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|
Attributes | |
ACN | 795836 |
Time | |
Date | 200807 |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | agl single value : 0 |
Environment | |
Flight Conditions | IMC |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | A320 |
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 |
Experience | flight time last 90 days : 160 flight time total : 12500 flight time type : 6200 |
ASRS Report | 795836 |
Events | |
Anomaly | aircraft equipment problem : critical |
Independent Detector | other flight crewa |
Resolutory Action | flight crew : rejected takeoff |
Consequence | other |
Supplementary | |
Problem Areas | Aircraft Maintenance Human Performance |
Primary Problem | Aircraft |
Narrative:
After previously bringing aircraft X into ZZZ and experiencing an airspeed indicator difference of 20 KTS between the first officer's and my airspeed indicator; we were subsequently assigned to use the same aircraft to fly to ZZZ1. Maintenance found some differences in the adiru's and reset them and signed off the aircraft as ready to dispatch. We proceeded to preflight and depart for takeoff. We were assigned runway xxl for takeoff and were at a gross weight of approximately 160000 pounds. I was doing the takeoff. As I was looking at the airspeed indicator to confirm they were accurate; the first officer made the 80 KT call -- I was showing between 58-60 KIAS; a difference of 20 KTS. I aborted the takeoff using maximum reverse and autobrakes. The autobrakes were used to bring the aircraft to a full stop. We had the customers remain in their seats; taxied clear at intersection P and taxied back to the gate; uneventfully. We had hot brakes from the heavy abort -- about 500 degrees maximum. Debriefed maintenance once arriving at the gate on the hot brakes; airspeed discrepancy and an engine #2 fire detent fault we had on the ECAM screen. The abort procedures set by air carrier X and practiced at every simulator visit worked well and allowed us to safely bring the aircraft to a stop in less than ideal WX and heavy weight.
Original NASA ASRS Text
Title: AN A320 CAPT REJECTED THE TKOF WHEN A 20 KT AIRSPD DIFFERENCE WAS DETECTED AT THE 80 KT AIRSPD CHK.
Narrative: AFTER PREVIOUSLY BRINGING ACFT X INTO ZZZ AND EXPERIENCING AN AIRSPD INDICATOR DIFFERENCE OF 20 KTS BTWN THE FO'S AND MY AIRSPD INDICATOR; WE WERE SUBSEQUENTLY ASSIGNED TO USE THE SAME ACFT TO FLY TO ZZZ1. MAINT FOUND SOME DIFFERENCES IN THE ADIRU'S AND RESET THEM AND SIGNED OFF THE ACFT AS READY TO DISPATCH. WE PROCEEDED TO PREFLT AND DEPART FOR TKOF. WE WERE ASSIGNED RWY XXL FOR TKOF AND WERE AT A GROSS WT OF APPROX 160000 LBS. I WAS DOING THE TKOF. AS I WAS LOOKING AT THE AIRSPD INDICATOR TO CONFIRM THEY WERE ACCURATE; THE FO MADE THE 80 KT CALL -- I WAS SHOWING BTWN 58-60 KIAS; A DIFFERENCE OF 20 KTS. I ABORTED THE TKOF USING MAX REVERSE AND AUTOBRAKES. THE AUTOBRAKES WERE USED TO BRING THE ACFT TO A FULL STOP. WE HAD THE CUSTOMERS REMAIN IN THEIR SEATS; TAXIED CLR AT INTXN P AND TAXIED BACK TO THE GATE; UNEVENTFULLY. WE HAD HOT BRAKES FROM THE HVY ABORT -- ABOUT 500 DEGS MAX. DEBRIEFED MAINT ONCE ARRIVING AT THE GATE ON THE HOT BRAKES; AIRSPD DISCREPANCY AND AN ENG #2 FIRE DETENT FAULT WE HAD ON THE ECAM SCREEN. THE ABORT PROCS SET BY ACR X AND PRACTICED AT EVERY SIMULATOR VISIT WORKED WELL AND ALLOWED US TO SAFELY BRING THE ACFT TO A STOP IN LESS THAN IDEAL WX AND HVY WT.
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.