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 : Users cannot be edited or removed once added to your Multi user PDF.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 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 |
| 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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