Piper Comanche PA-24 User Manual

PIPER COMANCHE SERVICE MANUAL
7
10
12
5
8
2
'~
?j
I I
I 8
8
4
2
1 BOLT
2 PLAIN WASHER
3 SELf-LOCKING NUT
"' STARTER RING GEAR SUPPORT
5 SPINNER ADAPTOR RING
6 --0-- RING SEAl.
7 PROPELlER
8 HUB MOUNTING BOLT
9 WASHER
10 SPlHNER
11 TRUSS HEAD SCREW
12 FIBER WASHER
FIGURE 7-1. PROPELLER INSTALLATION (McCAULEY)
7-9 Removal Of PropeUer_ (McUwey) (Reier to Figure 7-1 )
NOTE
In some manner identify the position of each put in relation to the
other to facilitate installation.
a. Remove the Sp1lU1CT (10) by removing the screws (11) that secure it [0 the spinner bulkhead (5)
b. PlAce. dri? pUl under the propeUer to c.tch oil .pillage.
c. Cut the safety wU'c around the propeller mounting bolts (8) ~d remove the bolts tram tile engme
<fUlks;'.!t t1Ulge.
-i. Pull the propeller from the engine cr.nl<sh.ft.
e. Remove the propeller "0" nng (6) from the propeller hub bore_
f The spmnc! bulkhnd may be remo\'cd from the startcr ring icar (4) by :-emovmg :lues. wasners
and bolts ( 1)
POWER PLANT
ISSUED: 8/18/72
2 A14
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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)