37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
|
Attributes | |
ACN | 921509 |
Time | |
Date | 201012 |
Environment | |
Flight Conditions | IMC |
Aircraft 1 | |
Make Model Name | B757-200 |
Operating Under FAR Part | Part 121 |
Flight Phase | Initial Climb |
Flight Plan | IFR |
Component | |
Aircraft Component | Air Data Computer |
Person 1 | |
Function | Pilot Not Flying Check Pilot Captain |
Qualification | Flight Crew Air Transport Pilot (ATP) |
Experience | Flight Crew Last 90 Days 200 Flight Crew Total 24000 Flight Crew Type 9000 |
Person 2 | |
Function | First Officer Pilot Flying |
Experience | Flight Crew Last 90 Days 70 Flight Crew Total 12000 Flight Crew Type 3000 |
Events | |
Anomaly | Aircraft Equipment Problem Critical |
Narrative:
On climb out at approximately 600 feet first officer's flight director bars failed and vs and airspeed indicator began to give erroneous indications. This was followed by several EICAS messages: mach trim speed; rudder ratio; airspeed. The first officer pitched down and applied max thrust. As I saw him do this I looked at his instruments and saw they disagreed with mine. I verified my airspeed indicator was working properly by comparing to the standby airspeed indicator and took control of the aircraft. We leveled off at 800 feet to try to stay below the bases and declared an emergency. Flap 5 speed limit may have been exceeded momentarily. Tower let us circle to land on the departure runway . Aircraft was difficult to control on final as trim was unresponsive. Normal flap 30 landing made without any additional problems.
Original NASA ASRS Text
Title: B757 flight crew experiences Air Data Computer failure due to apparent faulty wiring shortly after takeoff; resulting in loss of First Officer's pitot static instruments and associated EICAS warnings. The Captain took control and returned visually for landing on the departure runway.
Narrative: On climb out at approximately 600 feet First Officer's flight director bars failed and VS and airspeed indicator began to give erroneous indications. This was followed by several EICAS messages: mach trim speed; rudder ratio; airspeed. The First Officer pitched down and applied max thrust. As I saw him do this I looked at his instruments and saw they disagreed with mine. I verified my airspeed indicator was working properly by comparing to the standby airspeed indicator and took control of the aircraft. We leveled off at 800 feet to try to stay below the bases and declared an emergency. Flap 5 speed limit may have been exceeded momentarily. Tower let us circle to land on the departure runway . Aircraft was difficult to control on final as trim was unresponsive. Normal flap 30 landing made without any additional problems.
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.