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|
Attributes | |
ACN | 977337 |
Time | |
Date | 201110 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | IMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | B757-200 |
Operating Under FAR Part | Part 121 |
Flight Phase | Initial Climb |
Flight Plan | IFR |
Component | |
Aircraft Component | PFD |
Person 1 | |
Function | Pilot Not Flying Captain |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Person 2 | |
Function | First Officer Pilot Flying |
Events | |
Anomaly | Deviation - Procedural Published Material / Policy Deviation - Speed All Types |
Narrative:
Departed on flat-panel display aircraft. Due to rain showers and wind gusts in the vicinity; we elected to perform a max power takeoff. Aircraft weight was approximately 200;000 pounds. First officer was pilot flying and has not often seen or operated a flat-panel aircraft on the line. Due to lighter aircraft weight; wind gusts and pitch fluctuations of the command v-bar and a higher initial pitch up with max power; airspeed began to bleed back toward V2. As pilot not flying; I reminded first officer of pitch attitude and nudged the yoke forward to assist recovery of airspeed. Flaps remained at takeoff setting until airspeed recovered. Continued climb out and clean-up on schedule as airspeed increased. I believe that first officer's lack of regular and recent experience with the flat-panel display allowed for pitch and airspeed transgressions out of the normal takeoff range. Also; I could have provided more timely pitch and airspeed feedback to pilot flying to help avoid this situation. Continued and discussed what could have prevented a re-occurrence of this situation.
Original NASA ASRS Text
Title: A First Officer allowed the aircraft to slow during takeoff in foul weather because he was unfamiliar with the new flat panel PFD so the Captain nudged the yoke forward to aid airspeed recovery.
Narrative: Departed on Flat-Panel Display aircraft. Due to rain showers and wind gusts in the vicinity; we elected to perform a max power takeoff. Aircraft weight was approximately 200;000 LBS. First Officer was pilot flying and has not often seen or operated a Flat-Panel aircraft on the line. Due to lighter aircraft weight; wind gusts and pitch fluctuations of the command V-bar and a higher initial pitch up with max power; airspeed began to bleed back toward V2. As pilot not flying; I reminded First Officer of pitch attitude and nudged the yoke forward to assist recovery of airspeed. Flaps remained at takeoff setting until airspeed recovered. Continued climb out and clean-up on schedule as airspeed increased. I believe that First Officer's lack of regular and recent experience with the flat-panel display allowed for pitch and airspeed transgressions out of the normal takeoff range. Also; I could have provided more timely pitch and airspeed feedback to pilot flying to help avoid this situation. Continued and discussed what could have prevented a re-occurrence of this situation.
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.