Piper Comanche PA-24 User Manual

COMPONENT LUBRICANT FREQUENCY
1. STABILATOR TRIM TAB AND RUDDER HINGES MIL-PRF-7870C 100 HRS.
2. STABILATOR TRIM PULLEYS MIL-PRF-7870C 100 HRS.
3. BAGGAGE DOOR HINGES MIL-PRF-7870C 100 HRS.
4. FLAP TRANSMISSION (See Spec. Instr. 13) MIL-PRF-23827C 500 HRS.
5. STABILATOR TRIM PULLEY MIL-PRF-7870C 100 HRS.
6. FLAP CONTROL ARMS AND CABLE ENDS MIL-PRF-7870C 100 HRS.
7. BRAKE RESERVOIR (See Spec. Instr. 5) MIL-PRF-5606H AS REQUIRED
8. PILOT AND PASSENGERS SEAT TRACK MIL-PRF-7870C 100 HRS.
9. AIR FILTER (See Spec. Instr. 7) CLEAN 50 HRS.
10 GOVERNOR, THROTTLE AND MIXTURE CABLE ENDS MIL-PRF-7870C 100 HRS.
11. NOT USED
12. LANDING GEAR RETRACTION MECHANISM MIL-PRF-7870C 100 HRS.
13. LANDING GEAR RETRACTION TRANSMISSION (See Spec. Instr. 13) MIL-PRF-23827C 500 HRS.
14. AILERON HINGES, RIGHT AND LEFT MIL-PRF-7870C 100 HRS.
15. STABILATOR CONTROL CABLE ENDS AND TRIM PULLEY MIL-PRF-7870C 100 HRS.
63. FLAP CONTROL ROD ENDS, CABLE ENDS AND BELLCRANK BEARINGS MIL-PRF-7870C 100 HRS.
CAUTION
: DO NOT USE A HYDRAULIC FLUID WITH A CASTOR OIL OR ESTER BASE.
CAUTION
: DO NOT OVER LUBRICATE PEDESTAL CONTROLS AND COCKPIT CONTROLS.
PIPER COMANCHE SERVICE MANUAL
04/01/09 II - HANDLING AND SERVICING
1C47
Figure 2-21. Lubrication Chart - PA-24-260

Piper Comanche PA-24 Specifications

General

Manufacturer	Piper Aircraft
Model	Comanche PA-24
Type	Light aircraft
First Flight	May 24, 1956
Number Built	4, 857
Seating Capacity	4
Engine	Lycoming O-360
Wingspan	36 ft (11 m)
Length	24 ft 8 in (7.5 m)
Stall Speed	62 mph (100 km/h, 54 kn)
Height	7 ft 6 in (2.3 m)