Piper Cherokee LANCE, Service Manual

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PIPER CHEROKEE SIX / LANCE SERVICE MANUAL
III - INSPECTION 03/27/08
4C22
TABLE III-I. INSPECTION REPORT - PA-32-260/300 (cont.)
Inspection
NATURE OF INSPECTION Interval (Hrs)
50 100
D. FUSELAGE AND EMPENNAGE GROUP (CONT.)
27. Inspect rudder, stabilator, and stabilator trim cable tensions using a tensiometer.
(See Note 11.) ........................................................................................................ O
28. Inspect stabilator trim mechanism for condition, security, and operation ............. O
29. Clean and lubricate stabilator trim drum screw ..................................................... O
30. Clean and lubricate all exterior needle bearings .................................................... O
31. Lubricate per Lubrication Chart, Section II ........................................................... O
32. Inspect rotating beacon/anti-collision light for security and operation.................. O
33. If installed, inspect security of Autopilot bridle cable clamps. (See Note 10.)...... O
34. Inspect all controls, air ducts, electrical leads, harnesses, lines, radio
antenna leads, and attaching parts for security, routing, chafing deterioration,
wear, and correct installation .................................................................................
O
35. Inspect ELT battery for condition/date per FAR 91.207........................................ O
36. Inspect ELT installation and antenna for condition and security.
Replace antenna if bent or damaged ...................................................................... O
37. Install inspection plates and panels........................................................................ O
E. 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 ailerons 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. (See Note 17.)...................
O
4. Inspect aileron hinge pins for condition and security ............................................ O
5. Inspect aileron control stops to ensure stops have not loosened
and locknuts are tight .............................................................................................
O
6. Inspect aileron cables and cable terminals, turnbuckles, fittings, guides, pulleys,
and bellcranks for safety, condition, and operation. (See Note 10.) ......................
O
7. Inspect aileron cable tension using a tensiometer. (See Note 11.)......................... O
8. Inspect pitot tube for damage and condition.......................................................... O
CAUTION: SEVERE BURNS CAN RESULT FROM COMING IN CONTACT
WITH A HEATED PITOT TUBE.
9. Check pitot heat ..................................................................................................... O
10. 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