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|
Attributes | |
ACN | 595339 |
Time | |
Date | 200309 |
Day | Fri |
Local Time Of Day | 0001 To 0600 |
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 | B737-700 |
Flight Plan | None |
Person 1 | |
Affiliation | company : air carrier |
Qualification | technician : powerplant technician : airframe |
ASRS Report | 595339 |
Events | |
Anomaly | aircraft equipment problem : critical maintenance problem : improper documentation maintenance problem : improper maintenance non adherence : published procedure non adherence : far |
Independent Detector | other other : person 1 |
Resolutory Action | none taken : detected after the fact |
Consequence | other other |
Factors | |
Maintenance | contributing factor : briefing performance deficiency : logbook entry performance deficiency : inspection performance deficiency : non compliance with legal requirements |
Supplementary | |
Problem Areas | Aircraft Maintenance Human Performance |
Primary Problem | Maintenance Human Performance |
Narrative:
Upper ('B' system) elevator autoplt actuator input rod attach bolt/nut may not have been fully tight/secure during right&right of 'B' system elevator autoplt actuator on aircraft. This attach bolt is sometimes removed to aid removal of the input crank arm from the actuator shaft. I started to remove this bolt, but decided to try the crank removal first. (The nut on input rod was loosened approximately 3-4 turns.) the crank arm, however, came off without a problem so the input rod bolt did not have to be removed. After finishing the job (including inspection) and on my drive home, I did not specifically remember rechking this bolt/nut. So as precaution, notified my supervisor and maintenance control to have this checked at first station stop.
Original NASA ASRS Text
Title: A B737-700 WAS DISPATCHED IN NON COMPLIANCE WITH THE 'B' SYS ELEVATOR AUTOPLT ACTUATOR INPUT ROD ATTACH BOLT NOT TORQUED TO SPECS.
Narrative: UPPER ('B' SYS) ELEVATOR AUTOPLT ACTUATOR INPUT ROD ATTACH BOLT/NUT MAY NOT HAVE BEEN FULLY TIGHT/SECURE DURING R&R OF 'B' SYS ELEVATOR AUTOPLT ACTUATOR ON ACFT. THIS ATTACH BOLT IS SOMETIMES REMOVED TO AID REMOVAL OF THE INPUT CRANK ARM FROM THE ACTUATOR SHAFT. I STARTED TO REMOVE THIS BOLT, BUT DECIDED TO TRY THE CRANK REMOVAL FIRST. (THE NUT ON INPUT ROD WAS LOOSENED APPROX 3-4 TURNS.) THE CRANK ARM, HOWEVER, CAME OFF WITHOUT A PROB SO THE INPUT ROD BOLT DID NOT HAVE TO BE REMOVED. AFTER FINISHING THE JOB (INCLUDING INSPECTION) AND ON MY DRIVE HOME, I DID NOT SPECIFICALLY REMEMBER RECHKING THIS BOLT/NUT. SO AS PRECAUTION, NOTIFIED MY SUPVR AND MAINT CTL TO HAVE THIS CHKED AT FIRST STATION STOP.
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.