Piper PA-34-200T Seneca II, Service Manual

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PIPER SENECA II SERVICE MANUAL
TABLE III-I. INSPECTION REPORT
(cont.)
K. NOTES:
(cont.)
CAUTION: IF TIME-IN-SERVICE FOR MAIN GEAR TRUNNION ASSEMBLIES OTHER
THAN P/N’S 67926-030, 67926-032, 67926-040, OR 67926-042 (LEFT) AND
67926-031, 67926-033, 67926-041 OR 67926-043 (RIGHT) (EACH EMBOSSED
WITH FORGING NUMBER 02599-2) CANNOT BE DETERMINED, THEN
THOSE MAIN GEAR TRUNNION ASSEMBLIES MUST BE REPLACED
BEFORE FURTHER FLIGHT.
11. For airplanes which have not installed new main landing gear trunnion assemblies P/N’s
67926-030, 67926-032, 67926-040, or 67926-042 (Left) and 67926-031, 67926-033, 67926-041,
or 67926-043 (Right) (each embossed with forging number 02599-2); and, have accumulated
500 hours time-in-service on one or both of the installed main landing gear trunnion assemblies:
perform Main Gear Trunnion Assembly Dye-Penetrant Inspection (see paragraph 7-21ab) on
one or both trunnion assemblies, as required.
12. Replace engine-driven fuel pump at engine overhaul.
13. Early Seneca II’s had inline filters in the cabin; later airplanes have a filter located in each nacelle.
14. Refer to Section V, paragraph 5-34 for allowable rudder tab and trim free play.
15. Maintain cable tensions specified in Section V.
16. Replacement brushes are no longer available. When brushes wear out, replace the Prestolite pump
with a new Oildyne pump.
17. See also AD 78-21-03.
18. For airplanes equipped with TCM/Bendix Magnetos: inspect magneto(s) per the procedures in the
Periodic Maintenance section of the applicable Service Support Manual, available from Teledyne
Continental Motors, Inc., PH: (800) 718-3411, or http://www.tcmlink.com/.
19. The compressor oil level should not be checked unless a Freon leak has occurred which requires
an addition of Freon to the system.
20. Not Used.
21. Not Used.
22. Refer to flight manual supplement for preflight and flight check, for intended function in all
modes.
23. Refer to the latest revision of Bendix Service Bulletin 612 for inspection of magnetos and ignition
harness.
24. Refer to Teledyne Continental Service Bulletin M86-11, latest revision.
25. Not used.
26. Flexible hose replacement times are in-service times. In-service must be determined by (1) the
date the aircraft was licensed, if new or (2) the date entered in the logbook for the replacement
hose placed in service. Do not use the date stamped on the hose, as time may be included for shelf
life, and not in-service use.
III - INSPECTION 01/01/09
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