Piper Cherokee LANCE, Service Manual

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TABLE III-I. INSPECTION REPORT - PA-32-260/300 (cont.)
K. NOTES (CONT.)
PIPER CHEROKEE SIX / LANCE SERVICE MANUAL
III - INSPECTION 03/27/08
4D4
21. In PA-32-260 S/N’s 32-1 thru 32-1110, PA-32-300 S/N’s 32-40001 thru 32-40565, for
airplanes with the original equipment “butterfly” control wheels still installed,
perform the 100
Hour Control Wheel Inspection (see Special Inspections, Procedures).
22. In PA-32-260 S/N’s 32-1thru 32-7700023; and, PA-32-300 S/N’s 32-40001 thru 32-7840043;
for those airplanes which have not installed Piper Kit No. 760-910 or a new greaser bolt P/N
79543-002 and have accumulated 500 hours time-in-service:
perform Main Landing Gear
Torque Link Greaser Bolt Inspection (see Special Inspections, Procedures).
23. Verify initial compliance with Piper Service Bulletin No. 886.
24. For airplanes equipped with Parker Hannifin (Cleveland) main wheels 40-90 and brake disc
164-02201 (or 164-022A),
perform 164-02201 Brake Disc 100 Hour Inspection (see Special
Inspections, Procedures).
25. In the PA-32-260, for airplanes which have not installed the improved forged main landing
gear strut cylinders (P/N 65489-002) on both left and right main gear,
conduct the Cast Main
Landing Gear Strut Cylinder 100 Hour Inspection (see Special Inspections, Procedures) on the
remaining cast main landing gear strut cylinders.
26. Check throttle body attaching screws for tightness; the correct torque for these screws is 40 to 50
inch-pounds.
27. For airplanes equipped with Aero Accessories Inc., Tempest Dry Air Pumps only, for pumps
which have accumulated 500 hours time-in-service or more,
inspect vacuum pump vane wear
per Vacuum Pump Vane Wear Inspection (see Special Inspections, Procedures).
28. Inspect magnetos:
(a) For airplanes equipped with Slick Magnetos: inspect magneto(s) per the appropriate 100
Hour Inspection in the Slick F1100 Master Service Manual, available from Unison
Industries, PH: (904) 739-4000, or http://www.unisonindustries.com/.
(b) 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/.
29. In PA-32-260 S/N’s 32-03, 32-04, and 32-1 thru 32-7400049; and, PA-32-300 S/N’s 32-15, 32-
21, and 32-40000 thru 32-7440160, for airplanes which have not installed Piper Kit No. 757-
158 (with the 1-H65-2 valve) or 760-895:
perform the Fuel Selector Valve 50 hour Leak Check
(see Special Inspections, Procedures).
30. In PA-32-260 S/N’s 32-03, 32-04, and 32-1 thru 32-7300001; and PA-32-300/32S-300 S/N’s
32-15, 32-21, and 32-40000 thru 32-7240102; for airplanes which have not installed either
Piper Kit No. 760-634V, 760-637V, or 760-650V per Piper Service Bulletin No. 360:
each 50
hours, conduct the Induction Air Inlet Duct and Alternate Heat Duct Inspection (see Special
Inspections, Procedures).
31. For aircraft equipped with Hartzell two-blade, aluminum hub, “compact” ( )HC-( )2Y( )-( )
series propellers manufactured before April 1997 that do not have a suffix letter “B” at the end
of the hub and propeller serial number,
verify compliance with Hartzell Service Bulletin No.
HC-SB-61-227 per Piper Service Bulletin No. 927.
32. Verify compliance with Parker Hannifin/Airborne Service Bulletin No. 72.