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|
Attributes | |
ACN | 974682 |
Time | |
Date | 201109 |
Local Time Of Day | 1801-2400 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Light | Night |
Aircraft 1 | |
Make Model Name | B737-300 |
Operating Under FAR Part | Part 121 |
Flight Plan | IFR |
Component | |
Aircraft Component | Pressurization Control System |
Person 1 | |
Function | Technician |
Qualification | Maintenance Airframe Maintenance Powerplant |
Events | |
Anomaly | Aircraft Equipment Problem Critical Inflight Event / Encounter Other / Unknown |
Narrative:
Removed and replaced (right/right) overhead pressurization control module on aircraft X. Aircraft was terminated over the night. I did everything by the maintenance manual (M/M). In the morning; next day when the aircraft left the gate; [flight crew] had to perform air return back due to uncontrollable cabin pressure. When fellow technician troubleshot the system he found two wires behind the pressure indication (psi) control panel [that] were chafing; which could have been chafing for long time. The right/right [of the control panel] caused the problem for wiring to pop up. That could have happened when the airframe vibration was induced by aircraft movement; either on the ground or during flight.
Original NASA ASRS Text
Title: A Line Mechanic reports about a B737-300 aircraft that returned to field due to uncontrollable cabin pressurization after he had changed the pressure control panel on the P-5 overhead panel. Troubleshooting later discovered two chafed wires behind the pressure indication panel.
Narrative: Removed and Replaced (R/R) overhead pressurization control module on aircraft X. Aircraft was terminated over the night. I did everything by the Maintenance Manual (M/M). In the morning; next day when the Aircraft left the gate; [flight crew] had to perform air return back due to uncontrollable cabin pressure. When fellow Technician troubleshot the system he found two wires behind the pressure indication (PSI) control panel [that] were chafing; which could have been chafing for long time. The R/R [of the control panel] caused the problem for wiring to pop up. That could have happened when the airframe vibration was induced by aircraft movement; either on the ground or during flight.
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.