, Serial Number 684240, Time: 1712.4 TTE, Work Order: W057748, Date: 29 NOV 2021. Installed Cam Gear P/N: 2078-1. This satisfies the requirements of MSB05-8D. The engine and/or component identified above was overhauled and inspected IAW current FAA Regulations and found Airworthy for return to service. Pertinent details of this repair are on file at this repair station under above work order. FORM 201E.

annualCompleted annual inspection per service manual and FAR 43 appendix D. Changed oil and filter, checked filter and found clean, service with 10 qts. Phillips 20W-50 check for leaks. Compressions: #1- 78/80, #2- 58(ex)/80, #3- 70/80, #4- 78/80, #5- 78/80, #6- 78/80. I certify this engine was inspected IAW an annual inspection and was determined to be in airworthy condition.

repairRemoved starter adapter p/n 642083A12 serial K230 due to starter slippage. Reinstalled starter adapter after overhaul by Corona Aircraft Engines. Removed starter p/n 646275R1 serial 3081528. Reinstalled after overhaul by Modified Aircraft Accessories. Replaced fuel line from fuel pump to flow divider with new Aeroquip AE466. Installed Shadin fuel totalizer p/n FS201 serial 112714 on crankcase spine in accordance with Shadin installation guide. Installed new fuel line from fuel totalizer to flow divider using Aeriquip AE466. Removed factory fuel pressure reference lines. Engine ground run, leak checked, and test flown, all found satisfactory. ~~~ Nothing follows. ~~~

annualI certify this engine was repaired and inspected in accordance with an annual inspection and was found to be in an airworthy condition. Drained oil, removed oil filter, serviced engine with (10) qts of Philips X/C 20W-50 oil. Performed compression check, results as follows: 1) 74/80 2) 68/80 3) 67/80 4) 60/80 5) 74/80 6) 74/80. Adjusted idle to specification. Cleaned, inspected, and tested spark plugs. Replaced (12) M674 Gaskets on spark plugs. Cleaned and inspected fuel injectors. All airworthiness directives through January 2020 checked for compliance and recurrence. AD 91-15-20 Engine Mount Inspection - Complied with by inspection, no defects noted. Next Due AFTT: 4909.00. This engine identified above was repaired and inspected in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. Details of the work performed are on file with Waypoint Aviation Services under work order 5259.

oil changeRemove and replaced oil filter, installed (1) CH48109-1 Filter. This engine identified above was repaired and inspected in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. Details of the work completed are on file with Waypoint Aviation Services under work order 5111.

replacementPerformed 100 hour inspection with reference to TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 46/80. 1) 78/80, 2) N/A, 3) 71/80, 4) 72/80, 5) 76/80, 6) 78/80. Serviced engine with 11 qts Phillips 20/50XC. Cleaned, Gapped, Rotated Spark Plugs. Removed #2 Cylinder Assembly due to Exhaust Valve Leakage. Replaced with New Superior P/N SA52006-A23P Assembly (Ser# 526B1832596). I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition. Douglas Durning A&P-IA 3275089

repairRemoved TCM Fuel Controller due to leaks. Inspection and Repair performed by Martin Induction Systems. 8130-3 in Aircraft Records. Reinstalled unit and performed TCM SB SID97-3E. Operational Checks Good. Doug Durning A&P-IA 3275089

100 hourPerformed 100 hour inspection with reference to TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 44/80. 1) 77/80, 2) 74/80, 3) 73/80, 4) 76/80, 5) 72/80, 6) 68/80. Changed Oil & Filter CH48109, serviced engine with 11 qts Phillips 20/50XC. Cleaned, Gapped, Rotated Spark Plugs. Replaced Vacuum Pump with O/H 212CW S/N 174991. R&R magnetos for 500 hr inspection, reinstalled and set ignition timing. Adjusted Fuel Pressure I/A/W TCM SB SID97-3E. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition. Douglas Durning A&P-IA 3275089

100 hourPerformed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 46/80. 1) 77/80, 2) 72/80, 3) 76/80, 4) 68/80, 5) 76/80, 6) N/A. Changed Oil & Filter CH48109, serviced engine with 11 qts Aeroshell 100 Mineral Oil. Replaced pneumatic garter filter. Replaced Air Filter with new element. Replaced #6 Cylinder assembly with exchange part from D&B Aircraft Engines, See 8130 in aircraft records. Cleaned, Gapped, Rotated Spark Plugs. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition. Douglas Durning A&P-IA 3275089

100 hourMake: TCM IO-550-C7F Ser# 271787-R. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 48/80. 1) 78/80, 2) 76/80, 3) 72/80, 4) 71/80, 5) 76/80, 6) 71/80. Changed Oil & Filter CH48109, serviced engine with 11 qts Phillips 20/50XC. Replaced pneumatic garter filter. R&R Magnetos for 500 hour Inspection by D&B Engines. Cleaned, Gapped, Rotated Spark Plugs. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

oil change6/21/15 HOBBS: 1641.2 CHANGED OIL. SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50 XC & CAMGUARD Dave Durning A&P 3275089 IA

100 hourMake: TCM IO-550-C7F Ser# 271787-R. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 47/80. 1) 78/80, 2) 76/80, 3) 77/80, 4) 76/80, 5) 77/80, 6) 74/80. Changed Oil & Filter CH48109, serviced engine with 11 qts Phillips 20/50XC + Camguard. Replaced pneumatic garter filter. Ignition timing checked. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

oil change8/20/14 1707.8 HOBBS CHANGED OIL - SERVICED AIRCRAFT WITH 10 QTS 20/50XC & AVBLEND Dan Durning A&P-IA 3275089

oil changeDATE = 4-22-2014 HOBBS: 1575.3 CHANGED OIL - SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50XC & AVBLEND Doug Durning A&P-IA 3275089

replacementFAA-PMA tag (Form CC1108-1): Sky-Tec Model No. C24ST5, Serial No. 4C5-471323, manufactured new on 03 Dec 2013 by Sky-Tec under FAA-PMA No. PQ0852SW, Supplement No. 6. 'This article has been determined to be airworthy.' Starter Installed on N 18MD by Doug Durning (Mechanic) A&P-IA 3275089, 2/25/2014.

repairREMOVED #4 CYLINDER DUE TO EXHAUST LEAKAGE. O/H PERFORMED BY D&B AIRCRAFT ENGINES. REINSTALLED CYLINDER ASSY IAW TCM MANUAL. OPS CHECK GOOD. Dave Durning A&P-IA 3275089

100 hourMake: TCM IO-550-C7F Ser# 271787-R. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Replaced bottom spark plugs with new URHB32E spark plugs. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 46/80. 1) 78/80, 2) 73/80, 3) 75/80, 4) 73/80, 5) 77/80, 6) 70/80. Changed Oil & Filter, serviced engine with 11 qts Phillips 20/50XC + Camguard. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

oil changeTACH: 1484.3 CHANGED OIL. SERVICED ENGINE WITH 11 QTS 20/50 XC PHILLIPS AND AVBLEND. Doug Durning 3275089 A&P-IA

