1967 Beech D55

repairRemoved 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. Removed 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. Lubricated 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.

inspectionAirframe Entries. Complied 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.

repairCentury 10 395 autopilot computer was repaired by Autopilots Central. Ground Ops check satisfactory.

inspectionComplied 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

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 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 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.

inspectionLubricated 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 filter. 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 ~~~

repair1. Removed left alcohol discharge tube and installed AN4 cap on elbow. 2. Labeled prop anti-ice switch INOP.

repairRemoved 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 26875-48 – no leaks detected. This aircraft is approved for return to service with respect to the above work performed.

inspection1. 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 the above work performed.

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 ~~~

repairWork 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: 139909B102, 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.

repairTroubleshot 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. Reinstated 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 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.

alterationNew Aircraft Empty Weight 3410.41 lbs. Various alternate configurations listed with empty weights ranging from 3364.01 lbs to 3398.21 lbs.

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. ~~~

replacementReplaced 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. Installed Flight Stream 210 p/n 011-03257-40 s/n 3RE008869 IAW Garmin manual 190-01700-00 Rev G. Unit installed on top of copilots glovebox and receives power from an inline 1A fuse. NDN. 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.

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

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.

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. ~~~

repairN18MD 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.

annualAnnual 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.

annualAnnual 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.

replacementREPLACED L/H AUXILIARY FUEL PUMP WITH O/H UNIT P/N 4404-00-7NV. SEE AIRCRAFT RECORDS FOR 8130. OPS CHECK GOOD. REPLACED MLG & NG TIRES WITH NEW GOODYEAR FLIGHT II. REPLACED CALIPER SEALS & BRAKE LININGS WITH NEW PARTS

replacementREPLACED R/H AUXILARY FUEL PUMP WITH O/H UNIT P/N 4404-00-7NV. SEE AIRCRAFT RECORDS FOR 8130. OPS CHECK GOOD.

annualAnnual 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.

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 NEGLIDABLE. 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.

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

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 WO 16237 I CERTIFY THE STATIC SYSTEM TEST REQUIRED BY F.A.R. PART 91.411, HAVE BEEN PREFORMED

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

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

replacementCV1J4 Filter Installation Record. FAA-PMA SER No. 011686

replacementCV1J4 Filter Installation Record. FAA-PMA SER No. 011692

replacementREMOVED ARTIFICIAL HORIZON. REPLACED WITH O/H 52D67 PART FROM AIRCRAFT QUALITY INSTRUMENTS, INC. SERIAL# 5745BX. OPS CHECK GOOD.

replacementREPLACED AIRCRAFT BATTERIES WITH NEW GILL G25S

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. Installed new seals L/H MLG Strut. 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. 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. TIMETER, MOD. 5934P-3. CERTIFIED UNDER PART 43, ND TESTED AS PER 91.411 FEET ON 3/11/14. W.O. NO. 15785. STATIC SYSTEM TESTS REQUIRED 91.411 HAVE BEEN PERFORMED 3/11/14. SIG. [illegible]

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. [illegible] CRS AT2R702K

inspectionTHIS 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 SIG. [illegible] CRS AT2R702K

repairREPLACED MLG BRAKE ROTORS WITH NEW RAPCO P/N RA164-02706 & NEW BRAKE LININGS P/N RA66-44. LUBRICATED ALL WHEEL BEARINGS

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.

replacementREMOVED O2 BOTTLE FOR RECERTIFICATION HYDROSTATIC TEST PERFOMED BY CITY CARBONICS. SEE A/C DOCUMENTS FOR INVOICE. REINSTALLED & RECHARGED O2 SYSTEM. NO LEAKS DETECTED. RECERTIFICATION NEXT DUE 5/2017.

replacementREPLACED AIRCRAFT BATTERIES WITH NEW GILL G-35S. 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. Altimeter #1 Mfg by United Instr. Model No. 59348-3 S/N 43319 has been certified to an altitude of 20 thousand feet. Static/Encoding system has been inspected, tested, and found to comply with FAR 91.411 Reference W.O. 87815.

replacementREPLACED MAIN GEAR & NOSE WHEEL TIRES WITH NEW GOODYEAR FC III TIRES. HUBS CLEANED & REPAINTED. BEARINGS LUBRICATED.

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 PROBE ALCOR EGT GUAGE. 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 ovehauled P/N 58-380090-1 see A/C recorsd 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. Altimeter #1 Mfg by United Instr. Model No. 59348-3 S/N 43319 has been certified to an altitude of 20 thousand feet. Static/Encoding system has been inspected, tested, and found to comply with FAR 91.411 Reference W.O. 87742.

annualAnnual Inspection complied with this date. All AD's complied with at this time. I certify that this A/E was Inspected IAW an ANNUAL Inspection and was determined to be in Airworthy condition.

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.

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.

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 I CERTIFY THE STATIC SYSTEM TESTS REQUIRED BY F.A.R. PART 91.411 HAVE BEEN PERFORMED

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 AD's in compliance @ this time. I certify that this Aircraft was inspected IAW an ANNUAL Inspection and was Determined to be in Airworthy Condition.

replacementREPLACED ELT BATTERY WITH NEW BP-1010. OPS CHECK GOOD. EXT 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

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.

alterationRemoved Avionics #1 N/C ADF R-Na. and Northstar GPS installed New Garmin GNS-530 W with GA 35W Antenna and Mid-continent MD41 Annunciator as per STC # SA01933LA. Installed DAC GDC 31 Roll Steering as per STC # SA10230SC see FAA forms 337 this 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

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.

annualI certify 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 27134 has been tested, inspected, and found to comply with FAR 91.413 Reference W.O. 87649

annualAnnual Inspection completed this date. Jacked aircraft, performed retraction and extension check in both normal and emergency, All checks and clearences 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 Retractor 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

replacementREPLACED ELT BATTERY WITH NEW # BP1010 DUE AUG 2008

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 R/H wing Root position, Cockpit entrance stair cracked, verified 4130 steel with Raytheon welded per AC 4313-1B 4-74 d and (5) a through(5) ok for service

repaircheck R/H brake for leak, cleaned op ck good ok for service. Investigate R/H prop ferrous blade blends see prop log ok for service

inspectionR&R ELT Batt op ck 1/2 g switch good Batt due 9/05. Inspect starter vibrator and switching for intermittent kick back R/H engine - Adjust Retard breaker to open at proper crankshaft position - all switching verified - vibrator suspect if persists ok for service ops cked good

repairoil leak R/H engine oil pump cover is Resealed using silkthread method Ref 10-550 O.M. left oil temp plug resoldered. LH RPM transmitter R&R with overhaul 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 F/C good I certify this aircraft inspected IAW annual inspection and determined to be in airworthy condition and ok for continued service

inspectionLube MLG uplock Rollers iaw AD 72-22-01 ok for service

inspection[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. [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. [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 96-910011-205, cowl strips P/N 96-910011-193 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, [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. [352] Fabricated, primed, painted and installed nose door actuator bracket. Operationally checked good. [354] Nose gear torque link bushings, bolts and pins replaced. [500] ANNUAL INSPECTION – complied with in accordance with the Beech Baron 58 Shop Manual inspection guide.

annual[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.

inspectionALTIMETER TEST: 1000' (20 scale error), 2000' (40), 3000' (40), 10000' (60), 16000' (80), 20000' (90). ALTIMETER SERIAL NO. 67H4046. CASE LEAK O. HYSTERESIS TEST PERFORMED.

