2009 Annual Inspection Airframe Logbook Entry

Transcription

1 2009 Annual Inspection Airframe Logbook Entry N724MC Cessna 150L ,528.4 Engine Lycoming O-320-A2B RL A 2, Propeller McCauley 1C172/TM-7456 E 8764 (Position) (Make and Model) (Serial Number) (Total Time) (TSO) The following inspections were complied with at this time: Annual inspection completed in accordance with FAR 43 appendix D. Aircraft lubricated in accordance with Cessna 150 service manual. 50 hour inspection in accordance with Cessna 150 service manual. 100 hour inspection in accordance with Cessna 150 service manual. 200 hour inspection in accordance with Cessna 150 service manual. ELT inspected in accordance with FAR (d). Changed engine oil with 7 quarts of Aeroshell SAE 50 straight mineral oil for engine break in period due replacement in 25 hours. Engine compression readings #1: 72, #2: 70, #3: 73, #4: 72. The following special inspections were complied with at this time: Complied with 5 year replacement of engine compartment flexible fuel and oil hoses. 50 hour battery inspection. 100 hour ELT check. 100 hour flap actuator jack screw thread inspection and lubrication. 200 hour magneto timing. 500 hour alternator brush inspection. 500 hour wheel bearing inspection. 500 hour gyros central air filter replacement, p/n D ,000 hour replacement of vacuum relief valve filter, p/n B ,000 hour fuel tank inspection. 1,000 hour magnetic compass compensation 1,000 hour elevator trim tab actuator lubrication and inspection. The following maintenance tasks were performed at this time: Replaced induction air filter with new Bracket Element, p/n BA Replaced throttle control cable, p/n C S. Replaced forward crankshaft seal, p/n LW Re-routed and secured engine ignition wires. Re-located oil breather line and added secondary vent hole. Replaced fuel pressure indicator line. Replaced fuel strainer o-ring, p/n MS Replaced all engine scat-tubing. Replaced oil screen gasket, p/n Installed new Sky-Tec engine starter, p/n 149NL, s/n FN New Weight & Balance computed. Installed 4 new primer line clamps to intake tubes, p/n LW Replaced #3 cylinder oil return line, p/n Removed and installed number 1 cylinder after repair by Scott Dodge, A&P See logbook entry dated 9/1/09. Replaced 4 valve cover gaskets. Number 1 exhaust riser repaired by Aero Structural Services CRS# F8VR234O. Muffler baffles replaced by Aero Structural Services CRS# F8VR234O. 1

2 Adjusted and secured mixture control cable clamp. Installed new instrument panel placards and fuel placards. Re-positioned and secured fuel strainer control. Crack in pilot door repaired by Aero Structural Services CRS# F8VR234O. Installed new door handle assembly covers, p/n Installed new right hand door catch, p/n Installed 4 new seat stop kits, p/n s Replaced left wing fuel drain, p/n CAV-170. Installed 2 vented fuel caps, p/n C in accordance with Cessna Service Letter SE77-6. Removed unused radio antenna from forward portion of aircraft belly and fabricated a blanking cover. Replaced battery with Gill G25 model, s/n G Cleaned corrosion in battery box and surrounding skin and painted with epoxy primer. Replaced positive battery cable. Installed new battery vent hose grommet. Re-located primer line outside of brake cable underneath instrument panel. Adjusted aileron and elevator cable tensions in accordance with Cessna 150 service manual. Replaced ELT batteries with 6 Duracell D-cells. Batteries due replacement March Cleaned and re-packed wheel bearings. Replaced all wheel bearing seals, p/n s , , , and Replaced tires and tubes with Goodyear Flight Custom II tires, 6x6, 4 ply. Installed new brake discs, p/n Installed new brake pads, p/n RA Replaced brake caliper o-rings, p/n AN Bled brakes and filled reservoirs with MIL-H Tailwheel assembly removed from aircraft. Cleaned and re-packed tailwheel bearings and swivel assembly. Replaced left main landing gear inboard casting lower attach angle with a fabricated angle of 2024T3.040 in accordance with Custom Aircraft Conversions modification drawings incorporated in STC # SA2846SW. Replaced lower tail skin doubler with a fabricated skin of 2024T3.040 in accordance with Custom Aircraft Conversions modification drawings incorporated in STC # SA2846SW. Replaced tail wheel mounting hardware and internal doubler with a fabricated doubler of 2024T3.040 in accordance with Custom Aircraft Conversions modification drawings incorporated in STC # SA2846SW. Installed new tailwheel spring spacer, p/n Flight controls were removed from aircraft, aircraft was stripped to bare metal, and all corrosion removed. Aircraft treated with acid-etch and alodine, and primed with a 2-part epoxy primer. Aircraft painted with Sherwin Williams Jet Glo Polyurethane paint. Colors used: Jet Stream-08486, Gloss Black-UA01955, Flight Red Changed aircraft registration number to N724MC. Balanced and installed flight controls in accordance with Cessna 150 Service Manual. Propeller removed, stripped, treated with acid-etch and alodine, primed with a 2-part epoxy primer and painted and installed on aircraft. Installed new carpet and seats refinished by Aero Plus Interiors. 2

