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SOURCE APPROVAL AND ENGINEERING TEST REQUIREMENTS FOR ALTERNATE SOURCES OF HELICOPTER DRIVE SYSTEM ASSEMBLIES AND COMPONENTS

contributor authorARMY - AV - Aviation and Missile Command
date accessioned2017-09-04T18:32:22Z
date available2017-09-04T18:32:22Z
date copyright01/23/1997
date issued1997
identifier otherJBGOPAAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho15137D83081DAC4261598F1EFDEC9FCD/handle/yse/214600
description abstractThis Aeronautical Design Standard (ADS) specifies Source Approval and Engineering Test requirements for alternate sources of helicopter drive system assemblies and components. These requirements are necessary to insure that an alternate source has the advanced manufacturing and assembly skills required to produce these complex parts. Completion of these requirements before contract award is necessary to reduce procurement risk associated with overcoming technical issues with first-time producers of these parts. Fielding of parts before the capabilities of the alternate source is substantiated could result in failures and/or early removals in the field, which may significantly impact the safety and reliability of the weapon systems they are used on. These requirements are based on the requirements used to qualify the original source of the part. The requirements specified in this ADS must be substantiated by a candidate alternate source before they will be approved to bid on a contract for that part.
languageEnglish
titleADS-39A-HDBKnum
titleSOURCE APPROVAL AND ENGINEERING TEST REQUIREMENTS FOR ALTERNATE SOURCES OF HELICOPTER DRIVE SYSTEM ASSEMBLIES AND COMPONENTSen
typestandard
page39
statusActive
treeARMY - AV - Aviation and Missile Command:;1997
contenttypefulltext


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