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NASA-LLIS-0914
Lessons Learned – Genesis Canister Lift Incident (2000)
Year: 2000
Abstract: Abstract:
Genesis: In 2000 the Genesis canister detached from a lift fixture fitting just prior to system-level thermal vacuum testing. Fabrication or test organizations should inspect all MGSE for fastener engagement and specified torque prior to delivery for use by a project. Where feasible, threaded components that are to be placed under tension should be designed with a positive locking device. Flight projects should conduct and document visual and physical inspections of MGSE prior to use. Personnel safety should be addressed, as appropriate, by all procedures. In addition, all test personnel should constantly remain at a safe distance during operations involving suspended loads.
Genesis: In 2000 the Genesis canister detached from a lift fixture fitting just prior to system-level thermal vacuum testing. Fabrication or test organizations should inspect all MGSE for fastener engagement and specified torque prior to delivery for use by a project. Where feasible, threaded components that are to be placed under tension should be designed with a positive locking device. Flight projects should conduct and document visual and physical inspections of MGSE prior to use. Personnel safety should be addressed, as appropriate, by all procedures. In addition, all test personnel should constantly remain at a safe distance during operations involving suspended loads.
Subject: Crane
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:25:27Z | |
| date available | 2017-09-04T16:25:27Z | |
| date copyright | 07/20/2000 | |
| date issued | 2000 | |
| identifier other | TXTEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/88696 | |
| description abstract | Abstract: Genesis: In 2000 the Genesis canister detached from a lift fixture fitting just prior to system-level thermal vacuum testing. Fabrication or test organizations should inspect all MGSE for fastener engagement and specified torque prior to delivery for use by a project. Where feasible, threaded components that are to be placed under tension should be designed with a positive locking device. Flight projects should conduct and document visual and physical inspections of MGSE prior to use. Personnel safety should be addressed, as appropriate, by all procedures. In addition, all test personnel should constantly remain at a safe distance during operations involving suspended loads. | |
| language | English | |
| title | NASA-LLIS-0914 | num |
| title | Lessons Learned – Genesis Canister Lift Incident (2000) | en |
| type | standard | |
| page | 4 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;2000 | |
| contenttype | fulltext | |
| subject keywords | Crane | |
| subject keywords | Ground Equipment | |
| subject keywords | Hardware | |
| subject keywords | Industrial Safety | |
| subject keywords | Lift Procedure | |
| subject keywords | Lifting Devices | |
| subject keywords | Mechanical Integration | |
| subject keywords | NDI | |
| subject keywords | Nondestructive Inspection | |
| subject keywords | Packaging Handling Storage | |
| subject keywords | Quality Assurance | |
| subject keywords | Safety & Mission Assurance | |
| subject keywords | System Integration and Test | |
| subject keywords | System Safety | |
| subject keywords | Test Facility | |
| subject keywords | Test Procedures |