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|
Attributes | |
ACN | 958437 |
Time | |
Date | 201107 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | B727 Undifferentiated or Other Model |
Operating Under FAR Part | Part 121 |
Flight Phase | Takeoff |
Flight Plan | IFR |
Component | |
Aircraft Component | Airspeed Indicator |
Person 1 | |
Function | Captain Pilot Flying |
Qualification | Flight Crew Multiengine Flight Crew Flight Engineer Flight Crew Instrument |
Experience | Flight Crew Last 90 Days 10 Flight Crew Total 3500 Flight Crew Type 1000 |
Events | |
Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy |
Narrative:
On takeoff roll; we rejected the takeoff around 90 KTS due to no airspeed indication on the first officer's side. The 80 KTS crosscheck was missed by the first officer due to him still trying to set the power. The second officer was new and had less than two months in the airplane and had never really been taught to bring airspeed into his crosscheck during takeoff roll. During the abort I initiated the reject around 90 KTS; deployed the spoilers and reversers; and tested the brakes. Due to our heavy weight; 165;000 pounds; I elected to roll to almost the end of the runway to save the brakes. We cleared the runway; ran the appropriate checklists; and contacted maintenance control and the company for parking. Taxi in was uneventful.
Original NASA ASRS Text
Title: A B727 flight crew rejected their takeoff above 80 KTS when they determined the First Officer's ASI had failed.
Narrative: On takeoff roll; we rejected the takeoff around 90 KTS due to no airspeed indication on the First Officer's side. The 80 KTS crosscheck was missed by the First Officer due to him still trying to set the power. The Second Officer was new and had less than two months in the airplane and had never really been taught to bring airspeed into his crosscheck during takeoff roll. During the abort I initiated the reject around 90 KTS; deployed the spoilers and reversers; and tested the brakes. Due to our heavy weight; 165;000 LBS; I elected to roll to almost the end of the runway to save the brakes. We cleared the runway; ran the appropriate checklists; and contacted Maintenance Control and the company for parking. Taxi in was uneventful.
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.