inspectionI CERTIFY THAT THE STATIC PRESSURE SYSTEM, ALTIMETER INSTRUMENTS, AND AUTOMATIC PRESSURE ALTITUDE REPORTING SYSTEM HAVE BEEN TETED 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: 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 W/O: AG-01-02479

repairFOUND RIGHT MAIN FUEL CELL LEAKING. REMOVED OLD FUEL CELL AN INSTALLED NEW FUEL CELL PART NO 35-9009-2S, SERIAL NO 426. LEAK CHECKED SATISFACTORY

annualC/W 100 HR/ ANNUAL INSP. REPLACED ELT BATT PACK NRXT DUE JUN 02, ADJUSTED R/H INBD GEAR DOOR INSTALLED NEW ELT ANTENNA P/N 110-324. INSTALLED NEW TAXI LAMP REPLACED R/H FWD FUSELAGE QUICK FUEL DRAIN. REMOVED R/H ENG COWL FLAP MOTER AND INSTALLED NEW POWER WIRES. C/W AD 72-22-01 UP LOCK ROLLER. C/W AD 76-02-12 ENG MOUNT INSP. C/W AD 91-15-20 BINDEX IGN 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 AIR-WORTHY 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 S/N none. Details of this inspection are on file at this repair station under WO #9194-1 Date 7-13-99

inspectionI certify that each automatic pressure altitude reporting system tests and inspections required by FAR 91.411 have been performed. LH Altimeter S/N 67H4046 Tested To 20000 ft. Encoder S/N 24566 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 LINNINGS, INSTALLED NEW SEALS L/H BRAKE CALIPER, SERVICED ALL SYSTEMS, C/W AD 72-22-01 UP LOCK ROLLERS, AD 91-15-20 ENG MOUNT, 76-07-12 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.

inspectionC/W BEECHCRAFT BARON 55 100 HR INSPECTION. C/W AD 72-22-01 INSP & LUBE UPLOCK ROLLERS NEXT DUE 382.0, C/W AD 76-07-12 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 OUTBORD BEARING P/N MS28795-35600003 AND CENTER BEARING K3L4S160, INSTALLED NEW ELT BATT PACK P/N 00-10-009 NEXT DUE JUNE 2000, INSTALLED NEW O RINGS P/N MS28775-222 R/H BRAKE CALIPER.

annualI CERTIFY THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

replacementINSTALLED OVERHAULED DUKES FUEL BOOST PUMP R/H SIDE.

alterationINSTALLED INFLATABLE DOOR SEAL KIT BY AEROCESSORIES STC# 4184WE, COMPLIED WITH AD 97-14-15 CABIN DOOR LATCH OPS CK GOOD

repairReplaced 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 each automatic pressure altitude reporting system tests and inspections required by FAR 91.411 have been performed. LH Altimeter S/N 74404 Tested To 20000 ft. RH Altimeter S/N 24566 Tested To 20000 ft.

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

annualPerformed an Annual inspection/service This date per FAR 43 Appendix D and Beech maint manual. Engs ran-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 5/4/97 for details. See individual engine logs for details of engine insp/service. Engines RAN + 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

repairRemoved L/H Engine Tri-Guage and installed P/N 22804-08-1 S/N 39513P overhauled gauge. Overhauled by S.D Chapdelaine under their WO # 55745. Operationally checked - leak tested + found OK.

alteration1) Removed Northstar Loran, Antenna and Antenna Coupling unit. 2) Installed GPS Receiver and GPS Antenna. Also 3way c/b for GPS, also coupled to HSI. 3) Installed Argus 5000 - 2way c/b, Remote Info & Select Switches. 4) Hard wired Intercom into aircraft. All systems ground checked good.

repairREPAIRED #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.

otherA/C Paint Colors: Alumagrip Blue-G5041, Gray-G1009, White-G8003, Burgundy-G7305

repairAircraft stripped etched primed and painted Controls balanced after painting installed new NO 2 Rudder [illegible] & LH INBD & center elevator bearings all work done in occodance with A/C Service manual and appropriate F.A.R.

annualI 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. Removed 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.

repairInstalled 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.

inspectionATC Transponder test, King KT-76, S/N 37134, WO# 17800. Altimeter test, Weston, P/N 22-374-B01, S/N 67H 4046.

inspectionATC Transponder test, King KT-76, S/N 37134, WO# 17800. Altimeter test, Weston, P/N 22-374-B01, S/N 67H 4046.

annualAnnual inspection completed; all controls checked & lubed; wheels & brakes checked; Replaced Hobbs meter with new; Replaced right vacuum regulator & adjusted; wheels & brakes checked; replaced right tire tube with Goodyear FLC II; ELT removed for repair - Placard installed on panel; Gear retraction checked OK; emergency extension checked; landing gear greased - C/W A.D. 72-22-01 By lubing up locks; C/W A.D. 91-15-20 By inspection of engine mounts; C/W A.D. 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; brakes bled; replaced left main tire with new AC-II; replaced all four engine cowl door hinges; replaced right up lock cable system rerigged; lights checked & repaired as needed; batteries serviced; replaced gear door rods at transmission; repaired shorted wire in right throttle switch; replaced right alternator & drive assy with overhauled units; see yellow tag; C/W A.D. 72-22-01 By greasing up fork roller; 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. Oxygen bottle hydrostatic tested see yellow tag

otherLog book closed - see log book #2.

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

ad compliance89-25-8 dye penetrant spar fitting check for [illegible] rivets

annual100 HR/ANNUAL INSP. COMPLETED. AIRFRAME & CONTROL SYST INSP. AND LUBRICATED. LOOSE ELEVATOR AND AILERON CABLES LOOSE, RE-ADJUSTED AS NECESSARY. REPLACED BOTH AILERON PUSH ROD BEARINGS, LEFT PUSH RODS. REPLACED, RESEALED ELEVATOR PUSH ROD BEARINGS. REPLACED LEFT ELEVATOR TRIM TAB BOLT WHEEL BEARINGS CLEANED INSP AND PACKED. BRAKE SYST INSP. AND SERVICED. GEAR SYSTEM INSPECTED & LUBRICATED. NOSE WHEEL STEERING AND TORQUE LINK BUSHINGS AND BOLTS REPLACED AS NECESSARY, STRUTS SERVICED, GEAR RETRACTION CHECK COMPLETED. UPKEEP NUTRIENT LUBRICATED AS PER PART A.D. 72-12-01. ANTI-ICING FLUID SYST SERVICED. ELECTRICAL SYSTEM SERVICED, BATTERY SERVICED, INSP. PITOT HEAT/AIR SPEED HEAD. REPLACED BOTH ENGINE MOUNTS INSP. FOR CRACKS AS PER AD 91-15-20. VACUUM/PRESSURE SYSTEM FILTERS REPLACED. (CONTINUED NEXT PAGE)

annual100/ANNUAL CONTINUED) BOTH ENG COWLS CRACK REPAIRED. NEW G47 BATTERY WITH REPLACEMENT DATE OF NOV. 95, INSTALLED. AD 91-17 ENGINE. FUEL FLOW AND GEAR UP WARNING HORN, ACT TESTED FOR SYSTEM OPERATION OK. AD STATUS THRU. 93-23 CHECKED. SEE A.D. STATUS PRENABLE. I CERTIFY THAT THIS ACFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE AIRWORTHY CONDITION

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

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 20000 ft. on 8-3-93

alterationInstalled Engine Model # IO-550-C, Serial # 271787-R in Lt. hand position and IO-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.

alterationMajor repair and alteration performed.

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 data 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.

ad complianceAD 90-15-20 Eng Mounts, c/w insp. eng mounts per BE BL 2362.

ad complianceAD 72-22-01 Clean & Lube Up Lock Rollers

ad complianceAD 77-13-22 Left Crankcase Cracks, c/w one (1) inch crack at #2 cyl thru bolt.

ad complianceAD 77-13-22 Right Crankcase Cracks, c/w no cracks observed.

ad complianceAD 91-17-01 Elev Trim Actuators, c/w per BE BL 2374 dtd Mar 91.

ad complianceAD 91-15-04 Props are oil filled, Check for leaks inw, Phr ok.

inspectionThis 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 301-015-090 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 ops 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 72-22-01 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

ad complianceAD 91-15-20 Inspect Eng Mounts, c/w by insp. eng mounts in accordance with BE BL 2362. No cracks noted.

ad complianceAD 72-22-01 Lube Up Lock Rollers

ad complianceAD 77-13-22 Left Eng Crankcase Cracks, c/w one inch crack at #2 cyl thru bolt.

ad complianceAD 77-13-22 Rt Eng Crankcase Cracks, c/w no cracks noted.

replacementREPLACED RIGHT MAIN TIRE & TUBE WITH USED TIRE & TUBE. REPLACED NOSE TIRE & TUBE WITH NEW TIRE & TUBE.

