• There are no items in your cart

MIL-A-8861 Revision B:1986

Current

Current

The latest, up-to-date edition.

AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS

Available format(s)

PDF

€17.95
Excluding VAT

1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES

Describes requirements for strength and rigidity for flight loading conditions.

Committee
FSC 1510
DevelopmentNote
Supersedes MIL A 008861 (A). (07/2005)
DocumentType
Standard
Pages
33
ProductNote
NEW CHILD NOT 1 2019 IS NOW ADDED.
PublisherName
US Military Specs/Standards/Handbooks
Status
Current
Supersedes

SAE AIR 5451 : 2017 A GUIDE TO LANDING GEAR SYSTEM INTEGRATION
MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
MIL-A-8866 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
SAE ARP 94910 : 2012 AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR
MIL-A-23121 Revision C:1970 AIRCREW ENVIRONMENTAL, ESCAPE AND SURVIVAL COCKPIT CAPSULE SYSTEM, 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)/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)/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)/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)/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
MIL F 9490 : D FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-HDBK-244 Revision A:1990 GUIDE TO AIRCRAFT - STORES COMPATIBILITY
MIL STD 1763 : A AIRCRAFT STORES CERTIFICATION PROCEDURES
MIL-A-8870 Revision C:1993 AIRPLANE STRENGTH AND RIGIDITY VIBRATION, FLUTTER, AND DIVERGENCE
SAE AS 8860 : 2012 LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS
JSSG-2001 Revision B:2004 Air Vehicle
MIL-DTL-9490 Revision E:2008 FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
SAE AS 94900 : 2007 AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-HDBK-1763 Base Document:1998 AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES
MIL-A-8871 Revision A:1971 AIRPLANE, TESTS, STRENGTH AND RIGIDITY FLIGHT AND GROUND OPERATIONS
MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-F-8785 Revision C:1980 FLYING QUALITIES OF PILOTED AIRPLANES

MIL-A-8868 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
MIL-A-8867 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS
MIL-A-8866 Revision C:1987 AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE
MIL-D-8708 Revision C:1991 DEMONSTRATION REQUIREMENTS FOR AIRPLANES
MIL-A-8860 Revision B:1987 AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.