TM-55-2320-280-14 HMMWV Transportability Guidance M998 Series Download
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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 AP- 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 Designation Capacity in 1,000 lb Type Capacity in 1,000 lb Attach to Item B5......................... F5......................... B19....................... C19 ...................... E19....................... F19 ....................... 10 10 10 10 10 10 MB1 MB1 MB1 MB1 MB1 MB1 10 10 10 10 10 10 Right rear bumper tiedown fitting. Left rear bumper tiedown fitting. Right front bumper tiedown fitting. Right front bumper tiedown fitting. Left front bumper tiedown fitting. Left front bumper tiedown fitting. 4-4