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MIL
MIL-STD-1290 Revision A:1988

MIL-STD-1290 Revision A:1988

Current

Current

The latest, up-to-date edition.

LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE

Amended by

MIL-STD-1290 Revision A Notice 3 - Validation:2019

Available format(s)

PDF

Publisher

US Military Specs/Standards/Handbooks

1 SCOPE
2 REFERENCED DOCUMENTS
3 DEFINITIONS
4 GENERAL REQUIREMENTS
5 DETAIL REQUIREMENTS
6 NOTES

Defines minimum crash resistance requirements for implementation in the initial stages of aircraft system design.

Committee
FSC 15GP
DevelopmentNote
A NOTICE 1 - Notice of Cancellation without replacement. (04/2004) A NOTICE 2 - Notice of Reinstatement (01/2006)
DocumentType
Standard
Pages
51
ProductNote
NEW CHILD NOT 3 2019 NOW ADDED
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
JSSG-2010-7 Base Document:1998 Crew Systems Crash Protection Handbook
SAE ARP 1616 : 2017 SELF-SEALING BREAKAWAY VALVES FOR CRASH-RESISTANT AIRCRAFT FUEL AND OIL SYSTEMS
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)/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)/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
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(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)SEC4/13(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION
SAE AIR 4566 : 2015 CRASHWORTHY LANDING GEAR DESIGN
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)SEC4/10(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)
SAE AIR 1664 : 2013 AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS
MIL-HDBK-516 Revision C:2014 AIRWORTHINESS CERTIFICATION CRITERIA
JSSG-2009 Revision A:2013 Air Vehicle Subsystems

MIL-H-38360 Revision B:1966 HOSE, ASSEMBLIES, TETRAFLUOROETHYLENE, HIGH-TEMPERATURE, HIGH PRESSURE, 3000 PSI HYDRAULIC AND PNEUMATIC
MIL H 25579 : E HOSE ASSEMBLY, TETRAFLUOROETHYLENE, HIGH TEMPERATURE MEDIUM PRESSURE, GENERAL REQUIREMENTS FOR
MIL-S-58095 Revision A:1986 SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR
MIL H 83282 : C HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, AIRCRAFT, METRIC, NATO CODE NUMBER H 537
MIL-S-85510 Base Document:1981
MIL H 83796 : 0 HOSE ASSEMBLY, RUBBER, LIGHTWEIGHT, MEDIUM PRESSURE, GENERAL SPECIFICATION FOR

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