JSSG-2010-5 Base Document:1998
Current
The latest, up-to-date edition.
Crew Systems Aircraft Lighting Handbook
English
30-10-1998
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
3.7 Crash Survivability
3.8 Energetic
3.9 Life Support/Personal Protection
3.10 Oxygen System
3.11 Emergency Egress
3.12 Deployable Aerodynamic Decelerator (DAD) Systems
3.13 Survival, Search, and Rescue (SSAR)
3.14 Aircraft Windshield/Canopy Systems and Transparent Enclosures
4 VERIFICATION (WITH REQUIREMENTS)
5 DEFINITIONS AND ABBREVIATIONS
5.1 Definitions
5.2 Acronyms, abbreviations, and symbols
6 NOTES
6.1 Intended use
6.2 Subject term (key word) listing
Describes guidance for the development requirements and verifications for interior and exterior airborne lighting equipment, including specific requirements for interior lighting compatible with type I or II and class A or B night vision imaging systems (NVIS).
DevelopmentNote |
Supersedes AFGS 87240 (A) and MIL STD 1776 (A). (04/2004)
|
DocumentType |
Standard
|
Pages |
114
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Current
|
Supersedes |
JSSG-2001 Revision B:2004 | Air Vehicle |
SAE ARP1088B | Aircraft Indicating Systems |
MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
ADS-63-SP : 2001 | AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS |
MIL-HDBK-87213 Revision A:2005 | Electronically / Optically Generated Airborne Displays |
SAE AS5498A | Minimum Operational Performance Specification for Inflight Icing Detection Systems |
ADS-65-HDBK : 2004 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS |
MIL-L-6503 Revision H:1975 | LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
MIL-PRF-22885-101 Revision E:2010 | SWITCH, PUSHBUTTON, ILLUMINATED, 4-LAMP, SPDT AND DPDT, 5.0 AMPERES SILVER CONTACTS, 1 AMPERE MAX. GOLD CONTACTS, DRIPPROOF, SUNLIGHT READABLE, EMI/RFI SHIELDED, NVIS COMPATIBLE |
MIL P 7788 : F | PANEL, INFORMATION INTEGRALLY ILLUMINATED |
MIL-L-85314 Revision A:1983 | LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
MIL-STD-411 Revision F:1997 | AIRCREW STATION ALERTING SYSTEMS |
MIL-L-18276 Revision C:1964 | LIGHTING, AIRCRAFT INTERIOR, INSTALLATION OF |
MIL-STD-1757 Revision A:1983 | LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE |
MIL-L-27160 Revision C:1972 | LIGHTING, INSTRUMENT, INTEGRAL, WHITE GENERAL SPECIFICATION FOR |
MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
MIL-L-5667 Revision B:1964 | LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG] |
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