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 lugs and painted to match existing paint scheme.

ad complianceComplied with AD 90-08-14 by inspection in accordance with AD paragraph (a) and Beechcraft service bulletin No. 2269 Revision 1. Inspection performed using ZYGLO penetrate inspection method. No cracks noted, due again at 2972.2 total acft time.

ad complianceAD 77-13-22 Crankcase Cracks, Left Engine, c/w by insp. one inch crack at #2 cyl top thru bolt.

ad complianceAD 77-13-22 Crankcase Cracks, Right Engine, c/w by insp. no cracks noted.

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.

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

inspectionMETER CORRECTION SHEET: TCI D120 P2-T, SN 24566. Altitude pressure and friction test, barometric scale error, and case leak test performed.

inspectionMETER CORRECTION SHEET: 374, SN 67H4046. Altitude pressure and friction test, barometric scale error, and case leak test performed.

inspectionALTIMETER CORRECTION SHEET: Model 374, Part No 20-374-301, Serial No 67H4046. Altitude pressure and friction test, barometric scale error, and case leak test performed.

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

replacementREPLACED LEFT ENGINE GUAGE WITH OVERHAULED UNIT.

inspectionReplaced all brake linings. C/W AD 77-22-01 [illegible] cleaning & lubing uplock roller. C/W AD 76-7-12 ops check mag switch C/W AD 77-13-22 Check both crankcase for cracks. O.K. C/W AD 87-05-02 and 99-4144 Elevator fitting inspection as per SB 2242 fittings are aluminum O.K.) Clean & Repaired Battery Bell & control drain. Reseal Rt wheel cyl. Replaced outer bearing & bushings left elevator. Replaced landing lights. Replace left hyd accumulator. C/W Beech SB 2269 check center section spar attach fitting AD

ad compliance77-13-22 Eng case insp check visual oil; 72-22-01 Lube & cln

ad compliance87-05-07 Elevator attach [illegible] inspect per SB aluminum

repairReplaced left fuel boost pump P/N [illegible] [illegible] installed S/N 1406

annualAll routine maintenance performed this date IAW inspection form. Gear retraction performed IAW service manual, L/H cowl flap actuator O/H. G27 battery due Jul 1990, shimmy dampner O-rings, Gill G-25 battery replaced, brake linings replaced, taxi lite bracket replaced, nose seal foam

ad compliance77-13-22 ENGINE CASES Check for cracks.

ad compliance72-22-01 UROCK ROLLERS Grease rollers.

ad compliance76-7-12 BENDIX SWITCH Operational check

repairREPLACED MIXTURE CONTROL CABLE ASSY ON LEFT SIDE

replacementREPLACED ALL LIERT BRAKE LININGS P/N 66-22- TEST O.K. - LUBE NOSE STRUT. ALSO SERVICED BRAKE RESERVOIR.

replacementREPLACE L/H VACUUM PUMP & FILTER

inspectionGear retraction test done. Changed both main tires. Lubed aircraft. Checked flight controls. I certify that this aircraft has been inspected in accordance with a annual inspection and was determined to be in airworthy condition. Researched A.D's through issue no. 8-25-86

replacementReplaced 52D67 Horizon gyro with same P/N gyro P/N X78270H OP's chkd OK. David [illegible] Austin Jet Corp. R.S.# 210-74

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

repairMAIN TIRES rotated and BEARINGS checked and REINSTALLED.

inspectionRamp Check VOR/LOC for #1 Nav/Com KK170B +/- 1 degree #2 Nav/Com +/- 1 degree

annualReplace ELT Batts dated "June 87", the altimeter & digitizer repaired & checked by [illegible] Co for IFR & certify the static system test required by FAR 91.171 have been performed this date. Replace Lt vac filter & gaskets, press check & leak check A/C & fuel system, rev. blades & battery. Replace Rt prop spinner bulkhead.

replacementReplaced the right vacuum pump & filter. Replaced the left tach generator.

replacementReplaced all prop anti ice boots, replaced the heater fuel pump and the heater ignition unit.

repairClutch heater apparatus, clean fuel pumps & screens. Repair cabin door handle.

inspectionNew Main Wheel Tires & Brake Disc. Repack all wheel brgs. Reseal wheel cyls & service. 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. Press Check Cabin Heater, Replace Press Filter RT eng. Rework Escape Window & Install Placard per ST 1241 & AD 84-9-1. C/K AD 76-7-12.

ad compliance94-9-1 Emergency Egress trim latch & [illegible]

replacementINSTALLED FUEL QTY GAGE KIT P/N 55-9019-5S S/N 150 IN LEFT WING AS PER BSI 925R3

replacementReplaced Lft & Right main tires and tubes 6.50 x 8 6 ply Flight Custom II tires & 6.50 x 8 new tubes. Replaced nose tire 500 x 5 10 ply.

repairCheck Installation of New Botts by owner; Install R.H. landing light.

alterationInstalled 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. The Altimeter and Static System Test required by F.A.R. 91.171 has been performed. Altimeter Mfg. Weston Model # 22-374-801 S/N 69H494 Certified To 20,000 Feet by Garner Instrument Dated 6/13/83. System meets operational requirements of F.A.R. 91.71.

inspectionAll work filed under work order # 37053. The Blind Encoder and Static System Test required by F.A.R. 91.171 has been performed. Blind Encoder Mfg. Transcal Model # D120P2-T S/N 24864. Certified to 20000 Feet by Garner Inst. Dated 6/13/83. System meets operational requirements of F.A.R. 91.171.

inspectionAll work filed under work order # 37053. 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 S/N 37134. Transponder Model # N/A S/N N/A.

annualInstall new main tires, repach brg. Replace brake linings. Reseal LT master cyl. Replace vac system filters. Reseal fuel drains as needed. Serv brakes & batteries. Jock A/C gear & adj LT up lock. Check heater for leaks. Hobbs 36.6. AD 82-7-3 NA model. New ELT battery dated 'Jan 85', serv shimmy damper. I CERTIFY THAT THIS A/C HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

otherMake Beechcraft Model D55 N N18MJ SN TE-455. The aircraft identified above was painted in accordance with current FAR's. [illegible] controls were balanced in accor [illegible] with curren [illegible] is recommendations and is approved for return to svc.

repairProp OK & conformed to oil filled Hubs by Hartzell. New S/N Hubs RT S/N 815854 RT S/N 815857. Install taxi light on nose gear. [illegible] from nose gear [illegible] gear close

alterationCOMPLIED WITH BS1 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

repairCheck elevator system & cable tension

repairInstall new nose wheel tire, repack wheel brg. New LT cowl flap actuator

annualJanitrol Heater AD 82-7-3 [illegible] on Heater Hobbs Meter or [illegible] which ever first. M.C. Canly Prop Dye Checked 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 & Leube up Loh Rollers aileron Trim Tab Bushings Tightend, Service Brakes & Battries Repair RT Nacell cowling. Bendix Mag Serv CK OK Per AD 76-7-12

alterationPLACARD Panel showing R-NAV Approval for IFR enroute & Approach per 337 Dated 9-17-81.

repairclean prop alchol pump Filter & orifice at each prop. Remove O2 manifold

repairReseal Nose strut, Install Single Control wheel assy, Club Seats & Lube Throttle Swich

replacementReplace all Fuel Cells with Factory New Kit # 35-9009-15, 359009-25, 359009-35 359009-45 - Baffled Fuel Cells. LT main S/N 45775 Uniroyal 35-380135-11 TSO-C80. RT main SN W5122 Uniroyal OCT, 80. 35-380135-12 TSO-C80. LT Aux SN 81-13449 Goodyear BJC-85 P/N 95-920011-13 LH June 81. RT Aux SN 80-10164 Goodyear BJC85 P/N 95-920011-14 RH mar 80. AD 78-5-6 no Longer applicable. Install New vac system filter in off Months.

repairReplace plastic Lines to vac instrument, Replace Batteries Lube Elevator trim system, Replace Garlock filters on vac Reg's Replace Brakes Disc & Linings

repairRemove Hobbs Reading 475 & Install New Unit Reading 00. Replace vac Line to Art Horizon

alterationRemove King KX-160, KS-505, KR-201C, ADF T12B System, Beech B-11 antenna & misc wiring. Install King KMA-20, KR-86, KA-42B, KX-175B, KI-204, KN-73, Narco B.B. Comm ant, and Dorm Magoxim 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.

