Search Results

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Landing Gear Fatigue Spectrum Development For Part 25 Aircraft

2020-02-28

CURRENT

AIR5914

This SAE Aerospace Information Report (AIR) provides guidelines for the development of landing gear fatigue spectra for the purpose of designing and certification testing of Part 25 landing gear. Many of the recommendations herein are generalizations based on data obtained from a wide range of landing gears. The aircraft manufacturer or the landing gear supplier is encouraged to use data more specific to their particular undercarriage whenever possible.

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RECOMMENDED PRACTICES FOR LUBRICATING OIL FILTERS, GENERAL AVIATION RECIPROCATING ENGINE (PISTON TYPE) AIRCRAFT

1992-08-01

HISTORICAL

ARP1400A

The recommended practice establishes the requirements for lubricating oil filters for general aviation reciprocating engine applications with lubricating oil systems normally operating in a pressure range of 345 - 689 kPa (50 - 100 psig).

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Landing Gear Shock Absorption Testing of Civil Aircraft

2019-04-17

HISTORICAL

ARP5644

The intent of this document is to provide recommended practices for conducting shock absorption testing of civil aircraft landing gear equipped with oleo-pneumatic shock absorbers. The primary focus is for Part 25 aircraft, but differences for Part 23, 27, and 29 aircraft are provided where appropriate.

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Landing Gear Shock Absorption Testing of Civil Aircraft

2020-07-14

CURRENT

ARP5644A

The intent of this document is to provide recommended practices for conducting shock absorption testing of civil aircraft landing gear equipped with oleo-pneumatic shock absorbers. The primary focus is for Part 25 aircraft, but differences for Part 23, 27, and 29 aircraft are provided where appropriate.

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Tail Bumpers for Piloted Aircraft

2017-07-14

CURRENT

ARP1107C

This recommended practice covers the fixed structure, or independent energy absorbing system affixed to the airframe to afford protection to the control surfaces, engine and other portions during ground handling, take-off and landing.

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TAIL BUMPERS FOR PILOTED AIRCRAFT

1971-07-01

HISTORICAL

ARP1107

This recommended practice covers the fixed structure, or independent energy absorbing system affixed to the airframe to afford protection to the control surfaces, engine and other portions during ground handling, take-off and landing.

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TAIL BUMPERS FOR PILOTED AIRCRAFT

1991-06-11

HISTORICAL

ARP1107A

This recommended practice covers the fixed structure, or independent energy absorbing system affixed to the airframe to afford protection to the control surfaces, engine and other portions during ground handling, take-off and landing.

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Tail Bumpers for Piloted Aircraft

2012-05-03

HISTORICAL

ARP1107B

This recommended practice covers the fixed structure, or independent energy absorbing system affixed to the airframe to afford protection to the control surfaces, engine and other portions during ground handling, take-off and landing.

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Landing Gear Stability

2017-10-18

CURRENT

AIR4894

This SAE Aerospace Information Report (AIR) discusses the nature of landing gear stability, describes many common landing gear stability problems, and suggests approaches and methods for solving or avoiding them.

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Arresting Hook Installation, Land-Based Aircraft

2019-04-17

HISTORICAL

ARP1538B

This SAE Aerospace Recommended Practice (ARP) covers the recommended criteria and performance requirements for the design and installation of land-based aircraft emergency and operational arresting hooks for use on runway arresting systems. Design criteria for fully operational hooks and for carrier-based aircraft hook installations are contained in specification MIL-A-18717.

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Arresting Hook Installation, Land-Based Aircraft

2022-07-08

CURRENT

ARP1538C

This SAE Aerospace Recommended Practice (ARP) covers the recommended criteria and performance requirements for the design and installation of land-based aircraft emergency and operational arresting hooks for use on runway arresting systems. Design criteria for fully operational hooks and for carrier-based aircraft hook installations are contained in specification MIL-A-18717.

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Arresting Hook Installation, Land Based Aircraft, Emergency

2007-08-09

HISTORICAL

ARP1538A

This document covers the recommended criteria and performance requirements for the design and installation of an aircraft emergency arresting hook intended for use with emergency runway arresting systems. Design criteria for fully operational hooks and for carrier based aircraft hook installations are contained in specification MIL-A-18717.

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ARRESTING HOOK INSTALLATION, LAND BASED AIRCRAFT, EMERGENCY

1978-04-01

HISTORICAL

ARP1538

This document covers the recommended criteria and performance requirements for the design and installation of an aircraft emergency arresting hook intended for use with emergency runway arresting systems. Design criteria for fully operational hooks and for carrier based aircraft hook installations are contained in specification MIL-A-18717.

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Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications

2012-10-03

HISTORICAL

AS8860A

This specification contains landing gear strength and rigidity requirements, which, in combination with other applicable specifications, define the structural design, analysis, test, and data requirements for fixed wing piloted airplanes. These requirements include, but are not limited to the following: a General Specifications 1 The shock-absorption characteristics and strength of landing-gear units and the strength and rigidity of their control systems and of their carry-through structures.

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Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications

2012-05-03

HISTORICAL

AS8860

This specification contains landing gear strength and rigidity requirements, which, in combination with other applicable specifications, define the structural design, analysis, test, and data requirements for fixed wing piloted airplanes. These requirements include, but are not limited to the following: a General Specifications 1 The shock-absorption characteristics and strength of landing-gear units and the strength and rigidity of their control systems and of their carry-through structures.

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Gland Design: Nominal 3/8 in Cross Section for Custom Compression Type Seals

2012-06-29

HISTORICAL

AS4832

This SAE Aerospace Standard (AS) offers gland details for a 0.364 cross section gland (nominal 3/8 in) with proposed gland lengths for compression type seals with two backup rings over a range of 8 to 20 in in diameter. A dash number system is proposed similar to AS568A. A 600 series has been chosen as a logical extension of AS568A and the 625 number has been arbitrarily chosen for the initial number. (Both 300 and 400 series begin with 325 and 425 sizes.) Seal configurations and design are not a part of this document. This gland is for use with custom compression type seals including, but not limited to, O-rings, T-rings, D-rings, etc.

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DISPOSITION OF LANDING GEAR COMPONENTS INVOLVED IN ACCIDENTS/INCIDENTS

1997-11-01

HISTORICAL

ARP4915

This document establishes a procedure for disposition of landing gear components that have been involved in accidents/incidents. The recommendations in this document apply to high heat treat steel components (FTU = 180 ksi and above).

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Landing Gear Shock Strut Hydraulic Fluid

2015-04-27

HISTORICAL

AIR5358

This SAE Aerospace Information Report (AIR) was prepared by a panel of the SAE A-5 Committee. This document establishes the specifications for fluids used in landing gear shock struts with extreme pressure and antiwear additives that have been added for improved lubrication. This document requires qualified products.