MIL-DTL-27422 Revision F:2014
Current
The latest, up-to-date edition.
Tank, Fuel, Crash-Resistant, Ballistic-Tolerant, Aircraft
English
06-02-2014
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Specifies the requirements and verification testing for crash-resistant, ballistic-tolerant fuel cells for use in fixed wing and rotary-wing aircraft (including tilt rotor).
| DevelopmentNote |
Supersedes MIL T 27422 (B) (01/2002)
|
| DocumentType |
Standard
|
| Pages |
46
|
| ProductNote |
NEW CHILD NOT 1 2019 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers the requirements and verification testing for crash-resistant, ballistic-tolerant fuel cells for use in fixed wing and rotary-wing aircraft (including tilt rotor). Exact design criteria such as fuel cell dimensions, total weight, and interface requirements will be dependent upon the intended aircraft specified in the contract or purchase order.
| 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)/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)/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)/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-HDBK-510 Revision A:2014 | Aerospace Fuels Certification |
| MIL-HDBK-510-1 Revision A:2010 | Aerospace Fuels Certification (S/S by MIL-HDBK-510) |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-STD-801 Revision E:2017 | INSPECTION AND ACCEPTANCE STANDARDS FOR FLEXIBLE FUEL CELLS AND FITTINGS |
| SAE AIR4170B | Reticulated Polyurethane Foam Explosion Suppression Material for Fuel Systems and Dry Bays |
| 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-DTL-5624 Revision W:2016 | Turbine Fuel, Aviation, Grades JP-5 (NATO F-44) |
| ASTM D 413 : 1998 | Standard Test Methods for Rubber Property-Adhesion to Flexible Substrate |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| MIL-DTL-83133 Revision J:2015 | Turbine Fuel, Aviation, Kerosene Type, JP-8 (NATO F-34) and NATO F-35 |
| MIL-STD-662 Revision F:1997 | V50 Ballistic Test for Armor |
| FED-STD-791 Revision D:2007 | Testing Method of Lubricants, Liquid Fuels, and Related Products |
| ASTM D 471 : 2016-02 | TEST METHOD FOR RUBBER PROPERTY - EFFECT OF LIQUIDS |
| MIL-STD-801 Revision E:2017 | INSPECTION AND ACCEPTANCE STANDARDS FOR FLEXIBLE FUEL CELLS AND FITTINGS |
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