MIL I 18373 : B
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INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF
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Details requirements for the installation of such equipment, both government furnished and contractor furnished, for Navy aircraft.
| Committee |
FSC 6605
|
| DevelopmentNote |
B NOTICE 1 - Notice of Inactivation for New Design. (07/2016)
|
| DocumentType |
Standard
|
| Pages |
21
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MS28042 Revision F:1982 | CLAMP, INSTRUMENT MOUNTING, AIRCRAFT (S/S BY NASM28042) |
| MIL-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for |
| MIL-P-26292 Revision C:1969 | PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF (NO S/S DOCUMENT) |
| MIL-C-18244 Revision A:1962 | Control and Stabilization Systems: Automatic, Piloted Aircraft, General Specification for |
| MIL-STD-1353 Revision C:2014 | Electrical Connectors, Plug-in Sockets and Associated Hardware, Selection and Use of |
| MS33558 Revision C:1968 | Numeral and Letters, Aircraft Instrument Dial, Standard Form of |
| MS33620 Revision B:1964 | CHART, HOSE SELECTION (S/S BY SAE-AIR797) |
| MS28028 Revision D:2011 | Thermometer, Self-Indicating, Bimetallic |
| MS33549 Revision B:1969 | CASE, INSTRUMENT, 2-3/4 DIAL, WITH SUMP, STANDARD DIMENSIONS FOR (NO S/S DOCUMENT) |
| MIL-C-6818 Revision D:1973 | Clamp, Instrument Mounting, Aircraft (S/S by NASM6818) |
| MIL-F-17874 Revision B:1965 | Fuel Systems, Aircraft, Installation and Test of |
| MS33632 Base Document:1960 | Wiring Diagram Two Pole Tachometer Generator and Percent RPM Tachometer Indicator |
| MIL-C-7188 Base Document:1951 | Compasses, Pilot\'s Standby, Installation of |
| MS33572 Revision C:1968 | Instrument, Pilot, Flight, Basic, Standard Arrangement for Helicopters |
| MS33638 Revision C:1969 | Cases, Instrument, Flange Mounted, Aircraft (No S/S Document) |
| MS33639 Revision D:1988 | Cases, Instrument, Clamp - Mounted, Aircraft |
| MIL-O-19838 Base Document:1956 | Oil Systems: Aircraft, Installation and Test of |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MS28112 Base Document:1960 | INSTRUMENT, BASIC STANDARD ARRANGEMENT FOR FIXED WING AIRCRAFT (NO S/S DOCUMENT) |
| MIL-STD-1247 Revision D:2009 | Markings, Functions and Hazards Designations of Hose, Pipe, and Tube Lines for Aircraft Missile, and Space Systems |
| MIL-C-6136 Revision A:1965 | Conduit: Electrical, Flexible, Shielded, Aluminum Alloy for Aircraft Installations (Use SAE-AS6136) |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| SAE AIR46B | The Preparation and Use of Chromel-Alumel Thermocouples for Aircraft Gas Turbine Engines |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| MIL-C-6390 Revision B:1959 | Clamps and Instruments, Aircraft, Installation of |
| MIL-G-7940 Revision C:1971 | Gages, Liquid Quantity, Capacitor Type, Installation and Calibration of (No S/S Document) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
| MIL N 25027 : G | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| MIL-STD-765 Revision A:1967 | Compass Swinging, Aircraft, General Requirements for (See Notice 5 for Replacement Information) |
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