Piper Comanche PA-24 Service Manual page 61

TABLE II-I. LEADING PARTICULARS AND PRINCIPLE DIMENSIONS (CONT.)
MODEL
PROPELLER
Manufacturer
Type
Hub model
Blade model
Diameter,
Diameter, min.,
Blade angle (low pitch)
Blade angle (high pitch)
Control governor
Governor model Hartzell
FUEL SYSTEM
Inboard (main) fuel cells
Capacity (each)
Unusable fuel (each)
Outboard (auxiliary) fuel cells
Capacity (each)
LANDING GEAR
Type
Shock strut type
Fluid required (struts and brakes)
Strut exposure (exposure under static load)
Wheel tread
Wheel base
Nose wheel travel
Wheel, Nose
Wheel, Main
Brake type
Tire, Nose
Tires, Main
Tire pressure, Nose
Tire pressure, Main
OVERALL
Gross weight
Gross landing weight
7. Blade angle at 30 in. radius
04/01/09
PIPER COMANCHE SERVICE MANUAL
7
7
PA-24-400
Hartzell
Constant speed (three blades)
HC-A3VK-4
V8433-7
77.25 in.
75.25 in.
14°
36°
Hartzell
F-4-1
Two
30 U.S. gal
3 U.S. gal
Two
35 U.S. gal
Electrically operated
Combination air and oil
MIL-H-5606
2.50 in.
9 ft. 8.375 in.
6 ft. 6.62 in.
Left 20°, Right 20°
Cleveland 38501
Goodrich 3-1038-1 or Cleveland 40-90
Goodrich 2-8521
(S/N's 26-2 tthru 26-129)
6:00 x 6, 6 ply rating
6:00 x 6, 6 ply rating
42 psi
42 psi
3600 Lbs.
3600 Lbs.
II - HANDLING AND SERVICING
1B15
Cleveland 30-23
(S/N's 26-130 and up)