100 hourMake: TCM IO-550-C7F Ser# 271787-R. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Replaced spark plugs with new URHB32E spark plugs. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 46/80. 1) 75/80, 2) 76/80, 3) 77/80, 4) 74/80, 5) 77/80, 6) 76/80. Replaced air filter element with new P/N BA6205. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

oil changeTACH: 1447.0 - CHANGED OIL. REPLACED OIL FILTER WITH NEW CH48109 OIL FILTER. SERVICED ENGINE WITH 12 QTS PHILLIPS 20/50 XC & CANGUARD ADDITIVE. Doug Durning A&P-IA 3275089

repairRemoved #5 cylinder for crack. Replaced #5 cylinder with exchange O/H cylinder. Removed #3 cylinder for O/H. Cylinder overhauled by D&B Aircraft Engines. Replaced #3 cylinder. OPS check good both cylinders. R&R alternator reworked by D&B Aircraft Engines with new brushes and bearings. R&R prop governor for reseal & flow check by Byam Propeller Service. See aircraft records for 8130-3's.

oil change2-25-12 1398.4 HOBBS OIL CHANGE - REPLACED OIL FILTER WITH NEW CH48108-1 FILTER. SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50 XC & AUBLEND ADDITIVE. CUT & INSPECTED OIL FILTER - NO METAL DETECTED.

inspectionPerformed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Removed, cleaned, gapped and reinstalled spark plugs. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 47/80. 1) 77/80, 2) 75/80, 3) 72/80, 4) 77/80, 5) 75/80, 6) 67/80. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

oil changeHOBBS 1364.2 CHANGED OIL SERVICED WITH 11 QTS PHILLIPS 20/50XC. Dave Durning A&P-IA 3275089

replacement3/29/11 - REPLACED #1 CYLINDER WITH OVERHAULED ASSEMBLY - CHANGED OIL, SERVICED WITH 11 QTS 50W MINERAL OIL FOR BREAK-IN. OIL CHECK GOOD.

inspectionPerformed 100 hour inspection this date. Drained oil, replaced oil filter with new P/N 48-108, serviced with 12 qts Phillips 20/50XC. Removed, cleaned, gapped and reinstalled spark plugs. Checked ignition timing. Checked compressions: #1-65/80, #2-75/80, #3-70/80, #4-76/80, #5-71/80, #6-72/80. Master Orifice Reading; 46/80. Inspected fluid lines, hoses, and electrical harnesses. Installed new Garter Filter, P/N ARB3-5-1. Installed new Air Filter P/N BA-6205. I certify that this engine has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

oil change3/7/2010 HOBBS 1272.1 OIL CHANGE - 20/50 PHILLIPS x/c Dave Durning A+P 3275089

inspectionPerformed 100 hour inspection this date. Drained oil, replaced oil filter with new P/N 48-108, serviced with 12 qts Aeroshell 100. Removed, cleaned, gapped and reinstalled spark plugs. Checked ignition timing. Checked compressions: #1-57/80, #2-75/80, #3-70/80, #4-77/80, #5-75/80, #6-70/80. Master Orifice Reading; 45/80. Inspected fluid lines, hoses, and electrical harnesses. Replaced Starter with OH P/N 646275-1. Replaced Vacuum Pump with Rapco P/N 212CW, Ser# 135953. Installed new Garter Filter, P/N ARB3-5-1. Ajusted fuel pressures and mixture IAW TCM SB SID97-3E. Replaced Tach Generator Canon Plug. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

replacement6/24/2008 HOBBS 1194 HRS. REPLACED IGNITION LEADS WITH NEW P/N [illegible]-435-11. Doug Durning A&P 3275059

replacement6/20/2008 HOBBS 1194 HRS. REPLACED ALL COLD ENGINE MOUNTS WITH NEW P/N 3-10778-14. Doug Durning A&P 3275059

inspection6/14/2008 HOBBS 1192 HRS. REPLACED SPARK PLUGS WITH NEW RHB32E. REPLACED IGNITION LEAD SPRINGS. REMOVED MAGNETOS - 500 HR INSPECTION PERFORMED BY D&B AIRCRAFT ENGINES. REINSTALLED MAGNETOS, SET IGNITION TIMING. OPS CHECK GOOD. Doug Durning A&P 3275089

100 hour11/2/2007 HOBBS: 1153.1 TSMOH: 1369.1 N18MD Make: TCM IO-550-C7F Ser# 271787-R Left Engine. Performed 100 hour inspection this date. Drained oil, replaced oil filter with new P/N 48-108, serviced with 12 qts 20/50W Phillips XC. Removed, cleaned, gapped and reinstalled spark plugs. Checked ignition timing. Checked compressions: #1-66/80, #2-76/80, #3-74/80, #4-76/80, #5-67/80, #6-78/80. Inspected fluid lines, hoses, and electrical harnesses. Replaced pressure pump filter with new P/N 3-5-1. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

100 hour[11/1/2007 handwritten over struck-through 11/2/2007] HOBBS: 1208.0 TSMOH: 1424.0 N18MD Make: TCM IO-550-C7F Ser# 271787-R Left Engine. Performed 100 hour inspection this date. Drained oil, replaced oil filter with new P/N 48-108, serviced with 12 qts 20/50W Phillips XC. Removed, cleaned, gapped and reinstalled spark plugs. Checked ignition timing. Checked compressions: #1-62/80, #2-76/80, #3-71/80, #4-76/80, #5-71/80, #6-74/80. Inspected fluid lines, hoses, and electrical harnesses. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition. Douglas Durning A&P116503811

100 hourN18MD Hobbs 1066.8 11/01/06 100Hour Inspection completed this date. Oil previously changed. Ran compressions: #1 69/80, #2 73/80, #3 70/80, #4 79/80, #5 62/80, #6 73/80. Inspected all fluid lines, hoses and electrical harnesses. I certify that this engine was inspected IAW a 100 hour inspection and was determined to be in airworthy condition. A&P2896101IA

100 hourN18MD 10-25-2005 L/E. 100hr insp completed this date. Drained oil, changed filter, serviced with 10qts. X/C 20W50. Checked compressions, Replaced # 6 cylinder with O/H unit due to low compression. Installed GAMI injectors (See 337 for Details.) Ran engine, ops and leak check normal. I certify that this engine was inspected IAW a 100hr inspection and was determined to be in airworthy condition.

repairDALLAS AIR REPAIR-NW REGIONAL AIRPORT LEFT N# 18MD S/N: 271787-R HOBBS: 932.9 MAKE/MODEL: TCM IO-550-C7F TTAF: 3901.2 SMOH: 1148.9 PROP O/H: REPLACED # 4 POWER ASSEMBLY. PISTON P/N 648046, RING SET, P/N SA5000-SC5, PISTON PIN, P/N 643846, ROCKER PINS (2ea.) P/N SA652984, FACED ROCKER ASSY'S, P/N'S 641633 AND 534397, EXH. NO-BLOW P/N SA628260 (3ea.), INTAKE GASKETS (3ea.) P/NSA536413. GROUND RUN ENGINE TO CHECK FOR LEAKS. NONE NOTED AT THIS TIME. RETURN TO SERVICE. (NOTE: SMOH CORRECTED THIS DATE.)

