|
| |
TM 5-4930-235-13&P
f. Testing.
WARNING
High pressures used during testing may cause rupturing or bursting of faulty hoses and result in
serious injury. To prevent injury, cover hoses with a suitable safety shield. Be sure pressures
are bled off before exposing or touching hoses.
CAUTION
Failure of any test is cause for rejection of nozzle assembly until fault is corrected. Refer to
Troubleshooting, Table 5-1, to determine probable cause of failure.
If strainer housing or coupling threads leak, tighten one thread. Do not over tighten. Failure to
comply can result in damage to parts.
NOTE
For testing, unisex coupling must be replaced with cam-lock assembly MS27026-1 1 (FSCM
96906) complete with gasket MS27030-6 (FSCM 96906). When testing is completed, reassemble
nozzle using instructions in chapter 4.
(1) After repair and prior to release for aircraft refueling, test nozzle in an operating, pressurizing refueling
system to ensure no leakage occurs.
All data on pages 5-22.1/(5-22.2 blank and 5-23, including Figure 5-10, have been deleted.
Change 2
5-22
|
