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
Free
Excluding VAT
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 Refueling Systems, General Specification for |
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