annualThis date performed an annual inspection on this engine. Ran compression check on all cylinders, Cylinders #1 & #6 were found to be below acceptable limits and were removed for repair. Replaced Intake and Exhaust Guides, Exhaust Valves, Intake Seal and exhaust studs. The valve seats were ground, and the cylinders were reassembled and leak checked. They were found to be leak free and reinstalled on the engine in accordance with Continental Overhaul Manual. Deteriorated exhaust studs were replaced on the other cylinders as needed. For complete list of all applicable engine AD's, see attached list. I certify that this aircraft has been inspected in accordance with an annual inspection and was determined to be in airworthy condition

oil changeDRAINED OIL AND SERVICED WITH 12 QTS. OF AEROSHELL 100W. REPLACED OIL FILTER CH48108. REPLACED LH EGT PROBE P/N 86255. REPLACED LT. TACH GENERATOR, P/N 22A667, S/N 1286. RETURN TO SERVICE.

annual[500] ANNUAL INSPECTION – complied with in accordance with the Beech Baron 58 Shop Manual inspection guide. Compression: #1=58/80, #2=70/80, #3=59/80, #4=49/80, #5=60/80, #6=42/80. Drained oil, removed and inspected oil filter, installed a new oil filter and serviced engine with 12 quarts Aeroshell W100. I certify that this ENGINE has been inspected in accordance with an annual inspection and was determined to be in airworthy condition. Pertinent details are on file at this agency under work order PG-01-02872.

inspection[451] C/W 500 hour inspection of the left and right magnetos. Installed new points, condensers, distributor blocks and gears in both magnetos. Installed magnetos on engine with new gaskets.

replacement[058] Installed new alternator base gasket.

replacementReplaced instrument air pump with overhauled unit from Aero Accessories, Inc. (Airborne 212CW S/N 09144). Ground run OK. J K Davis 4116001 54 A&P

oil changeDrained oil. Changed oil filter Champion CH48108. Inspected old filter for metal particles - none found. Installed 11 qt. Aeroshell W-100. Ground run OK, no leaks. J K Davis 4116001 54 A&P

replacementFAA Form 8130-3 tag, tracking ref AA 32306, work order 32306: Item 1, Airborne Dry Air Pump, P/N 212CW, eligibility TBV by installer, qty 1, S/N 09144, status Newly Overhauled. Remarks: Overhauled & Tested in accordance with FAA Process Specification 203-6-1009. Block 19 return to service signed by Vic Harris.

100 hourFragment visible: '...INSPECTION REPLACED #3) 20 H4) 51 ... ENGINE HAS BEEN INSPECTED ... INSPECTION AND WAS ... CONDITION. H.F. Ruff 266263280 IA'. Oil filter Champion CH48108 - none found. Ran OK no leaks. '...with overhauled unit ... 212CW S/N 09144 ... A&P'.

100 hourC/W 100 HR INSPECTION. Spark plugs replaced. Comp ck #1) 65 #2) 74 #3) 20 #4) 51 #5) 25 #6) 51. I certify this engine has been inspected in accordance with an annual inspection and was determined to be in airworthy condition. H.F. Ruff 266263280 IA

100 hourC/W 100HR INSP. Changed oil with 50W Aeroshell oil. Replaced filter. I certify this ENG has been inspected in accordance with an annual inspection and has determined to be in airworthy condition. H.F. Ruff 266263280 IA

repairRemoved #2 position cyl and valve assy (CIRMINEL? [illegible]) and installed. Ran up and checked. H.F. Ruff A&P 266263280

otherAdjusted metered and unmetered fuel pressure and idle mixture. H.F. Ruff A&P 266263280

100 hourC/W 100 HR INSP AS PER Duncraft Baron 55 manual. Replaced induction air filter element BA6205. Replaced lower spark plugs with new RHD22E. Comp ck over holes #1) 60 #2) 78 #3) 69 #4) 50 #5) 54 #6) 54. I certify this engine has been inspected in accordance with an annual inspection and was determined to be in airworthy condition. H.F. Ruff A&P 266263280 IA

100 hourEng 100 hr insp/service performed this date in conjunction with AFS Annual Insp. Per FAR 43 App D and mfr's manuals. Eng run up, oil drained & filter replaced. Screens cleaned. Spark plugs cleaned, gapped, checked, rotated & reinstalled. Compression check (Hold 80 psi): #1-70 #2-60 #3-72 #4-63 #5-72 #6-60. Clamps & fasteners retorqued as required. Eng serviced with 12 quarts Aeroshell 100W detergent oil. Ran eng. No leaks noted, all pressures and indications normal. I certify that this engine was inspected IAW a 100 hour insp and was found to be in airworthy condition. [signature]

100 hourWFH S/O # 1017. C/W 100 inspection iaw Continental maintenance manuals and inspection checklists. Drained oil, changed filter and reserviced with 12 quarts of AS100W. Removed spark plugs, cleaned, gapped tested, rotated and reinstalled. Performed a cold cylinder compression test with the following results: #1 67/80, #2 60/80, #3 72/80, #4 66/80 #5 70/80 and #6 65/80. Checked and adjusted engine to magneto timing. Operationally tested the starting vibrator. Adjusted fuel flow, fuel pressure, mixture and idle speed iaw Continental maintenance overhaul manuals. Ground ran aircraft, leak checked and approved for return to service.

100 hourCompression 1) 78 2) 69 3) 79 4) 72 5) 79 6) 75 New Time 0000. Mag timing checked ok; oil changed - refilled with Aeroshell 15W50; oil filter inspected & replaced; fuel nozzle cleaned; spark plug cleaned + gapped; air filter cleaned; exhaust inspected ok. I certify that this engine has been inspected in accordance with a 100 hr inspection and was determined to be in airworthy condition.