replacementExchanged the KSG 100 Remote DG.

replacementRemoved KSG-100 S/N 1582 and installed original slaved gyro. Repaired KPI-550A S/N LH39.

inspectionKing KT-76 Transponder tested in accordance with F.A.R. Part 43, Appendix F, and meets the requirements of F.A.R. 91.177. The 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. Next test due by 16 April 1983.

inspectionPress check fuel cells per Beech SI 895 & AD 78-5-6. Tighten vent line fitting, lt aux fuel cell. Lube up lock rollers, replace ELT batty dated 'Dec 82'. Install new batteries 1. P56-9 S/N 545108 & 1. P-25 Refat. Replace all fuel cap O-ring seals, replace seal lt main fuel cell drain, repair fuel leak rt main generator belt. AD 79-1-1 Tail hinge screw - NB has 'x' marked screw. Installed AD 80-9-10 NB mark of heater. I certify that this a/c has been inspected in accordance with a annual inspection and was determined to be in airworthy condition.

otherA/C OK for ferry flight TCC NM to Hereford

inspectionCheck trim tabs per Beech SI 0846-152 Rev 1. Replace two bolts in aileron trim tab rod ends. Reseal shimmy dampener. Repair aft front hinge at rt gear door. Press check fuel cells per SI 895. AD 78-5-6 (Cked & has BTC-39 cells installed). Mag switch ok per AD 76-7-12. Lube sd. gear. Replace hose in vac system. Replace flap rubber bumpers. E.H. & Battery replaced (Mar 1980). Replaced bulb in upper strobe light. I certify that this a/c has been inspected in accordance with a annual inspection and was determined to be in airworthy condition.

ad compliance76-19-4 McCauley Prop Dye checks

ad compliance76-7-12 Bendix Sw [illegible]

ad compliance77-13.22 TCM C.case visual

ad compliance78-5-6 Goodyer Fuel Cells Press ck

otherA/C ck ok Ferry Flt TCC to H.Pd

annualChuck Airframe Repair & John [illegible] Install New Filter - R&L prepump. Repair Door Latch. Install new Nose Wheel Tire & Repair Wheel Brgs. Lube & gear uplock Rollers. I CERTIFY THAT THIS A/C HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

alterationRemoved: Regency Control Head RT, Antenna Coupler, Coax & Harness, Installed King KT-76 & Transcal Digitizer D120P2-T. Static system leaked checked per FAR 91.120. New Empty Weight (lbs.) 3365.55 New Empty Weight (C.G.) 28.56, New Useful Load 1934.45

repairPer AD-75-16-10 Par 'A' Install new Rad P# 96-520013-7) (Par 'B' install nose Rivet & step Rim #M520435 P3-8 & 96-524032 - Beech Kit # 55-4020-15 S/N 1526.) (Par 'C' N/A Model & S/N) (Par 'D' Install New Tubing # 96-610006-69 & 70) (Par 'E' N/A S-N) (Par 'F' N/A model) The Above installed per Beech SI 0610-152 All Controls Painted & Elevators Re Balanced per Beech Maint manual. Install Beech Airplane Fuel Boost Pump Kit 55-9011-19 S/N 153 per SI 0584-285. Both R&L Main Gear Reseal R&L Main gear shock struts & service Brakes. A/C jacked & gear Lubed & Retraction Test Run OK.

ad compliance75-16-10 Elevator Trim Tab C/w

ad compliance76-4-7 window Emergency C/w Nos markings

ad compliance76-7-12 Bendix switch Run up ck Manuals

annualInstall nose gear retract Rodt ends. Per Beech SI 0600-205, Chuck Gear retraction & Lube. Install Kit Per Beech SI 0118-243 Kit # 55-40274 S/N 246 on nose caps of engine Nacells. & Repair side of cowling. Chuck Complete A/C & Contrs. Clean out rats nest Insulation in wingst Engin Nacally. Serv Prop accumlator. Install New Broke & linings. Serv nose gear Struts with Fluid. AD 75-5-3 Due another 100 hr. I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

alterationE.L.T Installed. + 2.2 lbs PT 240" + 480 New Ewt 3373.5 New CG 78.29 New moment 264122.1

annualInstall new nose tires Ck & lube Gear Retraction Altimetry Ckd & Certified to 20,000' By Galvin [illegible] I certify that the static system ck per FAR 91.170 Have been Performed. Installe Fuel flow per Ad 73-21-2 I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

ad complianceAD 73-13-3 Fuel Hose Sept c/w.

ad complianceAD 73-21-2 Fuel Hoses c/w.

alterationInstall KN-74 RNav- Placard VFR only, KX-170A/KA39/KN-73 KN-65/265/KPF-550A System per manufacturers Instru. fwd 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

annualChuck Controls & Cables. AD 72-11-2 Fuel Cells & Placards C/W. & Flt manual Bpt To Date 72-17-2 Grease Bolts in Sd Gear [illegible]. C/w this date 72-22-1 Grease Rollers in Sd Gear C/w. this date Left oil Temp Ckt Rep By Damer Just. alternator drives to be Checked at 400 hr. A/C Jacked & Gear Lube & Cked OK. I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

ad complianceAD 72-11-2 Fuel Cells & phascady c/w.

ad complianceAD 72-17-2 Grease Bolts c/w.

ad complianceAD 72-22-1 Grease Rollers c/w.

inspectionInspected as per applicable Beech Inspection guide. Repaired L.H. aux fuel cap. Replaced both battery terminal boots Replaced static cable. Reseald Shimmy 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 scissors. 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 (inspt pneumatic press. reg valves & lines). Complied with BSI 0442-324 (rerouting cig lighter wire). Rebushed L/H & R/H elev. trim tab actuating brackets. Lubed uplock rollers as per BSL 66-13. AD 68-26-6 has been previously complied with. The altimeter was certified for IFR flight by Garner instrument to 20,000ft & the static system was checked as per FAR 91.170. Continued Next page

ad compliance71-18-2 Counterwt. Due before 950 hrs. P/c/w

ad complianceAD 72-1-2 Remove plastic oil drain c/w.

repairReplaced the control wheel adapter as per AD 71-12-4. Removed D.G. for repair at Garner Instrument & replace.

ad complianceAD 71-24-10 Control wheel adpt. c/w.

repairInstalled Gyro pressure filter covers Both Engs. - Installed Both Voltage Regulators - Sys operates Normal -

annualChech controls & cables. Chech gear retraction & lube. Service brakes & battery. D.G. Gyro removed & O.H. by Garner Inst. Co. AD 70-15-18 Mitchell auto pilot P/N - Has new style clamp. - I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

inspectionAD 68-26-6 C/w. Removed Grime [illegible]. Install Horton whelen WDTW Strobe lite. Mt [illegible] Neg[illegible] New nose Tire. Rep. [illegible]. I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

ad complianceS.B. #67-37 complied with.

ad complianceAD 68-10-7 Trim Tab Rep c/w.

alterationInstalled Bendix 504A 3 lite marker in accordance with AC 43.13-2. Weight change negligible.

