SAE AIR4094A
Current
The latest, up-to-date edition.
AIRCRAFT FLIGHT CONTROL SYSTEMS DESCRIPTIONS
Hardcopy , PDF
English
18-07-2016
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. APPLICABLE DOCUMENTS
3. FIXED WING MILITARY AIRCRAFT
4. FIXED WING COMMERCIAL AIRCRAFT
5. ROTARY WING MILITARY AIRCRAFT
6. ROTARY WING COMMERCIAL AIRCRAFT
7. NOTES
This SAE Aerospace Information Report (AIR) supplies information on the flight control systems incorporated on various current and historic fixed wing, rotary wing, and tilt rotor aircraft.
| Committee |
A-6A3
|
| DocumentType |
Revision
|
| Pages |
112
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
| SAE ARP 5007 : 2012 | DEVELOPMENT PROCESS - AEROSPACE FLY-BY-WIRE ACTUATION SYSTEM |
| SAE AIR 4922A : 2015 | PRIMARY FLIGHT CONTROL HYDRAULIC ACTUATION SYSTEM INTERFACE DEFINITION |
| MIL-F-8785 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-PRF-5606 Revision H:2002 | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT, MISSILE, AND ORDNANCE |
| SAE AS5440A | HYDRAULIC SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-PRF-87257 Revision C:2017 | HYDRAULIC FLUID, FIRE RESISTANT, LOW TEMPERATURE, SYNTHETIC HYDROCARBON BASE, AIRCRAFT AND MISSILE |
| SAE AIR4253B | DESCRIPTION OF ACTUATION SYSTEMS FOR AIRCRAFT WITH FLY-BY-WIRE FLIGHT CONTROL SYSTEMS |
| MIL-PRF-83282 Revision D:1997 | HYDRAULIC FLUID, FIRE RESISTANT, SYNTHETIC HYDROCARBON BASE, METRIC, NATO CODE NUMBER H-537 |
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