MIL-A-8863 Revision C:1993
Current
Current
The latest, up-to-date edition.
Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes
Available format(s)
PDF
Language(s)
English
Published date
19-07-1993
Publisher
€16.67
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PACKAGING
6. NOTES
Describes strength and rigidity requirements for ground loading conditions applicable to Navy acquired airplanes.
| DevelopmentNote |
Supersedes MIL A 8862 (1960) and MIL A 008862 (A). (06/2004)
|
| DocumentType |
Standard
|
| Pages |
39
|
| ProductNote |
NEW CHILD NOT 1 2019 NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification defines the strength and rigidity requirements applicable to land-based and ship-based airplanes for the following ground loading conditions:
a. Take-offs.
b. Landings
c. Ground maneuvering.
d. Ground handling.
e. Supplemental loads.
| MIL A 8862 : 0 | AIRPLANE STRENGTH AND RIGIDITY, LANDPLANE, LANDING AND GROUND HANDLING LOADS |
| DEFSTAN 00-970(PT1)SEC4/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| 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 |
| MIL-HDBK-2066 Base Document:1999 | Catapulting and Arresting Gear Forcing Functions for Aircraft Structural Design |
| JSSG-2010-7 Base Document:1998 | Crew Systems Crash Protection Handbook |
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| 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)/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)/12(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)/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 |
| SAE ARP1311C | Landing Gear Structures and Mechanisms |
| 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)SEC4/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4 - DESIGN AND CONSTRUCTION |
| MIL-HDBK-244 Revision A:1990 | Guide to Aircraft/Stores Compatibility |
| 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)SEC4/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
| MIL-A-8870 Revision C:1993 | Airplane Strength and Rigidity Vibration, Flutter, and Divergence |
| DEFSTAN 00-970(PT1)SEC4/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 4: DESIGN AND CONSTRUCTION |
| MIL-DTL-85110 Revision B:1997 | Bar, Repeatable Release Holdback (RRHB), Aircraft Launching, General Requirement for |
| MIL-HDBK-516 Revision C:2014 | Airworthiness Certification Criteria |
| MIL-A-8867 Revision C:1987 | Airplane Strength and Rigidity Ground Tests |
| MIL-STD-2066 Base Document:1981 | CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (S/S BY MIL-HDBK-2066) |
| SAE ARP1107C | Tail Bumpers for Piloted Aircraft |
| JSSG-2001 Revision B:2004 | Air Vehicle |
| SAE AIR6906 | Impulse Towing Loads |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-STD-805 Revision B:1987 | TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR |
| MIL-HDBK-1763 Base Document:1998 | Aircraft/Stores Compatibility: Systems Engineering Data Requirements and Test Procedures |
| JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL-W-5013 Revision L:1991 | Wheel and Brake Assemblies, Aircraft General Specification For |
| SAE AS8860 | Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications |
| MIL-STD-2066 Base Document:1981 | CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (S/S BY MIL-HDBK-2066) |
| MIL-T-81259 Revision B:1991 | Tie-downs, Airframe Design, Requirements for (S/S by MIL-STD-81259) |
| MIL-L-22589 Revision D:1991 | Launching System, Nose Gear Type, Aircraft |
| MIL-A-8867 Revision C:1987 | Airplane Strength and Rigidity Ground Tests |
| MIL-A-18717 Revision C:1993 | Arresting Hook Installation, Aircraft (S/S by MIL STD-18717) |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
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