TABLE III-I. INSPECTION REPORT (cont)
Nature of Inspection
F. FUSELAGE GROUP (CONT.)
24.Inspect stabilator and trim tab hinge bolts and bearings for excessive
wear. (Replace as required).......................................................................................
O
O
O
25.Inspect stabilator control stops to ensure stop has not
become loose and that the jamb nut is tight..............................................................
O
O
O
26.Inspect stabilator trim mechanism............................................................................
O
O
O
27.Inspect fuselage wing attach fittings for corrosion, general condition and security.
O
O
O
28.Check all cable tensions (Use tensionmeter) (Read Note 17) ..................................
O
O
O
29.Inspect cables, aileron, rudder, stabilator, stabilator trim, turnbuckles,
guides and pulleys for safety, damage, and operation (Read Notes 23 and 34) .......
O
O
O
30.Clean and lubricate stabilator trim drum screw (Refer
O
O
O
31.Inspect stabilator balance weight attachments and arm for security and condition .
O
O
O
32.Inspect emergency locator transmitter battery for replacement date per
Service Manual (Read latest revision of Piper Service Letter 820).......................... O O O
33.Clean and lubricate all exterior needle bearings ......................................................
O
O
O
34.Lubricate per lubrication chart in Service Manual, Section II..................................
O
O
O
O
35.Inspect rotating beacon for security and operation ..................................................
O
O
O
36.Inspect security of autopilot bridle cable clamps (Read Note 23)............................
O
O
O
37.Inspect all control cables, air ducts, electrical leads, harnesses, lines, radio
antenna leads, and attaching parts for security, routing, chafing,
deterioration, wear, and correct installation (Read Note 23)....................................
O
O
O
38.Install inspection plates and panels ..........................................................................
O
O
O
G. WlNG GROUP
WARNING
Read Note 28 before completing this inspection group.
1. Remove inspection plates and fairings ....................................................................
O
O
O
2. Inspect surfaces and tips for damage, loose rivets, and condition of wing walkway
O
O
O
3. Inspect aileron hinges and attachments ....................................................................
O
O
O
4. Inspect aileron balance weight and arm for security and condition .........................
O
O
O
5. Inspect aileron cables, pulleys, and bellcranks for
damage and operation (Read Note 23) .....................................................................
O
O
O
6. Inspect aileron control stops to ensure stops have not
become loose and that locknuts are tight .................................................................
O
O
O
7. Inspect flaps and attachments for damage and operation.........................................
O
O
O
50
500
1000
100
Inspection Time (Hrs)
CHEROKEE ARROW III SERVICE MANUAL
1D12
Interim Revision: 2/21/95
INSPECTION
Summary of Contents for ARROW III
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