Piper Comanche PA-24 User Manual

PIPER COMANCHE SERVICE MANUAL
FUEL INLET
SECTION-AA
IDLE VALVE LEVER
CONNECTE 0 TO
FLOW DIVIDER VALVE
THROTTLE LEVER
LINKAGE
MANUAL MIXTURE
CONTROL AND IDLE
CUT-OFF LEVER
CONSTANT HE
IDLE SPRINIGG'FO'RT.f.~r~~~~~~N~~;~
CONSTANT EI
~!fLLL'DLE MIXTURE
ADJuSTMENT
AIR I n~_J~~=~~\1:.:::~~
FUEL DIAPHRAGM '1 IMPACT TUBE
BALL SERVO VALVE
A
Fi8U~ 78-5. Schematic Diagram of RSA Fuel Injector System (PA-24400)
lF8
POWERPlA8
REVISED: 4/10/81

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)