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TM 5-4930-234-13&P
54. Install strainer (8) in nozzle (10). See Figure 5-6.
55. Install cam-lock coupling (5) or unisex coupling (7) on nozzle (10). Hand- tighten only.
Failure of any test is cause for rejection of nozzle assembly until fault is corrected.
f.
Testing. After repair and prior to release for aircraft refueling, test nozzle in an operating, pressurized
refueling system to ensure no leakage occurs.
All data on pages 5-29 and 5-30, including Figure 5-24, have been deleted.
Change 4 5-28
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