Casualties unknown

Egyptian A321 Landing Incident at Cairo International Airport (SU-BQL)

Sharm Elsheikh Airport, EG

On May 21, 2021, an A320 -231 AIRBUS (registration SU-BQL) was involved in an aviation accident near Sharm Elsheikh Airport, EG. Investigators recorded the probable cause as: Failure of the auto-brake system to activate maximum deceleration during landing, resulting in an insufficient braking distance and runway overrun. This summary draws on records from the Egyptian Aircraft Accident Investigation Directorate (EAAID).

Sourcesthe Egyptian Aircraft Accident Investigation Directorate (EAAID)Primary reportUpdated 2026-06-11Data APIEditorial standards
A320 -231  AIRBUS
Photo: Tosaka / CC BY 3.0, via Wikimedia Commons

An Egyptian Airlines Airbus A321 (SU-BQL) experienced a brake system fault during landing at Cairo International Airport on May 13, 2021. The aircraft overshot the runway due to an auto-brake failure and low deceleration rates.

Incident Overview

On May 13, 2021, an Airbus A321-231 operated by Egyptian Airlines with registration SU-BQL landed at Cairo International Airport (CAI). The incident occurred during the approach to runway 04R. The flight crew reported a flat tire and Foreign Object Debris (FOD) concerns prior to landing.

Operational Sequence

The aircraft touched down at approximately 13:15 local time. Flight Data Recorder (FDR) data indicates that upon touchdown, the auto-brake system failed to engage effectively. The FDR recorded an "Auto Brake Fault" and a deceleration rate significantly lower than expected for a maximum braking scenario. Specifically, the longitudinal acceleration was recorded at -0.1872 g initially, dropping further as the aircraft continued down the runway.

Technical Findings

Investigation into the Flight Crew Operation Manual (FCOM) highlights that the auto-brake system is designed to establish and maintain a selected deceleration rate during landing. For MAX mode activation, the system requires specific conditions, including ground spoiler extension and wheel speeds above 40 knots. In this instance, despite the crew selecting the appropriate braking mode, the system did not provide the expected maximum deceleration. The FDR data shows that at a ground speed of 77 knots, the auto-brake was off, and the brake paddle angle indicated manual intervention rather than automatic control.

Outcome

Due to the insufficient braking force, the aircraft failed to stop within the available runway length and overshot the end of runway 04R. The investigation noted that the anti-skid system was active, but the primary issue remained the failure of the auto-brake function to engage as per standard operating procedures.

Probable cause

Failure of the auto-brake system to activate maximum deceleration during landing, resulting in an insufficient braking distance and runway overrun.