ATP 3.3.4.6 : 2016
Current
The latest, up-to-date edition.
AIR-TO-AIR (AERIAL) REFUELING EQUIPMENT: PROBE-DROGUE INTERFACE CHARACTERISTICS
Hardcopy , PDF
English
28-06-2016
Important note : Users cannot be edited or removed once added to your Multi user PDF.
CHAPTER 1 - INTRODUCTION
CHAPTER 2 - SPECIFICATIONS
ANNEX A - RECEPTION COUPLING - MATING DIMENSIONS
ANNEX B - NOZZLE MATING DIMENSIONS
ANNEX C - AAR PROBE CLEARANCE ENVELOPE
ANNEX D - AAR PROBE NOZZLE LATCH TEST GAUGE
Gives air-to-air refueling (AAR) systems requirements and to standardize the interfaces required to engage in probe-drogue refueling operations to facilitate AAR between aircraft of NATO forces.
| DocumentType |
Standard
|
| Pages |
26
|
| PublisherName |
NATO
|
| Status |
Current
|
| 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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