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|  MIL-T-18232B(AS)
(Cont)
7.
PARAGRAPH
Starting system
3.10.12
Priming system (reciprocating)
3.10.12.2
Starter
3.10.12.1
Pulse-Jet engine
3.10.12.1.3
Reciprocating engines
3.10.12.1.1
Rocket engine
3.10.12.1.4
Starting sequence (pulse-jet, ram-jet, liquid and solid
rockets, and other engine propulsion types)
3.10.12.1.5
Turbo-jet engine
3.10.12.1.2
Steel.:
Brazing
3.1.20.24
Fittings
3.1.20.3.2
Selection
3.2.8.1
Tubing
3.2.8.1
Welding
3.2.10.1.7
Stops, elevator and rudder
3.6.6
Storage and transit
3.1.18.1
Strength requirements
3.3.1, 3.3.2,1
Structural design criteria
3.3
Detail strength requirements
3.3.2
Captive flight conditions
3.3.2.3
Free flight conditions
3.3.2.2
Handling loads
3.3.2.5
Launching loads
3.3.2.4
Malfunction
3.3.2.2.1
Properties of material
3.3.2.6
Mass balance of control surfaces
3.3.3
Substitute materials
3.1.20.3
Supply catalog of Navy material
2.1.4
Surface covering:
Control
3.1.20.10.5
Fabric
3.1.20.10.4
Metal
3.1.20.10.3
Wood
3.1.20.10.4
Tabs
3.4.1
Tail group
3.5
Description
3.5.1
Elevator and rudder stops
3.5.6
Elevators
3.5.3
Fins
3.5.4
Rudder
3.5.5
Stabilizer
3.5.2
Tanks, fuel (fixed)
3.10.20.2
Capacity
3.10.10.2.1
Installation
3.10.10.2.2
63
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