MIL-DTL-38769E
APPENDIX A
TABLE I. Systems codes (aircraft) - Continued
18
VERTICAL OR SHORT TAKEOFF AND LANDING (V/STOL) POWER AND CONTROL
TRANSMISSION SYSTEM
19
ENGINE STARTING
21
RECIPROCATING POWER PLANT
22000
TURBOPROP/TURBOSHAFT PROPULSION SYSTEM
23000
TURBOJET/TURBOFAN PROPULSION SYSTEM
(Those basic engine components as deined in TO 2J-1-24, Equipment Comprising a Complete Basic
Gas Turbine Engine)
NOTE: Constant Speed Drives will be coded to System 42, Electrical Power Supply
24
AUXILIARY POWER PLANT
25
ROCKET POWER PLANT
26
HELICOPTER ROTARY WING DRIVE SYSTEM
27
TURBO JET/TURBO FAN PROPULSION SYSTEM ACCESSORY GEAR BOX (B-1 only)
31
ELECTRIC PROPELLER
32
HYDRAULIC PROPELLER
33
ELECTRO HYDRAULIC PROPELLER
34
MECHANICAL AND FIXED PITCH PROPELLERS
39
ICE AND RAIN PROTECTION
41
AIR CONDITIONING, PRESSURIZATION, AND SURFACE ICE CONTROL
42
ELECTRICAL POWER SUPPLY
43
ELECTRICAL MULTIPLEX (EMUX)
44
LIGHTING SYSTEM
45
HYDRAULIC AND PNEUMATIC POWER SUPPLY
46
FUEL SYSTEM
47
OXYGEN SYSTEM
48
INDICATING/RECORDING
49
MISCELLANEOUS UTILITIES
51
INSTRUMENTS
52
AUTOPILOT
53
DRONE AIRBORNE LAUNCH AND GUIDANCE SYSTEMS
54
TELEMETRY
55
MALFUNCTION ANALYSIS AND RECORDING EQUIPMENT
56
AUTOMATIC ALL WEATHER LANDING SYSTEM
57
INTEGRATED GUIDANCE AND FLIGHT CONTROL (Includes auto pilot when part
of integrated system)
59
CREW COMMUNICATIONS (Use if ground communications is desired, i.e., VHF, UHF, etc.)
60
VERY LOW FREQUENCY/LOW FREQUENCY (VLF/LF) COMMUNICATIONS
26
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