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|
Attributes | |
ACN | 299128 |
Time | |
Date | 199503 |
Day | Tue |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : sfo |
State Reference | CA |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Light | Daylight |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | Commercial Fixed Wing |
Operating Under FAR Part | Part 121 |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | other personnel other |
Qualification | other other : other |
ASRS Report | 299128 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : declared emergency none taken : detected after the fact |
Consequence | faa : investigated Other Other |
Supplementary | |
Primary Problem | Aircraft |
Narrative:
On mar/tue/95, an airline flight departing from sfo had a fire warning on the #1 engine shortly after takeoff requiring an engine shutdown. The aircraft returned to sfo at which time an air leak was discovered at the thrust reverser blocker valve location. This leak heated the fire loop which is within approximately 4-6 inches of this area causing the fire indication. The blocker valve had been replaced per our airline's operational and maintenance manual written documentation. This paperwork did not contain a leak check requirement, only an operational check per our airline's jet handbook section which checks reverser operation with engine running. The engineering department for this aspect of engine maintenance was contacted and will be incorporating a leak check into the aforementioned paperwork, as well as evaluating a preload problem at the same area. This condition has been noted with some installations where a gap of up to 1 inch will exist between the mating flanges of the blocker valve and the pneumatic ducting with one of the connecting 'V' clamps removed.
Original NASA ASRS Text
Title: INFLT FIRE. ACR CREW HAS AN INFLT FIRE INDICATION DUE TO IMPROPER MAINT WORK.
Narrative: ON MAR/TUE/95, AN AIRLINE FLT DEPARTING FROM SFO HAD A FIRE WARNING ON THE #1 ENG SHORTLY AFTER TKOF REQUIRING AN ENG SHUTDOWN. THE ACFT RETURNED TO SFO AT WHICH TIME AN AIR LEAK WAS DISCOVERED AT THE THRUST REVERSER BLOCKER VALVE LOCATION. THIS LEAK HEATED THE FIRE LOOP WHICH IS WITHIN APPROX 4-6 INCHES OF THIS AREA CAUSING THE FIRE INDICATION. THE BLOCKER VALVE HAD BEEN REPLACED PER OUR AIRLINE'S OPERATIONAL AND MAINT MANUAL WRITTEN DOCUMENTATION. THIS PAPERWORK DID NOT CONTAIN A LEAK CHK REQUIREMENT, ONLY AN OPERATIONAL CHK PER OUR AIRLINE'S JET HANDBOOK SECTION WHICH CHKS REVERSER OP WITH ENG RUNNING. THE ENGINEERING DEPT FOR THIS ASPECT OF ENG MAINT WAS CONTACTED AND WILL BE INCORPORATING A LEAK CHK INTO THE AFOREMENTIONED PAPERWORK, AS WELL AS EVALUATING A PRELOAD PROB AT THE SAME AREA. THIS CONDITION HAS BEEN NOTED WITH SOME INSTALLATIONS WHERE A GAP OF UP TO 1 INCH WILL EXIST BTWN THE MATING FLANGES OF THE BLOCKER VALVE AND THE PNEUMATIC DUCTING WITH ONE OF THE CONNECTING 'V' CLAMPS REMOVED.
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.