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| MIL-T-46616C
6.3 No-load testing. Permanent yielding of the trunnion mounting lugs, end cap, and piston is not cause
for rejection when thrusters are tested under "no load" on the piston.
6.4 Load firing. The expected performance of the thruster, under conditions simulating those existing
in aircraft, is obtained when the thruster satisfactorily meets the conditions of the "load" firing.
6.5 Hazard notice. The thruster described herein and certain of its components are flammable or
explosive and present hazards in manufacture, handling, storage, and shipment. The contractor should
recognize these properties and take appropriate measures to guard and protect against fire, explosion, adverse
environment, corrosive atmosphere, rough handling, and electrically induced incidents.
6.6 Definition.
6.6.1 Mechanical failure. Mechanical failure is any deformation or breakage of a part, the occurrence
of which is other than a design function.
6.7 Subject term (keyword) listing.
Ejection systems, aircrew
Emergency escape systems, aircrew
Escape systems, aircrew
Life-saving systems, aircrew
6.8 Changes from previous issue. Marginal notations are not used to identify changes with respect to
the previous issue because of the extensiveness of the changes.
Custodian:
Preparing activity
Navy - OS
Navy - OS
Air Force - 99
(Project 1377-0D92)
Review activity:
Air Force - 70
12
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