100 hourCompression 1) 70 2) 68 3) 69 4) 70 5) 72 6) 70 oil filter inspected + changed; oil changed; spark plugs cleaned + gapped; fuel nozzle cleaned; exhaust system inspected ok. Timing checked ok; [illegible] cleaned + gapped. I certify that this [illegible] has been inspected in accordance with a 100 hr inspection and was determined to be in airworthy condition.

repairDynamic Balanced & Vibration Tracked This A/C Spinner - Propeller Engine Comb. as per "spec". See Aircraft Log for complete Entry.

otherEngine log entry 3-26-93 (R.P.M. Air: Tach; Time on Ground: 2182.7). Partial handwritten note at right edge is not legible. Attached yellow Maintenance Release tag: W/O No. AT-9332, S/N AT-5728, Part EM8000RX/0850350-5RX, Name TACH GENERATOR, MFR ELECTRO-MECH, MFR S/N 563, Service Bulletin Accomplished Date 10-24-92, Overhauled by Charles E Moore, Aero Electric, Inc., 3414 West 29th South, Wichita, Kansas 67217, FAA Certificate No. NV2R045L. Tag signature partly illegible.

replacementInstalled this Engine in Left hand position of Aircraft N 18MD, Model D-55, Serial # TE-455. This installation performed IAW D'Shernan Products STC # SA3845SO Drawings + Instructions. Washed ground run + adjusted per TCM Bulletin m59-10. See 337 Form, Weight + Balance Equipment List. Revised this Date, Details on File under W.O.# 10169. Installed using New or Existing Accessories + hardware.

overhaulThis engine model IO550C7F, Serial No. 271787-R, was rebuilt/zero timed on 02/25/93 by Teledyne Continental Motors in accordance with an FAA approved Quality Control System, using FAA approved Engineering design data and the applicable requirements of FAR Part 21 of the Federal Aviation Regulations. The approved design data for this engine incorporated the following Service Bulletins and Airworthiness Directives. SB M86-7 / AD 86-13-04 REPLACED WITH NEW PART; SB M88-4 / AD 88-03-06 REPLACED WITH NEW PART; SB M90-21 ULTRASONIC INSPECTION OF BARRELS; SB M91-6 ULTRASONIC INSPECTION OF BARRELS; SB M92-6 ROCKER SHAFT RETENTION IMPROVED; SB M92-13 REPLACED WITH NEW PART; SB M92-14 VISUAL INSPECTION; SB M91-7 ULTRASONIC INSPECTION OF BARRELS; AD 91-19-03 REPLACED OIL FILTER. Records reflecting this rebuilding are on file at Teledyne Continental Motors, P.O. Box 90, Mobile, Alabama, 36601. TELEDYNE CONTINENTAL MOTORS PRODUCTION CERTIFICATE NO. 508

100 hour100 hr insp. Compression check #1 = 70, #2 = 66, #3 = 70, #4 = 76, #5 = 64, #6 = 70 (per entry). Oil screen clean. Mags checked. Fuel injection nozzles cleaned. Air filter insp. Engine operationally checked. I certify that this engine has been inspected in accordance with a 100 hr inspection and was determined to be in airworthy condition.

oil changeThe left engine showed down two quarts from her normal 10. The right side remained unchanged. This was the first abnormal oil consumption since overhaul and break-in... we pressed onward without a second thought after adding in two fresh quarts of XC 20W/50.

repairAfter securing the plane, we went looking for the misbehaving prop governor and nuisance puddle of oil. Imagine our surprise at finding what's in the photos instead. That is our #6 connecting rod, found lounging on top of the #2 and #4 cylinders. The hole it left behind was still steaming with oil vapor. ... 5. The engine's oil sump still held eight quarts.

replacementUpon arrival, Ryan's team had the engine pulled in five hours and returned it to Montrose... Eric listened carefully... pull the engine, return it to Montrose, build up its replacement, and reinstall, all in-situ at Taos. Larry, Ryan, and team were able to build up a replacement engine in just under three weeks, burned in and ready to install.

repairRyan discovered a nick on the backside of my propeller, something I had overlooked, and took the propeller to Montrose for repair as well.

replacementThe propeller blade took some time to track down, but it was replaced. The propeller took a little longer, as Hartzell had its own supply chain problems, but it was soon sorted out.

otherMy IO-550C was supposed to receive a camshaft with an oil plug, however, they shipped one with the plug missing. That's the correct part on certain 550 variants, but not mine. ... Because the oil pressure gauge is plumbed between the oil pump and the camshaft, all indications were that oil pressure was great.

otherThe left engine had a superfluous chimney hole rendering it unfit for its purpose.

oil changeDrained oil from Left Engine. Removed and inspected oil filter, no contaminants found. Serviced engine with 11 quarts Philips XC 20W50 oil and installed new Tempest AA48109 oil filter in accordance with TCM SB96-7D. Operational check satisfactory.

oil change[illegible] ...OF AEROSHELL 100W. REPLACED [illegible] ...OBE P/N 86255. REPLACED LT. ...URN TO SERVICE.

replacementREPLACED INBOARD EXHAUST ASSEMBLY WITH NEW PART FROM KNISELY. Dave Durning A&P-IA 3275089

oil changeOct 12, 2026 N18MD Right Engine IO-550-C SN 686473 Hobbs 2535.3 TT 1922.9 SMOH 60.8. Drained engine oil. Removed and replaced oil filter with new Champion AA48108. Serviced with 10 qts Phillips X/C 20W-50 and 1 pt CamGuard. Leak check good. Nothing follows.

annualAnnual inspection this date. Compression check: #1-70, #2-70, #3-70, #4-76, #5-76, #6-76. Spark plugs serviced and reinstalled with new gaskets. Changed oil and filter. Serviced with 10 qts Phillips X/C 20W-50 oil and Camguard. Installed new CH48108 oil filter. Old filter inspected, no visible contamination. I certify that this Engine has been inspected in accordance with the requirements of FAR 43, App. D and Maintenance Manual for an Annual inspection and determined to be in an airworthy condition.

replacementWO 25-39247, Engine R page 1 of 2. N18MD, CONT MOTOR, IO-550-C, S/N: 686473. 1. Removed Continental IO-550-C S/N:271786-R and installed overhauled Continental IO-550-C, S/N: 686473, in accordance with Continental Motors Overhaul Manual and applicable manufacturer's instructions. Engine hauled by Western Skyways on 24 NOV 2025, Engine TT:1862.1 TTSOH: 0 hours. Installed engine accessories, controls, fuel, oil, induction, exhaust, ignition, and electrical connections. Serviced with 10 qts. Mineral oil. Performed ground engine runs, with satisfactory operation noted with normal oil pressure, fuel flow, RPM, and temperatures. No leaks noted at this time in accordance with Continental IO-550-C Overhaul Manual and Beechcraft Baron D55 Maintenance Manual. 2. Alternator installed after overhaul P/N 1100723 S/N H-010726 Per MM E 24 Sec. 13 Ran and ops checked ok. 3. Installed Overhauled Alternator drive clutch from Quality Aircraft accessories W/O M 732370. MM ref E24 Sec.13. Next check 500 hours. 4. Engine baffling in poor condition Customer declined repair at this time. 5. Replaced gear warning switch at FCU. Per. MM E-17 Sec 5. 6. Replaced missing exhaust stud per Mm IO 550 overhaul. 7. C/W AD 91-15-20 Engine mount inspection per SB 2362R 1. No problem noted at this time. Next due 5539.2 TT.