100 hourh. meter reads 81 h. Installed new hour meter. Insp. all Cables, pulleys, turnbuckles & Control surfaces repack wheel bearings. Clean fuel screens Ser. Spring 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. Part to /w A.D. 68-10-7 are on back order from beech. Cey- A/c must be reiven when parts ARE Avizble. for compliance of Ad. Inspection

annualI certify that this Aircraft has been inspected in accordance with a Annual inspection and was determined to be in airworthy condition

inspectionChecked VORs

alterationInstalled King KX-160, KI-211, UDI-2 DME, 505 transponder, Mitchell AK 194 autopilot and Sky ox oxygen system. See FAA Form 337 this date for details

inspectionIn accordance with F. A. R. 91.25 Omni directional receivers were found to be accurate to [illegible] degrees

inspectionI have inspected this aircraft and found it complies with the requirements of FAR 21.183. Certificate of Airworthiness dated 11-16-67 was issued by.

replacementPROPELLER MODEL 2AF34C55H/S78FF-0 HUB SER'AL NO. 674659 Anti-icer feed shoes installed per FAA Spec. P5EA-11

replacementPROPELLER MODEL 2AF34C55H/S78FF-0 HUB SERIAL NO. 674659 Anti-icer feed shoes installed per FAA Spec. P5EA-11

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

otherManufacturer: Beech, Model: D55, Date of Mfg: 1968, Serial Number: TE-455, Registration Number: N18MD

inspectionALTIMETER INDICATOR CALIBRATION SERIAL NO. 433119. Data table: Test Settings -1000 to 12000, Reading values recorded.

inspection1. 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. #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.

otherEXTERIOR: NUMBER AF5 CUSTOM PAINTED BY Cimarron Aircraft Corp. BASE COAT 4321 Moondust PRIMARY 78387 Blue SECONDARY 63203 Blue 99 Black INTERIOR: BANFF BLUE 66004

otherManufacturer BEECH AIRCRAFT CORP. Place WICHITA, KANSAS License No. N5472U 18MD Type D55 Serial No. TE-455

other[illegible]

annual- Continued from previous page - I certify that this aircraft has been inspected in accordance with a Annual inspection and was determined to be in airworthy condition.

ad complianceChecked Mag Launch Per AD 76-7-12 Par 'A' Found to operate satisfactorily.

annualI CERTIFY THAT THIS A/C HAS BEEN INSPECTED IN ACCORDANCE WITH A ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

otherELT Battery Date 'July 77'

inspectionOperational checks per FAR Part 43, Appendix F, have been performed on King KT-76, serial number 34134, using IFR 200434 TIC-33B test equipment. Unit meets operational requirements as stated in above FAR.

otherELT Battery Date 'OCT 78'

annualJack aircraft run retraction test. ck emergency gear extend system. Remove right landing flap make and install skin patch. Clean all fuel filters. Service air induction filters. Repair left top cowling. Replace right top cowling with serviceable part. CK brake linings. Service battery and brake service. Inspect in accordance with Beech inspection data. Replenished air fuel boost pump for left engine with new pump.

repairRan gear check. Replaced nose wheel bearing & races

inspectionI certify that the transponder test required by FAR 91.413 has been performed this date and found to comply. Transponder King K 176 sn 37134.

replacementInstalled New 8.50x8 8ply Tires L&R New Tube RH MAIN

annualI certify that this aircraft has been inspected IAW an annual inspection and was determined to be in an airworthy condition

annualAcft 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 & rotated tires. Installed new taxi lamp & left lower nav light. CW AD 72-22-01 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 Hans CW AD 91-17-01 DTD 15 NOV 91 by color coding elev trim actuators Blue/Light Black Rust. CW AD 91-15-04 DTD 7 Aug 91 by insp oil filter props IAW PHAF" 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

ad compliance72-2-6 Mitchel Bridle cable clamp - Nos New Style

ad compliance82-7-3 Janitrol Heater NA model of heater

ad compliance72.24-4 McCauley prop Dye ck

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. ~~~ Nothing follows ~~~

annualAnnual 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.

other***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.

annualMaintenance 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 10-550 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.

otherDrained 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 ~~~

otherDrained 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 ~~~

annualCompleted 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.

otherDrained 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 [illegible] and checked RPM, MAP and fuel flow

overhaulDisassembled 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 Inc. 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 the W/O: W059700 dated 12 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: F211A065R 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.

repairRemoved engine IO-550-C serial number 684240 for repairs.

otherDrained 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 ~~~

otherDrained 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.

otherDrained 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.

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- 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.

repairInstalled IO-550C engine serial 684240 after major overhaul from Western Skyways Inc. 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. 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.

overhaulEngine overhaul by Western Skyways, Inc. Engine serial 684240, model IO-550-C. Overhauled to Factory New Tolerances per Overhaul Manual M-16 and Repair Specification WSI-100.

ad complianceCompliance recorded for ADs: 74-26-09, 82-13-01, 82-20-01, 86-13-04 R3, 88-03-06, 81-19-03, 93-08-17, 93-10-82, 93-16-15, 94-01-03 R2, 94-06-09, 95-03-14, 95-21-15, PL98-01-08, 99-19-01, 2000-23-21, 2004-08-10, 2007-04-19, 2007-04-19R1, 2009-19-07, 2010-11-04, 2012-06-06, 2014-05-29, 2016-16-12.

repairInstalled Cam Gear P/N: 2078-1. This satisfies the requirements of MSB05-8D.

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.

repairRemove 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 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 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.

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 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.

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.

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

100 hour11/2/2015 HOBBS: 1664.2 TSOH: 1880.2 Left Engine Make: 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

100 hour11/4/2014 HOBBS: 1596.3 TSOH: 1812.3 Left Engine Make: 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 changeRATE = 4-22-2014 HOBBS: 1575.3 CHANGED OIL - SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50XC & AVBLEND

replacementSky-Tec Starter Model C24ST5 Serial No. 4C5-471323 installed on N18MD.

repairREMOVED #6 CYLINDER DUE TO EXHAUST LEAKAGE. O/H PERFORMED BY D&B AIRCRAFT ENGINES. REINSTALLED CYLINDER ASSY IAW TCM MANUAL. OPS CHECK GOOD.

100 hour11/10/2013 HOBBS: 1531.4 TSOH: 1747.4 Left Engine Make: 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.

100 hour11/02/2012 HOBBS: 1465.3 TSOH: 1682.3 Left Engine Make: 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 & CAMGUARD ADDITIVE.

repairREMOVED #5 CYLINDER FOR CRACK. REPLACED #5 CYLINDER WITH EXCHANGE O/H CYLINDER. REMOVED #3 CYLINDER FOR O/H. CYLINDER OVERHAULED BY DEB AIRCRAFT ENGINES. REPLACED #3 CYLINDER. OPS CHECK GOOD BOTH CYLINDERS. R&R ALTERNATOR REWORKED BY DEB 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.

repairREPLACED INBOARD EXHAUST ASSEMBLY WITH NEW PART FROM KMISELY.

oil changeOIL CHANGE - REPLACED OIL FILTER WITH NEW CH48108-1 FILTER. SERVICED ENGINE WITH 11 QT 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 changeCHANGED OIL SERVICED WITH 11 QTS PHILLIPS 20/50 XC.

repairREPLACED #1 CYLINDER WITH OVERHAULED ASSEMBLY. CHANGED OIL, SERVICED WITH 11 QTS 50W MINERAL OIL FOR BREAK-IN. OPS 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 changeOIL CHANGE - 20/50 PHILIPS

100 hourPerformed 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.

replacementREPLACED IGNITION LEADS WITH NEW P/N C14-435-11

replacementREPLACED ALL LORD ENGINE MOUNTS WITH NEW P/N J-10778-14

repairREPLACED 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

100 hourPerformed 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 hourPerformed 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.

100 hour100Hour 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.

100 hour100hr 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.

repairREPLACED # 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

repairDALLAS AIR REPAIR-NW REGIONAL AIRPORT LEFT. DATE: 10/02/03. N# 18MD. MAKE/MODEL:TCM IO-550-C7F. S/N: 271787-R. TTAF: 923.1. SMOH: 2[illegible]113?. PROP O/H: 923.1. DRAINED 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.

annualANNUAL 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. 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. Installed new alternator base gasket.

replacementReplaced instrument air pump with overhauled unit from Aero Accessories, Inc. (Airborne 212CW S/N 09144) Ground run ok

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.

annualC/W 100hr inspection. Replaced spark plugs, comp ck #1) 65 #2) 74 #3) 70 #4) 51 #5) 75 #6) 51. I certify this engine has been inspected in accordance with an annual inspection and was determined to be in airworthy condition.

annualC/W 100hr insp. Changed oil with 10W Aeroshell oil replaced filter. I certify this eng has been inspected in accordance with an annual inspection and was determined to be in airworthy condition.

repairAdjusted metered and unmetered fuel pressure and idle mixture

annualC/W 100hr insp as per Beechcraft Baron 55 manual, replaced induction air filter element BA6205, replaced lower spark plugs with new RHB32E, comp ck over poles #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.

repairRemove #2 position and installed overhauled cyl and valve assy (Cirminela) ran up and leak cked

annualEng log insp/service performed this date in conjunction with A&P Annual insp per FAR 43 App D and MFG's manuals, eng ran up, oil drained, filter replaced, screen cleaned, spark plugs cleaned, gapped, checked, rotated & reinstalled. Compression check hot @ 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 I.A.W.A 100 hour insp and was found to be in airworthy condition.

