Piper ARROW III Service Manual

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.
(See latest revision of Piper Service Bulletin 977.).................................................. 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
to lubrication chart in Service Manual, Section II ................................................... 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 1000100
Inspection Time (Hrs)
CHEROKEE ARROW III SERVICE MANUAL
1D12
Interim Revision: 2/21/95 INSPECTION

Piper ARROW III Specifications

General

Manufacturer	Piper Aircraft
Model	ARROW III
Engine	Lycoming IO-360-C1C6
Horsepower	200 hp
Maximum Takeoff Weight	2, 750 lb (1, 247 kg)
Seating Capacity	4
Propeller	2-blade, constant speed
Length	24 ft 7 in (7.49 m)