LOCKHEED L-100 HERCULES
The Lockheed L-100 Hercules is a civilian cargo variant of the C-130 aircraft, with common specifications including a crew of 3–4, a maximum payload of about
51,05051 comma 050
51,050
lbs (
23,15023 comma 150
23,150
kg), and a maximum takeoff weight of
155,000155 comma 000
155,000
lbs (
70,30070 comma 300
70,300
kg). It is powered by four Allison 501-D22A turboprops, has a maximum speed of
354354
354
mph (
570570
570
km/h), and a range of
1,5351 comma 535
1,535
mi (
2,4702 comma 470
2,470
km).
General characteristics
- Crew: 3–4 (two pilots, navigator, flight engineer/loadmaster)
- Capacity:
51,05051 comma 050
51,050
lbs (
23,15023 comma 150
23,150
kg)
- Length:
112112
112
ft
99
9
in (
34.3534.35
34.35
m)
- Wingspan:
132132
132
ft
77
7
in (
40.440.4
40.4
m)
- Height:
3838
38
ft
33
3
in (
11.6611.66
11.66
m)
- Empty weight:
77,74077 comma 740
77,740
lbs (
35,26035 comma 260
35,260
kg)
- Maximum takeoff weight:
155,000155 comma 000
155,000
lbs (
70,30070 comma 300
70,300
kg)
Powerplant
- Engines: 4 × Allison 501-D22A turboprops
- Power:
4,5104 comma 510
4,510
shp (
3,3603 comma 360
3,360
kW) each