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Accidents · NTSB ERA16FA161 · Final report

Cessna 172 accident near Westmoreland, New York, April 18, 2016

On April 18, 2016 at about 11:10 pm local time, a 1962 Cessna 172, registered N1863Y, was destroyed in an accident during takeoff near Westmoreland, New York (Sophie'S Choice airport). It was a personal flight under general aviation rules (Part 91). 2 people were killed and 1 person had minor injuries. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The pilot's decision to takeoff on the grass runway given the conditions at the time; his excessive aft control input during the takeoff roll, which resulted in the aft fuselage contacting the runway surface; and his failure to attain sufficient airspeed and exceedance of the airplane's critical angle of attack, which resulted in an aerodynamic stall.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
April 18, 2016 · about 11:10 pm local time
Place
Westmoreland, New York · Sophie'S Choice · map
Type
Accident
Injuries
2 people were killed and 1 person had minor injuries.
Weather
visual conditions (good weather)
Aircraft
Cessna 172 C, built 1962 · all 172s on the register
Registration
N1863Y · no longer on the register · serial 17249463
Damage
Destroyed
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The private pilot was taking off for a personal flight from a private turf airstrip to return to his home base airport. He initiated takeoff with a 10° flap extension and about 1,130 ft of the 1,344 ft of usable runway remaining, despite a recommendation from the airstrip owner that he begin the takeoff from a point that would have provided an additional 200 feet of runway. After beginning the takeoff, and as the airplane approached the departure end of the runway, the aft fuselage bottom contacted the runway several times due to the pilot's control input, which likely slowed the airplane. Shortly after becoming airborne while in a nose-high attitude, the airplane entered an aerodynamic stall before colliding with a tree and then the ground. After coming to rest, all occupants were conscious and alert, but the rear seat occupant required assistance exiting the airplane. The pilot attempted to assist him from the wreckage, but an explosion occurred about that time. The pilot and rear seat occupant sustained burns and died 6 days and 1 day after the accident, respectively, due to their injuries from the fire. Examination of the flight controls, engine, and engine accessories revealed no evidence of preimpact failure or malfunction that would have precluded normal operation. Extensive heat damage to the engine and engine accessories precluded an operational test of the engine. A sound spectrum analysis of a video recording of the takeoff provided by the airstrip owner revealed that the reduced engine rpm near rotation was attributed to the slow airspeed and not a loss of engine power. The airplane was within weight and center of gravity limits. Takeoff performance data for the airplane indicated that, given the weather at the time of the accident, the distance required for the airplane to take off was about 786 ft and to clear a 50-ft obstacle was about 1,370 ft with no flaps on a hard surface runway. The chart did not contain figures for a soft, grass runway, which would increase the takeoff distance. Flaps at 10° would decrease the ground run by about 10% but would the advantage was lost to climb over a 50-ft obstacle. A speed study using the video showed that the average groundspeed between becoming airborne and the time of impact was about 47 knots, or 54 mph, which was the stall speed at gross weight and 0° bank angle. Even if the pilot had used the full usable runway distance, his decision to takeoff on this runway was poor given the performance capabilities of the airplane and the fact that the grass runway would likely have increased the takeoff and climb distance beyond that available. Further, it is likely that the pilot, when he noted that the airplane was nearing the end of the runway, increased the airplane's pitch, which resulted in the tail dragging, and lifted off the airplane with inadequate airspeed and exceeded the airplane's critical angle of attack, which resulted in an aerodynamic stall.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Dragged wing/rotor/float/other during takeoff
  2. Loss of control in flight during takeoff defining event
  3. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent
  4. Fire/smoke (post-impact) during post (impact)
  5. Explosion (post-impact) during post (impact)

The NTSB's findings

  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • factor Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Pitch control › Incorrect use/operation
  • factor Personnel issues › Action/decision › Action › Incorrect action performance › Pilot
  • factor Personnel issues › Task performance › Planning/preparation › (general) › Pilot
  • factor Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot
  • factor Environmental issues › Physical environment › Runway/land/takeoff/taxi surface › (general) › Compliance w/ procedure

Pilot

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 457.3 hours in all; 381.5 in this make and model; 40 in the last 90 days; 21.8 in the last 30 days; 351.5 as pilot in command
  • Last flight review: August 16, 2014
  • Medical certificate: Class 1 (without waivers/limitations)
  • Seat: left
  • Injury: fatal

Pilot-Rated Passenger

  • Certificate: private
  • Ratings: single-engine land
  • Flight time: 200 hours in all
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: minor injuries

The aircraft

  • Airframe total time: 3,302.6 hours
  • Last inspection: annual inspection, April 5, 2016; 6 hours since
  • Maximum gross weight: 2,250 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Cont Motor O-300-D (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: NA Westmoreland NY at 11:10 pm
  • Destination: RME Rome NY
  • Flight plan: none
  • Runway 8, 1,980 ft by 70 ft
  • A second pilot was aboard

Weather at the time

  • Light: dusk
  • Wind: from 300° at 10 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 68°F (20°C), dew point 30°F (-1°C)
  • Altimeter: 30.12 inHg
  • Observation at 10:53 pm from RME, 7 miles away

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers11

Documents from the investigation the NTSB's docket: the evidence folder behind the report

15 documents, released by the NTSB on February 14, 2018. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.