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Page Title:
Section III. TRANSPORT BY US ARMY AIRCRAFT |
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 25 August 1988
TM 55-2320-280-14
LEGEND:
C-5 AIRCRAFT
o
ALL CARGO TIEDOWN FITTING RATINGS 25000 LB EACH
NOTE: FLOOR TIEDOWN FITTINGS ARE LOCATED IN ROWS A THROUGH G ANC COLUMNS 1 THROUGH 38.
COLUMNS OF TIEDOWNS ARE LOCATED ON THE RAMPS: FOUR ON THE FORWARD RAMP AND
FIVE ON THE AFT RAMP. THIS IS A TYPICAL TIEDOWN PROCEDURE AND ONLY COLUMNS 6
THROUGH 24 ARE SHOWN. ITEM BEING SHIPPED CAN BE TIED DOWN AT ANY LOCATION A P-
PROVED BY THE LOADMASTER.
Figure 4-4. Tiedown diagram for HMMWV in C-5A aircraft.
Section III. TRANSPORT BY US ARMY AIRCRAFT
4-7. Fixed-Wing Aircraft
The HMMWVs cannot be transported in any US Army fixed-wing aircraft, because the vehicles exceed the air-
craft size and weight limitations.
Table 4-1. Tiedown Data for HMMWV in US Air Force C-130 Aircraft (Fig. 4-2)
Tiedown Fitting
Tiedown Device
Capacity
Capacity
Attach to Item
Designation
in 1,000 lb
Type
in 1,000 lb
B5.........................
10
MB1
10
Right rear bumper tiedown fitting.
F5.........................
10
MB1
10
Left rear bumper tiedown fitting.
B19.......................
10
MB1
10
Right front bumper tiedown fitting.
C19 ......................
10
MB1
10
Right front bumper tiedown fitting.
E19.......................
10
MB1
10
Left front bumper tiedown fitting.
F19 .......................
10
MB1
10
Left front bumper tiedown fitting.
4-4
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