Piper Aircraft Corporation Cherokee 140 PA-28-140, Service Manual

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PIPER CHEROKEE SERVICE MANUAL
III - INSPECTION 01/31/08
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TABLE III-II - INSPECTION REPORT - PA-28R-180/200
Refer to Notes 1, 2, 3, and 4 before performing the following inspections.
Inspection
NATURE OF INSPECTION Interval (Hrs)
50 100
D. FUSELAGE AND EMPENNAGE GROUP (CONT.)
30. Inspect ELT battery for condition and date per FAR 91.207 ................................ O
31. Inspect ELT installation and antenna for condition and security.
Replace antenna if bent or damaged ..................................................................... O
32. Inspect hydraulic pump motor brushes. (See Notes 22 & 23.) ............................. O
33. Inspect hydraulic pump fluid level. Fill as required ............................................. O O
34. Inspect hydraulic pump lines for damage and leaks ............................................. O
35. Inspect for obstructions and contamination in inlet of backup landing gear
extender actuator inlet head .................................................................................. O O
36. 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 the condition
of walkways. (See Note 24.) ................................................................................. 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 ...........................................
O
4. Inspect aileron hinges, attachments, balance weight and arm for security
and condition. (See Note 25.) ............................................................................... 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 14.) ................................... O
7. Inspect pitot tube for damage and condition ......................................................... O
CAUTION: 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, damaged or worn hardware ...........................
O
10. Inspect condition of bolts used with hinges. Replace as required ........................ O
11. Lubricate per Lubrication Chart, Section II .......................................................... O O
12. Inspect wing fore and aft attach fittings, and bolts for security, corrosion
and condition. (See Notes 30 & 31.) ..................................................................... O
13. Inspect fuel tanks and lines for leaks and water. (See Note 18.) ........................... O
14. Fuel tanks marked for capacity ............................................................................. O