TM
55-1730-229-34
320A0-MME-000
AG
TO
35C2-3-473-2
TM
1730-34/1
Tabulated Data (continued)
Table 1-1.
Aviation Ground Power Unit (AGPU) (continued)
1.
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 450F (232C)
26.5 lb/minute at 24 psi , 10,000 (3048m) feet altitude -
Temperature 420F (232C)
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)
1-10
