Figure 2-2. Mooring Pad Maximum Load Conditions

Figure 2-1. Mooring Pad Hardpoint Spacing

TM-1-1500-250-23 Aircraft Tie-down and Mooring Procedures Manual
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TM 1-1500-250-23 THE LOADS SHOWN ARE THE MAXIMUMS CALCULATED TO MOOR ARMY HELlCOPTERS IN 100 KNOT WINDS, IT IS RECOMMENDED THAT THE MOORING DEVICE BE CAPABLE OF WITHSTANDING THE MAXIMUM LOADS SHOWN. Figure 2-2. Mooring Pad Maximum Load Conditions 2-5

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