20190410012269A

Accident · Substantial damage

FAA accident report · Airbus Industrie A321-231 · New York, NY · April 10, 2019

Date
April 10, 2019 · 21:15 local
Place
New York, NY
Airport
John F Kennedy International
Phase of flight
Takeoff: Rotation
Operating rules
Air carrier (Part 121)
Operator
AALA
Damage
Substantial damage
Aircraft
N114NN
NTSB investigation
NTSBDCA19LA134
Reported as
Airbus Industrie A321-231
Reported engine
IAE V2533-A5
People aboard
109
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
19,563 total3,000 in this make and model198 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

American airlines 300 departed jfk runway 31L enroute to lax. Approximately 30 minutes later the flight returned to jfk where the pilots reported a flight control malfunction resulting in an uncommanded steep roll to the left on rotation. The resulting roll caused the aircraft to sustain substantial damage to the left winglet, wing, aileron, leading edge slat, and trailing edge flaps. The aircraft struck the 5,000' remaining marker and a runway edge light. Analysis of recorded data and reconstructed animation does not indicate any uncommanded flight control movements. The recorded data suggests the steep roll on rotation to have been caused by incorrect flight control inputs by the pilot flying during takeoff with a sustained crosswind.

As the FAA filed it

AMERICAN AIRLINES 300 DEPARTED JFK RUNWAY 31L ENROUTE TO LAX. APPROXIMATELY 30 MINUTES LATER THE FLIGHT RETURNED TO JFK WHERE THE PILOTS REPORTED A FLIGHT CONTROL MALFUNCTION RESULTING IN AN UNCOMMANDED STEEP ROLL TO THE LEFT ON ROTATION. THE RESULTING ROLL CAUSED THE AIRCRAFT TO SUSTAIN SUBSTANTIAL DAMAGE TO THE LEFT WINGLET, WING, AILERON, LEADING EDGE SLAT, AND TRAILING EDGE FLAPS. THE AIRCRAFT STRUCK THE 5,000' REMAINING MARKER AND A RUNWAY EDGE LIGHT. ANALYSIS OF RECORDED DATA AND RECONSTRUCTED ANIMATION DOES NOT INDICATE ANY UNCOMMANDED FLIGHT CONTROL MOVEMENTS. THE RECORDED DATA SUGGESTS THE STEEP ROLL ON ROTATION TO HAVE BEEN CAUSED BY INCORRECT FLIGHT CONTROL INPUTS BY THE PILOT FLYING DURING TAKEOFF WITH A SUSTAINED CROSSWIND.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.