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ERA19FA189 · Beech A36

8 Jun 2019 · Southold, NY, United States

Ri Aviation Services Beech A36 · Accident: loss of engine power (total) en route

From Long Island MacArthur Airport (ISP) to Laurence G Hanscom Field (BED)

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Event

NTSB case
ERA19FA189
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
2 · all aircraft and ground
Ground fatalities
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Beech A36

Aircraft type
Beechcraft 36
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N8014T
Onboard fatalities
Unknown
Route
From Long Island MacArthur Airport (ISP), New York, NYTo Laurence G Hanscom Field (BED), Bedford, MA
Aircraft age
About 29 years (built 1990)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
En route · climb to cruise
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of engine power (total)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Aircraft › Aircraft oper/perf/capability
  • Aircraft › Aircraft power plant
  • Personnel issues › Action/decision

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

The pilot departed on a cross-country flight when, shortly after takeoff, he announced to air traffic control that the airplane had experienced an engine failure and that he would perform a forced landing in a field. Radar data showed the airplane descending over an area of open fields, and surveillance video near the accident site captured the airplane at low altitude in a steep left bank before it descended out of view behind trees and impacted the ground.

A mechanic stated that, several weeks before the accident, the pilot asked him to look at the airplane due to higher-than-normal engine oil temperature and lower than normal oil pressure. The mechanic subsequently discovered metal debris in the oil filter. He stated that he expressed concern to the pilot about operating the airplane multiple times in the weeks and days before the accident, as he felt the engine was rapidly degrading and was susceptible to a catastrophic loss. Postaccident examination of the engine revealed that the No. 1 main aft bearing had shifted, was separated from the crankshaft, and sustained extensive thermal damage. The rear of the crankshaft was no longer connected to the main bearing and there was extensive internal and thermal damage. It is likely that the bearing shift resulted in the loss of engine power.

The pilot’s decision to fly the airplane with known engine deficiencies increased the risk of a loss of engine power in flight. Following the loss of engine power, the pilot failed to maintain a proper glidepath to the forced landing site, which resulted in his low altitude maneuvering and impact with terrain.

Probable cause

A total loss of engine power due to a main bearing shift and the pilot’s subsequent failure to maintain a proper glide path to the selected forced landing site. Contributing to the accident was the pilot’s decision to operate the airplane with known mechanical deficiencies.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA19FA189
Event ID
20190608X05856
Case number
ERA19FA189
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, cause areas. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 536007cacc31b38ae5aa37d2cf4bff5864ca7253970eaf2fd163a4aa964a5646; retrieved 2026-09-15T06:59:33.117Z.