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37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
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| Attributes | |
| ACN | 811750 |
| Time | |
| Date | 200811 |
| Local Time Of Day | 1201 To 1800 |
| Place | |
| Locale Reference | airport : zzz.airport |
| State Reference | US |
| Altitude | agl single value : 0 |
| Environment | |
| Flight Conditions | VMC |
| Light | Daylight |
| Aircraft 1 | |
| Operator | common carrier : air carrier |
| Make Model Name | MD-80 Series (DC-9-80) Undifferentiated or Other Model |
| Operating Under FAR Part | Part 121 |
| Flight Phase | ground : takeoff roll |
| Flight Plan | IFR |
| Person 1 | |
| Affiliation | company : air carrier |
| Function | flight crew : captain oversight : pic |
| Qualification | pilot : flight engineer pilot : multi engine pilot : instrument pilot : commercial pilot : atp |
| Experience | flight time last 90 days : 220 flight time total : 13500 flight time type : 10500 |
| ASRS Report | 811750 |
| Events | |
| Anomaly | aircraft equipment problem : critical |
| Independent Detector | aircraft equipment other aircraft equipment : brake over temp guage |
| Resolutory Action | flight crew : rejected takeoff |
| Consequence | other |
| Supplementary | |
| Problem Areas | Aircraft |
| Primary Problem | Aircraft |
Narrative:
Initiated abort during takeoff roll due to brake overtemp gauge indicating a brake overheat. I observed the temperature gauge needle fluctuating full scale; followed by the overheat light illuminating. At 100-110 KTS; abort was initiated with approximately 12000 ft of runway remaining. Runway was dry. Aircraft weighed approximately 144000 pounds; V1 was 150 KTS. Runway was cleared and crash fire rescue equipment requested to inspect landing gear area. It was found that the #1 wheel had experienced a wheel bearing failure and the wheel had damaged the brake assembly. Aircraft could not be taxied/towed until wheel assembly was replaced. Given the conditions; i.e.; long dry runway; I felt aborting was the prudent option.
Original NASA ASRS Text
Title: AN MD82 FLIGHT CREW EXPERIENCED BRAKE OVER TEMP WARNING ON TAKEOFF ROLL AND REJECTED THE TAKEOFF AT APPROX 100 - 110 KTS.
Narrative: INITIATED ABORT DURING TKOF ROLL DUE TO BRAKE OVERTEMP GAUGE INDICATING A BRAKE OVERHEAT. I OBSERVED THE TEMP GAUGE NEEDLE FLUCTUATING FULL SCALE; FOLLOWED BY THE OVERHEAT LIGHT ILLUMINATING. AT 100-110 KTS; ABORT WAS INITIATED WITH APPROX 12000 FT OF RWY REMAINING. RWY WAS DRY. ACFT WEIGHED APPROX 144000 LBS; V1 WAS 150 KTS. RWY WAS CLRED AND CFR REQUESTED TO INSPECT LNDG GEAR AREA. IT WAS FOUND THAT THE #1 WHEEL HAD EXPERIENCED A WHEEL BEARING FAILURE AND THE WHEEL HAD DAMAGED THE BRAKE ASSEMBLY. ACFT COULD NOT BE TAXIED/TOWED UNTIL WHEEL ASSEMBLY WAS REPLACED. GIVEN THE CONDITIONS; I.E.; LONG DRY RWY; I FELT ABORTING WAS THE PRUDENT OPTION.
Data retrieved from NASA's ASRS site as of May 2009 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.