SAE AIR 5451 : 2017
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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A GUIDE TO LANDING GEAR SYSTEM INTEGRATION
Hardcopy , PDF
10-09-2022
English
12-07-2017
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. SCOPE
2. REFERENCES
3. LANDING GEAR SYSTEM CONFIGURATION REQUIREMENTS
4. LANDING GEAR SYSTEM FUNCTIONAL REQUIREMENTS
5. LANDING GEAR SYSTEM INTEGRITY REQUIREMENTS
6. LANDING GEAR SYSTEM PROGRAM REQUIREMENTS
7. NOTES
Gives guidelines and useful references for developing an integrated landing gear system for an aircraft.
| Committee |
A-5
|
| DocumentType |
Revision
|
| Pages |
42
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| SAE AIR1569A | Handling and Installation Practice for Aerospace Hose Assemblies |
| RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
| SAE ARP4752B | Aerospace - Design and Installation of Commercial Transport Aircraft Hydraulic Systems |
| RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
| SAE AS5440A | Hydraulic Systems, Military Aircraft, Design and Installation, Requirements For |
| SAE AS 8091 : 2014 | AIRCRAFT JACKING PADS ADAPTERS AND SOCKETS DESIGN AND INSTALLATION OF |
| MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
| SAE ARP 6137 : 2015 | TIRE PRESSURE MONITORING SYSTEMS (TPMS) FOR AIRCRAFT |
| SAE ARP 6152 : 2013(R2018) | AIRCRAFT TIRES SERVICE OVERLOAD CAPABILITY |
| SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
| SAE ARP994B | Design of Tubing Installations for Aerospace Hydraulic Systems |
| SAE AS1145C | Aircraft Brake Temperature Monitor Systems (BTMS) |
| SAE AIR 1800 : 1997 | AIRCRAFT TAIL BUMPERS |
| SAE ARP 5257 : 2015 | TIRE OVERSPEED LANDING TEST |
| MIL-A-8861 Revision B:1986 | AIRPLANE STRENGTH AND RIGIDITY FLIGHT LOADS |
| SAE AS50881F | Wiring Aerospace Vehicle |
| SAE ARP4925B | Aerospace Design and Installation of Commercial Transport Helicopter Hydraulic Systems |
| SAE AIR 4004 : 2015 | GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
| SAE ARP 4404 : 2013 | AIRCRAFT ELECTRICAL INSTALLATIONS |
| SAE AIR 1083 : 2012 | AIRBORNE HYDRAULIC AND CONTROL SYSTEM SURVIVABILITY FOR MILITARY AIRCRAFT |
| MIL-A-8860 Revision B:1987 | AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR |
| SAE ARP1107B | Tail Bumpers for Piloted Aircraft |
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