Piper PA-34-200T Seneca II, Руководство по обслуживанию

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PIPER SENECA II SERVICE MANUAL
TABLE III-I. INSPECTION REPORT
(cont.)
Inspection
NATURE OF INSPECTION Interval (Hrs)
50 100
9. Inspect flaps for surface damage or irregularities (i.e. - skin cracks, distortion,
dents, corrosion, and excessive paint build up); structural defects (i.e. - loose
or missing rivets); misrigging or structural imbalance; hinge damage, excessive
wear, freedom of movement and proper lubrication; and attachment points
for missing or worn hardware ................................................................................
O
10. Inspect flap hinge bolts for condition and security. Replace as required............... O
11. Lubricate per Lubrication Chart, Section II ........................................................... O O
12. Inspect aft wing rib assembly, WS 49.25., per paragraph 4-16a............................ O
13. Inspect wing fore and aft attach fittings, and bolts, for security, corrosion
and condition.......................................................................................................... O
14. Retorque wing aft spar attach bolts per paragraph 4-16b. ..................................... O
15. Inspect fuel tanks and lines for leaks and water .................................................... O
16. Remove, drain and clean fuel filter bowls ............................................................. O O
17. Inspect fuel tanks for minimum octane and capacity markings............................. O
18. Inspect fuel tank vents. .......................................................................................... O
19. Inspect all control cables, air ducts, electrical leads, lines, and attaching parts
for security, routing, chafing, deterioration, wear, and correct installation. .......... O
20. Install inspection plates and fairings...................................................................... O
G. LANDING GEAR GROUP
NOTE: The following inspections incorporate the requirements of Piper Service
Bulletin (PSB) No. 1123B. Any later revisions to PSB No. 1123 must be
complied with separately. See also AD 2005-13-16.
1. Inspect main gear trunnion assembly for condition. (See Note 11.) ..................... O
2. Check oleo struts for proper extension and evidence of fluid leakage.
(See Oleo Struts, Section II.) ................................................................................
O O
3. Inspect wheel alignment, if required ..................................................................... O
4. Put airplane on jacks. (per Section II) ................................................................... O
5. Inspect tires for cuts, uneven or excessive wear and slippage .............................. O
6. Remove wheel, clean, check and repack bearings ................................................ O
7. Inspect wheels for cracks, corrosion and broken bolts. ........................................ O
8. Check tire pressure per Section II, Table II-I ........................................................ O O
9. Inspect brake linings and discs for condition and wear.
(Refer to paragraph 7-52.) .....................................................................................
O O
10. Inspect brake backing plates ................................................................................. O
11. Inspect brake lines and retaining clamps .............................................................. O
12. Inspect condition of nose gear centering spring and bungees ............................... O
13. Inspect gear forks for damage ............................................................................... O
14. Inspect nose and main gear actuators .................................................................... O
15. Inspect main gear trunnion pin. Replace, if necessary .......................................... O
16. Inspect hydraulic lines, electrical leads, and attaching parts for
condition and security (i.e. - routing, chafing, damage, wear, etc.) ....................... O
17. Inspect drag and side brace link bolts. (Replace as required.) .............................. O
01/01/09 III - INSPECTION
1C51