Flight Crew Error Leads to Altitude Loss During Go-Around at Paris CDG

Casualties unknown • FR

An Airbus A319 experienced a momentary loss of flight path control and a GPWS warning during a go-around at Paris Charles de Gaulle due to improper thrust lever positioning and autopilot engagement.

What happened

On September 23, 2009, an Airbus A319-111, registration F-GRHU, operating a passenger flight from Moscow to Paris, initiated a go-around at Paris Charles de Gaulle airport. The crew was performing an ILS approach to runway 27R when weather conditions deteriorated, reaching the decision height of 200 feet without visual contact with the runway.

During the go-around maneuver, the pilot flying attempted a "soft" go-around by advancing the thrust levers gradually rather than to the full TOGA detent. Because the levers were not moved to the TOGA position, the aircraft's automated go-around modes failed to engage. As the crew transitioned through various flight phases, the pilot engaged the autopilot (AP) while the aircraft was still in a descent mode. This resulted in the autopilot commanding a nose-down pitch, causing the aircraft to descend to a minimum altitude of 76 feet and triggering a GPWS "Sink Rate" warning. The crew eventually stabilized the aircraft and continued the climb.

The investigation

The BEA investigation focused on the automation settings, the crew's flight path management, and the specific thrust lever positions used during the maneuver. Investigators examined the flight crew's use of the Flight Management Guidance System (FMGS) and the interaction between manual inputs and the autopilot. The investigation also reviewed the company's standard operating procedures (SOPs) and identified discrepancies between the manufacturer's documentation and the airline's internal manuals regarding go-around execution.

Findings

  • The primary cause of the altitude loss was the engagement of the autopilot in an inappropriate mode.
  • The failure to activate the correct go-around modes was a direct result of the thrust levers not being moved to the TOGA detent.
  • There was a lack of adequate monitoring of the aircraft's pitch attitude by the crew.
  • Contributing factors included imprecise wording in the airline's operational procedures and a tendency for the crew to adapt procedures to meet operational constraints (such as passenger comfort or minimizing altitude gain) rather than strictly following safety-critical protocols.
  • The investigation also noted that the co-pilot's attention was divided by the need to communicate with Air Traffic Control during the critical phase of the maneuver.

Probable cause

The incident was caused by the pilot engaging the autopilot in an unsuitable mode because the thrust levers were not moved to the TOGA detent, combined with a failure to monitor the aircraft's pitch.

Frequently asked questions

What happened in the 2009-09-23 Bureau d’Enquêtes et d’Analyses pour la sécurité de l’aviation civile Zone Sud - Bâtiment 153 200 rue de Paris Aéroport du Bourget 93352 Le Bourget Cedex - France T : +33 1 49 92 72 00 - F : +33 1 49 92 72 03 www.bea.aero Incident grave survenu le 23 septembre 2009 sur l’aérodrome Paris Charles de Gaulle accident near FR?

An Airbus A319 experienced a momentary loss of flight path control and a GPWS warning during a go-around at Paris Charles de Gaulle due to improper thrust lever positioning and autopilot engagement.

What aircraft was involved and where did it happen?

The accident on 2009-09-23 involved a Bureau d’Enquêtes et d’Analyses pour la sécurité de l’aviation civile Zone Sud - Bâtiment 153 200 rue de Paris Aéroport du Bourget 93352 Le Bourget Cedex - France T : +33 1 49 92 72 00 - F : +33 1 49 92 72 03 www.bea.aero Incident grave survenu le 23 septembre 2009 sur l’aérodrome Paris Charles de Gaulle, registration F-GRHU, at FR.

What was the probable cause of the accident?

The incident was caused by the pilot engaging the autopilot in an unsuitable mode because the thrust levers were not moved to the TOGA detent, combined with a failure to monitor the aircraft's pitch.

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