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A306, vicinity JFK New York USA, 2001 (WAKE HF AW)
|On November 12, 2001, an Airbus Industries A300-600 operated by American Airlines crashed into a residential area of Belle Harbour, New York, after take-off from John F. Kennedy International Airport, New York. Shortly after take off, the aircraft encountered mild wake turbulence from a departing Boeing 747-400.|
|Event Type||AW, HF, LOC, WAKE|
|Type of Flight||Public Transport (Passenger)|
|Origin||New York/John F Kennedy International Airport|
|Intended Destination||Santo Domingo International Airport|
|ICL / ENR|
|Location - Airport|
|Airport vicinity||New York/John F Kennedy International Airport|
|Tag(s)|| Inappropriate crew response - skills deficiency|
Procedural non compliance
|Tag(s)|| Airframe Structural Failure|
Flight Control Error
|Tag(s)|| ICAO Standard Wake Separation prevailed|
In trail event
Pilot over compensation
|Damage or injury||Yes|
|Aircraft damage||Hull loss|
|Injuries||Most or all occupants|
|Fatalities||Most or all occupants|
|Causal Factor Group(s)|
|Group(s)|| Aircraft Operation|
On November 12, 2001, an Airbus A300-600 being operated by American Airlines on a scheduled passenger flight crashed into a residential area of Belle Harbour, New York, after take-off from John F. Kennedy International Airport, New York. Shortly after take off, the aircraft encountered mild wake turbulence from a departing Boeing 747-400.
This is an extract from the official report of the accident published by the National Transportation Safety Board (NTSB).
“[…] The effect of the turbulence was typical of a minor wake encounter—a momentary 0.3 G drop in normal load factor, a 0.04 G drop in longitudinal load factor, and a 0.07 G shift in lateral load factor. However, the first officer reacted to this first wake turbulence encounter by moving the control wheel rapidly right and left several times, with large control wheel deflections up to 37 degrees right and 34 degrees left.”
Following the wake turbulence encounter, the first officer had provided excessive rudder pedal inputs which ultimately resulted in in-flight break up of the aircraft vertical stabiliser.
“The airplane’s vertical stabiliser and rudder separated in flight and were found in Jamaica Bay, about 1 mile north of the main wreckage site. The airplane’s engines subsequently separated in flight and were found several blocks north and east of the main wreckage site. All 260 people aboard the airplane and 5 people on the ground were killed, and the airplane was destroyed by impact forces and a post-crash fire.”
The Report makes the following conclusion:
“[…]The National Transportation Safety Board determines that the probable cause of this accident was:
- the in-flight separation of the vertical stabilizer as a result of the loads beyond ultimate design that were created by the first officer’s unnecessary and excessive rudder pedal inputs.
- Contributing to these rudder pedal inputs were characteristics of the Airbus A300-600 rudder system design and
- elements of the American Airlines Advanced Aircraft Manoeuvring Program.
The Report's recommendations, beginning on page 161, also address institutional, manufacturing and organisational issues (see Further Reading).
For further information see the full accident report published by NTSB.