3 The following Airworthiness Directives were complied with at this time: AD R3 Wing flap jack screw: Aircraft was determined to have been modified with Cessna service kit SK150-37B in accordance with Cessna service letter SE72-2, Supplement 1. Lubricated flap jack screw with MIL-G Next service due: Visual inspection at each 100 hour and annual inspection. Clean and lubricate as AD Defective spar attachment fittings: Not applicable due to aircraft serial number. No AD Engine lubrication: Not applicable. STC SA2219WE not installed on aircraft. No AD R1 Fuel tank vented caps: Installed two vented fuel caps, p/n C in accordance with Cessna Service Letter SE77-6. AD Vertical fin aft bracket nutplates: Inspected nutplates with no defects noted. Next service due at 5,628.4 ACTT. AD Aileron balance weights: Not applicable. STC s SA2191WE or SA2192WE not installed on aircraft. No AD Engine control attachment modification: Complied with in accordance with Cessna Service Letter SE79-6. No AD R2 Seat track and seat pin engagement: Inspected seat tracks with no defects noted. Next service due at next annual inspection. AD Placard-spins: Not applicable. STC 4795SW not installed on aircraft. No AD Wing stall fence: Not applicable. Bush Conversions STOL kit not installed on this aircraft. No AD S51-10 type oil, fuel and hydraulic hoses: Not applicable. No hoses with p/n S51-10 were replaced or installed on this aircraft between March 1995 and February 3, No AD Fuel strainer assembly: Not applicable to p/n s , , or not installed on this aircraft after December 12, No further action AD Pilot and co-pilot shoulder harness adjuster: Not applicable due to aircraft serial number and the affected accessory kits not installed on this aircraft. No further action AD AFM, placard, rudder travel stops: Complied with Option #1 by installing required placard on instrument panel and adding required text to the limitations section of the airplane flight manual and the pilot s operating handbook. AD R1 AFM, placard, rudder travel stops: Complied with Option #1 by installing required placard on instrument panel and adding required text to the limitations section of the airplane flight manual and the pilot s operating handbook. AD Oil seal failure: Not applicable to p/n s or not installed on this aircraft. No AD Oil filter adapter gasket: Not applicable to engine serial number. No AD Oil filler extension: Not applicable to engine series. No further action AD Rocker box covers, arms, fulcrums, ect.: Not applicable to engine series. No AD Oil pump: Not applicable to engine series. No AD Crankshaft assembly: Not applicable to engine series. No further action AD Fuel injector center body bellows seal: Not applicable to engine not being fuel injected. No 3

