MIL I 18373 : B
Current
Current
The latest, up-to-date edition.
INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF
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Important note : All end users must be registered with an Account prior to user licenses being assigned.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 |
| SAE ARP 426 : 2001 | COMPASS SYSTEM INSTALLATIONS |
| MS28042 Revision F:1982 | CLAMP, INSTRUMENT MOUNTING, AIRCRAFT |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| MIL-P-26292 Revision C:1969 | PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF |
| 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 LETTER, AIRCRAFT INSTRUMENT DIAL, STANDARD FORM OF |
| MS33620 Revision B:1964 | CHART, HOSE SELECTION |
| MS28028 Revision D:2011 | THERMOMETER, SELF-INDICATING, BIMETALLIC |
| MS33549 Revision B:1969 | CASE, INSTRUMENT, 2 3/4 DIAL, WITH SUMP, STANDARD DIMENSIONS FOR |
| MIL-C-6818 Revision D:1973 | CLAMP, INSTRUMENT MOUNTING AIRCRAFT |
| 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 | CASE, INSTRUMENT, FLANGE MOUNTED, AIRCRAFT |
| MS33639 Revision D:1988 | CASE, INSTRUMENT, CLAMP MOUNTED AIRCRAFT (ASG) |
| MIL-O-19838 Base Document:1956 | Oil Systems: Aircraft, Installation and Test of |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MS28112 Base Document:1960 | INSTRUMENT, BASIC STANDARD ARRANGEMENT FOR FIXED WING AIRCRAFT |
| 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 LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| SAE AIR 46B : 2014 | THE PREPARATION AND USE OF CHROMEL-ALUMEL THERMOCOUPLES FOR AIRCRAFT GAS TURBINE ENGINES |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-C-6390 Revision B:1959 | CLAMPS AND INSTRUMENTS, AIRCRAFT, INSTALLATION OF |
| MIL-G-7940 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE, INSTALLATION AND CALIBRATION OF |
| 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 |
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