6. Scheduled Maintenance - PA-32-301XTC Piper 6XT (S/N’s 3255001 & up) (continued)
THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 22
Feb 19/04
1D16
5-20-00
Inspection
NATURE OF INSPECTION Interval (Hrs)
50 100
F. WING GROUP
1. Remove inspection plates and fairings.................................................................. O
2. Inspect wing surfaces and tips for damage, loose rivets,
and condition of walkway ...................................................................................... O
3. Inspect airlerons 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
4. Inspect aileron hinges and attachments................................................................ O
5. Inspect aileron control stops to ensure stops have not loosened
and locknuts are tight ............................................................................................ O
6. Inspect aileron cables, fittings, turnbuckles, pulleys, and bellcranks
for damage and operation, and cable tensions. (See Note 11.) ............................ O
7. Inspect pitot tube for damage and condition ......................................................... O
CA
UTION: SEVERE BURNS CAN RESULT FROM COMING IN CONTACT WITH
A HEATED PITOT TUBE.
8. Check pitot heat .................................................................................................... O
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 condition of bolts used with hinges. Replace as required......................... O
11. Lubricate per Lubrication Chart, 12-20-00.) .......................................................... O O
12. Inspect wing attachment bolts and brackets. (See Note 13.) ................................ O
13. Inspect fuel tanks and lines for leaks and water. (See Note 14.)........................... O
14. Inspect fuel tanks for minimum octane markings .................................................. O
15. Inspect fuel cell vents............................................................................................ O
16. Inspect all control cables, air ducts, electrical leads, lines, and attaching parts
for security, routing, chafing, deterioration, wear, and correct installation.
(See Note 11.)....................................................................................................... O
17. Install inspection plates and fairings...................................................................... O
G LANDING GEAR GROUP
1. Check oleo struts for proper extension and evidence of fluid leakage.
See Landing Gear, 12-10-00................................................................................. O O
2. Inspect nose gear steering control and travel ....................................................... O
3. Remove wheel fairings .......................................................................................... O
4. Inspect wheel alignment........................................................................................ O
5. Put airplane on jacks. (Refer to 7-10-00.).............................................................. O
6. Inspect tires for cuts, uneven or excessive wear, and slippage............................. O
7. Remove wheels, clean, inspect, and repack bearings .......................................... O
8. Inspect wheels for cracks, corrosion, and broken bolts......................................... O
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