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ADS-39A-HDBK
SOURCE APPROVAL AND ENGINEERING TEST REQUIREMENTS FOR ALTERNATE SOURCES OF HELICOPTER DRIVE SYSTEM ASSEMBLIES AND COMPONENTS
Organization:
ARMY - AV - Aviation and Missile Command
Year: 1997
Abstract: This 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.
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| contributor author | ARMY - AV - Aviation and Missile Command | |
| date accessioned | 2017-09-04T18:32:22Z | |
| date available | 2017-09-04T18:32:22Z | |
| date copyright | 01/23/1997 | |
| date issued | 1997 | |
| identifier other | JBGOPAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho15137D83081DAC4261598F1EFDEC9FCD/handle/yse/214600 | |
| description abstract | This 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. | |
| language | English | |
| title | ADS-39A-HDBK | num |
| title | SOURCE APPROVAL AND ENGINEERING TEST REQUIREMENTS FOR ALTERNATE SOURCES OF HELICOPTER DRIVE SYSTEM ASSEMBLIES AND COMPONENTS | en |
| type | standard | |
| page | 39 | |
| status | Active | |
| tree | ARMY - AV - Aviation and Missile Command:;1997 | |
| contenttype | fulltext |