Piper Comanche PA-24 User Manual

PIPER COMANCHE SERVICE MANl:AL
TABLE \'11-1
PROPELLER SPECIFICATlO'\S
Blade Angle
10\\ Pilch (High RPM)
McCaule~
1::!7°,±()::!c
Hartlell
I ~o
High Pilch (Low RPM)
McCaule~
17 50
Hartlell
27°
Propeller RPM Selling Engine Stalic High RPM 1700 RPM Max
Engine Sialic Lo\\ RPM IK50;; 50 RPM Min
Propeller Torque Limits Description
Requtred Torque
( Dry)
Spinner Bulkhead 100 inch pounds
Propellcr Mounting
Bolt- 55 to (,0 foot pounds
Spinner Auachmcnt
Sere" ..
40 inch pound,
ISSl'ED: 8/18/72
2A19

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)