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|
Attributes | |
ACN | 377204 |
Time | |
Date | 199708 |
Day | Mon |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : dca |
State Reference | DC |
Altitude | agl bound lower : 1500 agl bound upper : 1500 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tracon : dca |
Operator | common carrier : air carrier |
Make Model Name | B727-200 |
Operating Under FAR Part | Part 121 |
Flight Phase | climbout : takeoff other |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : commercial pilot : flight engineer pilot : instrument pilot : atp |
Experience | flight time last 90 days : 140 flight time total : 14900 flight time type : 1245 |
ASRS Report | 377204 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : commercial pilot : instrument |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | aircraft equipment other aircraft equipment : unspecified other flight crewa |
Resolutory Action | other |
Consequence | Other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | other |
Narrative:
After takeoff, just as flaps were being retracted, strut overheat light for #1 engine illuminated. Followed operating manual procedures, to attempt to isolate problem. When attempting to restore throttle (it had been retarded to idle during procedure, and light had gone out), overheat light illuminated again. Returned to dca for uneventful landing. Callback conversation with reporter revealed the following information: the reporter stated the strut overheat light was on only at a high power setting and with the engine at idle the light was out. Reporter states that maintenance found a flexible pneumatic hose leaking where it rubbed against the stub wing structure.
Original NASA ASRS Text
Title: A B727-200 ON TKOF DIVERTED DUE TO A #1 ENG STRUT OVERHEAT WARNING CAUSED BY A FRAYED AND LEAKING PNEUMATIC FLEXIBLE HOSE.
Narrative: AFTER TKOF, JUST AS FLAPS WERE BEING RETRACTED, STRUT OVERHEAT LIGHT FOR #1 ENG ILLUMINATED. FOLLOWED OPERATING MANUAL PROCS, TO ATTEMPT TO ISOLATE PROB. WHEN ATTEMPTING TO RESTORE THROTTLE (IT HAD BEEN RETARDED TO IDLE DURING PROC, AND LIGHT HAD GONE OUT), OVERHEAT LIGHT ILLUMINATED AGAIN. RETURNED TO DCA FOR UNEVENTFUL LNDG. CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: THE RPTR STATED THE STRUT OVERHEAT LIGHT WAS ON ONLY AT A HIGH PWR SETTING AND WITH THE ENG AT IDLE THE LIGHT WAS OUT. RPTR STATES THAT MAINT FOUND A FLEXIBLE PNEUMATIC HOSE LEAKING WHERE IT RUBBED AGAINST THE STUB WING STRUCTURE.
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.