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SAE AIR 5451 : 2017

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

A GUIDE TO LANDING GEAR SYSTEM INTEGRATION
Available format(s)

Hardcopy , PDF

Superseded date

10-09-2022

Language(s)

English

Published date

12-07-2017

Publisher

SAE International

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Superseded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 AIR 1569 : 1993 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 ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
SAE ARP 4752 : 2013 AEROSPACE - DESIGN AND INSTALLATION OF COMMERCIAL TRANSPORT AIRCRAFT HYDRAULIC SYSTEMS
RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
SAE AS 5440 : 2011 HYDRAULIC SYSTEMS, 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 ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
SAE ARP 994 : 2016 DESIGN OF TUBING INSTALLATIONS FOR AEROSPACE HYDRAULIC SYSTEMS
SAE AS 1145 : 2016 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 AS 50881 : 2015 WIRING AEROSPACE VEHICLE
SAE ARP 4925 : 2014 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 ARP 1107 : 2012 TAIL BUMPERS FOR PILOTED AIRCRAFT

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Hardcopy - English
PDF - English
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