MIL-PRF-57267 Base Document:2017
Current
Current
The latest, up-to-date edition.
COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5
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English
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
CONCLUDING MATERIAL
Specifies aerial refueling fuel reception couplings that provide redundant regulated fuel pressure and suppression of surges generated by the receiver aircraft using the probe and drogue method of aerial refueling.
| Committee |
FSC 1680
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| DevelopmentNote |
New child NOT 1 2022 is added
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| DocumentType |
Standard
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| Pages |
52
|
| ProductNote |
New child NOT 1 2022 is added
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
|
| SAE AMS 2447 : 2012 | COATING, THERMAL SPRAY, HIGH VELOCITY OXYGEN/FUEL PROCESS |
| MIL-PRF-7024 Revision F:2012 | CALIBRATING FLUIDS, AIRCRAFT FUEL SYSTEM COMPONENTS |
| SAE AMS 1424 : 2016 | FLUID, AIRCRAFT DEICING/ANTI-ICING, SAE TYPE 1 |
| MIL-I-8500 Revision D:1980 | INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR AEROSPACE VEHICLES |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| SAE AMS 1428 : 2017 | FLUID, AIRCRAFT DEICING/ANTI-ICING, NON-NEWTONIAN, (PSEUDOPLASTIC), SAE TYPES 2, 3 AND 4 |
| MIL-STD-130 Revision N:2007 | IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY |
| MIL-DTL-5624 Revision W:2016 | TURBINE FUEL, AVIATION, GRADES JP-4 AND JP-5 |
| NASM33588:2010 | NUT, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR |
| SAE AMS 2175 : 2010 | CASTINGS, CLASSIFICATION AND INSPECTION OF |
| SAE ARP 868 : 2013 | METHOD - PRESSURE DROP TESTS FOR FUEL SYSTEM COMPONENTS |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| GOST 10227 : 1986 AMD 6 2012 | |
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| SAE AS 568 : 2014 | AEROSPACE SIZE STANDARD FOR O-RINGS |
| NASM25027:2012 | NUT, SELF-LOCKING, 250 DEGREES F, 450 DEGREES F, AND 800 DEGREES F |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| NASM33540:2003 | SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR |
| MIL-DTL-5541 Revision F:2006 | Chemical Conversion Coatings on Aluminum and Aluminum Alloys |
| MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
| DEFSTAN 91-091/9(2016) : 2016 | TURBINE FUEL, AVIATION KEROSINE TYPE, JET A-1 NATO CODE: F-35 JOINT SERVICE DESIGNATION: AVTUR |
| SAE AMS 7259 : 2013 | RUBBER: FLOUROCARBON (FKM), HIGH TEMPERATURE/FLUID RESISTANT, LOW COMPRESSION SET/85 TO 95 HARDNESS, FOR SEALS IN FUEL SYSTEMS AND SPECIFIC ENGINE OIL SYSTEMS |
| MS24358 Revision B:2016 | FITTING, HOSE END - TYPE MA-2, FLIGHT PRESSURE REFUELING, RECEPTION COUPLING, OUTLINE DIMENSIONS FOR |
| NASM20995:2012 | WIRE, SAFETY OR LOCK |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| SAE AMSSTD595A:2017 | COLORS USED IN GOVERNMENT PROCUREMENT |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-DTL-83133 Revision J:2015 | TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34), NATO F-35, AND JP-8+100 (NATO F-37) |
| MIL-DTL-27426 Revision C:1998 | RINGS, RETAINING, SPIRAL (UNIFORM CROSS SECTION) |
| SAE AS 83485 : 2016 | O-RING MOLDED FROM AMS7287 MATERIAL |
| MS24361 Revision C:2016 | RING, SPLIT - TYPE MA-2, FLIGHT PRESSURE REFUELING, RECEPTION COUPLING |
| MS24362 Revision A:1961 | Sleeve - Type MA-2, Flight Pressure Refueling, Reception Coupling |
| MIL-DTL-25988 Revision C:2006 | RUBBER, FLUOROSILICONE ELASTOMER, OIL- AND FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES |
| ASME Y14.100 : 2017 | ENGINEERING DRAWING PRACTICES - ENGINEERING DRAWING AND RELATED DOCUMENTATION PRACTICES |
| SAE AS 29513 : 2016 | PACKING, PREFORMED, HYDROCARBON FUEL RESISTANT, 'O' RING |
| MIL-S-7742 Revision D:1991 | SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR |
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