Incident Airbus A320-211 F-GJVA,
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ASN Wikibase Occurrence # 174122
 
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Date:Wednesday 28 March 2012
Time:20:20
Type:Silhouette image of generic A320 model; specific model in this crash may look slightly different    
Airbus A320-211
Owner/operator:Air France
Registration: F-GJVA
MSN: 144
Year of manufacture:1990
Engine model:CFMI CFM56-5A1
Fatalities:Fatalities: 0 / Occupants:
Aircraft damage: None
Category:Incident
Location:Hamburg-Fuhlsbüttel Airport (HAM/EDDH) -   Germany
Phase: Approach
Nature:Passenger - Scheduled
Departure airport:Paris-Charles de Gaulle Airport (CDG/LFPG)
Destination airport:Hamburg-Fuhlsbüttel Airport (HAM/EDDH)
Investigating agency: BEA
Confidence Rating: Accident investigation report completed and information captured
Narrative:
An Airbus A320-211 of Air France operated a passenger service, flight AF2510, from Paris-CDG, France to Hamburg, Germany. The captain was Pilot Flying.
While the aircraft was descending towards Hamburg, there was a change in runway utilization. Runway 33 was being used for takeoffs and landings until runway 23 was opened for landings. The A320 was the second aircraft using runway 23 for landing since the change. After intercepting the runway 23 ILS glideslope, the Pilot Flying reprogrammed the FMGS (Flight Management and Guidance System) for this approach.
At the same time Air Berlin flight AB6660, a Boeing 737-700 (D-AHXA) had just landed on runway 33. The 737 taxied towards the terminal building but had to cross runway 23 to get there. Since the A320 was on final approach, the flight crew of the 737 was instructed to hold short on taxiway D.
From that moment on the Primary Flight Display (PFD) of the A320 began displaying erroneous glidepath information. The aircraft descended below the glideslope while the PFD showed the airplane to be on the glideslope. The A320 descended even further below the glideslope, yet the PFD showed it to be almost one dot above the glideslope.
The first officer suggested to abort the approach, which was accepted by the captain. The captain raised the nose but did not change the throttle setting. The speed decreased to 143 knots and the "Speed, speed, speed" aural alarm activated. The captain progressively moved the throttles to Maximum Continuous Thrust (MCT).
Meanwhile the Alpha Floor protection activated, moving the throttles to TOGA (Takeoff Go Around). The speed had dropped to a 121 knots. Subsequently the captain lowered the nose and allowed the airplane to pick up speed. The flight circled and made a safe approach and landing on runway 23.

An investigation revealed that the Boeing 737 that was holding short on the taxiway was positioned in an area that was considered a critical zone near the Glide Slope antenna. The aircraft caused a disturbance in the glideslope signal, leading to erroneous information being displayed on the PFD of the approaching aircraft.

Accident investigation:
cover
  
Investigating agency: BEA
Report number: BFU TX004-12
Status: Investigation completed
Duration:
Download report: Final report

Sources:

http://www.bea.aero/docspa/2012/f-va120328/pdf/f-va120328.pdf

Images:


Hamburg airport map showing critical zone (BEA)


Approach profile (BEA)

Revision history:

Date/timeContributorUpdates
25-Feb-2015 20:05 harro Added
25-Feb-2015 20:11 harro Updated [Photo, ]
25-Feb-2015 20:11 harro Updated [Photo, ]
25-Feb-2015 20:18 harro Updated [Narrative]
25-Feb-2015 20:43 harro Updated [Narrative]

Corrections or additions? ... Edit this accident description

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