4 AD Fuel injector regulator diaphragm: Not applicable to engine not being fuel injected. No AD R2 Aircraft mounting bracket attach bolts: Not applicable to engine series. No AD R2 Exhaust hydraulic lifters and upper exhaust valve: Not applicable to engine series. No AD Upper exhaust valve spring seats: Not applicable to engine series. No AD R2: Superseded by AD AD R1 Rocker arm assemblies: Not applicable to engine serial number. No AD R1 Rear mounted propeller governor: Not applicable to propeller governor not being installed on this aircraft. AD Fuel pump diaphragm and vent fitting: Not applicable to engine series. No AD : Superseded by AD AD Piston pin recall: Not applicable to p/n LW not installed on this aircraft. No AD Low pressure diaphragm fuel pump: Not applicable to fuel pump not being overhauled by AAI. Nor AD Low octane engine damage: Not applicable to engine series. No further action AD Engine oil pump impeller: Not applicable. AD was previously complied with. AD Piston pin recall: Not applicable to engine serial number. No further action AD Corrosion pits in I.D. of crankshaft: Not applicable to engine horsepower rating. No AD Crankshaft cracks: Not applicable to crankshaft not being repaired by Nelson Balancing Service. No AD Oil filter converter plate gasket: Not applicable to engine series. No further action AD C1 Crankshaft gear and gear retaining bolt: Not applicable. AD only required after a prop-strike. AD Engine Components Inc. P/N AEL65102 classic cast : Not applicable to p/n AEL65102-NST04 not installed on aircraft. No AD R1: Not applicable, Superior Air Parts, Inc. cast cylinder assemblies not installed on this aircraft. No AD Engine Components Inc. P/N AEL65102 Titan cylinders: Not applicable to p/n s AEL65102-NST04 or AEL85099 not installed on this aircraft. No further action AD : Not applicable, T&W Propellers, Inc. not returning this propeller back to service. No AD : Not applicable, Southern California not returning this propeller back to service. No AD MA-4 series carburetors: Not applicable to carburetor model number. No AD MA-4 series carburetors: Not applicable to carburetor serial number. No AD Slick magnetos: Not applicable to magneto model number. No further action 4

5 AD : Altimeter was determined to have been modified United Instruments Service Bulletin #1. No AD : Not applicable, Kollsman instruments not installed on this aircraft. No AD : Inspected and performed function test of Bendix ignition switch with no defects noted. Next service due at 5,628.4 ACTT. AD Slick magnetos: Not applicable to magneto model number. No further action AD Brackett air filters: Not applicable to air filter part number. No further action AD Slick magnetos: Not applicable to magneto model number. No further action AD United Instruments altimeters P/N 5934: Not applicable to altimeter serial number. No AD MA-4 series carburetors: Not applicable to carburetor model number. No AD Brackett air filters: Complied with by inspection. Next service due at 5,628.4 ACTT. AD Airborne dry air pumps: Not applicable to vacuum pump serial number 2AJ155. No AD Narco AT150 transponders: Not applicable to transponder serial number No AD s researched with T-Data through The following Service Letters were complied with at this time: Cessna Service Letter SE72-2, Supplement 1. Cessna Service Letter SE77-6. Cessna Service Letter SE79-6. I certify this aircraft has been inspected and or repaired in accordance with an Annual Inspection CFR 14 Part 43 appendix D and the Cessna 100 Series service manual and was determined to be in an airworthy condition and approved for return to service. Date: Signed: Stuart MacKenzie A&P IA 5

