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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

June 2, 2022 · Trojan TA16 · N36YR

Ray, MI

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 2, 2022
Injury Outcomes
No injuries (1 uninjured)
Location
Ray, MI
Aircraft
Trojan TA16 (2017)
Tail Number
N36YR
Injuries
None
Aircraft Damage
Substantial
NTSB Number
CEN22LA251

The pilot, who was the builder of the experimental, amateur-built airplane, reported that shortly after takeoff the engine surged rapidly three times and then lost total power. The pilot turned the airplane back toward the airport to try to land on the runway. While maneuvering toward the airport, the pilot attempted to restore engine power, but was not successful. Unable to make the runway, the pilot performed a forced landing to a rough field, during which the airplane sustained substantial damage to the fuselage and wings. A postaccident examination of the engine found that the bearings connecting the piston arms to the crankshaft were seized and displayed signatures consistent with a lack of oil lubrication and cooling. Reviewed data stored in the electronic flight instrument system did not provide indications of an impending oil system malfunction. The pilot stated that he purchased the engine as a “firewall forward” package and speculated that the engine could have benefitted from the installation of a secondary oil cooler.

NTSB Probable Cause

A lack of lubrication and inadequate cooling, which resulted in internal damage to the engine and a subsequent total loss of engine power.

Full Narrative

On June 2, 2022, about 1315 eastern daylight time, an experimental, amateur-built Trojan TA16 airplane, N36YR, was substantially damaged when it was involved in an accident near Ray, Michigan. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot, who was the owner and builder of the airplane, stated that the preflight, engine run-up, and takeoff were all normal. During the departure climb, the engine surged rapidly three times and then stopped producing power. The pilot scanned the cockpit instruments and noted that the tachometer displayed 0 rpm. The pilot turned the airplane back toward the runway while attempting to restore engine power. Unable to restore engine power or reach the runway, the pilot performed a forced landing, during which the airplane collided with small trees, resulting in substantial damage to the fuselage and wings. A postaccident examination of the engine found that the pistons in cylinders Nos. 1 through 5 were seized at the bearings connecting the piston arms to the crankshaft. Those bearings displayed signatures consistent with a lack of adequate oil lubrication and cooling. Reviewed data stored in the electronic flight instrument system did not provide indications of an impending oil system malfunction. The pilot reported that he purchased the engine as a “firewall forward” package. He speculated that the engine could have benefitted from additional oil cooling, such as a secondary oil cooler.

Flight

Event TypeAccident
Event Time13:15 EDT
Nearest AirportRay Community (0.2nm N)
Runway28
Runway Length2495 ft
Runway Width60 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftTrojan TA16
Tail NumberN36YR
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsGeneral Motors · LS1 · Reciprocating · 350
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 75 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind340° @ 4 kt
Visibility10 sm
CeilingBroken clouds 9000 ft
Temperature / Dew Point61 F / 52 F
Altimeter29.88 inHg
Observation Time12:56
Weather SourceWFAC

Appendix: Source Data