THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 3
Jun 1/03
1F3
6-00-00
CHART 1 (Sheet 2 of 3)
LEADING PARTICULARS AND PRINCIPAL DIMENSIONS
MODEL PA-32-301FT (6X) PA-32-301XTC (6XT)
PROPELLER THREE BLADE
Manufacturer Hartzell
Hub and Blade Model HC-I3YR-1RF / F7663DR
Diameter 78 in.
Diameter, Minimum 77 in.
Blade Angle:
Low Pitch (High RPM)
1
12.4° ± 0.2° 15.2° ± 0.2°
High Pitch (Low RPM)
1
32°± 1° 34.0° ± 0.5°
Governor Control Hartzell
Governor Model V-5-4 V-5-6
Note: (1) Measurement taken at 30 inch station.
FUEL SYSTEM
Fuel Tanks: (2 interconnected
each wing / 4 total)
Capacity: 53.5 U.S. Gallons / Wing
Total Fuel Onboard 107 U.S. Gallons
Total Usable Fuel 102 U.S. Gallons
Electric Fuel Pump:
Weldon (28 volt) P/N 461-750
LANDING GEAR
Type Fixed
Shock Strut Type Combination Air and Oil Oleo
Fluid Required
(Struts & Brakes) MIL-H-5606
Wheel Tread 10 ft. 7 in.
Wheelbase 7 ft. 8 in.
Nose Wheel Travel 30° ± 2° Left and Right
Turning Distance (Min.) 59 ft., 10.8 in.
Turning Radius (Minimum):
Nose Wheel 22 ft., 11 in.
Wing Tip
Wheel, Nose 6.00 x 6
Cleveland 40-56B or
40-30665
Wheel, Main 6.00 x 6
Cleveland 40-120C
Brake Type Cleveland 30-83A
Tire, Nose Type III, 6:00 x 6, 8 ply
(Michelin Air)
Tire, Main, Type III, 6:00 x 6, 8 ply
(Michelin Air)
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