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 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 mag timing checked ok; oil changed- refilled with Aeroshell 15W50; oil filter inspected & replaced; fuel nozzle cleaned; spark plugs cleaned & gapped; air filter cleaned; exhaust inspected ok.

100 hourCompression 1)70 2)68 3)69 4)70 5)72 6)70 mag timing checked ok; oil filter inspected & changed; oil changed; spark plugs cleaned & gapped; fuel nozzle cleaned; exhaust system inspected ok.

100 hour78.0 since annual; 78.0 since rebuild. 100 HR INSP. COMPLETED. DIFF. COMPRESSION CHECKS #1: 70, #2: 66, #3: 71, #4: 76, #5: 64, #6: 70 over 80. OIL SCREEN RNS MAG. TO ENGINE. TIMING CHECKED. SPARK PLUGS CLEANED. EXHAUST SYS INSP. FUEL INJECTION NOZZLES CLEANED. AIR FILTERS INSP. ENG OPERATIONALLY CHECKED OK.

otherDynamic Balanced & Vibration Tracked This A/C Spinner - Propeller - Engine Comb. as per "specs". See Aircraft Log for Complete Entry.

replacementTach 2182.7. Maintenance release from Aero Electric, Inc. for overhauled Tach Generator, P/N EM8000RX/0850350-5RX, S/N 563.

repairInstalled this Engine in Left hand position of Aircraft N 18MD, Model D-55, Serial # TE-455. This Installation performed IAW D'Shannon Products STC # SA 3845 SW Drawings + instructions. Washed ground run + adjusted per TCM Bulletin M 89-10. 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 IO-550C7F, 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: M86-7: REPLACED WITH NEW PART; M88-4: REPLACED WITH NEW PART; M90-21: ULTRASONIC INSPECTION OF BARRELS; M91-6: ULTRASONIC INSPECTION OF BARRELS; M92-6: ROCKER SHAFT RETENTION IMPROVED; M92-13: REPLACED WITH NEW PART; M92-14: VISUAL INSPECTION; M91-7: ULTRASONIC INSPECTION OF BARRELS; 91-19-03: REPLACED OIL FILTER

otherIO-550C engine encountered abnormal oil consumption, followed by smoke from the left propeller spinner, leading to an emergency landing at Taos, New Mexico (KSKX).

repairEngine failure investigation at Taos, New Mexico. #6 connecting rod failure resulted in a hole in the engine case. The engine was subsequently removed and replaced by Western Skyways.

replacementReplacement of IO-550C engine and propeller repair performed by Western Skyways. Failure determined to be a missing oil plug in the camshaft (Continental manufacturing defect) which caused internal oil leakage and eventual #6 main bearing failure.

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.

inspectioninspected, replaced #3) 70 #4) 51 ... engine has been inspected in accordance with an annual inspection and was determined to be in airworthy condition. Oil filter Champion CH48108 - none found. Run ok - no leaks. Replaced with overhauled unit 212CW S/N 09144, A&P.

repairDALLAS AIRPORT LEFT. N# 18MD. S/N: 271787-R. HOBBS: 923.1. DRAINED OIL. SERVICED WITH 12 QTS. OF AEROSHELL 100W. REPLACED LH EGT PROBE P/N 86255. REPLACED LT. TACH GENERATOR. RETURN TO SERVICE.

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.

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.

replacementRemoved 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 overhauled 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 qtrs. 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. Alternator installed after overhaul P/N 1100723 S/N H-010726 Per MM E 24 Sec. 13 Ran and ops checked ok. Installed Overhauled Alternator drive clutch from Quality Aircraft accessories W/O M 732370. MM ref E24 Sec.13. Next check 500 hours. Engine baffling in poor condition Customer declined repair at this time. Replaced gear warning switch at FCU. Per. MM E-17 Sec 5. Replaced missing exhaust stud per Mm IO 550 overhaul. C/W AD 91-15-20 Engine mount inspection per SB 2362R 1. No problem noted at this time. Next due 5539.2 TT.

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.

ad complianceAirworthiness Directives Compliance Report for Continental IO-550-C S/N 686473. Lists compliance for ADs: 88-13-04 R3, 88-03-06, 91-19-03, 93-10-02, 93-16-15, 85-03-14, 95-21-15, 98-01-08, 99-18-01, 2000-23-21, 2004-08-10, 2007-04-19 R1, 2009-19-07, 2010-11-04, 2012-03-06, 2014-05-29, 2016-16-12, 2022-16-03, 2023-02-12, 2023-05-16, 2023-17-04.

annualMaintenance at Annual: 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. 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

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 ~~~

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.

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- 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 changeDrained 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. ~~~

repairRemoved 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 changeDrained 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.

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 (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) 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

repairRight 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.

otherRemove 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 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 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 hourPerformed 100 hour inspection with reference to TCM & Beechcraft Service Manuals. Inspected all hoses, fluid lines, and hamesses. 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 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) 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.

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

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 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 changeCHANGED OIL. SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50 XC & CAMGUARD

replacementREPLACED ALTERNATOR WITH O/H P/N 1100723 PART FROM QUALITY AIRCRAFT ACCESSORIES. OPS CHECK GOOD

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 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.

oil changeCHANGED OIL-SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50 XC & AVBLEND

replacementSky-Tec Starter Model C24ST5 installed on N18MD.

100 hourPerformed 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.

repairRemoved #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 hourPerformed 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.

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.

oil changeOIL CHANGE. REPLACED OIL FILTER WITH NEW CH48108-1 FILTER. SERVICED ENGINE WITH 11 QTS PHILLIPS 20/50XC & AUBEND ADDITIVE. CUT & INSPECTED OIL FILTER - NO METAL DETECTED

100 hourPerformed 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.

repairR&R PROPELLOR GOVERNOR FOR REPAIR BY BYAM PROPELLER SERVICE. CHANGED OIL SERVICED WITH 11 QTS PHILLIPS 20/50 XC + 1 PT AUBEND ADDITIVE

repairR&R PROPELLOR FOR RESEAL BY THE PROP SHOP. SEE RECORDS FOR DOCUMENTATION REPLACED CRANKSHAFT NOSE SEAL. OPS 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. 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 hourPerformed 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 hourPerformed 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.

replacement6/24/2008 HOBBS 1194 HRS. REPLACED IGNITION LEADS WITH NEW P/N C16-4BS-11.

replacement6/20/2008 HOBBS 1194 HRS. REPLACED ALL ENGINE LORD MOUNTS WITH NEW P/N J-10478-14.

repair6/14/2008 HOBB 1192 HRS. REPLACED SPARK PLUGS WITH NEW RHB32E, REPLACED IGNITION LEAD SPRINGS. REMOVED MAGNETOS - 500HR INSPECTION PERFORMED BY D&B AIRCRAFT ENGINES. REINSTALLED MAGNETOS, SET IGNITION TIMING. OPS CHECK GOOD.

100 hour11/2/2007 HOBBS: 1153.1 TSMOH: 492.5 N18MD. Make: 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: #1-67/80, #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.

100 hourN18MD. 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.

repairDALLAS AIR REPAIR-NW REGIONAL AIRPORT RIGHT. DATE: 10/02/03. N# 18MD. MAKE/MODEL: TCM IO-550-C7F. S/N: 271786-R. TTAF: SMOH: 263.1 PROP O/H: HOBBS: 923.1. DRAINED 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.

repairDALLAS AIR REPAIR-NW REGIONAL AIRPORT. DATE: 10/02/03. MAKE/MODEL: TCM IO-550-C7F. TTAF: SMOH: [illegible]. DRAINED 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.

oil changeoil change ch48108 nonetial infilter w100 okforserv

inspectionResealed engine oil leak at oil pump housing using silk thread method per IO550 S/M. C/W Annual inspection, compression within serviceable limits. Replaced engine oil CH48109. Filter, no debris in filter ok for service. I have inspected this engine I/A/W Annual inspection and have determined it to be airworthy and ok for continued service.

