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NPFC - MIL-DTL-6839 - INDICATOR, POSITION, LANDING GEAR Organization: NPFC
Date: 2011-07-22
Description: This specification covers requirements for individual 28-volt direct current (VDC) electrical landing gear position indicators. The individual landing gear position indicator covered by this specification is intended for use on all aircraft with retractable landing gear where indication of the position of the landing gear is desired.
SAE ARP5936 - LANDING GEAR STORAGE Organization: SAE
Date: 2005-04-01
Description: This document categorizes the different types of storage requirements, either on the aircraft or new unused or overhauled on the shelf, for aircraft landing gears/components. Recommendations and examples of proper landing gear storage are outlined.
AIR FORCE - AFGS-87139B CONT. DIST. - LANDING GEAR SYSTEMS - *** NOT AVAILABLE AT IHS * CONTROLLED DISTRIBUTION *** Organization: AIR FORCE
Date: 2013-09-04
Description: This specification establishes the performance, development, compatibility, and verification requirements for a conventional Landing Gear system and its components.
SAE ARP5908 - LANDING GEAR SERVICING Organization: SAE
Date: 2008-03-01
Description: The Present document addresses gas and hydraulic fluid servicing required on commercial and military aircraft landing gears, for both single and dual chamber shock struts.
SAE AIR5556 - LANDING GEAR ALIGNMENT Organization: SAE
Date: 2009-05-01
Description: The purpose of this Aerospace Information Report is to provide the industry with methodologies for measuring tire/wheel gear alignment and the range of acceptable alignment settings for various types of non-military landing gear. This AIR will focus on the general aviation, corporate, and regional aircraft landing gear but could have applicability to commercial aircraft.
SAE AIR4566 - CRASHWORTHY LANDING GEAR DESIGN Organization: SAE
Date: 2010-05-01
Description: The intent of this SAE Aerospace Information Report (AIR) is to document the design requirements and approaches for the crashworthy design of aircraft landing gear. This document covers the field of commercial and military airplanes and helicopters.
SAE AIR5885 - LANDING GEAR COMMON REPAIR Organization: SAE
Date: 2004-12-01
Description: This document outlines the most common repairs used on landing gear components. It is not the intention of this AIR to replace Overhaul/Component Maintenance or Technical Order Manuals, but it can serve as a guide into their preparation.
SAE AIR6168 - LANDING GEAR STRUCTURAL HEALTH MONITORING Organization: SAE
Date: 2012-04-01
Description: This SAE Aerospace Information Report (AIR) discusses past and present approaches for monitoring the landing gear structure and shock absorber, methods for transient overload detection, techniques for measuring the forces seen by the landing gear structure, and methods for determining the fatigue state of the landing gear structure.
SAE PT-169 - ADVANCES IN AIRCRAFT LANDING GEAR - TO PURCHASE CALL 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE Organization: SAE
Date: 2015-08-24
Description: The paper reflects the importance of proper interaction between landing gear design and other disciplines and above all underlines the fact that landing gear design should be treated as an equally important design parameter, just as any other, in the final choice of aircraft configuration.
SAE AIR5024 - LANDING GEAR SWITCH SELECTION CRITERIA Organization: SAE
Date: 1999-04-01
Description: The scope of this document is to discuss the differences between electromechanical and proximity position sensing devices when used on landing gears. It also contains information, which may be helpful, when applying either type of technology after the selection has been made.
SAE ARP1598 - (R) LANDING GEAR SYSTEM DEVELOPMENT PLAN Organization: SAE
Date: 2013-04-01
Description: 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.
SAE AIR5883 - LANDING GEAR SHOCK STRUTS BEARING SELECTION Organization: SAE
Date: 2006-05-01
Description: This document defines the criteria used for the selection of landing gear shock strut upper and lower bearings. Common problems associated with shock strut bearings are presented
NASA-CR-2714 - LANDING GEAR AND CAVITY NOISE PREDICTION Organization: NASA
Date: 1976-01-01
Description: Prediction of airframe noise radiation from the landing gear and wheel wells of commercial aircraft is examined.
SAE AIR1594 - PLAIN BEARING SELECTION FOR LANDING GEAR APPLICATIONS Organization: SAE
Date: 2010-07-01
Description: This document is intended to give advisory information for the selection of plain bearings and bearing materials most suitable for aircraft landing gear applications. Information included herein was derived from bearing tests and service experience/reports.
SAE AIR4846 - EXTRAORDINARY AND SPECIAL PURPOSE LANDING GEAR SYSTEMS Organization: SAE
Date: 2012-10-01
Description: Section 2 of this document describes the features of landing gear which are addressed in the specific descriptions of various landing gears (Category A).
SAE AS6053 - TESTS, IMPACT, SHOCK ABSORBER LANDING GEAR, AIRCRAFT Organization: SAE
Date: 2012-10-01
Description: This specification covers definition of landing impact tests which are to be conducted on landing gear assemblies including shock absorbers, suggested instrumentation for the tests and required data of the resulting test report.
SAE ARP1311 - (R) LANDING GEAR STRUCTURES AND MECHANISMS Organization: SAE
Date: 2009-02-01
Description: This SAE Aerospace Recommended Practice (ARP) applies to landing gear structures and mechanisms (excluding wheels, tires, and brakes and other landing gear systems) for all types and models of civil and military aircraft.
SAE AIR5552 - DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS Organization: SAE
Date: 2010-10-01
Description: This information report provides general guidance for the design considerations, qualification in endurance, strength and fatigue of landing gear using composite components as principle structural elements.
SAE AIR1494 - VERIFICATION OF LANDING GEAR DESIGN STRENGTH Organization: SAE
Date: 2010-04-01
Description: Verification of landing gear design strength is accomplished by dynamic and static test programs. This is essentially a verification of the analytical procedures used to design the gear.
SAE AIR5358 - (R) LANDING GEAR SHOCK STRUT HYDRAULIC FLUID Organization: SAE
Date: 2016-05-01
Description: This document describes fluids used in landing gear shock struts with extreme pressure and antiwear additives that have been added for improved lubrication.

1 - 20 of 886 results