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Aviation safety reports, made easier to study

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January 21, 2021 · Randy Wayne Maloney M1 · N322TR

Eagle Point, OR

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
January 21, 2021
Injury Outcomes
2 injuries (2 minor injuries)
Location
Eagle Point, OR
Aircraft
Randy Wayne Maloney M1 (1998)
Tail Number
N322TR
Injuries
Minor
Aircraft Damage
Destroyed
NTSB Number
WPR21LA094

The pilot reported that, in cruise flight at 3,000 ft mean sea level, the engine began to sputter, and the airplane began to descend. The pilot maneuvered toward open fields, and about 50 ft above ground level, the engine rpm increased slightly. The airplane subsequently impacted a cable and terrain. The airplane was destroyed by a postcrash fire. An engine examination revealed no evidence of a mechanical failure or malfunction that would have precluded normal operation. The reason for the partial loss of engine power was not determined.

NTSB Probable Cause

A partial loss of engine power for reasons that could not be determined based on available evidence.

Full Narrative

On January 25, 2021, about 1200 Pacific standard time, an experimental, amateur-built M1 airplane, N322TR, was destroyed when it was involved in an accident near Eagle Point, OR. The pilot and passenger received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that, during cruise flight at 3,000 ft mean sea level (msl), the engine began to sputter, and the airplane began to descend. In anticipation of a forced landing, he flew toward farm fields. About 50 ft above ground level, the engine rpm began to increase slightly, but the pilot did not attempt to climb. The airplane subsequently impacted a cable and terrain. The airplane was destroyed by the postaccident fire. Examination of the engine revealed impact damage and heat distress. The propeller remained attached to the propeller crankshaft flange. All engine accessories remained attached to the engine via their respective mounts. The intake and exhaust rocker arms were intact and undamaged. Mechanical continuity was established throughout the engine and valve train when the propeller was rotated by hand. Thumb compression was obtained on all six cylinders in proper firing order when the propeller was rotated by hand. Equal movement of the intake and exhaust valve rocker arms was noted on all six cylinders. All four cylinders were examined internally using a lighted borescope. The pistons were unremarkable. A normal amount of carbon deposits was observed on the tops of all six pistons. There was no evidence of a mechanical failure or malfunction that would have precluded normal operation.

Flight

Event TypeAccident
Event Time12:00 PST
Nearest AirportEagle Apoint (0nm)
Runwayunk
Runway Length1275 ft
Runway Width35 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftRandy Wayne Maloney M1
Tail NumberN322TR
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 91
Engine TypeReciprocating
Engine DetailsLycoming · O-435-25A · Reciprocating · 150
Seats2

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 25 · Third Class · Minor
Crew 2Minor

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point41 C / 30 C
Altimeter30.04 inHg
Observation Time11:30
Weather SourcePILO

Appendix: Source Data