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NASA-LLIS-0857

Lessons Learned – SOFIA B747 Aircraft Towing Incident

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2000

Abstract: Description of Driving Event:
The SOFIA B747 aircraft was being towed into the large maintenance nosedock inside the 7500 hangar building at the Raytheon, Waco facility. As the aircraft approached the nose dock it made contact with the upper support structure of the nosedock. Labor and material costs were identified as less than $10,000. There were no personel injury associated with the incident. The damage is located at FS 480, stringer 2A, exterior top left side of fuselage. The exterior skin deformation is approximately 18" in lenght and 14" in width, with approximately .250 indentation of skin on either side of the frame. No fracturing of external skin is visible.
The cause of this incident was attributed to the following:
1. Insufficient clearance between top of the aircraft and nosedock support structure.
2. Lack of clear communication means between the aircraft/nosedock clearance observer and the tow task supervisor.
3. Supervisor failure to ensure tow team members were pre-briefed on specific duties and resposnsibilities prior to performance of the task.
4. Supervisor failure to properly plan aircraft tow operations prior to task performance.
5. Supervisor failure to ensure tow team personnel possessed required support equipment (Not all task assigned personnel possessed alert whistles/horns).
URI: https://yse.yabesh.ir/std/handle/yse/63066
Subject: Aircraft
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    NASA-LLIS-0857

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:59:55Z
date available2017-09-04T15:59:55Z
date copyright02/07/2000
date issued2000
identifier otherRGTEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/63066
description abstractDescription of Driving Event:
The SOFIA B747 aircraft was being towed into the large maintenance nosedock inside the 7500 hangar building at the Raytheon, Waco facility. As the aircraft approached the nose dock it made contact with the upper support structure of the nosedock. Labor and material costs were identified as less than $10,000. There were no personel injury associated with the incident. The damage is located at FS 480, stringer 2A, exterior top left side of fuselage. The exterior skin deformation is approximately 18" in lenght and 14" in width, with approximately .250 indentation of skin on either side of the frame. No fracturing of external skin is visible.
The cause of this incident was attributed to the following:
1. Insufficient clearance between top of the aircraft and nosedock support structure.
2. Lack of clear communication means between the aircraft/nosedock clearance observer and the tow task supervisor.
3. Supervisor failure to ensure tow team members were pre-briefed on specific duties and resposnsibilities prior to performance of the task.
4. Supervisor failure to properly plan aircraft tow operations prior to task performance.
5. Supervisor failure to ensure tow team personnel possessed required support equipment (Not all task assigned personnel possessed alert whistles/horns).
languageEnglish
titleNASA-LLIS-0857num
titleLessons Learned – SOFIA B747 Aircraft Towing Incidenten
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2000
contenttypefulltext
subject keywordsAircraft
subject keywordsGround Equipment
subject keywordsGround Operations
subject keywordsHardware
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DSpace software copyright © 2017-2020  DuraSpace
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