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FAA AC 25.981-1 : 2008

Current
Current

The latest, up-to-date edition.

FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2008

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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