MIL-P-26292 Revision C:1969
Withdrawn
PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF (NO S/S DOCUMENT)
12-03-1969
05-04-1998
Details requirements for installation and inspection of pitot-static tubes, flush static ports and pitot tubes on aircraft and missiles.
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
This specification covers the requirements for the installation and inspection of pitot-static tubes, pitot tubes, and flush static ports on aircraft and missiles.
| MIL I 5949 : G | INSTRUMENTS, FLIGHT AND ENGINE, AIRCRAFT, FUNCTIONAL TESTS AND TOLERANCES OF |
| MIL P 83207 : B | PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
| 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)/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)/12(2014) : 2014 | 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)/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 |
| MIL I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| MIL P 83206 : B | PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR |
| MIL A 87211 : NOTICE 1 | AIR DATA SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD ENES, WRIGHT PATTERSON, AFB OH 45433 6503 |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL P 83207 : B | PITOT STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR |
| MIL-T-8606 Revision C:1973 | Tubing, Steel, Corrosion-Resistant (18-8 Stabilized and Extra Low Carbon) (Use SAE-AMS5560, SAE-AMS5563, SAE-AMS5564, SAE-AMS5565, SAE-AMS5566, SAE-AMS5567, SAE-AMS5569, SAE-AMS5570, SAE-AMS5571, SAE-AMS5639 and SAE-AMS5668) |
| MIL P 83206 : B | PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR |
| AN 6270 : 0010 | HOSE ASSEMBLY - DETACHABLE SWIVEL FITTING, LOW PRESSURE |
| MIL H 25579 : E | HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR |
| MIL M 7793 : F | METER, TIME TOTALIZING |
| WW-T-700-4 Revision F:1983 | TUBE, ALUMINUM ALLOY, DRAWN, SEAMLESS, 5052 (S/S BY SAE-AMS-WW-T-700/4) |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MS33611 Revision A:1983 | TUBE BEND RADII (S/S BY SAE-AS33611) |
| MIL-STD-1247 Revision D:2009 | Markings, Functions and Hazards Designations of Hose, Pipe, and Tube Lines for Aircraft Missile, and Space Systems |
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