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  TM 55-1730-229-34
TO 35C2-3-473-2
Tabulated Data (continued)
Table 1-1.
2.
Engine (continued)
-40°F (-40°C) to 135°F (57°C)
MIL-T-5624 Grade JP-5,
or MIL-T-83133 Grade JP-8
-40°F (-40°C) to 135°F (57°C)
Commercial Jet A
Sea level, l15°F (46°C) at 10,000 feet (3048m)
Diesel MIL-G-5572 or VV-F-800
Emergency Fuel (25 hours maximum)
Fuel Consumption (approximate):
125 lb/br (19 gph)
With bleed air
110 lb/hr (17 gph)
Without bleed air
Exhaust Gas Temperature Limits:
Allowable below 60% rotor
1600°F (871°C) for 30 seconds maximum
speed during start cycle
1600°F to 1800°F (871°C to 982°C) for
2 seconds maximum
Allowable above 60%
1300°F (704°C) maximum
rotor speed
Allowable at 100% rotor
1255°F (679°C) maximum
(1230 ± 25°F)
speed
Battery.
3.
Type:
Lead-acid MIL-B-83769D, or optional NiCad MS24498
Voltage:
24 vdc
Amp-Hours:
53
4.
Battery Charger.
Leland Electrosystems, Inc.
Manufacturer:
(FSCM 62624)
DSH831-1A
Model:
Voltage:
Output selectable at 28.5, 30.5, or 32 vdc
output:
50 ampere nominal - battery
20 ampere nominal - control circuits
Change 5 1-13
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