NASA-LLIS-0500
Lessons Learned - Fasteners
| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T15:27:22Z | |
| date available | 2017-09-04T15:27:22Z | |
| date copyright | 33896 | |
| date issued | 1992 | |
| identifier other | NRBEQCAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/28256 | |
| description abstract | Description of Driving Event: For critical applications either run tests to develop actual torque-preload relationship, or use tables which were developed using the actual fastener material, joint material, and lubrication and/or locking system. On January 15, 1991 a failure occurred in the 8 foot transonic pressure tunnel during testing of a model wing with attached flap. During the test run, the flap peeled away from the wing, broke free, and proceeded down the tunnel. Extensive damage resulted. | |
| language | English | |
| title | NASA-LLIS-0500 | num |
| title | Lessons Learned - Fasteners | en |
| type | standard | |
| page | 2 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1992 | |
| contenttype | fulltext | |
| subject keywords | Parts Materials & Processes | |
| subject keywords | Test Facility |

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