FAA AC 20-144 : 0
Current
The latest, up-to-date edition.
RECOMMENDED METHOD FOR FAA APPROVAL OF AIRCRAFT FIRE EXTINGUISHING SYSTEM COMPONENTS
Hardcopy , PDF
English
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 PURPOSE
2 RELATED FAR SECTIONS
3 RELATED READING MATERIAL
4 DEFINITIONS
5 SCOPE
6 BACKGROUND (FIREX SYSTEM FUNCTIONAL OVERVIEW)
7 FIREX CARTRIDGE
8 PRECISION BURST DISC.
9 FILL/CHANGE FITTING
10 PRESSURE INDICATOR
11 DISCHARGE HEAD ASSEMBLY
Gives guidance on the various aspects that should be considered in the FAA approval process of fire extinguishing system components manufactured under a Production Certificate (PC), components to be FAA approved under the Part Manufacturer Approval (PMA) process, or design changes to components originally approved by either method.
| DocumentType |
Standard
|
| Pages |
15
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| MIL I 23659 : C | INITIATOR, ELECTRIC, GENERAL DESIGN SPECIFICATION |
| MIL-STD-1576 Base Document:1984 | ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS |
| MIL-C-22284 Revision A:1965 | Container, Aircraft Fire Extinguishing System, Bromotrifluoromethane, CF3BR |
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