37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
|
Attributes | |
ACN | 485875 |
Time | |
Date | 200009 |
Day | Wed |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | agl single value : 0 |
Environment | |
Light | Night |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | B727-200 |
Operating Under FAR Part | Part 121 |
Flight Phase | ground : maintenance ground : parked |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | maintenance : technician |
Qualification | technician : airframe technician : powerplant |
ASRS Report | 485875 |
Person 2 | |
Affiliation | company : air carrier |
Function | maintenance : technician |
Qualification | technician : powerplant technician : airframe |
Events | |
Anomaly | aircraft equipment problem : critical maintenance problem : improper maintenance non adherence : published procedure |
Resolutory Action | none taken : detected after the fact |
Consequence | other other |
Factors | |
Maintenance | contributing factor : schedule pressure performance deficiency : repair performance deficiency : installation performance deficiency : inspection |
Supplementary | |
Problem Areas | Maintenance Human Performance Aircraft |
Primary Problem | Maintenance Human Performance |
Narrative:
Aircraft xyz had a #1 main tire assembly worn to limits. Procedure calls for removing 2 each bolts from the main gear door, attach rod and extending the rod, to facilitate removing the tire. When the #1 main with tire assembly was changed, the main gear door rod is supposed to be returned to the original position, and the 2 bolts with nuts reinstalled. Due to thinking of GPS troubleshooting (both on dmi 'deferred maintenance item'), I neglected to reposition and reinstall the 2 bolts.
Original NASA ASRS Text
Title: A B727-200 WAS DISPATCHED IN NON COMPLIANCE WITH THE L MAIN GEAR DOOR SUPPORT ROD BOLTS MISSING.
Narrative: ACFT XYZ HAD A #1 MAIN TIRE ASSEMBLY WORN TO LIMITS. PROC CALLS FOR REMOVING 2 EACH BOLTS FROM THE MAIN GEAR DOOR, ATTACH ROD AND EXTENDING THE ROD, TO FACILITATE REMOVING THE TIRE. WHEN THE #1 MAIN WITH TIRE ASSEMBLY WAS CHANGED, THE MAIN GEAR DOOR ROD IS SUPPOSED TO BE RETURNED TO THE ORIGINAL POS, AND THE 2 BOLTS WITH NUTS REINSTALLED. DUE TO THINKING OF GPS TROUBLESHOOTING (BOTH ON DMI 'DEFERRED MAINT ITEM'), I NEGLECTED TO REPOSITION AND REINSTALL THE 2 BOLTS.
Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.