SAE AIR 1664 : 2013
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
AIRCRAFT FLEXIBLE TANKS GENERAL DESIGN AND INSTALLATION RECOMMENDATIONS
Hardcopy , PDF
07-05-2019
English
01-01-2013
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. REFERENCES
3. BACKGROUND
4. DESIGN RECOMMENDATIONS
5. TANK WEIGHT - ESTIMATING FOR DESIGN
6. TANK MARKING
7. TANK REPAIR
Describes general information about the various types and styles of flexible tanks and the tank-mounted fittings that adapt the tank to the surrounding structure and fluid-system plumbing.
| Committee |
AE-5A
|
| DevelopmentNote |
Supersedes SAE ARP 1664 (02/2006)
|
| DocumentType |
Standard
|
| Pages |
34
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AIR4170B | Reticulated Polyurethane Foam Explosion Suppression Material for Fuel Systems and Dry Bays |
| MS29559 Revision C:1974 | Fitting, (O) Ring, Circular, Thru Bolt Type, Single Groove, Tank |
| MS29560 Revision C:1974 | Fitting, (O) Ring, Circular, Threaded Insert Type, Single Groove, Tank |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| MIL B 83054 : B | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
| MIL-C-5040 Revision H:1994 | Cord, Fibrous, Nylon |
| MIL-P-8045 Revision B:1964 | PLASTIC SELF-SEALING AND NON SELF-SEALING TANK BACKING MATERIAL |
| SAE AIR4170B | Reticulated Polyurethane Foam Explosion Suppression Material for Fuel Systems and Dry Bays |
| SAE AIR1662A | Minimization of Electrostatic Hazards in Aircraft Fuel Systems |
| MIL F 87260 : 0 | FOAM MATERIAL, EXPLOSION SUPPRESSION, INHERENTLY ELECTRICALLY CONDUCTIVE, FOR AIRCRAFT FUEL TANK & DRY BAY AREAS |
| MS29558 Revision C:1974 | FITTING, "O" RING, CIRCULAR, COMPRESSION TYPE, SINGLE GROOVE, TANK |
| MIL T 6396 : E | TANKS, AIRCRAFT PROPULSION FLUID SYSTEM, INTERNAL REMOVABLE, NON-SELF-SEALING |
| MIL-STD-1290 Revision A:1988 | LIGHT FIXED & ROTARY-WING AIRCRAFT CRASH RESISTANCE |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL-STD-1472 Revision G:2012 | HUMAN ENGINEERING |
| MIL-STD-801 Revision E:2017 | INSPECTION AND ACCEPTANCE STANDARDS FOR FLEXIBLE FUEL CELLS AND FITTINGS |
| SAE AS4873A | Gland Design, Elastomeric O-Ring Seals, Static Radial and Face 800 psi Maximum Service |
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