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|  MIL-T-18232B(AS)
(Cont)
7.
PARAGRAPH
Readiness
Flight readiness
Installation on launcher
Ready storage checkout
Receptacles, electrical
Umbilical cord
Reciprocating engines:
Air intakes
Cooling systems
Cowl flaps
Cowling attachment
Cowling design
Dust protection System
Exhaust systems
Expansion and foaming space
Mounts
Oil tank capacity
Oil tanks
Priming system
Propeller components
Starter
Vibration islators
Recovery gear
Air recovery
Deployment mechanism
Location of component
Quick release device
Parachute
Ground recovery
Water recovery
Reinforced plastics
Reliable operating life
Reliability
Replaceability
Requirements
Residual oil and grease
Responsibility for inspection
Riveted construction
Riveting, flush
Rivets
Blind rivets
Hi-Shear rivets and lock bolts
Rocket engine:
Starter
Starting cycle
Rudders
61
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