Final
Report № AIFN/0010/2018, issued on 10 January 2022
13
1.11
Flight Recorders
The Aircraft was equipped with a Honeywell Solid State FDR, part number 980-4700-042,
and a Honeywell Solid State Cockpit Voice Recorder (CVR), part number 980-6022-001.
Both flight recorders were downloaded at Abu Dhabi Flight Recorders Laboratory. It was
found that the CVR had been overwritten and contained no recorded information related to the
Incident flight. The FDR data was valid.
At the request of the Investigation, the Aircraft manufacturer used the FDR data for
analyzing the Aircraft's performance. The performance report received from the manufacturer
revealed that the Commander did not take the side stick priority.
1.12
Wreckage and Impact Information
The Aircraft was intact.
1.13
Medical and Pathological Information
Post-Incident blood tests did not reveal any psychoactive materials that could have
degraded the flight crew
’s performance.
1.14
Fire
There was no evidence of fire.
1.15
Survival Aspects
None of the passengers or crew were injured.
1.16
Tests and Research
1.16.1 Rejecting take-off scenarios calculations
For flight ABY111, taking into consideration the dry runway surface, Aircraft take-off
weight, Aircraft configuration and performance, and take-off wind conditions, the Investigation
requested the Aircraft manufacturer to calculate if the Commander could have safely rejected the
takeoff based on the following two scenarios:
Applying maximum reverse thrust at the time when the Commander had selected
TOGA thrust when the Aircraft CAS was 57 knots.
Applying maximum reverse thrust instead of flap configuration 2 when the
Commander selected flap 2 configuration with Aircraft CAS was 109 knots.
According to the Aircraft’s manufacturer calculation that at the time of the take-off initiation,
the runway remaining was 984 meters. For both scenarios, it was possible to safely stop the Aircraft
if maximum engine reverse thrust was used, automatically applying maximum braking. The
calculated runway distance remaining were:
For the first scenario, the Aircraft would have stopped 653 meters before the end
of the runway.
For the second scenario, the Aircraft would have stopped 45 meters before the end
of the runway.