Piper Aircraft Corporation Malibu Mirage PA-46-350P, Airplane Maintenance Manual

Page: 64 / 1956

5-20-00
1D6
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
5. Scheduled Maintenance (continued)
Inspection
NATURE OF INSPECTION Interval (Hrs)
50 100
PAGE 12
Feb 28/07
D. CABIN AND COCKPIT GROUP (cont.)
31. Inspect aft face of F.S. 100.00 bulkhead and forward face
of F.S. 273.746 bulkhead for bulging, cracks, dents, loose,
or missing fasteners, condition and security of components.................................
O
32. If installed, inspect portable fire extinguisher minimum weight
as specified on nameplate. (See Note 25.) ........................................................... O
33. Inspect avionics compartment, components, and wiring
for condition, security, and operation. (See Notes 40 and 49.).............................. O
34. Inspect control cable boots for condition and security........................................... O
35. Check air conditioning evaporators (if installed).................................................... O
36. Lubricate per Lubrication Chart, 12-20-00 ............................................................ O
37. Install inspection covers and panels...................................................................... O
E. FUSELAGE AND EMPENNAGE GROUP
NOTE: Check that all fuselage and empennage drain holes are clear and open.
1. Remove inspection covers and panels.................................................................. O
2. Inspect skins, bulkheads, frames, stringers, and longerons for damage or
irregularities (i.e. - cracks, distortion, dents, corrosion and excessive paint
build up); structural defects (i.e. - loose or missing rivets); misrigging
or structural imbalance; and attachment points for missing or
worn hardware ......................................................................................................
O
CAUTION: PRESSURIZED FLIGHT IS PROHIBITED WITH DISCOLORATION,
CRACKS, OR CRAZING.
3. Inspect windshield and windows for nicks, scratches,
cracks, crazing, and discoloration .........................................................................
O
4. Inspect avionics compartment, components, and wiring
for condition, security, and operation.....................................................................
O
5. Inspect control cable boots for condition and security........................................... O
6. Check fuel sump drains for water and proper operation........................................ O O
7. Drain static lines. (Refer to 34-10-00.)................................................................... O
8. Inspect antennas/coaxial cables for condition and security .................................. O
9. Inspect dorsal fin for condition and security .......................................................... O
10. Inspect vertical fin and rudder for surface damage or irregularities
(i.e. - skin cracks, distortion, dents, corrosion, and excessive paint build up);
structural defects (i.e. - loose or missing rivets); misrigging or structural
imbalance; hinge damage, excessive wear, freedom of movement and proper
lubrication; and attachment points for missing or worn hardware .........................
O
11. Check rudder hinges and attachments for damage and operation ....................... O
12. Check rudder hinge bolts for excessive wear........................................................ O
13. Check rudder trim mechanism installation ............................................................ O
14. Check vertical fin attach points and wiring ............................................................ O
15. Check forward vertical fin attach fittings for corrosion and damage.
(See 55-30-00, Attach Fittings Corrosion Control.) ............................................... O
16. Inspect condition of deice system (if installed) ...................................................... O