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L-100-30 Hercules - Aircraft Technical Specification
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Weights |
Distance |
Speed |
Dimensions / Capacity |
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Imp. |
Metric. |
|
Imp. |
Metric. |
M.T.O.W |
155,00lbs |
70,308kgs |
Main Door (Ramp) |
H 108" X W 120" |
H 2.74M X W 3.04M |
M.L.W |
135,00lbs |
61,236kgs |
Fwd Door |
N/A |
N/A |
M.Z.F.W |
125,00lbs |
56,700kgs |
Read Door |
N/A |
N/A |
Dry Operating Wt |
74,000lbs |
33,566kgs |
Lower Door(s) |
N/A |
N/A |
Ferry Range Empty |
2,390NM |
4,430Klm |
Max. Vol. |
6,057 ft3 |
170M3 |
Max Range-Avail P/Load |
2,390NM
4,400LBS |
4,430Klm
2,500kgs |
Total Max Vol. |
6,057 ft3 |
170M3 |
Max Net Payload |
50,000lbs |
22,860kgs |
Average Useable Max. Vol. |
6057 ft3 |
170M3 |
Main Cabin Floor Load Limitation |
72,00lbs/Ft2 |
35,157Kg/M2 |
Uld/Pallet Capacity |
Special to aircraft type and only fitted for rapid turnround work. |
Main Cabin Floor Area |
554Ft2 |
50.4M2 |
Max Fuel Capacity |
5,830IG
7,000USG |
26,500Ltr |
Typical Block Speed |
235Kts
270MPH |
435Klm/Hr |
Average Fuel Consumption |
625IG
750USG |
2,839Ltr |
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