If you wish to contribute or participate in the discussions about articles you are invited to join SKYbrary as a registered user

 Actions

Difference between revisions of "B738, Limoges France, 2008"

From SKYbrary Wiki

Line 13: Line 13:
 
The flight crew used flaps 30° and set the auto-brake to “3“. The applicable [[Vref]] was [[speed::143 knots]] giving an approach speed of [[speed::158 knots]] taking into account the wind. The Operators FCOM notes that Flap 30° ”improves the handling on landing with a cross wind and gusts, compared to flaps at 40°, which allows a shorter landing.”
 
The flight crew used flaps 30° and set the auto-brake to “3“. The applicable [[Vref]] was [[speed::143 knots]] giving an approach speed of [[speed::158 knots]] taking into account the wind. The Operators FCOM notes that Flap 30° ”improves the handling on landing with a cross wind and gusts, compared to flaps at 40°, which allows a shorter landing.”
  
[[FDR]] data showed that the aircraft touched down about 690 metres from the displaced threshold, at an airspeed of [[airspeed::147 knots]] and a ground speed of [[speed::155 knots]] - an [[speed::8 knot]] tail wind component. Aircraft braking action was on average medium rather than the ‘good’ which would be expected on a wet (uncontaminated) runway. During the landing rollout, the thrust levers were set to “REVERSE IDLE“ and then to “IDLE“ for about ten seconds. Power up on the thrust reversers then took almost eight seconds.
+
[[FDR]] data showed that the aircraft touched down about 690 metres from the displaced threshold, at an airspeed of [[speed::147 knots]] and a ground speed of [[speed::155 knots]] - an [[speed::8 knot]] tail wind component. Aircraft braking action was on average medium rather than the ‘good’ which would be expected on a wet (uncontaminated) runway. During the landing rollout, the thrust levers were set to “REVERSE IDLE“ and then to “IDLE“ for about ten seconds. Power up on the thrust reversers then took almost eight seconds.
 +
 
 +
[[File:Limoges B738 RE.jpg|thumb|none|600px|Diagram of the runway overrun. "Source:"" ei-f080321a]]

Revision as of 17:00, 4 November 2010

Ambox content.png
The present article is under construction.
Reader enquiries are welcome, contact the editor: editor@skybrary.aero.
Ambox content.png


Description

On 21 March 2008, a Boeing 737-800 being operated by Ryanair on a scheduled passenger flight from Charleroi, Belgium to Limoges carried out a daylight approach at destination followed by a landing in normal ground visibility but during heavy rain and with a strong crosswind which ended with a 50 metre overrun into mud. None of the 181 occupants were injured but both engines were damaged by ingestion of debris.

Investigation

An Investigation was carried out by the French BEA. It was established that the First Officer had been acting as PF. The crew stated that they did not pay attention to the wind information provided by the controller when the aircraft was on final approach. Unfortunately, a meteorological analysis showed that a cold front had, as forecast, been in the immediate vicinity of Limoges at the time of the landing and, as the wind veered, the tail wind component increased considerably, possibly briefly exceeding 30 knots at its worst. Rainfall measurements also showed that the aircraft touched down at the time of very heavy rain - 1.6 mm fell during the six minutes that included the landing.

The surface of the 2440 metre long runway was noted to be of “tarred concrete” and not grooved. It had an upward slope for the first half, but then descended at a maximum gradient of approximately 0.5%. Friction measurements made on a wet runway were recorded to show that the friction level was within the regulatory requirements.

The flight crew used flaps 30° and set the auto-brake to “3“. The applicable Reference Speed (Vref) was 143 knots264.836 km/h <br />73.502 m/s <br /> giving an approach speed of 158 knots292.616 km/h <br />81.212 m/s <br /> taking into account the wind. The Operators FCOM notes that Flap 30° ”improves the handling on landing with a cross wind and gusts, compared to flaps at 40°, which allows a shorter landing.”

Flight Data Recorder (FDR) data showed that the aircraft touched down about 690 metres from the displaced threshold, at an airspeed of 147 knots272.244 km/h <br />75.558 m/s <br /> and a ground speed of 155 knots287.06 km/h <br />79.67 m/s <br /> - an 8 knot14.816 km/h <br />4.112 m/s <br /> tail wind component. Aircraft braking action was on average medium rather than the ‘good’ which would be expected on a wet (uncontaminated) runway. During the landing rollout, the thrust levers were set to “REVERSE IDLE“ and then to “IDLE“ for about ten seconds. Power up on the thrust reversers then took almost eight seconds.

Diagram of the runway overrun. "Source:"" ei-f080321a