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|
Attributes | |
ACN | 269833 |
Time | |
Date | 199404 |
Day | Tue |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : ord |
State Reference | IL |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | B727 Undifferentiated or Other Model |
Operating Under FAR Part | Part 121 |
Flight Phase | other |
Flight Plan | None |
Person 1 | |
Affiliation | company : air carrier |
Function | other personnel other |
Qualification | other other : other |
ASRS Report | 269833 |
Person 2 | |
Affiliation | company : air carrier |
Function | oversight : supervisor |
Qualification | other other : other |
Events | |
Anomaly | aircraft equipment problem : critical non adherence : published procedure other anomaly other |
Independent Detector | other other : unspecified |
Resolutory Action | none taken : detected after the fact |
Consequence | Other |
Supplementary | |
Air Traffic Incident | other |
Narrative:
On X/apr/94 I replaced a lower rudder actuator on a boeing 727. During installation, the maintenance manual called out to transfer a pressure switch and its mounting plate from the removed unit to the new actuator. This I did, as an assembly. New self-locking bolts were used and no leakage was noted when pressurized. Later in the month, I did a routine check of the plane's history and found that this mounting plate had been replaced as a cause of fluid loss at denver on Y/apr/94. Reviewing the manual, I found that this part should have been replaced in another section of the maintenance manual that was only listed as optional in the actuator replacement procedures. The note (in maintenance manual) should be revised that implies transferring this plate. The maintenance manual reference for replacement of this part should be listed as a required procedure. In addition, this part is not generally stocked in the inventory and should be part of the rudder actuator replacement kit.
Original NASA ASRS Text
Title: MECH REPLACES RUDDER ACTUATOR ONLY TO DISCOVER LATER THAT HE REUSED A PART THAT SHOULD ALSO HAVE BEEN REPLACED.
Narrative: ON X/APR/94 I REPLACED A LOWER RUDDER ACTUATOR ON A BOEING 727. DURING INSTALLATION, THE MAINT MANUAL CALLED OUT TO TRANSFER A PRESSURE SWITCH AND ITS MOUNTING PLATE FROM THE REMOVED UNIT TO THE NEW ACTUATOR. THIS I DID, AS AN ASSEMBLY. NEW SELF-LOCKING BOLTS WERE USED AND NO LEAKAGE WAS NOTED WHEN PRESSURIZED. LATER IN THE MONTH, I DID A ROUTINE CHK OF THE PLANE'S HISTORY AND FOUND THAT THIS MOUNTING PLATE HAD BEEN REPLACED AS A CAUSE OF FLUID LOSS AT DENVER ON Y/APR/94. REVIEWING THE MANUAL, I FOUND THAT THIS PART SHOULD HAVE BEEN REPLACED IN ANOTHER SECTION OF THE MAINT MANUAL THAT WAS ONLY LISTED AS OPTIONAL IN THE ACTUATOR REPLACEMENT PROCS. THE NOTE (IN MAINT MANUAL) SHOULD BE REVISED THAT IMPLIES TRANSFERRING THIS PLATE. THE MAINT MANUAL REF FOR REPLACEMENT OF THIS PART SHOULD BE LISTED AS A REQUIRED PROC. IN ADDITION, THIS PART IS NOT GENERALLY STOCKED IN THE INVENTORY AND SHOULD BE PART OF THE RUDDER ACTUATOR REPLACEMENT KIT.
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.