Interim Revision: February 28, 1995
INSPECTION
1E1
PIPER AIRCRAFT
PA-28-161 CADET
AIRPLANE MAINTENANCE M A N U A L
TABLE III-I. INSPECTION REPORT (cont.)
15. Refer to flight manual supplement for preflight and flight check for intended function in all modes.
16. Refer to latest revision of Piper Service Bulletin 631 for battery protection.
17. Refer to test procedure outlined in Section XI Electrical System.
18. Replacement of the auxiliary pump/motor assembly is required every 500 hours of operating time or 10
years, whichever occurs first.
19. Examine cables for broken strands by wiping the cable with a cloth along the length of the cable.
Visually inspect the cable thoroughly for damage not detected by the cloth. Replace damaged cables.
Refer to Advisory Circular 43.13-1A, Paragraph 198.
20. Special care should be taken to inspect stabilator control cables beneath aft baggage compartment floor.
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