ad complianceAirworthiness Directives Compliance Report. Continental IO-550-C, Tail #: N18MD, S/N: 686473, Engine: Continental IO-550-C, Hours: 1862.1 TTE. AD entries (Category Engine; Date/Hours at Compliance 24 NOV 2025 1862.1 TTE; signer Tory Nicholson WS9R575J): 88-13-04 R3 Cylinder Assemblies Pressure Test, installed new SAP cylinders, Rec Yes* (Terminating Action), Next Due N/A; 88-03-06 Oil Filter, affected part number oil filter not installed; 91-19-03 Collapsed Oil Filter Elements, affected part number oil filter not installed; 93-10-02 Missing Cylinder Valve Retainer Key, installed new SAP cylinders; 93-16-15 Fuel Pump Drive Shaft, installed coupler P/N 653359; 95-03-14 Engine Mount Bracket Cracks, installed the improved design engine mount brackets P/N 653306 or C/N 653299 and P/N 653305 or C/N 653298, Rec Yes* (Terminating Action), Next Due Terminating action completed; 95-21-15 Detonation Due To Low Octane, engine inspected during overhaul; 99-01-08 Exhaust Roller Rocker Arms, roller rocker arms not installed; 99-18-01 Crankshaft Cheek Cracks, N/A by crankshaft serial number; 2000-23-21 Crankshaft Connecting Rod Journal Failure, N/A by crankshaft serial number; 2004-08-10 ECI Reciprocating Engine Cylinder Head Cracks, ECI cylinders not installed; 2007-04-19 R1 Superior Air Parts Cylinder Assemblies, N/A by cylinder serial numbers; 2009-19-07 EQ3 Cylinder Head Cracks, EQ3 cylinders not installed, Rec Yes, Next Due N/A; 2010-11-04 Hydraulic Lifter Face Wear, installed lifters P/N 658088 & 658077; 2012-03-06 AVStar Fuel Servo Diaphragm, affected diaphragm not installed; 2014-05-29 SA52000-Axxx, SA55000-A1, and SA55000-A20P (SAP) Cast Cylinder Assemblies, N/A by cylinder serial numbers, Rec Yes, Next Due N/A; 2016-16-12 AEC/CMI Cylinder Assemblies, installed new SAP cylinders; 2022-16-03 S-1200 Series Magneto Roller Bearings, N/A by magneto serial numbers; 2023-02-12 Intake Valve Failures, N/A by cylinder serial numbers; 2023-05-16 Crankshaft Counterweight Retaining Rings, N/A by crankshaft serial number; 2023-17-04 Oil Filter Adapter Gasket, affected oil filter adapter not installed.

overhaulThis engine and accessories listed below were overhauled to "Factory New Tolerances" per Overhaul Manual No: M-16 and Western Skyways, Inc. Repair Specification WSI-100 "Use and Application of Hylomar Sealant" dated 11/10/2010 on all Teledyne Continental Motor Engines and Lycoming Engines as applicable. See back section for Airworthiness Directives and Service Bulletin compliance. This engine was run in a test cell. Total Previous Time: 1862.1 Hrs. This engine meets requirements of M-0 for 2000 Hour TBO. Engine Make: Continental, Model: IO-550-C, Serial Number: 686473, Warranty Number: K25340, Crankshaft Serial No: N06AA108, Cylinder Part Number: SA52006-A23P. Accessories: L/H Mag BL-349350-4 F25HA048; R/H Mag BL-349350-5 F25HA151; Fuel Pump 646212-41A1 B02JA045; Inj/Carb 646637A9 A02JA060; Man Valve 646508-14A4 C02JA062; Starter 646275-1 H-Z092489. Cylinder S/N: #1 526000031297, #2 526000031298, #3 526000031299, #4 526000031300, #5 526000031301, #6 526000031302, #7 NA, #8 NA. MAINTENANCE RELEASE: The engine and accessories listed above were overhauled and inspected in accordance with current Federal Aviation Regulations and were found airworthy for return to service. Pertinent details of this repair are on file at this Repair Station on above work order. Form 200 Rev. 2.

annualN18MD Beech Baron SN: TE-455. Maintenance at Annual: Set up idle, idle mixture, unmetered and metered in reference to SID97-3, rev g and I0-550 permold engine operating limitations 6-3.7.1 dated September, 1, 2014. Moved the spark plugs from the left engine to the right engine. Drained engine oil changed spin on filter and cut to inspect for debris, none found, serviced with 10 quarts Philips XC20W-50 and Camguard. Cylinder compressions are as follows: #1 68/80 #2 70/80 #3 70/80 #4 70/80 #5 70/80 #6 72/80. Removed, cleaned, reinstalled and leak checked GAMI injectors. Removed alternator and inspected coupling in reference to SB11-3, replaced failed coupler with overhauled coupling 646655OE, recommended coupling inspection interval is 500 hours. Removed both magnetos and had them 500 hour inspected by Aircraft Magneto Service of Stevensville Montana, see 8130-3's. Replaced altitude compensating fuel pump with overhauled non-altitude compensating fuel pump to match the other engine. Updated POH with Supplement from Deshannon for operating these fuel pumps in accordance with the 550 conversion. Removed throttle controller and had it overhauled by Mikes Fuel metering service, see 8130-3, reinstalled. Fabricated and installed new fuel flow divider drain per Deshannon engine conversion installation drawings. Fabricated and installed new TKS supply tube at the front of the engine. Replaced various engine hoses as needed with new type D hoses. Cleaned, gapped and tested spark plugs. Washed and test ran engine, no leaks. I certify this engine was inspected in accordance with FAR 43 app. D, Annual/100 hr inspection and determined airworthy.

oil changeN18MD Right Engine TCM IO-550C7F s/n 271786-R Hobbs 2311.5 1650.2 SMOH. Drained oil. Installed 10 qts new Philips 20/50XC oil and camguard. Installed new Tempest 108-1 filter. Old filter inspected for contaminants, none noted. Operation check successful. ~~~ Nothing follows ~~~

oil changeDrained oil. Installed 10 qts new Philips 20/50XC oil and camguard. Installed new Tempest 108-1 filter. Old filter inspected for contaminants, none noted. Operation check successful. ~~~ Nothing follows ~~~

replacementInstalled overhauled MS25038-2 Tach Generator serial 38062 from Accessories, Inc. Wichita. Test run satisfactory. ~~~ Nothing follows ~~~

annualCompleted annual inspection per service manual and FAR 43 appendix D. Compressions: #1- 76/80, #2- 78/80, #3- 70/80, #4- 76/80, #5- 76/80, #6- 78/80. I certify this engine was inspected IAW an annual inspection and was determined to be in airworthy condition.

annualN18MD Beech D55 Continental IO-550-C7F Hartzell PHC-C3YF-2UF. S/N LH: 271787-R RH: 271786-R; S/N LH: EB3411A RH: EB3410A. Completed annual inspection per service manual and FAR 43 appendix D. Changed oil and filter, checked filter and found clean, service with 10 qts. Phillips 20W-50 check for leaks. Compressions: #1- 74(ex)/80, #2- 78/80, #3- 78/80, #4- 68(ex)/80, #5- 78/80, #6- 78/80. I certify this engine was inspected IAW an annual inspection and was determined to be in airworthy condition.

