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Figure 4-3. Mooring Hardware Details in Configuration 1 (Figure 4-1)

TM-1-1500-250-23 Aircraft Tie-down and Mooring Procedures Manual
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TM 1-1500-250-23 Figure   4-1.   Mooring   Hardware   Installation   Assembly   Details   -   Configuration   1 NOTE Insure that adequate clearance for the MB1 chain adjuster is provided in relation to the aircraft and the aircraft hardpoint fitting. NOTE Either of the configurations shown can be used to secure the aircraft to the moor- ing pad. Figure   4-2.   Mooring   Hardware   Installation   Assembly   Details   -   Configuration   2 4-5







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