JSSG-2010-7 Base Document:1998
Current
The latest, up-to-date edition.
Crew Systems Crash Protection Handbook
30-10-1998
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1 SCOPE
1.1 Scope
2 APPLICABLE DOCUMENTS
2.1 General
2.2 Government documents
2.3 Non-Government publications
2.4 Order of precedence
3 REQUIREMENTS
3.1 Crew Systems Engineering
3.2 Crew Systems Automation, Information, and Control/Display
Management
3.3 Cockpit/Crew Station/Cabin
3.4 Aircrew Alerting
3.5 Aircraft Lighting
3.6 Sustenance and Waste Management (S&WM) Systems Requirements
3.7 Crash Survivability
4 VERIFICATION (WITH REQUIREMENTS)
5 DEFINITIONS
6 NOTES
6.1 Intended use
6.2 Supersession data
6.2 Subject term (key word) listing
Describes guidance for the development requirements and verifications for occupant crash protection and for crash protective aspects of seating, restraint, and crewstation and passenger/troop station design.
| DevelopmentNote |
Supersedes MIL STD 1776 (A) and MIL STD 1807 (1990). (04/2004) NOTICE 1 - Notice of Validation. (08/2008) NOTICE 2 - Notice of Validation. (06/2013) NOTICE 3 - Notice of Validation. (04/2018)
|
| DocumentType |
Standard
|
| Pages |
159
|
| ProductNote |
NEW CHILD NOT 3 2018 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| ADS-65-HDBK : 2004 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS |
| MIL-A-8865 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY MISCELLANEOUS LOADS |
| SAE J 885 : 2011 | HUMAN TOLERANCE TO IMPACT CONDITIONS AS RELATED TO MOTOR VEHICLE DESIGN |
| MIL-STD-1530 Revision D:2016 | AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) |
| SAE AS 8043 : 2014 | RESTRAINT SYSTEMS FOR CIVIL AIRCRAFT |
| MIL-A-8863 Revision C:1993 | AIRPLANE STRENGTH AND RIGIDITY GROUND LOADS FOR NAVY ACQUIRED AIRPLANES |
| MIL-S-7877 Revision B:1956 | Seat, Passenger, Cabin Folding |
| MIL-S-7852 Revision B:1968 | SEAT, AIRCREW, ADJUSTABLE SWIVEL TYPE E-1 |
| MIL-STD-1333 Revision B:1987 | AIRCREW STATION GEOMETRY FOR MILITARY AIRCRAFT |
| MIL S 25073 : 0 | |
| MIL W 4088 : K | WEBBING, TEXTILE, WOVEN NYLON |
| MIL-S-27174 Revision B:1985 | |
| MIL-F-8905 Revision B:1967 | FITTINGS AND CARGO RINGS, TIEDOWN, AIRCRAFT FLOOR |
| MIL-S-58095 Revision A:1986 | SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR |
| MIL-B-83787 Base Document:1972 | BELT, AIRCRAFT SAFETY, LAP, TROOP, TYPES MD-1 AND MD-2 |
| MIL-B-8242 Revision C:1979 | BELT, SAFETY, LAP, TROOP, TYPE C-3A |
| MIL-STD-1290 Revision A:1988 | LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
| MIL STD 1800 : A NOTICE 1 | HUMAN ENGINEERING PERFORMANCE REQUIREMENTS FOR SYSTEMS |
| SAE AS 8049 : 2015 | PERFORMANCE STANDARD FOR SEATS IN CIVIL ROTORCRAFT, TRANSPORT AIRCRAFT, AND GENERAL AVIATION AIRCRAFT |
| MIL H 5364 : D | HARNESS, SHOULDER SAFETY, GENERAL SPECIFICATION FOR |
| MIL-W-25361 Revision E:1990 | WEBBING, TEXTILE, POLYESTER, LOW ELONGATION |
| MIL-R-8236 Revision F:1995 | REEL, SHOULDER HARNESS, INERTIA LOCK |
| MIL-B-8437 Revision B:1985 | BELT, AIRCRAFT SAFETY, LAP, TROOP TYPE MC AND 1A |
| MIL-A-8867 Revision C:1987 | AIRPLANE STRENGTH AND RIGIDITY GROUND TESTS |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL-A-83469 Base Document:1976 | ADJUSTER, LAP BELT, 1-3/4 INCH WEBBING |
| MIL-B-5428 Revision B:1982 | BELT, SAFETY, SHOULDER, HARNESS, TROOP, TYPE D - 2 |
| MIL-S-81771 Revision A:1975 | Seat System; Aircrew, Crash Resistant; General Specification for |
| MIL-S-26688 Base Document:1959 | SEAT, PASSENGER, AFT FACING, TRANSPORT AIRCRAFT |
| MIL-S-5804 Revision C:1967 | SEAT, AIRCRAFT, TROOP, WALL STYLE |
| MIL-HDBK-221 Base Document:1965 | FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES |
| MIL-STD-209 Revision K:2005 | LIFTING AND TIEDOWN PROVISIONS |
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