Piper Comanche PA-24 User Manual

PIPER COMANCHE SERVICE MANUAL
7
10
\
11
12
2
8
;~
i I
B
I
!
9
4 2
, BOLT
2
PLAIN WASHER
3 SELF-LOCKING NUT
• Sf ~R RING GEAR SUPPORT
6 SPINNER ADAPTOR RING
a ··0" RING SEAl.
7 PROPELLER
B HUB MOUNTlNG BOLT
• WASHER
'0 SPINNER
, t TAUSS HEAD SCREW
12 FIBER WASHER
FIGURE 7A·1. PROPELLER INSTALLATION (MCCAULEY) PA·24-2S0
7A·12. Removal Of Propeller. (McCallicy) (PA-H·2S0) (Refer to Fig1.tre 7A·1 )
NOTE
In some manner idennfy the posItion of each part in relation to the
other to faciliute tnlUllanon.
a. Remove [he spmner ( 10) by removinl the screws ( 11) tha.t secure It to the spm.ncr bulkhead (5)
b. Place. drop pan under the propeller to ca"h oil spilUgc.
c. Cut the safety wire around the propeller mountin@: bolts (8) and remove the bolts from me engine
crankshaft tlangc.
d. Pull the propeller frem the engine crankshaft.
c. Remove the propeller "0" ring (6) from the propeller hub bore.
i The spinner bulkhead (S) may be removed from the starter ring geu ( .. ) by removmg nu[S. washers
and bolts
2 C7
POWER PLANT
ISSUED: 8/18172

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)