Vliegtuigongeval op 05 MAR 2015 met McDonnell Douglas MD-88 N909DL - New York-La Guardia Airport, NY (LGA)
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Status:Accident investigation report completed and information captured
Datum:donderdag 5 maart 2015
Type:Silhouette image of generic MD88 model; specific model in this crash may look slightly different
McDonnell Douglas MD-88
Luchtvaartmaatschappij:Delta Air Lines
Registratie: N909DL
Constructienummer: 49540/1395
Bouwjaar: 1987-07-02 (27 years 8 months)
Aantal vlieguren:71195
Aantal vluchten:54865
Motoren: 2 Pratt & Whitney JT8D-219
Bemanning:slachtoffers: 0 / inzittenden: 5
Passagiers:slachtoffers: 0 / inzittenden: 127
Totaal:slachtoffers: 0 / inzittenden: 132
Schade: Groot
Gevolgen: Written off (damaged beyond repair)
Plaats:New York-La Guardia Airport, NY (LGA) (   Verenigde Staten)
Fase: Landing (LDG)
Soort vlucht:Binnenlandse lijnvlucht
Vliegveld van vertrek:Atlanta Hartsfield-Jackson International Airport, GA (ATL/KATL), Verenigde Staten
Vliegveld van aankomst:New York-La Guardia Airport, NY (LGA/KLGA), Verenigde Staten
Delta Air Lines flight 1086, a McDonnell Douglas MD-88, N909DL, was landing on runway 13 at New York-LaGuardia Airport (LGA) when it departed the left side of the runway, contacted the airport perimeter fence, and came to rest with the airplane's nose on an embankment next to Flushing Bay. The 2 pilots, 3 flight attendants, and 98 of the 127 passengers were not injured; the other 29 passengers received minor injuries. The airplane was substantially damaged.
Flight 1086 was a regularly scheduled passenger flight from Atlanta-Hartsfield-Jackson Atlanta International Airport, Georgia, where it departed at 09:23 hours local time.
Given the winter weather conditions at LaGuardia, the flight crew was concerned about the available landing distance on runway 13 (7003 ft / 2135 m). While en route to LGA they spent considerable time analyzing the airplane’s stopping performance.
The flight crew also requested braking action reports about 45 and 35 minutes before landing, but none were available at those times because of runway snow clearing operations. The unavailability of braking actions reports and the uncertainty about the runway’s condition created some situational stress for the captain, who was the pilot flying.
After runway 13 became available for arriving airplanes, the flight crews of two preceding airplanes (which landed on the runway about 16 and 8 minutes before the accident landing) reported good braking action on the runway, so the flight crew expected to see at least some of the runway’s surface after the airplane broke out of the clouds. However, the flight crew saw that the runway was covered with snow, which was inconsistent with their expectations based on the braking action reports and the snow clearing operations that had concluded less than 30 minutes before the airplane landed. The snowier-than-expected runway, along with the relatively short runway length and the presence of Flushing Bay directly off the departure end of the runway, most likely increased the captain’s concerns about his ability to stop the airplane within the available runway distance, which exacerbated his situational stress.
The captain made a relatively aggressive reverse thrust input almost immediately after touchdown. Both pilots were aware that 1.3 EPR was the target setting for contaminated runways.
As reverse thrust EPR was rapidly increasing, the captain’s attention was focused on other aspects of the landing, which included steering the airplane to counteract a slide to the left and ensuring that the spoilers had deployed, which was a necessary action for the autobrakes to engage. The maximum EPR values reached during the landing were 2.07 on the left engine and 1.91 on the right engine, which were much higher than the target setting of 1.3 EPR. These high EPR values likely resulted from a combination of the captain’s stress; his relatively aggressive reverse thrust input; and operational distractions, including the airplane’s continued slide to the left despite the captain’s efforts to steer it away from the snowbanks alongside the runway. All of these factors reduced the captain’s monitoring of EPR indications. The high EPR values caused rudder blanking, which occurs on MD-80 series airplanes when smooth airflow over the rudder is disrupted by high reverse thrust, and a subsequent loss of aerodynamic directional control. Although the captain stowed the thrust reversers and applied substantial right rudder, right nosewheel steering, and right manual braking, the airplane’s departure from the left side of the runway could not be avoided because directional control was regained too late to be effective.
The airplane departed the left side of runway 13 about 3,000 feet from the approach end of the runway. The tracks were on a heading of about 10 degrees from the runway heading.
About 4,100 feet from the approach end of the runway, the airplanes left wing initially struck the airport’s perimeter fence, which is located on top of the berm, and the airplane tracks turn back parallel with runway 13. About 5,000 feet from the approach end of the runway, the airplane came to rest with its nose over the berm. The left wing of the airplane destroyed about 940 feet of the perimeter fence.

Probable Cause:

The National Transportation Safety Board determines that the probable cause of this accident was the captain’s inability to maintain directional control of the airplane due to his application of excessive reverse thrust, which degraded the effectiveness of the rudder in controlling the airplane’s heading. Contributing to the accident were the captain’s (1) situational stress resulting
from his concern about stopping performance and (2) attentional limitations due to the high workload during the landing, which prevented him from immediately recognizing the use of excessive reverse thrust.

Accident investigation:

Investigating agency: NTSB
Status: Investigation completed
Duration: 1 year and 6 months
Accident number: NTSB/AAR-16/02
Download report: Final report

» Flightradar24
» Liveatc.net

METAR Weather report:
15:24 UTC / 10:24 local time:
KLGA 051524Z 04007KT 1/4SM R04/2600V2800FT SN FZFG VV009 M03/M04 A3013 RMK AO2 P0004

15:51 UTC / 10:51 local time:
KLGA 051551Z 01008KT 1/4SM R04/2800V3500FT SN FZFG VV009 M03/M05 A3012 RMK AO2 SLP199 P0006 T10331050

16:22 UTC / 11:22 local time:
KLGA 051622Z 01008KT 1/4SM R04/3000VP6000FT SN FZFG VV011 M03/M05 A3012 RMK AO2 SFC VIS 1/2 P0003


NTSB issued 14 Safety Recommendations

Show all...


photo of MD-88-N909DL
accident date: 05-03-2015
type: McDonnell Douglas MD-88
registration: N909DL
photo of MD-88-N909DL
accident date: 05-03-2015
type: McDonnell Douglas MD-88
registration: N909DL
photo of MD-88-N909DL
accident date: 05-03-2015
type: McDonnell Douglas MD-88
registration: N909DL
photo of MD-88-N909DL
accident date: 05-03-2015
type: McDonnell Douglas MD-88
registration: N909DL
photo of MD-88-N909DL
events during landing
photo of MD-88-N909DL
FDR plot
photo of MD-88-N909DL
accident date: 05-03-2015
type: McDonnell Douglas MD-88
registration: N909DL

Video, social media

Thank God! No one hurt ?? we could of ended up in the water! #survive #thankgod #ice #safelanding

A video posted by _veeestchic_ (@_veeestchic_) on

Deze kaart geeft het vliegveld van vetrek weer en de geplande bestemming van de vlucht. De lijn tussen de vliegvelden geeft niet de exacte vliegroute weer.
De afstand tussen Atlanta Hartsfield-Jackson International Airport, GA en New York-La Guardia Airport, NY bedraagt 1216 km (760 miles).
Accident location: Approximate; accuracy within a few kilometers.

This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
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