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Accidents · NTSB ERA19FA196 · Final report

Amateur-built T-21 accident near Endicott, New York, June 17, 2019

On June 17, 2019 at about 3:25 pm local time, a 1949 amateur-built T-21, registered N450C, was substantially damaged in an accident during maneuvering near Endicott, New York (Tri Cities Airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A partial loss of engine power for reasons that could not be determined, and the pilot's subsequent exceedance of the airplane's critical angle of attack during an attempted return to the runway, which resulted in an aerodynamic stall/spin at an altitude that precluded recovery.

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

What the record shows

Date
June 17, 2019 · about 3:25 pm local time
Place
Endicott, New York · Tri Cities Airport · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built T-21, built 1949
Registration
N450C · no longer on the register · serial 106
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

According to a witness, the pilot of the experimental, amateur-built airplane had completed one takeoff and landing in the airport traffic pattern. Following the second takeoff, at an altitude about 300 ft above ground level, the witness heard the engine "pop." The airplane remained in a nose-high attitude as it entered a steep left turn as if to return toward the runway; the witness stated that the airplane then spiraled toward the ground. Another witness stated that he heard the accident airplane's engine power decrease as it climbed through about 300 ft after takeoff and the airplane subsequently entered a descending left turn before disappearing behind trees. Postaccident examination of the engine revealed no mechanical anomalies that would have precluded normal operation, and there was no evidence of fuel contamination. All major components of the airplane were located at the accident site, and flight control continuity was established from the cockpit to all flight control surfaces. Review of the airplane's logbook and a witness account indicated that, about 1 year before the accident, the pilot had experienced aerodynamic flutter of the rudders on at least two occasions and made subsequent airframe modifications as a result; however, there was no evidence to indicate that this contributed to the accident. The airplane's steep descent before impact and the limited wreckage distribution at the accident site were consistent with an aerodynamic stall/spin. It is possible that the pilot may have experienced a partial loss of engine power or other engine anomaly (based on the witness statements) and, in response, attempted to complete a 180° turn back to the runway. During the turn, the pilot exceeded the airplane's critical angle of attack, which resulted in an aerodynamic stall/spin and a loss of control. The reason for the loss of engine power could not be determined.

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. Loss of engine power (partial) during initial climb
  2. Aerodynamic stall/spin during maneuvering defining event
  3. Collision with terrain or object (not controlled flight into terrain) during uncontrolled descent

The NTSB's findings

  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • Aircraft › Aircraft power plant › Power plant › (general) › Unknown/Not determined
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
  • Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Not attained/maintained

Pilot

  • Certificate: flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; single-engine sea; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 23,107 hours in all; 26.6 in this make and model
  • Last flight review: February 1, 2003
  • Medical certificate: Unknown
  • Seat: left
  • Injury: fatal

The aircraft

  • Last inspection: condition inspection, June 22, 2018; 11 hours since
  • Maximum gross weight: 1,550 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Lycoming O-320 (piston); 0 hours total

The flight

  • Departed from: CZG Endicott NY at 3:15 pm
  • Destination: CZG Endicott NY
  • Flight plan: none
  • Runway 03, 3,900 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 040° at 5 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 63°F (17°C), dew point 54°F (12°C)
  • Altimeter: 30.02 inHg
  • Observation at 2:53 pm from BGM, 9 miles away

Injuries

FatalSeriousMinorNone
Flight crew1

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

13 documents, released by the NTSB on December 2, 2020. 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.