6 2009 Annual Inspection Engine & Propeller Logbook Entry N724MC Cessna 150L ,528.4 Engine Lycoming O-320-A2B RL A 2, Propeller McCauley 1C172/TM-7456 E 8764 (Position) (Make and Model) (Serial Number) (Total Time) (TSO) The following inspections were complied with at this time: Annual inspection completed in accordance with FAR 43 appendix D. 50 hour inspection in accordance with Cessna 150 service manual. 100 hour inspection in accordance with Cessna 150 service manual. 200 hour inspection in accordance with Cessna 150 service manual. Changed engine oil with 7 quarts of Aeroshell SAE 50 straight mineral oil for engine break in period due replacement in 25 hours. Engine compression readings #1: 72, #2: 70, #3: 73, #4: 72. The following special inspections were complied with at this time: Complied with 5 year replacement of engine compartment flexible fuel and oil hoses. 200 hour magneto timing. The following maintenance tasks were performed at this time: Replaced induction air filter with new Bracket Element, p/n BA Replaced forward crankshaft seal, p/n LW Replaced oil screen gasket, p/n Installed 4 new primer line clamps to intake tubes, p/n LW Replaced #3 cylinder oil return line, p/n Removed and installed number 1 cylinder after repair by Scott Dodge, A&P See logbook entry dated 9/1/09. Replaced 4 valve cover gaskets. Number 1 exhaust riser repaired by Aero Structural Services CRS# F8VR234O. Muffler baffles replaced by Aero Structural Services CRS# F8VR234O. Propeller stripped, treated with acid-etch and alodine, primed with a 2-part epoxy primer and painted. Propeller statically balanced and installed on aircraft in accordance with Cessna 150 Service Manual. The following Airworthiness Directives were complied with at this time: AD Oil seal failure: Not applicable to p/n s or not installed on this aircraft. No AD Oil filter adapter gasket: Not applicable to engine serial number. No AD Oil filler extension: Not applicable to engine series. No further action AD Rocker box covers, arms, fulcrums, ect.: Not applicable to engine series. No AD Oil pump: Not applicable to engine series. No AD Crankshaft assembly: Not applicable to engine series. No further action AD Fuel injector center body bellows seal: Not applicable to engine not being fuel injected. No AD Fuel injector regulator diaphragm: Not applicable to engine not being fuel injected. No 6

7 AD R2 Aircraft mounting bracket attach bolts: Not applicable to engine series. No AD R2 Exhaust hydraulic lifters and upper exhaust valve: Not applicable to engine series. No AD Upper exhaust valve spring seats: Not applicable to engine series. No AD R2: Superseded by AD AD R1 Rocker arm assemblies: Not applicable to engine serial number. No AD R1 Rear mounted propeller governor: Not applicable to propeller governor not being installed on this aircraft. AD Fuel pump diaphragm and vent fitting: Not applicable to engine series. No AD : Superseded by AD AD Piston pin recall: Not applicable to p/n LW not installed on this aircraft. No AD Low pressure diaphragm fuel pump: Not applicable to fuel pump not being overhauled by AAI. Nor AD Low octane engine damage: Not applicable to engine series. No further action AD Engine oil pump impeller: Not applicable. AD was previously complied with. AD Piston pin recall: Not applicable to engine serial number. No further action AD Corrosion pits in I.D. of crankshaft: Not applicable to engine horsepower rating. No AD Crankshaft cracks: Not applicable to crankshaft not being repaired by Nelson Balancing Service. No AD Oil filter converter plate gasket: Not applicable to engine series. No further action AD C1 Crankshaft gear and gear retaining bolt: Not applicable. AD only required after a prop-strike. AD Engine Components Inc. P/N AEL65102 classic cast : Not applicable to p/n AEL65102-NST04 not installed on aircraft. No AD R1: Not applicable, Superior Air Parts, Inc. cast cylinder assemblies not installed on this aircraft. No AD Engine Components Inc. P/N AEL65102 Titan cylinders: Not applicable to p/n s AEL65102-NST04 or AEL85099 not installed on this aircraft. No further action AD : Not applicable, T&W Propellers, Inc. not returning this propeller back to service. No AD : Not applicable, Southern California not returning this propeller back to service. No AD s researched with T-Data through I certify this engine and propeller have been inspected and or repaired in accordance with an Annual Inspection CFR 14 Part 43 appendix D and the Cessna 100 Series service manual and was determined to be in an airworthy condition and approved for return to service. Date: Signed: Stuart MacKenzie A&P IA 7