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

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

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

annual[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. [500] ANNUAL INSPECTION - complied with in accordance with the Beech Baron 58 Shop Manual inspection guide.

repairServiceable TCM Crankcase Model 10-520 Serial 860030. 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.

repairServiceable Continental camshaft Model 653058 A/H 649322A1 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. Work order no. 120002.

repairServiceable Part Tag for Continental IO-550-BB crankshaft. C/W AD 97-26-17 I/A/W PARA C 'ULTRASONIC INSPECT'.

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

replacementREPLACED VACUUM PUMP WITH OVERHAULED UNIT (C/W S/N 09145) A&P.

annualC/W 100 HR INSP. CHANGED OIL WITH 50 W. AARSHALL OIL REPLACED FILTER COMP CK GOOD. WASHED DOWN ENG I CERTIFY THIS ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

otherADJUSTED METERED AND UNMETERED FUEL PRESSURE AND IDLE MIXTURE.

annualC/W AN HUNDRED 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 LB #1) 46 #2) 24 #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

repairREMOVED #2 CYL AND INSTALLED OVERHAULD CYL AND VALVE ASSY (CIRMIRAL) RAN UP AND LEAK CK

annualEngine 100hr insp/service performed this date in conjunction with A/C Annual insp per FAR 43 App. D and MFG's manuals. ENG RAN up, oil drained, Filter repl, screen cleaned. Spark plugs cleaned, gapped, checked, rotated & reinstalled. Compression check Hot @ 80 psi #1-62 #2-60 #3-61 #4-62 #5-68 #6-62. Clamps & fasteners retorqued as req. ENG serviced with 12 quarts Aeroshell 100W detergent oil. Ran engine, no leaks noted, all pressures and indications normal. I certify that this engine was inspected I.A.W. A 100hr inspection and was found to be in airworthy condition.

inspectionC/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)68 mag Timing checked ok; oil changed-refilled with aeroshell 15w50; oil filter inspected ok & replaced; spark plugs cleaned & gapped; Exhaust system inspected ok; air filter cleaned;

inspectionCompression 1)71 2)70 3)69 4)71 5)69 6)71; oil changed - filter inspected ok; spark plugs cleaned & gapped; fuel nozzles cleaned; exhaust system inspected ok; magneto retimed; Engine washed & ground run ok.

100 hourCompression 1)71 2)70 3)69 4)71 5)69 6)71; oil changed - filter inspected ok; Spark plugs cleaned & gapped; fuel nozzles cleaned; exhaust system inspected ok; Magneto retimed; Engine washed & ground run ok.

replacementReplaced RH starter with O/H starter by Electro Systems. Operational checked ok.

replacementReplaced RH starter with O/H starter by Electro Systems. Operational checked ok.

repairReplaced RH eng pump, Adjusted unmetered press and pump operation.

repairReplaced RH engine driven fuel pump after repair by TCM. Adjusted unmetered pressure to 9.5 PSI @ 650 RPM. Eng run and pump operational checked OK.

replacementReplaced RH Fuel Pump (OH BY TCM)

replacementReplaced RH engine driven fuel pump. (OH By TCM) Pump failed to maintain pressure at low RPM.

repairPerformed compression check #1 70/80 #2 73/80 #3 71/80 #4 70/80 #5 72/80 #6 58/80. #6 cylinder has intake leak which persisted through several checks. Removed #6 cyl. Replaced intake valve ground exh valves and seats. Honed cylinder to ring finish. Cleaned pistons inspected, and installed new rings. Installed cyl. using new seals and gaskets. Eng run and checked OK.

otherDynamic Balanced This A/C Spinner - Propeller - Engine Comb. as per specs. See airframe log for complete entry.

replacementInstalled this Eng in Right hand position of Aircraft N18MD, model D-55, Serial# TE-455. This installation performed IAW D'Shannon Products STC# SA 3845SW Drawings & instructions, Washed ground run & adjusted per TCM Bulletin M89-10. See 337 Form, Wt & Balance/Equipment revised this date. Details on File under W.O. #10169, Installed using newer Existing Accessories & hardware.

overhaulThis engine model IO550C7F, Serial No. 271786-R, was rebuilt/zero timed on 02/24/93 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: M86-7 86-13-04 REPLACED WITH NEW PART, M88-4 88-03-06 REPLACED WITH NEW PART, M90-21 N/A ULTRASONIC INSPECTION OF BARRELS, M91-6 N/A ULTRASONIC INSPECTION OF BARRELS, M92-6 N/A ROCKER SHAFT RETENTION IMPROVED, M92-13 N/A REPLACED WITH NEW PART, M92-14 N/A VISUAL INSPECTION, M91-7 N/A ULTRASONIC INSPECTION OF BARRELS, N/A 91-19-03 REPLACED OIL FILTER

annualwith 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.

annual7/7 since rebuild 78.00. Hobbs 226.2. Annual insp completed. Diff comp: #1=77, #2=80, #3=76, #4=77, #5=77, #6=75 over 80. Oil screen insp ok. Mag to, eng timing corrected. Spark plugs cleaned and gapped. Fuel injector nozzles cleaned. Exhaust syst insp. Induction air filter insp. Eng compartment cleaned. CK. Fuel system check insp as per A.D. 93-16-15.

inspectionINSPECTION. REPLACED [illegible] #1) 72 [illegible] #6) 61 I CERTIFY IN ACCORDANCE WITH [illegible] AS DETERMINED TO BE [illegible] [illegible].

otherOIL FILTER CHAMPION CH48108 NONE FOUND. RUN OK - NO LEAKS.

annualC/W 100 HR ANNUAL INSPECTION. REPLACED BOTTOM SPARK PLUGS. COMP CK #1) 52 #2) 77 #3) 52 #4) 65 #5) 52 #6) 61. I CERTIFY THIS ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

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.

otherInstalled crankcase, New P/N 653058, s/n 860030, RH 1201 S/N A76804FB RT, X=47 and on Left, Ser# L168706F, X=49. Engine must be test run in accordance with M-89-7 Rev.1. Use non det. oil first 100 hrs.

overhaulEngine received for damage to Alt. drive gear, overhauled engine. Disassembled and inspected. Crankshaft inspected in accordance with AD 97-26-17C. Reassembled using new main bearings, rod bearings, rod bolts, nuts, certified camshaft, lifter assemblies, crankshaft seal, crankshaft gear bolts. Inspected cylinders, found no cracks, replaced guides, intake and exhaust valves, rocker shafts, piston and piston pin assy, and rings for steel cylinders. Complied with AD 96-12-07 on Bendix mags S6RN-1201.

leftinspectionPerformed routine inspection. Serviced hub and accumulator with dry nitrogen. I certify this propeller has been inspected in accordance with FAR 43 app. D, Annual/100hr Inspection criteria and determined airworthy.

rightannualPerformed routine inspection. Serviced hub and accumulator with dry nitrogen. I certify this propeller has been inspected in accordance with FAR 43 app. D, Annual/100hr Inspection criteria and determined airworthy.

leftinspectionCompleted annual inspection per service manual and FAR 43 appendix D. I certify this propeller was inspected IAW an annual inspection and was determined to be in airworthy condition.

rightannualCompleted annual inspection per service manual and FAR 43 appendix D. I certify this propeller was inspected IAW an annual inspection and was determined to be in airworthy condition.

leftreplacementRemoved propeller PHC-C3YF-2UF/FC7663B-2R for repairs. 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.

leftinspectionCompleted annual inspection per service manual and FAR 43 appendix D. I certify this propeller was inspected IAW an annual inspection and was determined to be in airworthy condition.

rightannualCompleted annual inspection per service manual and FAR 43 appendix D. Removed the propeller, rotated 180 degrees and reinstalled. I certify this propeller was inspected IAW an annual inspection and was determined to be in airworthy condition.

