STANAG 3447 : 2016
Current
Current
The latest, up-to-date edition.
AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS
Available format(s)
Hardcopy , PDF
Language(s)
English
Published date
28-06-2016
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Purpose of this agreement is to achieve and maintain the required compatibility among the interfaces required to engage in probe-drogue refuelling operations, to facilitate air-to-air refuelling between aircraft of NATO forces.
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
NATO
|
| Status |
Current
|
| Supersedes |
| DEFSTAN 00-970(PT0)/3(2003) : 2003 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| 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)/7(2011) : 2011 | 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)/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)/13(2014) : 2014 | 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)/16(2015) : 2015 | 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 |
| STANAG 7191 : 2013 | AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS |
| ATP 3.3.4.5 : 2013 | AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS |
| JSSG-2001 Revision B:2004 | Air Vehicle |
| ATP 3.3.4.7 : 2013 | AIR-TO-AIR REFUELLING SIGNAL LIGHTS IN HOSE AND DROGUE SYSTEMS |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| STANAG 7215 : 2013 | AIR-TO-AIR REFUELLING SIGNAL LIGHTS IN HOSE AND DROGUE SYSTEMS |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| DEFSTAN 00-970(PT0)/18(2017) : 2017 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| STANAG 3971 : 2013 | AIR-TO-AIR REFUELLING - ATP-56 |
| MS24359 Revision B:2016 | NOSE, PROBE MAST - TYPE MA-2, FLIGHT PRESSURE REFUELING NOZZLE, OUTLINE DIMENSIONS FOR |
| MS24356 Revision E:2016 | NOZZLE - TYPE MA-2, FLIGHT PRESSURE REFUELING |
| MS24355 Revision C:2016 | COUPLING, RECEPTION - TYPE MA-2, FLIGHT-PRESSURE-REFUELING, ASSEMBLY OF |
| ATP 3.3.4.2 : 2013 | AIR TO AIR REFUELLING |
| STANAG 7191 : 2013 | AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS |
| MS24358 Revision B:2016 | FITTING, HOSE END - TYPE MA-2, FLIGHT PRESSURE REFUELING, RECEPTION COUPLING, OUTLINE DIMENSIONS FOR |
| ATP 3.3.4.5 : 2013 | AIR-TO-AIR (AERIAL) REFUELLING EQUIPMENT: BOOM-RECEPTACLE SYSTEM AND INTERFACE REQUIREMENTS |
| MS24360 Revision C:2016 | RING, LOCK, FLIGHT PRESSURE REFUELING NOZZLE |
| JSSG-2001 Revision B:2004 | Air Vehicle |
| MIL-N-25161 Revision C:1969 | NOZZLE, AERIAL PRESSURE REFUELING, TYPE MA-2 |
| MS24357 Revision B:2016 | FLANGE, DROGUE CONE - TYPE MA-2 RECEPTION COUPLING, FLIGHT PRESSURE REFUELING, OUTLINE DIMENSIONS FOR |
| MIL-PRF-81975 Revision C:2008 | COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4 |
| 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 A 008865 : A NOTICE 1 | AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
| MIL-H-4495 Revision D:1985 | HOSE ASSEMBLY, RUBBER, AERIAL REFUELING |
| MIL-A-19736 Revision A:1960 | AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR |
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