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|
Attributes | |
ACN | 281866 |
Time | |
Date | 199408 |
Day | Thu |
Local Time Of Day | 0001 To 0600 |
Place | |
Locale Reference | atc facility : gve |
State Reference | VA |
Altitude | msl bound lower : 27000 msl bound upper : 27000 |
Environment | |
Flight Conditions | VMC |
Light | Night |
Aircraft 1 | |
Controlling Facilities | artcc : zdc |
Operator | common carrier : air carrier |
Make Model Name | B727-200 |
Operating Under FAR Part | Part 121 |
Flight Phase | climbout : intermediate altitude other other |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : atp |
Experience | flight time last 90 days : 120 flight time total : 9500 flight time type : 1000 |
ASRS Report | 281866 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : flight engineer pilot : atp pilot : cfi |
Experience | flight time last 90 days : 150 flight time total : 9000 flight time type : 3000 |
ASRS Report | 281221 |
Events | |
Anomaly | aircraft equipment problem : critical |
Independent Detector | aircraft equipment other aircraft equipment : unspecified |
Resolutory Action | flight crew : declared emergency none taken : unable other |
Consequence | Other |
Supplementary | |
Primary Problem | Aircraft |
Narrative:
I was the first officer on flight from phl to aby. The B727-200 had a lower aft body overheat indicator light illuminate during the climb to FL310. We asked ATC for a level off at FL270 while we ran the emergency checklists. We accomplished the emergency checklist in its entirety and could not isolate the overheat indication. We ran the checklist a second time and could not discover what was causing the problem. We had a phone patch to maintenance and flight dispatch going on during this time. Given the fact that we could not determine which engine if any was causing the indicator to stay intermittently illuminated, we chose to divert to rdu for maintenance rather than continue on to our destination of albany, GA, approximately 50 mins away. We coordinated the divert with flight dispatch at sdf and declared an emergency with rdu approach control. We had an uneventful landing at rdu. The emergency was terminated after the crash/fire/rescue personnel checked the aircraft over and didn't see any problems. We left the plane with the maintenance personnel at rdu and debriefed the rescue department. The aircraft had a previous maintenance write-up concerning a previous lower aft body overheat condition which had been corrected by having a clamp tightened. Because we could not isolate the problem and the mechanic didn't initially see any areas where a bleed air leak might have been present we may have had a problem with the indication system itself and not a real bleed air leak problem.
Original NASA ASRS Text
Title: CRITICAL ACFT EQUIP PROB INDICATED. DIVERSION TO ALTERNATE CARRIED OUT IN B-727-200 FREIGHTER.
Narrative: I WAS THE FO ON FLT FROM PHL TO ABY. THE B727-200 HAD A LOWER AFT BODY OVERHEAT INDICATOR LIGHT ILLUMINATE DURING THE CLB TO FL310. WE ASKED ATC FOR A LEVEL OFF AT FL270 WHILE WE RAN THE EMER CHKLISTS. WE ACCOMPLISHED THE EMER CHKLIST IN ITS ENTIRETY AND COULD NOT ISOLATE THE OVERHEAT INDICATION. WE RAN THE CHKLIST A SECOND TIME AND COULD NOT DISCOVER WHAT WAS CAUSING THE PROB. WE HAD A PHONE PATCH TO MAINT AND FLT DISPATCH GOING ON DURING THIS TIME. GIVEN THE FACT THAT WE COULD NOT DETERMINE WHICH ENG IF ANY WAS CAUSING THE INDICATOR TO STAY INTERMITTENTLY ILLUMINATED, WE CHOSE TO DIVERT TO RDU FOR MAINT RATHER THAN CONTINUE ON TO OUR DEST OF ALBANY, GA, APPROX 50 MINS AWAY. WE COORDINATED THE DIVERT WITH FLT DISPATCH AT SDF AND DECLARED AN EMER WITH RDU APCH CTL. WE HAD AN UNEVENTFUL LNDG AT RDU. THE EMER WAS TERMINATED AFTER THE CRASH/FIRE/RESCUE PERSONNEL CHKED THE ACFT OVER AND DIDN'T SEE ANY PROBS. WE LEFT THE PLANE WITH THE MAINT PERSONNEL AT RDU AND DEBRIEFED THE RESCUE DEPT. THE ACFT HAD A PREVIOUS MAINT WRITE-UP CONCERNING A PREVIOUS LOWER AFT BODY OVERHEAT CONDITION WHICH HAD BEEN CORRECTED BY HAVING A CLAMP TIGHTENED. BECAUSE WE COULD NOT ISOLATE THE PROB AND THE MECH DIDN'T INITIALLY SEE ANY AREAS WHERE A BLEED AIR LEAK MIGHT HAVE BEEN PRESENT WE MAY HAVE HAD A PROB WITH THE INDICATION SYS ITSELF AND NOT A REAL BLEED AIR LEAK PROB.
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.