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|
Attributes | |
ACN | 861723 |
Time | |
Date | 200911 |
Local Time Of Day | 0001-0600 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Light | Night |
Aircraft 1 | |
Make Model Name | Regional Jet 900 (CRJ900) |
Operating Under FAR Part | Part 121 |
Flight Phase | Parked |
Component | |
Aircraft Component | Reverser Actuator |
Person 1 | |
Function | Technician |
Qualification | Maintenance Powerplant Maintenance Airframe |
Person 2 | |
Function | Technician |
Qualification | Maintenance Powerplant Maintenance Airframe |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural FAR Deviation - Procedural Published Material / Policy |
Narrative:
Maintenance planning issued a task card to replace the right-hand (rh) engine upper transcowl (translating sleeve cowl) locking actuator. Amt mr. X complied with installation per our task card engineering order (eo). After completion of thrust reverser (T/right) locking actuator; inspector verified installation. Everything looked installed correctly. While performing verification of rod end actuator; looked up at actuator pin and everything looked correctly installed. Performed operational check. Thrust reverser moved back and forth normally several times. Verified no leaks. This event occurred due to minimal clearance of thrust reverser; to verify actuator rod end installation. Another out-station verified the problem; rectified the situation; no damage occurred. Aircraft returned to service. Suggest better lighting environment to verify correct installation.
Original NASA ASRS Text
Title: Two Line Mechanics report on their involvement with replacing the right engine upper translating sleeve cowl locking actuator on a CRJ-900 aircraft. The right engine would not spool-up on landing on the next flight; when engine lever was moved to reverse thrust.
Narrative: Maintenance Planning issued a task card to replace the Right-hand (RH) engine upper Transcowl (Translating Sleeve Cowl) Locking actuator. AMT Mr. X complied with installation per our task card Engineering Order (EO). After completion of Thrust Reverser (T/R) Locking actuator; Inspector verified installation. Everything looked installed correctly. While performing verification of rod end actuator; looked up at actuator pin and everything looked correctly installed. Performed Operational Check. Thrust reverser moved back and forth normally several times. Verified no leaks. This event occurred due to minimal clearance of thrust reverser; to verify actuator rod end installation. Another out-station verified the problem; rectified the situation; no damage occurred. Aircraft returned to service. Suggest better lighting environment to verify correct installation.
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.