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|
Attributes | |
ACN | 899021 |
Time | |
Date | 201007 |
Local Time Of Day | 0001-0600 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Aircraft 1 | |
Make Model Name | B747-400 |
Operating Under FAR Part | Part 121 |
Flight Phase | Takeoff |
Component | |
Aircraft Component | Air Data Computer |
Person 1 | |
Function | Captain Pilot Not Flying |
Experience | Flight Crew Last 90 Days 80 Flight Crew Total 22000 Flight Crew Type 8000 |
Person 2 | |
Function | Relief Pilot |
Experience | Flight Crew Last 90 Days 189 Flight Crew Total 14150 Flight Crew Type 5723 |
Events | |
Anomaly | Aircraft Equipment Problem Critical |
Narrative:
Takeoff was aborted at approximately 100 KTS due to discrepancies between my indicated airspeed and the first officer's indicated airspeed. [We] accomplished all applicable sops and relevant irregular procedures. After the first officer had applied takeoff thrust I briefly monitored the engine parameters (especially egt) for normal range and function. Then I briefly checked my airspeed indicator and the first officer's airspeed indicators for normal acceleration. My indicator appeared normal and showed smooth acceleration. When I glanced at the first officer's indicator it appeared to indicate less speed and was somewhat erratic. I thought this may be due to the right crosswind conditions. At 80 KTS I looked over at the first officer's indicator to verify. It was fluctuating and indicating something other than 80 KTS. I felt the safest thing to do was to reject the takeoff and sort out the issue on the ground rather than in the air. I did not make the 80 KTS call but announced and executed the abort maneuver. I believe my intentions and actions are in accord with the training I have received at my airline with regard to when and how to abort a takeoff.
Original NASA ASRS Text
Title: A B747 Captain rejected a takeoff at about 100 KTS because he detected a difference between his and the First Officer's airspeed. An air data computer was changed upon return to the gate.
Narrative: Takeoff was aborted at approximately 100 KTS due to discrepancies between my indicated airspeed and the First Officer's indicated airspeed. [We] accomplished all applicable SOPS and relevant irregular procedures. After the First Officer had applied takeoff thrust I briefly monitored the engine parameters (especially EGT) for normal range and function. Then I briefly checked my airspeed indicator and the First Officer's airspeed indicators for normal acceleration. My indicator appeared normal and showed smooth acceleration. When I glanced at the First Officer's indicator it appeared to indicate less speed and was somewhat erratic. I thought this may be due to the right crosswind conditions. At 80 KTS I looked over at the First Officer's indicator to verify. It was fluctuating and indicating something other than 80 KTS. I felt the safest thing to do was to reject the takeoff and sort out the issue on the ground rather than in the air. I did not make the 80 KTS call but announced and executed the abort maneuver. I believe my intentions and actions are in accord with the training I have received at my airline with regard to when and how to abort a takeoff.
Data retrieved from NASA's ASRS site as of April 2012 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.