TM 55-1730-229-12
TO 35C2-3-473-1
Table 1-1.
Tabulated Data (continued)
350 amperes continuous at 25 volts minimum
500 amperes for 1 minute
1000 amperes for 5 seconds
Pneumatic output:
60 lb/minute at 40 psig (sea level) Temperature 450F (232C)
26.5 lb/minute at 24 psig, 10,000 (3048m) feet altitude
Temperature 420F (232C)
3.5 inch (8.9 cm) diameter output hose, 30 ft. length (9.1m)
Hydraulic output:
15 gpm at 500 to 3,300 psig
Hydraulic fluid or MIL-H-83282 or MIL-H-5606
30-foot (9.1m) pressure and return hoses
Aircraft Interface single or dual connections
Operating Attitude:
Up to 15 degrees from horizontal any azimuth
Noise level:
Less than 85 dBA at 23 foot (7 meter) radius
Less than 90/93 dBA at operator panel
Less than 103/105 dBA at GTE air inlet
Capacities (Liquids):
Fuel Tank
65 gallons (246 liters)
Engine Oil Sump
2.3 quarts (2.2 liters)
Hydraulic System
9 gallons (34 liters)
Dimensions and Weights:
Overall length
90 inches (229 centimeters)
Overall width
58 inches (147 centimeters)
Overall height
60 inches (152 centimeters)
Weight empty
3550 pounds (1610 kilograms)
Weight filled-fluid
4275 pounds (1939 kilograms)
Shipping weight
3620 pounds (1642 kilograms)
Cubage
181 cubic feet (5.1 cubic meters)
2.
Engine.
Manufacturer:
Garrett Turbine Engine Co.
(FSCM 99193)
Model:
GTCP36-50(H)
Type:
Gas Turbine Engine (GTE), Pneumatic and Shaft Power
Change 8
1-17
