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|
Attributes | |
ACN | 530724 |
Time | |
Date | 200110 |
Day | Tue |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | agl single value : 0 |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | B737-300 |
Flight Phase | ground : maintenance |
Person 1 | |
Affiliation | company : air carrier |
Function | maintenance : inspector |
ASRS Report | 530724 |
Person 2 | |
Affiliation | company : air carrier |
Function | maintenance : technician |
Events | |
Anomaly | aircraft equipment problem : critical maintenance problem : improper maintenance maintenance problem : improper documentation non adherence : far non adherence : published procedure |
Independent Detector | other other : person 1 |
Resolutory Action | none taken : detected after the fact |
Consequence | other other |
Factors | |
Maintenance | contributing factor : schedule pressure performance deficiency : non compliance with legal requirements performance deficiency : scheduled maintenance performance deficiency : inspection |
Supplementary | |
Problem Areas | Aircraft Chart Or Publication Maintenance Human Performance |
Primary Problem | Maintenance Human Performance |
Situations | |
Publication | mx manual |
Narrative:
Recently it has been brought to my attention a problem which arose with aircraft X on oct/tue/01/. On the above date the spoiler miter was due for a time change. At that time was discovered that r-hand wing cables WSA1-2 and WSA2-2 (spoiler control) were wrapped around each other. The problem was rectified on that date. On may/thu/01, I originated discrepancies for spoiler control cables WSB2-1 corroded nr (non-routine write-up) B235193, WSA1-4 corrode nr B235189, WSB1-4 corroded nr B235191, WSA2-4 corroded nr B235190, WSB2-4 corroded nr B235192. I inspected the fabrication and partial installation of all the cables. Due to shift change I referenced the system rig, safety wiring of the turn-barrels after connection on nr B235435 which was accomplished by a different inspector/mechanic that day. The cables found crossed on oct/tue/01 were not written-up by me for corrosion, but were connected downstream in the spoiler control system. When I turned over the job on may/thu/01, none of the cables tensioned up and the turn-barrels were loose and might have been disconnected again during the rigging process later in the day. No damage to the cables or aircraft structure was found on oct/tue/01.
Original NASA ASRS Text
Title: A B737-300 WAS DISPATCHED AND OPERATED IN NON COMPLIANCE FOR 6 MONTHS WITH THE R SPOILER CTL CABLES CROSSED.
Narrative: RECENTLY IT HAS BEEN BROUGHT TO MY ATTN A PROB WHICH AROSE WITH ACFT X ON OCT/TUE/01/. ON THE ABOVE DATE THE SPOILER MITER WAS DUE FOR A TIME CHANGE. AT THAT TIME WAS DISCOVERED THAT R-HAND WING CABLES WSA1-2 AND WSA2-2 (SPOILER CTL) WERE WRAPPED AROUND EACH OTHER. THE PROB WAS RECTIFIED ON THAT DATE. ON MAY/THU/01, I ORIGINATED DISCREPANCIES FOR SPOILER CTL CABLES WSB2-1 CORRODED NR (NON-ROUTINE WRITE-UP) B235193, WSA1-4 CORRODE NR B235189, WSB1-4 CORRODED NR B235191, WSA2-4 CORRODED NR B235190, WSB2-4 CORRODED NR B235192. I INSPECTED THE FABRICATION AND PARTIAL INSTALLATION OF ALL THE CABLES. DUE TO SHIFT CHANGE I REFED THE SYS RIG, SAFETY WIRING OF THE TURN-BARRELS AFTER CONNECTION ON NR B235435 WHICH WAS ACCOMPLISHED BY A DIFFERENT INSPECTOR/MECH THAT DAY. THE CABLES FOUND CROSSED ON OCT/TUE/01 WERE NOT WRITTEN-UP BY ME FOR CORROSION, BUT WERE CONNECTED DOWNSTREAM IN THE SPOILER CTL SYS. WHEN I TURNED OVER THE JOB ON MAY/THU/01, NONE OF THE CABLES TENSIONED UP AND THE TURN-BARRELS WERE LOOSE AND MIGHT HAVE BEEN DISCONNECTED AGAIN DURING THE RIGGING PROCESS LATER IN THE DAY. NO DAMAGE TO THE CABLES OR ACFT STRUCTURE WAS FOUND ON OCT/TUE/01.
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.