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| MIL-D-23222A(AS)
(Cont)
2.1.1
Installation of Droppable Stores and Associated
MIL-I-8671
Release Systems
Installation and Test of Pyrotechnic Equipment
MIL-I-8672
in Aircraft, General specification for
Installation and Test of Aircraft Flexible
MIL-I-8673
Weapons Systems.
Installation: Aircraft armor
MIL-I-8675
Installation of Armament control systems and
MIL-I-8677
associated equipment in naval aircraft.
Cooling Requirements of Power Plant Installation
MIL-C-8678
Test Requirements Ground, Helicopter
MIL-T-8679
Installation of Oxygen Equipment in Aircraft
MIL-I-8683
Installation and Test of Electronic Equipment
MIL-I-8700
in Aircraft, General Specification for
Data and Tests Engineering Contract Requirements
MIL-D-8706
for Aircraft weapons systems.
De-Icing System, Pneumatic Boot, Aircraft General
MIL-D-8804
Specification for
Acoustical Noise Level in Aircraft; General
MIL-A-8806
Specification for
Airplane Strength and Rigidity, General Spec. for
MIL-A-8860
Fuel Systems, Aircraft, Installation and Test of
MIL-F-17874
Reports; Format and General Requirements
MIL-R-18136
Control and Stabilization Systems: Automatic,
MIL-C-18244
Piloted Aircraft; General Specification for
Lighting, Aircraft Interior, Installation of
MIL-L-18276
Heating and Ventilating Systems, Aircraft (General
MIL-H-18325
Specification for)
Test Procedures for Aircraft Cabin Pressurizing
MIL-T-18606
and Air Conditioning System
Thermal Anti-icing Equipment, Wing and Empennage
MIL-T-18607
Tank, Fuel, Aircraft, Auxiliary External, Design
MIL-T-18847
and Installation of
Environmental Systems, Pressurized Aircraft,
MIL-E-18927
General Requirements for
Oil Systems, Aircraft, Installation and Test Of
MIL-O-19838
Fire Warning systems, Aircraft, Radiation sensing
MIL-F-23447
Type, Test and Installation of
Weight and Balance Control Data (For Airplanes
MIL-W-25140
and Rotorcraft)
AERONAUTICAL REQUIREMENTS
Structural Design Requirements, Helicopters
AR-56
4
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