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|
Attributes | |
ACN | 852013 |
Time | |
Date | 200909 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Light | Daylight |
Aircraft 1 | |
Make Model Name | B767-300 and 300 ER |
Operating Under FAR Part | Part 121 |
Flight Phase | Parked |
Component | |
Aircraft Component | Main Gear Wheel |
Person 1 | |
Function | Technician |
Qualification | Maintenance Airframe Maintenance Powerplant |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy Deviation - Procedural Maintenance Deviation - Procedural FAR |
Narrative:
Our tire shop received a total of 22 reworked B767 main outboard (mob) wheel halves from a vendor. All received wheel halves had the proper FAA-8130 paperwork attached indicating the airworthiness of each wheel. Our shop procedure to return such wheels to service is to re-inspect according to our work documents and the component maintenance manual (cmm) 32-43-04. After completing the inspections on all 22 wheels; a total of three were found to be acceptable; for a failure rate of 86.4%. The majority of failures were related to improper blending procedures hidden under new paint and worn hub mating surfaces.
Original NASA ASRS Text
Title: A Tire Shop Mechanic reports they received 22 reworked B767-300 main outboard wheel halves from a vendor with FAA-8130 Airworthiness Tags attached. After performing re-inspection of the wheel halves per their Shop procedures and the Component Maintenance Manual (CMM); only three outboard wheel halves were found acceptable.
Narrative: Our tire shop received a total of 22 reworked B767 main outboard (MOB) wheel halves from a vendor. All received wheel halves had the proper FAA-8130 paperwork attached indicating the airworthiness of each wheel. Our Shop procedure to return such wheels to service is to re-inspect according to our work documents and the Component Maintenance Manual (CMM) 32-43-04. After completing the inspections on all 22 wheels; a total of three were found to be acceptable; for a failure rate of 86.4%. The majority of failures were related to improper blending procedures hidden under new paint and worn hub mating surfaces.
Data retrieved from NASA's ASRS site as of April 2012 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.