Figure 4-2. Tiedown diagram for bucket in C-130 aircraft.

TM 55-3805-262-14

Figure 4-4. Tiedown diagram for MW24C scoop loader in C-141

aircraft.

Figure 4-2. Tiedown diagram for bucket in C-130 aircraft.

g. Restraint factors (g loads) for minimum ac-

ceptable conditions specified for crew and passenger

safety in the event of a controlled emergency landing

are specified in applicable aircraft TO. Tiedown

diagram figures 4-3 through 4-5 and tiedown tables

4-1 through 4-3 are for general guidance. The figures

show representative tiedown patterns, and the tables

show the tiedown devices required (provided aboard

aircraft), tiedown points on the carrier, and cor-

Figure 4-5. Tiedown diagram for MW24C scoop loader in C-5

aircraft.

responding fitting on the aircraft floor to which the

devices are secured. Tiedowns will be applied as

directed by the aircraft loadmaster.

4-6. Transport by US Army Aircraft

The scoop loader exceeds size and weight limitations

for transport by US Army fixed or rotary wing

aircraft.

Figure 4-3. Tiedown diagram for MW24C scoop in C-130

aircraft.

4-2