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发表于 2015-8-14 11:34:59
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来自: 中国内蒙古鄂尔多斯
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ENGINESECTION: (Refer to engine manufacturers manual & Mooney Service& Maintenance Manual for appropriate model) | MECH | INSP | 1. Remove and clean engine cowling and baffling; in-spect for cracks, wash engine. |
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| 2. Perform a HOT enginedifferential compressioncheck. Cylinder Readings:123456 |
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| LUBRICATINGSYSTEM: |
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| 1. Drain sump and change oil filter(if installed). |
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| 2. Remove pressure and suction screens; check formetal particles. |
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| 3. Clean and inspect screens. Reinstall and safety wire screens. |
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| 4. Inspect condition of oil cooler. |
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| 5. Service engine with recommended lubricating oil,
(Refer to Textron Lycoming Specification 301E & Ser- vice Instruction1014 or TCMService Manual). |
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| 6. Check enginefor oil leaks(note &correct). |
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| IGNITION SYSTEM: |
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| 1. Inspect sparkplugs; replace or clean &re- gap. |
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| 2. Inspect ignition harness for general condition, free from fraying or chafing. |
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| 3. Inspect magnetos &points; checkmagneto timing;
check distributor block for erosion or cracks. Overhaul Bendix magnetos each 500 hours/4years per TCM SB 643B. |
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| ELECTRICALSYSTEM: |
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| 1. Inspect battery(ies) for security, battery box (or area) for corrosion &vent for obstruction. |
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| 2. Inspect generator/alternator(s) and accessories. |
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| 3. Inspect electrical components &wiring. |
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| 4. Inspect starter &starter drive; lubricate starter drive. |
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| 5. For Garmin G1000 equipped A/C, refer to G1000 documentation for continued airworthiness instruc- tions. |
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| INDUCTION SYSTEM: (Challenger Aviation Filter Equipped Aircraft) |
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| 1. Recharge filter every 100 hours.Inspect filterhousing for debris and component condition (hoses, clamps,etc.). Check opening pressure/operation of ALT air door. |
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| FUELSYSTEM- M20B,C, D, G: |
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| 1. Inspect &drain carburetor, clean screens and check fuel flow. |
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| 2. Inspect carburetor heat systemfor leaks &proper operation. |
| | 3. Remove, clean, inspect and re-oil air filter. |
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| 4. Inspect carburetor airbox &induction systemfor condition. |
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| 5. Inspect fuel selector valvefor operation &proper pointer indication. Verify positive valve selection while rotating fuel selector valvethrough selection range. Tighten/Loctite set-screw if required. |
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| 6. Operate boost pump, check pressure and all lines for leaks. |
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| 7. Clean electric fuel pump screen (1963 &previous models). |
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| 8. Drain fuel sumps and fuel selector valve (Right &Left tanks). |
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FUEL SYSTEM - M20E, F, J, K, M, R, S, TN: | MECH | INSP | 1. Inspect fuel injection system,clean screens& injec-tor nozzles (refer to Textron Lycoming O/H Manual, Section8 or TCM Service Manual). |
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| 2. Check power boost systemfor proper door opera-tion & sealfor leaks (M20E, F, J).
