Piper 6XT - Page 65

THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 19
Feb 19/04
1D13
5-20-00
6. Scheduled Maintenance - PA-32-301XTC Piper 6XT (S/N’s 3255001 & up) (continued)
Inspection
NATURE OF INSPECTION Interval (Hrs)
50 100
B. ENGINE GROUP (CONT.)
42. Inspect condition and tension of alternator drive belt.
(See Adjusting Alternator Belt Tension, 24-30-00.) ............................................... O O
43. If installed, inspect condition of A/C compressor belt and tension.
(See Adjusting Drive Belt Tension, 21-50-00.)....................................................... O O
44. If installed, check A/C compressor oil level. (See Note 9.).................................... O
45. If installed, inspect A/C compressor clutch security and wiring. (See Note 10.) ... O
46. If installed, inspect A/C compressor mounting for cracks, corrosion,
and security........................................................................................................... O
47. Check fluid in brake reservoir. Fill as required....................................................... O O
48. Inspect and lubricate all controls. (Refer to Lubrication Chart, 12-20-00.)............ O
49. Complete overhaul of engine or replace with factory rebuilt...................
50. Install engine cowl................................................................................................. O O
C. TURBOCHARGER GROUP
W
ARNING: FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S),
WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT
INSTALLED IN PIPER AIRCRAFT, MAY RENDER THE AIRCRAFT
UNAIRWORTHY. (SEE INTRODUCTION - SUPPLEMENTARY
PUBLICATIONS.)
NOTE: Read Note 5 prior to completing this group.
1. Inspect all oil inlet ducting and compressor discharge ducting for worn spots,
loose clamps, or leaks........................................................................................... O O
2. Inspect engine air inlet assembly for cracks, loose clamps, and screws............... O O
3. Inspect exhaust ducting and exhaust stacks for tightness ................................... O O
4. Inspect exhaust heat exchanger ........................................................................... O
5. Carefully inspect all turbo support brackets, struts, etc., for damage, sagging,
and wear................................................................................................................ O O
6. Inspect all oil hoses, lines, and fittings for wear, leakage, heat damage,
and fatigue............................................................................................................. O O
7. Inspect bypass valve for security and safety ......................................................... O O
8. Run up engine, and check all instruments for smooth, steady response .............. O O
D. CABIN AND COCKPIT GROUP
1. Inspect cockpit and cabin doors, latches, and hinges, and windows, and
aft baggage compartment door, latch, and hinge for damage, operation,
and security........................................................................................................... O
2. Inspect windows for scratches, crazing, and condition.......................................... O
3. Check window and door seals for deterioration, cracks, and voids....................... O
4. Inspect upholstery for tears................................................................................... O
5. Inspect seats, seat belts, shoulder harnesses, security brackets, and bolts.
(See Seat Belt and Shoulder Harness Inspection, 25-10-00.) .............................. O
As req’d by Lycoming
Svc. Instr. No. 1009