Skip to content
Please enter a keyword to search

  • SAE AIR 5451 : 2017

    View superseded by
    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
    View superseded by

    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    Superseded date:  10-09-2022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

    Add To Cart

    Table of Contents - (Show below) - (Hide below)

    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

    Abstract - (Show below) - (Hide below)

    Gives guidelines and useful references for developing an integrated landing gear system for an aircraft.

    General Product Information - (Show below) - (Hide below)

    Committee A-5
    Document Type Revision
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    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
    View more information

    • Access your standards online with a subscription

      Features

      • Simple online access to standards, technical information and regulations
      • Critical updates of standards and customisable alerts and notifications
      • Multi - user online standards collection: secure, flexibile and cost effective