20140313003339A

Accident · Substantial damage

FAA accident report · Airbus Industrie A320-214 · Philadelphia, PA · March 13, 2014

Date
March 13, 2014 · 18:25 local
Place
Philadelphia, PA
Phase of flight
Takeoff: Rotation
Operating rules
Air carrier (Part 121)
Operator
USAA
Damage
Substantial damage
Aircraft
N113UW
NTSB investigation
NTSBDCA14MA081
Reported as
Airbus Industrie A320-214
Reported engine
CFM International CFM56 series
People aboard
154
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Airline transport
Pilot’s flight hours
23,830 total4,457 in this make and model159 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

As the crew taxied onto the runway for departure the captain noticed that the wrong departure runway (27R) was displayed on his navigation display (ND). The first officer (fo) corrected this by entering runway 27L into the multifunction control display unit (mcdu). Changing the runway in the mcdu requires the crew to manually re-verify the ?v? Speeds and flex temperature in the mcdu. The crew failed to accomplish this step and so the aircraft had no data available to compute and perform a flex takeoff or display speeds on the PFD?s. as a result, when the captain advanced the throttles a chime was heard followed by the warning message: eng thr levers not set; set toga; displayed on the upper electronic centralized aircraft monitoring (ecam) display screen. The captain asked the fo what the chime was; the fo replied ?power not set? But failed to read the entire message, which instructed the flight crew to set the throttle to the take-off go around (toga) setting. The captain replied to the fo with :the power is set? And also stated that he only advanced the throttle just past the flexible take-off (flex) throttle position, then back to the flex position. Once the aircraft reached 80 knots a continuous ?retard retard retard?, (this message instructs the flight crew to move the throttle to the idle position during landing) aural warning message was sounded. The captain stated ?we?ll get that straight when we get airborne?.

Aircraft lifted off, climbed to approximately seventy feet. The captain stated that once the wheels were off the ground, he had the perception that the aircraft was unsafe to fly and moved the throttles to the idle position. Aircraft contacted the runway, the tail section of the aircraft stuck the runway, followed by the MLG, driving the nose landing gear into the runway causing the NLG tire?s to blow and the NLG to collapse. Aircraft slid approximately 2000? Feet and came to rest adjacent to taxiway S10 along the left runway edge. Left engine ingested runway edge lights and dirt.

As the FAA filed it

AS THE CREW TAXIED ONTO THE RUNWAY FOR DEPARTURE THE CAPTAIN NOTICED THAT THE WRONG DEPARTURE RUNWAY (27R) WAS DISPLAYED ON HIS NAVIGATION DISPLAY (ND). THE FIRST OFFICER (FO) CORRECTED THIS BY ENTERING RUNWAY 27L INTO THE MULTIFUNCTION CONTROL DISPLAY UNIT (MCDU). CHANGING THE RUNWAY IN THE MCDU REQUIRES THE CREW TO MANUALLY RE-VERIFY THE ?V? SPEEDS AND FLEX TEMPERATURE IN THE MCDU. THE CREW FAILED TO ACCOMPLISH THIS STEP AND SO THE AIRCRAFT HAD NO DATA AVAILABLE TO COMPUTE AND PERFORM A FLEX TAKEOFF OR DISPLAY SPEEDS ON THE PFD?S. AS A RESULT, WHEN THE CAPTAIN ADVANCED THE THROTTLES A CHIME WAS HEARD FOLLOWED BY THE WARNING MESSAGE: ENG THR LEVERS NOT SET; SET TOGA; DISPLAYED ON THE UPPER ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM) DISPLAY SCREEN. THE CAPTAIN ASKED THE FO WHAT THE CHIME WAS; THE FO REPLIED ?POWER NOT SET? BUT FAILED TO READ THE ENTIRE MESSAGE, WHICH INSTRUCTED THE FLIGHT CREW TO SET THE THROTTLE TO THE TAKE-OFF GO AROUND (TOGA) SETTING. THE CAPTAIN REPLIED TO THE FO WITH :THE POWER IS SET? AND ALSO STATED THAT HE ONLY ADVANCED THE THROTTLE JUST PAST THE FLEXIBLE TAKE-OFF (FLEX) THROTTLE POSITION, THEN BACK TO THE FLEX POSITION. ONCE THE AIRCRAFT REACHED 80 KNOTS A CONTINUOUS ?RETARD RETARD RETARD?, (THIS MESSAGE INSTRUCTS THE FLIGHT CREW TO MOVE THE THROTTLE TO THE IDLE POSITION DURING LANDING) AURAL WARNING MESSAGE WAS SOUNDED. THE CAPTAIN STATED ?WE?LL GET THAT STRAIGHT WHEN WE GET AIRBORNE?.

AIRCRAFT LIFTED OFF, CLIMBED TO APPROXIMATELY SEVENTY FEET. THE CAPTAIN STATED THAT ONCE THE WHEELS WERE OFF THE GROUND, HE HAD THE PERCEPTION THAT THE AIRCRAFT WAS UNSAFE TO FLY AND MOVED THE THROTTLES TO THE IDLE POSITION. AIRCRAFT CONTACTED THE RUNWAY, THE TAIL SECTION OF THE AIRCRAFT STUCK THE RUNWAY, FOLLOWED BY THE MLG, DRIVING THE NOSE LANDING GEAR INTO THE RUNWAY CAUSING THE NLG TIRE?S TO BLOW AND THE NLG TO COLLAPSE. AIRCRAFT SLID APPROXIMATELY 2000? FEET AND CAME TO REST ADJACENT TO TAXIWAY S10 ALONG THE LEFT RUNWAY EDGE. LEFT ENGINE INGESTED RUNWAY EDGE LIGHTS AND DIRT.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.