Piper Arrow IV Turbo Maintenance Manual page 37

NOTES (cont):
16. Fly the aircraft to check the landing gear system in accordance with instructions given in chapter 32 of
the maintenance manual (refer to latest revision of Piper Service Letter 810).
17. More frequent ignition system maintenance is required for operation above 12,000 feet.
18. Check torque of mounting bolts on Continental engine installation.
19. Maintain cable tensions specified in chapter 27 of this maintenance manual.
20. Refer to latest revision of Piper Service Bulletin 578 for nose gear down lock replacement.
21. Refer to latest revision of Piper Service Bulletin 625, Fuel and Vapor Return Lines Support.
22. Refer to flight manual supplement for preflight and flight check, for intended function in all modes.
23. Refer to latest revision to Bendix Service Bulletin 612 for inspecting magneto and ignition harnesses.
24. Refer to VSP 69.
Printed copies of this 100 Hour/Annual Inspection Report can be
obtained from Piper Service Sales - under Piper Part Number
230 818. Refer to Piper Parts Price List Aerofiche last card for
revision check list to insure obtaining latest copy of Inspection
Report.
25. Inspect Teflon bushing (lower to upper cowling attachment) for condition at each 100 hours. Replace
bushing on condition, but no later than 500 hours time in service. Inspect pin for condition and replace
as necessary.
26. If not already installed, add access panels per instructions in Chapter 51. See latest revision of Piper
Service Bulletin 977.
27. Special care should be taken to inspect stabilator control cables beneath aft baggage compartment
floor. Add access panels per instructions in Chapter 51, to ease this inspection.
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
PERIODIC INSPECTIONS (cont)
—NOTE—
1B13
Interim Revision: February 27, 1995
5-20-01
Page 5-14