BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR

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US Military Specs/Standards/Handbooks

Describes bleed air systems for turbo-jet, turbo-shaft and turbo-prop aircraft.

DevelopmentNote	Notice 1 - Notice of Inactivation for New Design (12/2001)
DocumentType	Standard
Pages	13
PublisherName	US Military Specs/Standards/Handbooks
Status	Current

DEFSTAN 00-970(PT1)SEC4/11(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
SAE AS 81366 : 2002	BOUNDARY LAYER CONTROL SYSTEM; PRESSURE
DEFSTAN 00-970(PT1)SEC4/4(2006) : 2006	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
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)/14(2014) : 2014	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)/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)/15(2015) : 2015	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)/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
DEFSTAN 00-970(PT1)SEC4/13(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/12(2014) : 2014	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/8(2011) : 2011	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/6(2010) : 2010	DESIGN AND AIRWORTHINESS REQUIREMENTS FORD SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/14(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT7)SEC2/SUPP4/5(2015) : INTERIM	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)
DEFSTAN 00-970(PT1)SEC4/9(2012) : 2012	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/5(2007) : 2007	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT1)SEC4/10(2013) : 2013	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
DEFSTAN 00-970(PT7)SEC2/SUPP4/6(2015) : 2015	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 4: DESIGN AND CONSTRUCTION (SUBPART D)
DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010	DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS
MIL-D-8804 Revision B:1993	DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-E-18927 Revision E:1983	ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR
SAE ARP 292 : 2014	ENVIRONMENTAL CONTROL SYSTEMS FOR HELICOPTERS

MIL-STD-704 Revision F:2004	AIRCRAFT ELECTRIC POWER CHARACTERISTICS
MIL-E-6051 Revision D:1967	ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM
MIL C 27536 : B	COUPLING, CLAMP, GROOVED, V-BAND
MIL-S-8879 Revision C:1991	SCREW THREADS, CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER, GENERAL SPECIFICATION FOR
MIL C 5015 : G	CONNECTOR, ELECTRICAL, CIRCULAR THREADED AN TYPE, GENERAL SPECIFICATION FOR
MIL-W-5088 Revision L:1991	Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
MIL C 6021 : H NOTICE 1	CASTINGS, CLASSIFICATION AND INSPECTION OF
MIL-E-7080 Revision B:1962	ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF
MIL-F-7179 Revision G:1993	FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM
MIL-S-7742 Revision D:1991	SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES, GENERAL SPECIFICATION FOR