oil changeRight Engine TCM IO-550C7F s/n 271786-R. Drained Oil and serviced with 12 quarts Philips XC 20/50 Oil. Replaced Oil Filter with Tempest AA48109. Previous filter inspected for metal particulates, none found. Engine ground run, leak checked and test flown, all found satisfactory. Engine returned to service. ~~~ Nothing follows. ~~~

repairRight Engine TCM IO-550C7F s/n 271786-R. Removed starter adapter p/n 642083A2 serial K188CE due to starter slippage. Reinstalled starter adapter after overhaul by Corona Aircraft Engines. Removed starter p/n 646275 serial C-2031674. Reinstalled after overhaul by Modified Aircraft Accessories. Replaced fuel line from fuel pump to flow divider with new Aeroquip AE466. Installed Shadin fuel totalizer p/n FS201 serial 133121 on crankcase spine in accordance with Shadin installation guide. Installed new fuel line from fuel totalizer to flow divider using Aeroquip AE466. Removed factory fuel pressure reference lines. Engine ground run, leak checked, and test flown, all found satisfactory. ~~~ Nothing follows. ~~~

oil changeContinental, IO-550-C, S/N: 271787-R. Drained oil, removed oil filter. Serviced engine with (10) qts of Phillips X/C 20W-50 oil and installed (1) AA48109 oil filter. Aircraft run-up leak checked. Results satisfactory. This engine identified above was repaired and inspected in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. Details of the work performed are on file with Waypoint Aviation Services under work order 5316.

repairContinental, IO-550-C, S/N: 271787-R. I certify this engine was repaired and inspected in accordance with an annual inspection and was found to be in an airworthy condition. Drained oil, removed oil filter, serviced engine with (11) qts of Aeroshell 100 mineral oil. Performed compression check, results as follows: 1) /80 2) /80 3) /80 4) /80 5)71/80 6) */80. Cleaned, inspected, and tested spark plugs. Replaced (12) M674 Gaskets on spark plugs. Replaced (1) SA628488 Lifter on cylinder #1. Replaced (1) SA646277 Lifter on cylinder #1. Removed cylinders 1, 2, 3, 4, 6. Installed (5) SA52006-A23P cylinders S/N as follows: 1) 526B2042033 2) 526B2042029 3) 526B2042030 5) 526B2042031 6) 526B2042032. Replaced (1) 641394 Crossover Tube. Replaced (1) SA628488 Lifter on cylinder #1 exhaust, replaced (1) SA646277 Lifter on cylinder #1 Intake. Cleaned and inspected fuel injectors. Installed (1) 631837 Sleeve on right engine 'Y' induction pipe, safety wired and torqued hardware. Replaced (1) 655528 Gasket on cylinder #4, replaced (1) SA625615BLK valve cover on cylinder #4. All airworthiness directives through January 2020 checked for compliance and recurrence. AD 91-15-20 Engine Mount Inspection - Complied with by inspection of engine mounts. No discrepancies noted. Next Due AFTT: 4909.0. This engine identified above was repaired and inspected in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. Details of the work performed are on file with Waypoint Aviation Services under work order 5259.

replacementN18MD Hobbs 1807.0 Right engine. Cylinder #4 removed; replaced with OHC unit supplied by Western Skyways, CRS WS9R575J, 8130-3 dated 06/SEP/2019, FTN W055930-202. Drained oil, check & changed filter; serviced engine with Phillips 20W50XC, washed as required, run-up / leak check sat.

oil changeContinental, IO-550-C, S/N: 271786-R. Remove and replaced oil filter, installed (1) CH48109-1 Filter. This engine identified above was repaired and inspected in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. Details of the work completed are on file with Waypoint Aviation Services under work order 5111.

100 hourMake: TCM IO-550-C7F Ser# 271786-R. Performed 100 hour inspection with reference to TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 46/80. 1) 71/80, 2) 64/80, 3) 71/80, 4) 75/80, 5) 75/80, 6) 71/80. Serviced engine with 11 qts Phillips 20/50XC. Cleaned, Gapped, Rotated Spark Plugs. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

repairRemoved TCM Fuel Controller due to leaks. Inspection and Repair performed by Martin Induction Systems. 8130-3 in Aircraft Records. Reinstalled unit and performed TCM SB SID97-3E. Operational Checks Good.

100 hourMake: TCM IO-550-C7F Ser# 271786-R. Performed 100 hour inspection with reference to TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 44/80. 1) 77/80, 2) 62/80, 3) 72/80, 4) 77/80, 5) 75/80, 6) 68/80. Changed Oil & Filter CH48109, serviced engine with 11 qts Phillips 20/50XC. Cleaned, Gapped, Rotated Spark Plugs. Replaced Vacuum Pump with O/H 212CW S/N 174979. R&R magnetos for 500 hr Inspection, reinstalled and set ignition timing. Adjusted Fuel Pressure I/A/W TCM SB SID97-3E. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

100 hourMake: TCM IO-550-C7F Ser# 271786-R. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 46/80. 1) 70/80, 2) 67/80, 3) 75/80, 4) 76/80, 5) 70/80, 6) 65/80. Changed Oil & Filter CH48109, serviced engine with 11 qts Aeroshell 100 Mineral Oil. Replaced pneumatic garter filter. Replaced Air Filter with New element. Cleaned, Gapped, Rotated Spark Plugs. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

100 hourMake: TCM IO-550-C7F Ser# 271786-R. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 48/80. 1) 78/80, 2) 62/80, 3) 71/80, 4) 75/80, 5) 70/80, 6) 73/80. Changed Oil & Filter CH48109, serviced engine with 11 qts Phillips 20/50XC. Replaced pneumatic garter filter. R&R Magnetos for 500 hour Inspection by D&B Engines. Cleaned, Gapped, Rotated Spark Plugs. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

oil change6/21/15 HOBBS: 1641.2 CHANGED OIL. SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50XC & CAMGUARD. Day Durning A&P 3275089 IA

replacement6/10/15 - HOBBS: 1638.4 REPLACED ALTERNATOR WITH O/H P/N 1100723 PART FROM QUALITY AIRCRAFT ACCESSORIES. OPS CHECK GOOD Day Durning A&P-IA 3275089

100 hour11/4/2014 HOBBS: 1596.3 TSMOH: 935.7 Right Engine Make: TCM IO-550-C7F Ser# 271786-R. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 47/80. 1) 78/80, 2) 67/80, 3) 74/80, 4) 75/80, 5) 70/80, 6) 70/80. Changed Oil & Filter CH48109, serviced engine with 11 qts Phillips 20/50XC + Camguard. Replaced pneumatic garter filter. Ignition timing checked. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition. Douglas Durning A&P-IA 3275089

oil changeCHANGED OIL - SERVICED AIRCRAFT WITH 10 QTS PHILLIPS 20/50XC & AUGLEND

oil changeDATE: 4-22-2014 HOBBS: 1575.3 CHANGED OIL-SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50XC & AVBLEND Doug Durning A&P IA 3275089

replacementFAA-PMA tag: This tag certifies that Sky-Tec Model No. C24ST5, Serial No. 4C5-051420 was manufactured new on 05 Feb 2014 by Sky-Tec under the authority of FAA-PMA No. PQ0852SW Supplement No. 6 in accordance with Sky-Tec's FAA-Approved Quality System (14CFR Part 21, Subpart K). This article has been determined to be airworthy. Starter Installed on N18MD by Doug Durning (Mechanic) A&P 3275089 IA. INSTALLED: 02-20-2014. Form CC1108-1.

