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NASA-LLIS-0006

Lessons Learned - Orbiter Exterior Panel Separation During Flight due to Incorrect Installation (Washers not Provided Under Fasteners)

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1991

Abstract: Description of Driving Event:
Following the shuttle mission STS-27, the right side orbital maneuvering system (OMS) pod carrier panel on the orbiter OV-104 was missing. It was concluded that the panel was installed incorrectly. Six flat washers were not installed under the mounting fasteners. This caused damage to the base panel material upon installation. The panel became loose during flight, produced a gap, and was pulled off by the air flow. No additional damage was sustained by the orbiter thermal protection system or other orbiter components. The panel installation procedures did not clearly identify the requirement for the washers. The procedures were revised to include the steps for installing the washers. Approximately 100 orbiter panels of similar configuration were recommended for inspection to assure this anomaly was not present elsewhere within the orbiter fleet.
URI: https://yse.yabesh.ir/std/handle/yse/51305
Subject: Configuration Management
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    NASA-LLIS-0006

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:48:24Z
date available2017-09-04T15:48:24Z
date copyright04/29/1991
date issued1991
identifier otherQAYCQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/51305
description abstractDescription of Driving Event:
Following the shuttle mission STS-27, the right side orbital maneuvering system (OMS) pod carrier panel on the orbiter OV-104 was missing. It was concluded that the panel was installed incorrectly. Six flat washers were not installed under the mounting fasteners. This caused damage to the base panel material upon installation. The panel became loose during flight, produced a gap, and was pulled off by the air flow. No additional damage was sustained by the orbiter thermal protection system or other orbiter components. The panel installation procedures did not clearly identify the requirement for the washers. The procedures were revised to include the steps for installing the washers. Approximately 100 orbiter panels of similar configuration were recommended for inspection to assure this anomaly was not present elsewhere within the orbiter fleet.
languageEnglish
titleNASA-LLIS-0006num
titleLessons Learned - Orbiter Exterior Panel Separation During Flight due to Incorrect Installation (Washers not Provided Under Fasteners)en
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1991
contenttypefulltext
subject keywordsConfiguration Management
subject keywordsFlight Equipment
subject keywordsFlight Operations
subject keywordsHardware
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