Piper PA-44-180 SEMINOLE Maintenance Manual page 41

CHART 601. LEADING PARTICULARS AND PRINCIPLE DIMENSIONS (cont)
MODEL
PROPELLER
Manufacturer
Hub and Blade Model:
Right Engine
Left Engine
Diameter
Diameter, Minimum
Blade Angle, Low Pitch
Blade Angle, Feather
2
Governor Control
Left Engine
Right Engine
Left Engine
1
Right Engine
1
NOTES:
1
PA-44-180T ONLY.
2
MEASUREMENT TAKEN AT 30 INCH STATION.
3
SYNCHROPHASER INSTALLATION ONLY.
4
Option not available on S/N 44-95001 and up.
FUEL SYSTEM
Fuel Tank
Capacity
Unusable Fuel
Total Capacity (Both)
Total Unusable Fuel
Total Usable Fuel
LANDING GEAR
Type
Shock Strut Type
Fluid Required (Strut, Brakes & Hydraulic System)
Wheel Tread
Wheel Base
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
TWO BLADE
Hartzell
HC-C2Y(K,R)-2CLEUF/FJC7666A-2R
HC-C2Y(K,R)-2CEUF/FC7666A-2R
74 inches
72 inches
12.4° ± 0.2°, 13.1° ± 0.2°
2
79° - 81°
Hartzell
E-3-2
E-3-2L, E-8-2L
3
E-3-5
E-3-5L, E-8-5L
3
PA-44-180 / 180T
THREE BLADE
Hartzell
HC-C3YR-2LEUF/FJC7663-5R
HC-C3YR-2EUF/FC7663-5R
73 inches
72 inches
10.6° ± 0.1°, 11.2° ± 0.1°
1
81° - 83°
Hartzell
Same
Same
Same
Same
2 (1 each wing)
55 U.S. Gallons
1 U.S. Gallons
110 U.S. Gallons
2 U.S. Gallons
108 U.S. Gallons
Fully Retractable
Air - Oil Oleo
MIL-H-5606
10.54 ft.
8.4 ft.
1B17
4
1
Page 6-02
Revised: May 15, 1989
6 - 1 0 - 0 0