100 hour11/10/2013 HOBBS: 1531.4 TSMOH: 870.8 Right Engine Make: TCM IO-550-C7F Ser# 271786-R. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Replaced bottom spark plugs with new URHB32E spark plugs. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 44/80. 1) 77/80, 2) 71/80, 3) 73/80, 4) 76/80, 5) 69/80, 6) 74/80. Changed Oil & Filter, serviced engine with 11 qts Phillips 20/50XC + Camguard. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition. Douglas Durning A&P-IA 3275089

repair02/19/2013 HOBBS: 1484.3 TSMOH: 824.7 Right Engine Make: TCM IO-550-C7F Ser# 271786-R. Removed #1 cylinder due to exhaust valve leakage. Cylinder replaced with overhauled cylinder by D&B Aircraft Engines using new seals and gaskets. See aircraft records for 8130-3 form. Replaced vacuum garter filter. Oil changed and serviced with 11 qts Phillips 20/50 XC and AvBlend. Checked ignition timing.

100 hour11/02/2012 HOBBS: 1465.3 TSMOH: 805.7 Right Engine Make: TCM IO-550-C7F Ser# 271786-R. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Replaced spark plugs with new URHB32E spark plugs. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 46/80. 1) 66/80, 2) 62/80, 3) 75/80, 4) 76/80, 5) 72/80, 6) 70/80. Replaced air filter element with new P/N BA6205. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition. Douglas Durning A&P-IA 3275089

oil changeTACH: 1447.0 CHANGED OIL. REPLACED OIL FILTER WITH NEW CH48109 OIL FILTER. SERVICED ENGINE WITH 12 QTS PHILLIPS 20/50/XC & CAMGUARD ADDITIVE. Doug Durning A&P IA 3275089

oil change1398.6 HOBBS OIL CHANGE- REPLACED OIL FILTER WITH NEW CH48108-1 FILTER. SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50XC & AUBLEND ADDITIVE. CUT & INSPECTED OIL FILTER- NO METAL DETECTED Doug Durning A&P 3275089 IA

100 hourMake: TCM IO-550-C7F Ser# 271786-R Right Engine. Performed 100 hour inspection IAW with TCM & Beechcraft Service Manuals. Removed, cleaned, gapped and reinstalled spark plugs. Inspected all hoses, fluid lines, and harnesses. Performed compression test as follows: M/O reading 47/80. 1) 65/80, 2) 60/80, 3) 73/80, 4) 75/80, 5) 68/80, 6) 73/80. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

repair1364.2 HOBBS - R&R PROPELLER GOVERNOR FOR REPAIR BY BHAM PROPELLER SERVICE, CHANGED OIL SERVICED WITH 11 QTS PHILLIPS 20/50 XC + 1 PT AUBLEND ADDITIVE. Doug Durning A&P/IA 3275089

repairR&R PROPELLER FOR RESEAL BY THE PROP SHOP. SEE RECORDS FOR DOCUMENTATION. REPLACED CRANKSHAFT NOSE SEAL. OPS GOOD. Dave Dunmy A&P/IA 3275089

annualMake: TCM IO-550-C7F Ser# 271786-R Right Engine. Performed 100 hour inspection this date. Drained oil, replaced oil filter with new P/N 48-108, serviced with 12 qts Phillips 20/50XC. Removed, cleaned, gapped and reinstalled spark plugs. Checked ignition timing. Removed #6 Cylinder Assembly for overhaul by D&B Aircraft Engines. Reinstalled cylinder assembly – Ops check good. Checked compressions: #1-64/80, #2-64/80, #3-71/80, #4-74/80, #5-70/80, #6-N/A. Master Orifice Reading; 46/80. Inspected fluid lines, hoses, and electrical harnesses. Installed new Garter Filter, P/N ARB3-5-1. Installed new Air Filter P/N BA-6205. I certify that this engine has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

oil changeOIL CHANGE 20/50 XC PHILLIPS

100 hourMake: TCM IO-550-C7F Ser# 271786-R Right Engine. Performed 100 hour inspection this date. Drained oil, replaced oil filter with new P/N 48-108, serviced with 12 qts Aeroshell 100. Removed, cleaned, gapped and reinstalled spark plugs. Checked ignition timing. Checked compressions: #1-73/80, #2-67/80, #3-72/80, #4-77/80, #5-68/80, #6-68/80. Master Orifice Reading; 45/80. Inspected fluid lines, hoses, and electrical harnesses. Replaced #4 Rocker Cover gasket and push rod tube seal with new. Replaced Vacuum Pump with Rapco P/N 212CW, Ser# 135479. Installed new Garter Filter, P/N ARB3-5-1. Ajusted fuel pressures and mixture IAW TCM SB SID97-3E. Replaced Tach Generator Canon Plug. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

100 hourMake: TCM IO-550-C7F Ser# 271786-R Right Engine. Performed 100 hour inspection this date. Drained oil, replaced oil filter with new P/N 48-108, serviced with 12 qts 20/50W Phillips XC. Removed, cleaned, gapped and reinstalled spark plugs. Checked ignition timing. Checked compressions: #1-70/80, #2-70/80, #3-72/80, #4-76/80, #5-70/80, #6-73/80. Inspected fluid lines, hoses, and electrical harnesses. Replaced #3 Rocker Cover gasket with new. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

replacementHOBBS 1194 HRS. REPLACED IGNITION LEADS WITH NEW P/N CLE-4B5-11.

replacementHOBBS 1194 HRS. REPLACED ALL ENGINE LOAD MOUNTS WITH NEW P/N 5-10778-14.

inspectionHOBBS 1192 HRS. REPLACED SPARK PLUGS WITH NEW RHB32E, REPLACED IGNITION LEAD SPRINGS. REMOVED MAGNETOS - 500 HR INSPECTION PERFORMED BY D&B AIRCRAFT ENGINES. REINSTALLED MAGNETOS, SET IGNITION TIMING. OKS CHECK GOOD.