leftotherBeech D55 s/n TE-455 N18MD LH IO-550C s/n 684240

leftoverhaulPropeller completely overhauled IAW OTM 1170 rev 19, BOM 1336 rev 40, SPM 201A Service Manuals. All A.D's, S/B's, S/L's complied with to date. Pertinent details of this overhaul are on file under W.O. 021-502

leftannualCompleted annual inspection per service manual and FAR 43 appendix D. I certify this propeller was inspected IAW an annual inspection and was determined to be in airworthy condition.

rightannualCompleted annual inspection per service manual and FAR 43 appendix D. I certify this propeller was inspected IAW an annual inspection and was determined to be in airworthy condition.

leftrepairI certify this propeller was repaired and inspected in accordance with an annual inspection and was found to be in an airworthy condition. Serviced propeller hub with nitrogen. All airworthiness directives through January 2020 checked for compliance and recurrence. This propeller 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.

rightannualI certify this propeller was repaired and inspected in accordance with an annual inspection and was found to be in an airworthy condition. Serviced propeller hub with nitrogen. All airworthiness directives through January 2020 checked for compliance and recurrence. This propeller 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.

right100 hourPerformed 100 hour inspection with reference to Hartzell Manual 115N. Lubricated hub with Aeroshell 6. I Certify that the PROPELLER has been inspected I/A/W with a 100 hr Inspection and was determined to be Airworthy.

leftinspectionPerformed 100 hour inspection with reference to Hartzell Manual 115N. Lubricated hub with Aeroshell 6. I Certify that the PROPELLER has been inspected I/A/W with a 100 hr Inspection and was determined to be Airworthy.

rightinspectionPerformed 100 hour inspection with reference to Hartzell Manual 115N. Lubricated hub with Aeroshell 6. Dressed and painted blades. Dynamically balanced propeller. I Certify that the PROPELLER has been inspected I/A/W with a 100 hr Inspection and was determined to be Airworthy.

leftinspectionPerformed 100 hour inspection with reference to Hartzell Manual 115N. Lubricated hub with Aeroshell 6. Dressed and painted blades. Dynamically balanced propeller. I Certify that the PROPELLER has been inspected I/A/W with a 100 hr Inspection and was determined to be Airworthy.

rightinspectionI certify that this propeller has been inspected IAW a 100 hr inspection & was determined to be airworthy.

rightinspectionI certify that this propeller has been inspected IAW a 100 hr inspection & was determined to be airworthy.

rightinspectionI certify that this propeller has been inspected I/A/W a 100 hr inspection & was determined to be in an airworthy condition

rightinspectionI certify that this propeller has been inspected IAW a 100 hr inspection and was determined to be in an airworthy condition.

rightannualI certify that this propeller has been inspected IAW an annual inspection and was determined to be in an airworthy condition.

rightrepairReseale the above propeller as per Hartzell manuals 117D and 202A. No further action taken at this time

rightinspectionPerformed 100 hour inspection and lubrication in accordance with Hartzell Manual 115N. I certify that this propeller has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

leftinspectionPerformed 100 hour inspection and lubrication in accordance with Hartzell Manual 115N. I certify that this propeller has been inspected in accordance with an ANNUAL inspection and was determined to be in an airworthy condition.

rightrepairRESEALED THE ABOVE PROPELLERS DOME ASSY, AS PER HARTZELL MANUALS 117D AND 202A.CUSTOMER INSTALLED SPINNER ASSY. NO FURTHER ACTION TAKEN AT THIS TIME.

leftrepairMODEL: PHC-C3YF-2UF S/N: EB3411A BLADE M/N - FC7663-2R BLADE S/N - 1. H53231 BLADE S/N - 2. H53220 BLADE S/N - 3. H53224 RESEALED THE ABOVE PROPELLER AS PER HARTZELL MANUALS 117D AND 202A. NO FURTHER ACTION TAKEN AT THIS TIME.

rightinspectionPerformed 100 hour inspection and lubrication in accordance with Hartzell Manual 115N. I certify that this propeller has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

left100 hourPerformed 100 hour inspection and lubrication in accordance with Hartzell Manual 115N. I certify that this propeller has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

right100 hourPerformed 100 hour inspection and lubrication in accordance with Hartzell Manual 115N. I certify that this propeller has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

rightinspectionPerformed 100 hour inspection and lubrication in accordance with Hartzell Manual 115N. I certify that this propeller has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

left100 hourPerformed 100 hour inspection and lubrication in accordance with Hartzell Manual 115N. I certify that this propeller has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

left100 hourPerformed 100 hour inspection and lubrication in accordance with Hartzell Manual 115N. I certify that this propeller has been inspected in accordance with a 100 hour inspection and was determined to be in an airworthy condition.

rightannualThis date performed an annual inspection on this Propeller. Removed all nicks and painted back of blades flat black. I have inspected and determined that this prop has been found to be in airworthy condition.

leftinspectionThis date performed an annual inspection on this Propeller. Removed all nicks and painted back of blades flat black. I have inspected and determined that this prop has been found to be in airworthy condition.

rightrepairEvaluate blade S/N H53230 for previous prop blend - blade determined to be within min chord and thickness limits as Ref Hartzell S/B 61-13-33 Page 1111 7663E blades ok for service

rightinspectionInspected IAW 100hr/annual inspection and determined this propeller to be in an airworthy condition ok for service

leftinspectioninspected i a w Annual/100FH, and determined to be in an airworthy condition

rightannualANNUAL INSPECTION - complied with in accordance with the Beech Baron 58 Shop Manual inspection guide. I certify that this PROPELLER 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.

leftannual[500] ANNUAL INSPECTION - complied with in accordance with the Beech Baron 58 Shop Manual inspection guide. I certify that this PROPELLER 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.

rightannualI CERTIFY THIS PROPELLER HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION

leftannualI CERTIFY THIS PROPELLER HAS BEEN INSPECTED IN ACCORDANCE WITH AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION.

right100 hourI certify that this propeller has been inspected iaw a 100 hour inspection and is considered to be in an airworthy condition

leftinspectionI certify that this propeller has been inspected iaw a 100 hour inspection and is considered to be in airworthy condition.

rightotherCrew hour meter installed

leftinspection(New hour meter installed) I CERTIFY THAT THIS Propeller HAS BEEN INSPECTED IN ACCORDANCE WITH A 100hr INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION

leftinspectionPropeller HAS BEEN INSPECTED IN ACCORDANCE WITH A 100hr INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION

right100 hourI CERTIFY THAT THIS Propeller HAS BEEN INSPECTED IN ACCORDANCE WITH A 100HR INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION

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

rightinspectionI CERTIFY THAT THIS PROP HAS BEEN INSPECTED IN ACCORDANCE WITH A 100 HR INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION

leftrepairDynamic Balanced & Vibration Tracked This A/C Spinner - Propeller-Engine Comb, as per "specs". See Airframe Log for Complete Entry.

rightotherReinstalled this Propeller in AC N18MD after STC# SA3845. See Airframe Log Book entry for details.

leftalterationReinstalled this Propeller on AC N18MD after installation of STC # SA 3845SW. See [illegible] Details. [illegible] [illegible] [illegible]

rightotherProp installed on aircraft Beech D-55 N18MD.

leftreplacementInstalled this propeller on aircraft Beech D-55 N18MD

rightreplacementPROP S/N EB3410A INSTALLED NEW C2131-3 DE-ICE BOOTS AND STATIC BALANCED. REF: W/O #9300130

leftrepairPROP S/N EB 3411A INSTALLED NEW C2131-3 DE-ICE BOOTS AND STATIC BALANCED. REF: W/O # 9300130

rightotherNEW inspection C174190. Hartzell Order No. 30826. Part Number PHC-J3Y-2UF/FC7663-2R. Hub No. EC3411A. Blade Numbers: 1: H53231, 2: 53232, 3: 153224. Comments: A 2476-9 [illegible] [illegible] [illegible] [illegible] [illegible] [illegible].

rightinspectionI CERTIFY THAT THIS PROPELLER HAS BEEN INSPECTED IAW A 100 HOUR INSPECTION & WAS DETERMINED TO BE AN AIRWORTHY CONDITION

leftinspectionI CERTIFY THAT THIS PROPELLER HAS BEEN INSPECTED IAW A 100 HOUR INSPECTION AND WAS DETERMINED TO BE IN AN AIRWORTHY CONDITION