MIL-C-38373 Revision B:1975
Withdrawn
Withdrawn
Cap, Fluid Tank Filler (No S/S Document)
Available format(s)
PDF
Published date
07-01-1975
Publisher
Withdrawn date
12-12-2007
US$20.00
Excluding Tax where applicable
Gives various types of gravity fill, filler caps for fluid tanks.
| DevelopmentNote |
B NOTICE 1 - Notice of Cancellation without Replacement. B NOTICE 2 - Notice of Reinstatement. B NOTICE 3 - Notice of Inactivation for New Design. B NOTICE 4 - Notice of Cancellation without Replacement. (01/2008)
|
| DocumentType |
Standard
|
| Pages |
37
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification covers gravity fill, filler caps for fluid tanks.
| DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| 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)/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)/12(2014) : 2014 | 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(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL F 38363 : B (3) | FUEL SYSTEM, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-F-87154 Base Document:1980 | FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
| MIL-T-5955 Revision C:1970 | TRANSMISSION SYSTEM, VTOL - STOL, GENERAL REQUIREMENTS FOR (NO S/S DOCUMENT) |
| MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| MIL L 23699 : E | LUBRICATING OIL, AIRCRAFT TURBINE ENGINES, SYNTHETIC BASE |
| RR-C-271 Revision G:2016 | Chains and Attachments, Carbon and Alloy Steel |
| MIL-L-27502 Base Document:1972 | Lubricating Oil, Aircraft Turbine Engine, Ester Base (No S/S Document) |
| MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
| MIL-STD-889 Revision C:2016 | Galvanic Compatibility of Electrically Conductive Materials |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MS27379 Revision A:1969 | ADAPTER, FLUID TANK FILLER (NO S/S DOCUMENT) |
| MS33588 Revision E:1984 | Nuts, Self-Locking, Aircraft, Reliability and Maintainability Usage Requirements for (S/Sby NASM33588) |
| TT-S-735 Revision A:1988 | STANDARD TEST FLUIDS, HYDROCARBON (S/S BY ASTM-D471) |
| MS20995 Revision E:1974 | WIRE, SAFETY OR LOCK (S/S BY NASM20995) |
| MIL L 6081 : C | LUBRICATING OIL, JET ENGINE |
| MIL-G-5572 Revision F:1969 | Gasoline, Aviation: Grades 80/87, 100/130, 115/145 (S/S by ASTM-D910) |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL T 25524 : D | TURBINE FUEL, AVIATION, THERMALLY STABLE |
| MIL-S-8879 Revision C:1991 | Screw Threads, Controlled Radius Root withIncreased Minor Diameter, General Specification for (S/S by SAE-AS8879) |
| MIL-STD-1523 Revision A:1984 | AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIEL (FOR AEROSPACE APPLICATIONS) (S/S BY SAE-AS1933 AND SAE-ARP5316) |
| MIL-L-22851 Revision D:1990 | Lubricating Oil, Aircraft Piston Engine (Ashless Dispersant) (S/S by SAE-J1899) |
| MIL-STD-794 Revision E:1982 | PART AND EQUIPMENT, PROCEDURES FOR PACKAGING AND PACKING OF |
| MIL-L-6082 Revision E:1990 | Lubricating Oil, Aircraft Piston Engine (Non-Dispersant Mineral Oil) (S/S by SAE-J1966) |
| MS33666 Revision C:1975 | PACKING, PREFORMED - AERONAUTICAL ELASTOMERIC, RANGE OF SIZES (S/S BY SAE-AS568) |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| O-E-760 Revision D:1987 | ETHYL ALCOHOL (ETHANOL); DENATURED ALCOHOL; PROPRIETARY SOLVENTS AND SPECIAL INDUSTRIAL SOLVENTS (S/S BY A-A-59282, A-A-51693, A-A-53880) |
| MIL N 25027 : G | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
Summarise
US$20.00
Excluding Tax where applicable
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