inspectionPerformed 100 hour inspection this date. Drained oil, replaced oil filter with new P/N 48-108, serviced with 12 qts 20/50W Phillips XC. Removed, cleaned, gapped and reinstalled spark plugs. Checked ignition timing. Checked compressions: #1-67/80, #2-68/80, #3-72/80, #4-77/80, #5-75/80, #6-67/80. Inspected fluid lines, hoses, and electrical harnesses. Replaced pressure pump filter with new P/N 3-5-1. I certify that this engine has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

inspectionN18MD Hobbs 1066.8 11/01/06 100Hour Inspection completed this date. Oil previously changed. Ran compressions: #1 75/80, #2 66/80, #3 72/80, #4 75/80, #5 72/80, #6 63/80. Inspected all fluid lines, hoses and electrical harnesses. I certify that this engine was inspected IAW a 100 hour inspection and was determined to be in airworthy condition. A&P2896101IA

repairDATE: 10/02/0[covered] MAKE/MODEL [covered] TTAF: SMOH: [covered] DRAINED OIL AND [covered] OIL FILTER CH48108. REPAIRED CHT CONNECTOR @ #2 CYLINDER. REMOVED, OVERHAULED AND REINSTALLED LEFT MAGNETO. MAGNETO OVERHAULED BY JOE'S AIRCRAFT IGNITION SERVICE, W/O 1257. RETURN TO SERVICE.

repairDRAINED OIL AND SERVICED WITH 12 QTS. OF AEROSHELL 100W. REPLACED OIL FILTER CH48108. REPAIRED CHT CONNECTOR @ #2 CYLINDER. REMOVED, OVERHAULED AND REINSTALLED LEFT MAGNETO. MAGNETO OVERHAULED BY JOE'S AIRCRAFT IGNITION SERVICE, W/O 1257. RETURN TO SERVICE.

other[illegible, mostly covered by yellow tag]

oil changeoil change CH48108 w/ [illegible] filter w/900 [illegible]

annualReplaced engine oil leak at oil pump housing resealed using silk thread method [illegible] 10550 G/M. Did annual inspection compression within allowable limits. Oil change CH48109 filter no metal infilter ok for service. I have inspected this engine IAW Annual inspection and have determined it to be airworthy and ok for continued service.

oil changeoil change CH48109 no metal infilter w-100 ok for service

oil changeoil change CH48101 no metal infilter w-100 ok for service

oil changeoil change CH48109 no metal infilter w-100 ok for service

replacement[001] Installed engine in right hand position of Beech model D55 serial number TE-455 at aircraft total time 3628.3 hours. Overhauled 24V 50A GD alternator P/N 1100723, S/N A108019 installed with serviceable alternator drive gear S/N 223097-72C supplied by customer.

annual[500] ANNUAL INSPECTION - complied with in accordance with the Beech Baron 58 Shop Manual inspection guide. I certify that this ENGINE has been inspected in accordance with an annual inspection and was determined to be in airworthy condition. Pertinent details are on file at this agency under work order PG-01-02872.

repairSERVICEABLE tag. Mfgr. Name: Continental. Component Name: Crankcase. Model #: IO-520. Serial #: [illegible]. The aircraft component identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Agency and is approved for return to service. WDC # 77660. Date 8-23-01.

repairSERVICEABLE tag. Mfgr. Name: Continental. Component: camshaft. Model: 653058 AL/649322AL. Serial No. 5120002-1. I certify that the repair identified on this tag was performed and inspected in conformance with Federal Aviation Regulations, and is approved for return to service. Pertinent details of the repair are on file at this repair station under Work Order No. 120002. Date 8/14/01. Signed RL Mendl.

otherSERVICEABLE PART TAG. MFG.: CONTINENTAL. MODEL: IO-550-C (handwritten C above struck-through "5 5 0-BB"). SERIAL NUMBER: "V/U J012203" (handwritten note "on Sludge 605910W"). PART NAME: CRANKSHAFT. C/W AD 97-26-17 I/A/W PARA C "ULTRASONIC INSPECT". CUSTOMER: JEWELL AVIATION. WO #: J369[illegible]. DATE: 8/09/01. SIGNATURE: A&P2088862 John T Jewell.

replacementReplaced instrument air pump with overhauled unit from Aero Accessories, Inc (Airborne 212CW SN 09145). Ground run OK.

100 hourC/W 100 hr insp. Changed oil with 50W Aeroshell oil. Replaced filter. Comp ck good. Washed down engine. I certify this engine has been inspected in accordance with an annual inspection and was determined to be in airworthy condition. IA Rolfs A&P 266763280 IA.

otherAdjusted metered and unmetered fuel pressure and idle mixture. IA Rolfs A&P 266763280.

100 hourC/W 100 hour insp as per Beechcraft Baron 55 manual, replaced induction air filter element P/N# BA 6205, replaced lower spark plugs with new RHB32E, comp ck over 80 lbs #1) 46 #2) [illegible] #3) 48 #4) 61 #5) 64 #6) 44. I certify this engine has been inspected in accordance with an annual inspection and was determined to be in airworthy condition. IA Rolfs A&P 266763280 IA.

replacementRemoved #2 cyl and valve assy (cir mini). Installed overhauled cyl and ran up and leak check. I.A.W. RM A&P 266263280.

annualEngine 100hr insp/service performed this date in conjunction with A&P annual insp per FAR 43 App. D and Mfgs. manuals. Eng ran up, oil & oil filter reqd. Screen cleaned. Spark plugs cleaned, gapped, checked, rotated & reinstalled. Compression check 80 psi. #1-62 #2-60 #3-61 #4-62 #5-68 #6-62. Clamps & fasteners torqued as req. Eng service with 12 quarts Aeroshell 100W detergent oil. Ran engine, no leaks noted. Oil pressure and indications normal. [Struck-through text] This engine was inspected I.A.W. ... inspection and was found to be in airworthy condition. A&P 2847112.

100 hourC/W 100 inspection iaw Continental maintenance manuals and inspection checklists. Drained oil, changed filter and reserviced with 12 quarts of AS100W. Removed spark plugs, cleaned, gapped tested, rotated and reinstalled. Performed a cold cylinder compression test with the following results: #1 65/80, #2 60/80, #3 70/80, #4 70/80, #5 70/80 and #6 73/80. Replaced main points in R/H magneto. Checked and adjusted engine to magneto timing. Operationally checked the starting vibrator. Installed a new gasket on engine oil temperature bulb. Adjusted fuel flow, fuel pressure, mixture and idle speed, iaw Continental maintenance and overhaul manuals. Ground ran aircraft, leak checked and approved return to service.

100 hourCompression 1) 69 2) 68 3) 68 4) 70 5) 69 6) 63 was [illegible]. Timing checked. Oil changed - filter with Aeroshell 15W50. Oil filter inspected & replaced. Spark plugs cleaned & gapped; exhaust system inspected ok; air filter cleaned. I certify that this engine has been inspected in accordance with a 100 hr inspection and was determined to be in airworthy condition.

otherDynamic Balanced This A/C Spinner - Propeller - Engine Comb, as per 'specs'. See Airframe log for Complete Entry.