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|
Attributes | |
ACN | 406435 |
Time | |
Date | 199806 |
Day | Tue |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : iad |
State Reference | DC |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | Marginal |
Light | Daylight |
Aircraft 1 | |
Operator | general aviation : personal |
Make Model Name | Learjet 60 |
Operating Under FAR Part | Part 91 |
Navigation In Use | Other Other |
Flight Phase | climbout : takeoff other |
Flight Plan | IFR |
Person 1 | |
Affiliation | Other |
Function | flight crew : first officer |
Qualification | pilot : atp |
Experience | flight time last 90 days : 140 flight time total : 3600 flight time type : 500 |
ASRS Report | 406435 |
Person 2 | |
Affiliation | Other |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Experience | flight time last 90 days : 125 flight time total : 4500 flight time type : 95 |
ASRS Report | 406444 |
Events | |
Anomaly | aircraft equipment problem : critical other anomaly other |
Independent Detector | aircraft equipment other aircraft equipment : unspecified other flight crewa |
Resolutory Action | none taken : unable |
Consequence | other |
Supplementary | |
Primary Problem | Aircraft |
Air Traffic Incident | other |
Narrative:
During takeoff from runway 1L at iad I was involved in a high speed high gross weight rejected takeoff due to a catastrophic failure of both right main tires. The approximately speed of the aircraft at the time of the abort was 120 KTS. The calculated V1 speed for the conditions was 131 KTS. The tire failure subsequently resulted in the disintegration of the entire right brake assembly which in turn severed the hydraulic lines and electrical connections to the anti skid and squat switch system. Because of this the thrust reversers were inoperative. Directional control was maintained throughout the entire abort procedure. However, due to very limited brake effectiveness and the high gross weight of the aircraft, we were unable to adequately stop the aircraft in the remaining runway length available. In order to avoid further damage to the aircraft by running through the runway end lights, we elected to exit the left side of the runway just short of the end at a speed of 20-30 KTS. At this point I have no explanation as to why the tires failed. All 4 tires were just recently replaced and visually were in excellent condition.
Original NASA ASRS Text
Title: FLC OF LR60 HAS HIGH SPD, HIGH GROSS WT REJECTED TKOF. THEY AVOID RUNNING THROUGH THE END RWY LIGHTS BY EXITING THE L SIDE OF THE RWY.
Narrative: DURING TKOF FROM RWY 1L AT IAD I WAS INVOLVED IN A HIGH SPD HIGH GROSS WT REJECTED TKOF DUE TO A CATASTROPHIC FAILURE OF BOTH R MAIN TIRES. THE APPROX SPD OF THE ACFT AT THE TIME OF THE ABORT WAS 120 KTS. THE CALCULATED V1 SPD FOR THE CONDITIONS WAS 131 KTS. THE TIRE FAILURE SUBSEQUENTLY RESULTED IN THE DISINTEGRATION OF THE ENTIRE R BRAKE ASSEMBLY WHICH IN TURN SEVERED THE HYD LINES AND ELECTRICAL CONNECTIONS TO THE ANTI SKID AND SQUAT SWITCH SYS. BECAUSE OF THIS THE THRUST REVERSERS WERE INOP. DIRECTIONAL CTL WAS MAINTAINED THROUGHOUT THE ENTIRE ABORT PROC. HOWEVER, DUE TO VERY LIMITED BRAKE EFFECTIVENESS AND THE HIGH GROSS WT OF THE ACFT, WE WERE UNABLE TO ADEQUATELY STOP THE ACFT IN THE REMAINING RWY LENGTH AVAILABLE. IN ORDER TO AVOID FURTHER DAMAGE TO THE ACFT BY RUNNING THROUGH THE RWY END LIGHTS, WE ELECTED TO EXIT THE L SIDE OF THE RWY JUST SHORT OF THE END AT A SPD OF 20-30 KTS. AT THIS POINT I HAVE NO EXPLANATION AS TO WHY THE TIRES FAILED. ALL 4 TIRES WERE JUST RECENTLY REPLACED AND VISUALLY WERE IN EXCELLENT CONDITION.
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.