Table 1-1. Tabulated Data

55-1730-229-34

320A0-MME-000

35C2-3-473-2

1730-34/1

Tabulated Data (continued)

Table 1-1.

Aviation Ground Power Unit (AGPU) (continued)

400 Hertz, 3 phase, 0.8 power factor, 115/200V

AC voltage output:

AC power output:

30 KW continuous (45 KW for 30 seconds) with no DC

27.5 KW continuous with 50 amperes DC available from battery charger

4-wire output cable, 60 foot (18.3m)

DC power output:

28 vdc 700 amperes (1,000 amperes for 30 seconds) with no AC

28 vdc 50 amperes from battery charger with 27.5 KW AC available

2-wire output cable, 60-foot (18.3m)

Pneumatic output:

60 lb/minute at 40 psig (sea level) - Temperature 450°F (232°C)

26.5 lb/minute at 24 psi , 10,000 (3048m) feet altitude -

Temperature 420°F (232°C)

3.5 inch (8.9 cm) diameter output hose, 30 foot 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 80 dBA at 23 foot (7 meter) radius

Capacities (Liquids):

65 gallons (246 liters)

Fuel Tank

2.3 quarts (2.2 liters)

Engine Oil Sump

Hydraulic System

9 gallons (34 liters)

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