FAA AC 25.981-1 : 2008
Current
The latest, up-to-date edition.
FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES
Hardcopy , PDF
English
01-01-2008
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1. Purpose
2. Applicability
3. Cancellation
4. Related Documents
5. Definitions
6. Background
7. Objective
8. Fuel Vapor Ignition Sources
9. Design Considerations
10. Safety Analysis
11. Component Qualification Considerations
12. Instructions for Continued Airworthiness of the Fuel
Tank System - section 25.1529
Specifies guidance for demonstrating compliance with the certification requirements for prevention of ignition sources within the fuel tanks of transport category airplanes.
| DocumentType |
Standard
|
| Pages |
39
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| SupersededBy |
| FAA AC 120-97 : 2012 | INCORPORATION OF FUEL TANK SYSTEM INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INTO OPERATOR MAINTENANCE OR INSPECTION PROGRAMS |
| FAA AC 25.1701-1 : 2007 | CERTIFICATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS ON TRANSPORT CATEGORY AIRPLANES |
| FAA AC 20-53 : 2006 | PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
| SAE ARP 6385 : 2017 | AIRCRAFT FUEL PUMP MECHANICAL AND ELECTRICAL SAFETY DESIGN |
| FAA AC 120-102 : 2012 | INCORPORATION OF ELECTRICAL WIRING INTERCONNECTION SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS INTO AN OPERATOR'S MAINTENANCE PROGRAM |
| SAE ARP 5794 : 2014 | CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD |
| SAE AIR5691A : 2017 | GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS |
| SAE ARP594 : 2017 | FUEL PUMP THERMAL SAFETY DESIGN |
| SAE AIR 6464 : 2013 | EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES |
| FAA AC 25-27 : 2010 | DEVELOPMENT OF TRANSPORT CATEGORY AIRPLANE ELECTRICAL WIRING INTERCONNECTION SYSTEMS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS USING AN ENHANCED ZONAL ANALYSIS PROCEDURE |
| SAE AS 7510 : 2017 | COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, SELF-LOCKING, FIXED CAVITY, HIGH CONDUCTIVITY, SELF-BONDING, PART SPECIFICATION |
| SAE AS 5830 : 2017 | COUPLING ASSEMBLY, THREADLESS, FLEXIBLE, FIXED CAVITY, CURRENT CARRYING, SELF-BONDING, PROCUREMENT SPECIFICATION |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| SAE AIR 4170 : 2016 | RETICULATED POLYURETHANE FOAM EXPLOSION SUPPRESSION MATERIAL FOR FUEL SYSTEMS AND DRY BAYS |
| FAA AC 25-26 : 2007 | DEVELOPMENT OF STANDARD WIRING PRACTICES DOCUMENTATION |
| SAE ARP 6461 : 2013 | GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT |
| SAE ARP 6078 : 2012 | AIRCRAFT FUEL TANK INERTING SYSTEMS |
| SAE AIR 5774 : 2012 | COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
| FAA AC 120-98 : 2012 | OPERATOR INFORMATION FOR INCORPORATING FUEL TANK FLAMMABILITY REDUCTION REQUIREMENTS INTO A MAINTENANCE OR INSPECTION PROGRAM |
| SAE AIR 7484 : 2018 | GUIDANCE ON THE IMPACT OF FUEL PROPERTIES ON FUEL SYSTEM DESIGN AND OPERATION |
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