NOTE: Power boost systemdeleted on 1990 &ON. |
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| 3. Remove, clean & inspect dry- airfilter. Replace paper induction filter@ 500 hours.Recharge K & N filter @ 100 hours and replace when wornor after 25 clean- ings. | |
| 4. Inspect air induction system & alternate air valve. |
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| 5. Inspect fuel selector valvefor operation &proper indication. Verify positive valve selection while rotating fuel selector valve throughselection range. Tighten/ Loctitesetscrew if required. |
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| 6. Operate boost pump; check pressure & all linesfor leaks. |
| | 7. Drain Right & Left tank fuel sumps;selector fuel valve or gascolator. |
| | 8. Check unmetered fuel pressure per Mooney Service & Maintenance Manual (M20K, M20R, M20S, M20TN). |
| | EXHAUSTSYSTEM: |
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| 1. Remove heater jacket & inspect exhaust system for leaks & cracks; removeexhaust cavities, inspect area. |
| | 2. Inspect clamps for tightness at turbocharger(s)(M20K, M20M, M20TN). |
| | 3. Inspect firewall for proper sealing &freedom from cracks. |
| | 4. Inspect tubular engine mount for cracks; bolts&rubber mounts for security. |
| | GENERALINSPECTION: |
| | 1. Lubricate engine controls & inspect for security, full travel &free movement. Inspectfor secure throttle, mixture &prop control arms and respective compo- nents. |
| | 2. Lubricate cowl flaps &inspect for proper opening &operation. NOTE: M20C &G, 1968 &ON, cowl flaps are fixed. M20R, M20S &M20TN haveno cowl flaps. |
| | 3. Remove propeller spinner & inspect for cracks &general condition. |
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| 4. Inspect propeller hub for greaseleakage; check hub bolts & mountingbolts for proper torque; inspect bladesfor cracks, nicks,and dents, lubricate as need- ed (referto appropriate manufacturer’s handbooks). |
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| 5. Reinstall spinner; check for correctinterference fit with prop. Wrap hub with Teflon tape asrequired for fit (M20J, K, L). Shim interference fit between hub and bulkhead (M20M, R, S, TN). |
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| AIRFRAME SECTION: (Refer to Mooney Service & Maintenance Manual) |
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| 1. Inspect exterior &interior of aircraft for general condition, collision damage, loose rivets, dents &corro- sion. |
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| 2. Inspect tubular structure lower longerons for corrosion (Reference SB M20- 208[ * ]) ( * latest revision). |
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| 3. Inspect wings &empennage for general condition,collision damage, loose rivets, dents &corrosion. |
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| 4. Inspect flight control surfaces for security of attachment, proper rigging, free movement, collision dam- age, loose rivets, dents and corrosion. |
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AIRFRAME SECTION(con’t.): |
MECH |
INSP | 5. Lubricate flight control system guide blocks,hinge points, rod end bearings &bell cranks. |
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| 6. Inspect all wing, fuselage &empennage drain holes for obstructions. |
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| 7. Inspect empennage trim systemfor proper operation & rigging. |
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| 8. Inspect downspring end loops, cable &pulley for wear and corrosion. Comply with Bendix/King Install Bulletin 343 (inspect & lube trim carrier bearing) for A/C withKAP/KFC 100 series autopilots. |
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| 9. Inspect flap systemfor proper operation &rigging;
lubrication accordance with Mooney Service &Mainte- nanceManual. |
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| 10. Inspect flight instruments, filters &vacuum system for proper operation, marking, and condition; clean vacuum air filter. |
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11. Inspect cabinlights, circuit breakers & electrical
components for proper operation. |
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| 12. Check operation of stall warning system. |
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| 13. Inspect P.C. systemcomponents for security, leaks& proper operation; servoseals for deterioration, all otherauto- pilotcomponents for security &proper op- eration. A/C equipped with Bendix/King Autopilots, complywith Honeywell Service Memo 292. |
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| 14. Inspect vacuumstep for security & properoperation; fixed step for security &damage. |
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| 15. Inspect wing interior in fuel tank area for fuel leaks,fuel tank vents for obstructions & fuel fillercaps for security & properoperation. |
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| 16. Inspect cabin &baggage doors for condition, proper operation & sealing. |
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| 17. Inspect windshield &windows for cracks, crazing,scratches and distortion. |
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| 18. Inspect seats,seat latch pins,seat belts & shoulder harnesses for security, proper operation and con- dition.If AMSAFE Restraint equipped, diagnostic test per AAIR Supplemental Maintenance Manual every 1,000 flight- hours or annually (whichever comes first). |
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| 19. Inspect compass & compass deviation card for proper indication & compensation.(Refer to Mooney Service Bulletin M20- 150A) |
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| 20. Inspect all radio equipment for proper installation &operation. |
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| 21. Inspect cabin for proper sealing. |
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| 22. Inspect oxygensystem for leaks,proper ON/OFF valve operation &filler for safety of operation. Perform hydrostatic test of oxygen bottle every3 yrs & regula- tor overhaul every 6 yrs. Composite bottlesexpire @ 15 yrs. |
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| 23. Inspect ELT as required by FAR 91.207d(1- 4). |
