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July 20, 2022 · Maule M-5-235C · N6224M

Three Forks, MT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 20, 2022
Injury Outcomes
No injuries (1 uninjured)
Location
Three Forks, MT
Aircraft
Maule M-5-235C (1978)
Tail Number
N6224M
Injuries
None
Aircraft Damage
Substantial
NTSB Number
WPR22LA262

During the first flight after the installation of avionics, and an overhauled engine, the engine started to lose power in the traffic pattern. The pilot continued to fly straight in the downwind leg of the traffic pattern and attempted to troubleshoot the problem. Despite his actions, he was unable to regain engine power and subsequently pitched for best glide and made a 180° right turn to land on the runway. By this time, the airplane had traveled too far on the downwind leg, and the airplane landed short of the runway. Postaccident examination of the engine’s single-drive dual magneto revealed that the right magneto capacitor wire was attached utilizing an automotive terminal, however, the wire had separated from the crimped portion of the terminal. Additionally, the left magneto P-lead had areas of exposed wire, which grounded the left magneto and prevented its operation. The compounded anomalies, on both the left and right magnetos, would have resulted in a total loss of engine power.

NTSB Probable Cause

A loss of engine power due to degraded and incorrectly maintained ignition system components. Contributing to the accident was the pilot’s delay in turning the airplane towards the runway when the engine began to lose power.

Full Narrative

On July 20, 2022, about 0815 mountain daylight time, a Maule M-5-235C, N6224M, sustained substantial damage when it was involved in an accident in Three Forks, Montana. The commercial pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, who held a mechanic certificate with airframe and powerplant ratings with inspection authorization, the accident flight was the first flight following an engine and magneto overhaul, in addition to the installation of new avionics. He reported his completion of several engine test runs and multiple full-power, high-speed test runs. Confident of the engine’s performance, the pilot departed on the local flight and continued with engine break-in procedures. He conducted several flight maneuvers and the engine operated normally. With the intent to land, he was established in the right traffic downwind leg of the airport traffic pattern when he noticed that the engine rpm was winding down slowly. He attempted to troubleshoot the anomaly without success. He pitched for best glide with no flaps applied and made a right 180° turn for runway 03. However, the airplane’s sink rate was too high to land on the runway. The airplane touched down about 1,000 ft short of the runway threshold on an unplowed pasture and collided with a barbed wire fence. The airplane sustained substantial damage to its longerons near the wing’s attach points, the left-wing spar, and lift struts. The postaccident examination of the engine’s single-drive dual magneto revealed that the right magneto capacitor wire was attached utilizing an automotive-style terminal, that was bent 90°, rather than a right-angle flag terminal. Further examination revealed that the wire had separated within the crimped section of the terminal. The left magneto P-lead was deteriorated, and had an area of exposed wire that resulted in a ground fault when the P-lead was tested with a multimeter. The pilot reported that he could have avoided the accident if he had immediately turned toward the runway when the engine began losing power, rather than continuing the downwind leg while troubleshooting.

Flight

Event TypeAccident
Event Time08:15 MDT
Nearest AirportThree Forks (1nm E)
Runway03
Runway Length5099 ft
Runway Width60 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftMaule M-5-235C
Tail NumberN6224M
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-540-J1A5D · Reciprocating · 235
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 71 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind70° @ 3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point59 F / 43 F
Altimeter30.19 inHg
Observation Time07:56
Weather SourceWFAC

Appendix: Source Data