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Landing Gear System Development Plan

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • ARP1598B
  • Current
Published 2018-09-02 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) is intended to document the process of landing gear system development. This document includes landing gear system development plans for commercial, military, fixed wing and rotary wing air vehicles.
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Inflator Assembly and Gage Elements, Pneumatic Pressure, Remote Control, Direct Reading

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • AS85352A
  • Current
Published 2018-04-09 by SAE International in United States
This specification covers a direct reading, remote control, pneumatic pressure inflator assembly, for use on aircraft tires and struts having pneumatic pressure requirements up to 600 psi. It includes pressure relief provisions to provide for safe inflation. Also included are dual chuck stem gages for measuring tire pressure.
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Environmentally Compliant Processes for Landing Gear

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • AIR5479B
  • Current
Published 2017-07-14 by SAE International in United States
This SAE Aerospace Information Report (AIR) describes the performance of plating’s and coatings for landing gear that potentially provide environmental compliance benefits versus the current baseline processes. The hazardous systems addressed in this version of the document include cadmium plating, chromated primers, and high VOC (volatile organic compounds) topcoats. The AIR applies to landing gear structures and mechanisms for all types of civil and military aircraft. The potential replacements apply to both Original Equipment Manufacturer (OEM) hardware and overhaul of in-service landing gears.
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A Guide to Landing Gear System Integration

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • AIR5451A
  • Current
Published 2017-07-12 by SAE International in United States
The landing gear system is a major and safety critical airframe system that needs to be integrated efficiently to meet the overall aircraft program goals of minimizing the penalties of weight, cost, dispatch reliability and maintenance. As the landing gear system business develops and large-scale teaming arrangements and acquisitions become increasingly common, it may be desirable in some instances to procure an Integrated Landing Gear System. This document provides guidelines and useful references for developing an integrated landing gear system for an aircraft. The document structure is divided into four sections: Landing Gear System Configuration Requirements (Section 3) Landing Gear System Functional Requirements (Section 4) Landing Gear System Integrity Requirements (Section 5) Landing Gear System Program Requirements (Section 6) The landing gear system encompasses all landing gear structural and subsystem elements. Structural elements include shock struts, truck beams, torsion links, braces, fittings, pins, wheels, tires, and brakes. The subsystem elements include the retraction/extension system (both normal and alternate), the steering system, the braking system (both normal and alternate, manual and automatic), the indication and monitoring…
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Tire Spray Suppression - Airplane Design and Consideration for

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • AIR1904B
  • Current
Published 2017-05-09 by SAE International in United States
This SAE Aerospace Information Report (AIR) relates considerations for design test procedures and test data evaluation for qualification of tire spray deflection devices.
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Aerospace Landing Gear Systems Terminology

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • AIR1489C
  • Current
Published 2017-05-09 by SAE International in United States
This report has been compiled by the Landing Gear Systems Terminology Panel of SAE Committee A-5 (Aerospace Landing Gear Systems). It represents an effort to gather together those terms commonly used within the discipline. Some terms are of course common to other disciplines as well. Others, however, are unique in form and/or meaning to the landing gear discipline. The need has been noted to set these terms down and provide a standard definition in order that communication within the discipline may be conducted with a common understanding. Full use has been made of available published information, and a list of references is provided. See also References (a) to (e). Terms listed are usually applicable to a general functional area of landing gear disciplines. These general functional areas include; landing impact, directional ground control, velocity control (acceleration, retardation, and arrestment), structural support, ground flotation, and ground maintenance. In the listing of terms and definitions, each term is followed by a code in parenthesis which indicates which basic functional area or major component to which the term…
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Steering Effect of Tilted, Free-Swiveling Nose Gears

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • AIR4358
  • Current
Published 2017-05-04 by SAE International in United States
This Aerospace Information Report (AIR) considers the origin of cornering forces generated by tilted, free-swiveling nose gears; the effect of various landing gear parameters on the measured cornering forces; and a method of towing aircraft to measure the resulting steering forces.
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Aircraft Ground Flotation Analysis Methods

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • ARP1821B
  • Current
Published 2016-12-01 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) includes recommended ground flotation analysis methods for both paved and unpaved airfields with application to both commercial and military aircraft.
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Aircraft Ground Flotation Analysis Methods

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • ARP1821A
  • Historical
Published 2016-04-10 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) includes recommended ground flotation analysis methods for both paved and unpaved airfields.
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A Guide to Landing Gear System Integration

A-5 Aerospace Landing Gear Systems Committee
  • Aerospace Standard
  • AIR5451
  • Historical
Published 2016-04-10 by SAE International in United States
The landing gear system is a major airframe system that needs to be integrated very efficiently to minimize the penalties of weight, cost, dispatch reliability and maintenance. As the landing gear system business develops and large scale teaming arrangements and acquisitions become increasingly common, it may be desirable in some instances to procure an Integrated Landing Gear System. This document provides guidelines and useful references for developing an integrated landing gear system for an aircraft and is divided into four sections: Landing Gear Configuration Requirements (Section 3) Landing Gear Functional Requirements (Section 4) Landing Gear System Integrity Requirements (Section 5) Landing Gear Program Requirements (Section 6) The landing gear system encompasses all landing gear structural and subsystem elements. Structural elements include shock struts, braces, fittings, pins, wheels, tires and brakes. The subsystem elements include the retraction/extension system (both normal and alternate), the steering system, the braking system (both normal and alternate, manual and automatic), the indication systems and control systems (mechanical, hydraulic, electrical and electronic).
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