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| LANDING GEAR OPERATIONAL CHECK: |
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| 1. Raise aircraft on jacks. |
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| 2. Inspect brakes, hydraulic brakecylinders &hydraulic system for leaks and general condition: Service reservoir with ML- H- 5606 (RED) fluid. |
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| 3. Remove wheels, inspect, repack bearings, reinstall and safety, lubricate brake guide pins using Silicone- based lubricant. Checkwheels for free rotation &prop- er brake action. |
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| 4. Lubricate & inspect landing gear pivot points &moving parts. |
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| 5. Inspect landing gear shockdiscs (main& nose gear) (Refer to MAC S & M manual). |
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| MANUALGEAR RETRACTION SYSTEM: |
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| 1. Raise aircraft on jacks. |
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| 2. Check operation &rigging (pre- loads). |
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| 3. Check warning systemlight & horn. |
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| 4. Check gear down lock preload (Mains &Nose). |
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| 5. Check landing gear doors for proper closing/rigging. |
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| 6. Check retract lever welds for cracks. |
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ELECTRICGEAR RETRACTION SYSTEM: |
MECH |
INSP | 1. Raise aircraft on jacks. |
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| 2. Check operation &rigging. |
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| 3. Check warning systemlights, horn &visual indicator. |
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| 4. Check air pressure safety switchor squat safety switch. |
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| 5. Check main& nose gear down lock preload. |
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| 6. Lubricate actuator gear box (Dukes &ITT actuators only) |
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| 7. Check landing gear doors for proper closing/rigging. |
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| 8. Check emergency landing gear extension system;
extend gear using emergency gear extension system. Do not attempt gear retraction using emergency sys- tem (Referto MAC S & M manual). |
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| 9. Inspect shockdiscs (main& nose gear) in accordance with Mooney Service & Maintenance Manual. |
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| FIXEDGEAR: |
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| 1. Inspect landing gear fairing (M20D only). |
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| 2. Check air sealsin wheel wellareas. |
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| POST-INSPECTIONOPERATIONALCHECK: (Refer to Mooney Owner’s Manual or POH) |
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| 1. Check propeller governor operation with engine running at 2000 RPM & pitch control at low pitch (High RPM):When propeller control is pulled out to high pitch (lowRPM), engine speed should decrease at least 500 RPM. |
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| 2. Check easeof operation for all enginecontrols with engine running. |
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| 3. Check generator/alternator output &indication. |
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| 4. Check oil pressure indication. |
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| 5. Check fuel pressure indication. |
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| 6. Check fuel quantity indication. |
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| 7. Check cylinder head temperature (CHT)indication. |
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| 8. Check oil temperature indication. |
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| 9. Check idleRPM, idle mixture &idle cut- off. |
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| 10. Check propeller pitch through complete range. |
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| 11. Check operation of cabin &panel lights. |
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| 12. Check Radios/Avionics operation. |
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| 13. Check Auto Pilot operation. |
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| 14. Check magneto drop and grounding circuits. |
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| 15. Check operation of brakes. |
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| 16. Check fuel selector valvefor smooth operation. |
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| 17. Check vacuumwarning lights &instruments for proper operation. |
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| 18. Check flap position indicator (Take- Off &Full down). |
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| 19. Check trim position indicator and smooth operation of Trim System. |
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| 20. Flight check gear- up warninghorn at:12” manifold pressure (MP)(M20J prior to S/N 24- 3154); 14- 16” MP (M20K [231, 252]) & with throttle 1/4- 3/8 inchfrom idle position M20J (after S/N 24- 1354),M20K (Encore), M20L,M20M, M20R, M20S,M20TN. |
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| 21. Flight check aircraft flight control rigging. |
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| 22. Flight check P.C. or other Autopilot systems for proper operation. |
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| 23. Check cabin ventilation and heating systemfor carbon monoxide. |
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| 24. Check EGT/TITgauge and any other itemsof installed equipment. |
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| 25. Check operation of remote ELT switchbetween top of hour and 5 min afterthe hour. |
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| 26. Other checks (Specify as necessary): |
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