| Dimensions |
| Wingspan |
40.41m
(132 ft 7") |
| Length |
34.37m
(112 ft 9") |
| Height |
11.66m
(38 ft 2") |
| |
| Maximum
certified take-off weight |
70 307
kg (155 000 lbs) |
| Maximum
certified landing weight |
61 235
kg (135 000 lbs) |
| Maximum
ceritfied zero fuel weight |
57 727
kg (127 000 lbs) |
| Basic
empty weight |
34 545
kg (76 000 lbs) |
| Average
APS weight |
35 000
kg (77 000 lbs) |
Cargo
Compartment |
| Length |
17.07m
(54 ft) |
| Width |
3.02m
(10 ft 3") |
| Height |
2.74m
(9 ft) |
| Cubic
capacity |
140
cubic meter (excluding ramp) |
| Floor
height (above ground) |
0.99
- 1.04m (3 ft 3" - 3 ft 5") |
| Cargo
floor |
Aircraft
can be supplied with either a flat metal floor, a wooden
floor or an adjustable roller system. |
| Maximum
Payloads |
| Palletized |
21 500
kg (47 395 lbs) |
| Break
bulk |
22 954
kg (50 600 lbs) |
| Maximum
load per Pallet |
| 300
cm x 224 cm pallets |
4 545
kg (10 019 lbs) maximum 7 pallets |
| 275
cm x 224 cm pallets |
3 636
kg (8 015 lbs) maximum 7 pallets |
| Pallet
height |
Maximum
259 cm |
| |
Landing
Requirements
The
maximum landing weight for the Hercules L100/30
is 135 000 lbs (61 235kg).
At
this weight the following landing distances are
required.
|
Airfield
Elevation |
Runway
Length (zero wind) |
| Sea
Level |
4
800 ft |
| 1
000 ft |
5
000 ft |
| 2
000 ft |
5
200 ft |
| 3
000 ft |
5
300 ft |
| 4
000 ft |
5
500 ft |
| 5
000 ft |
5
700 ft |
