Pilot Debrief

AIRBUS A320 near Denver, CO — 2009-05-04

Final reportDCA09FA047
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Date
2009-05-04
Location
Denver, CO, USA
Airport
KDEN
Aircraft
AIRBUS A320
Registration
N311US
Category
Airplane
Highest injury
Minor
Fatalities
0
Phase of flight
Landing

Probable cause

The first officer’s excessive pitch-up of the airplane while landing with a tailwind, which resulted in a tailstrike following a bounced landing. Contributing to the bounced landing were a high descent rate and excessive thrust resulting from the first officer’s delay in retarding the thrust levers to idle, thereby providing residual thrust and preventing spoiler deployment.

Contributing factors

Contributing to the bounced landing were a high descent rate and excessive thrust resulting from the first officer’s delay in retarding the thrust levers to idle, thereby providing residual thrust and preventing spoiler deployment.

NTSB narrative

The flight crew was conducting a straight-in approach during visual meteorological conditions. The approach was backed up by an instrument landing system and was stable at 1000 feet above touchdown. During the final approach the crew noted an increasing tailwind. As the first officer (FO) entered the flare, the “retard” automatic callout sounded; this automatic call-out is designed to remind the pilot to move the thrust levers to idle. Despite the callout, the thrust levers remained at climb and the autothrust system commanded increased engine power in an attempt to recover airspeed. The airplane touched down, but then bounced as a result of excess thrust and the position of the thrust levers forward of idle, which prevented deployment of the spoilers. The FO then retarded the thrust levers, which allowed spoiler deployment, and the airplane touched down firmly. During the second touchdown, the FO began pitching the airplane nose up to about 12.5 degrees, which is greater than the specified maximum pitch angle and which resulted in the tailstrike. The captain attempted to add nose-down pitch to prevent the tailstrike but was too late. The aircraft experienced heavy abrasions, dents, and perforations of the skin; the aft galley drain mast and two aircraft antennas were broken; the auxiliary power unit air intake sustained damage and the rear pressure bulkhead was buckled and cracked.

Analysis

Primary failure mode
Loss of control
First missed decision gate
Thrust levers should have been moved to idle during the flare.

NTSB coding

Evidence available

  • CVR
  • FDR / data
  • Photos
  • 15 docket documents
View NTSB final reportView NTSB docket

Docket documents15

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