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May 29, 2021 · Stoddard Hamilton Glasair II FT · N8176J

Darby, MT

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
May 29, 2021
Injury Outcomes
2 injuries (2 serious injuries)
Location
Darby, MT
Aircraft
Stoddard Hamilton Glasair II FT (1999)
Tail Number
N8176J
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
WPR21LA219

The pilot was conducting a local flight with a passenger when he received a low oil pressure warning, and he decided to perform a precautionary landing to a nearby grass runway. While on final approach for landing, the pilot determined that the airplane was high and fast, and he attempted to slip to slow the airplane and descend quickly, but about halfway down the runway, chose to go around and began a turn to land in the other direction. About three-quarters of the way through the turn, the pilot “felt the airplane begin to stall.” He pushed the nose down and the airplane contacted the ground in a left-wing-low, nose-down attitude. The automotive conversion engine was rotated by hand after removal of the flywheel dampener plate. About 2 quarts of oil was drained from the engine. Examination of the crankshaft and connecting rods revealed no anomalies. The oil filter and adapter were removed, and black RTV sealant was noted around the base of the filter adapter. The oil filter element was inspected and found to contain a sliver of black RTV material; however, based on the available information, the reason for the low oil pressure indication could not be determined.

NTSB Probable Cause

The pilot’s impact with terrain during a go-around following an attempted precautionary landing due to a low oil pressure indication. The reason for the low oil pressure indication could not be determined based on the available information.

Full Narrative

On May 29, 2021, about 1015 mountain daylight time, an experimental, amateur-built Glasair II S FT airplane, N8176J, was substantially damaged when it was involved in an accident near Darby, Montana. The pilot and the passenger sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot reported that, during the flight, while at an altitude of about 6,800 ft, the engine monitor alerted him to a low oil pressure indication. The oil pressure continued to drop, and the pilot began a descent toward a nearby private grass strip for a precautionary landing. During the final approach, the pilot determined that the airplane was high and fast, and he attempted a slip to slow the airplane and descend quickly. About halfway down the runway, the pilot elected to go around and added engine power before he started a turn. About three quarters of the way through the turn, the pilot “felt the airplane begin to stall.” To avoid powerlines, the pilot pushed the nose down and the airplane contacted the ground in a left-wing-low, nose-down attitude. The airplane was substantially damaged and both occupants were transported to the hospital with serious injuries. Postaccident examination of the experimental, Eggenfellner Subaru engine revealed that the engine crankshaft would not rotate until the dampener off the fly wheel was removed. The crankshaft then rotated through several complete cycles. No binding or abnormal noise was noted, and compression was developed in each cylinder. All six sparkplugs displayed normal operating signatures. About 2 quarts of engine oil was drained out of the engine. The oil sump was removed with no abnormalities noted. The oil filter and oil filter adapter were removed and RTV sealant was noted around the base of the oil filter adapter. The O-ring was nicked and deteriorated. The open oil filter had about an inch long sliver of RTV sealant around the base of the oil filter adapter. Due to engine design and lack of specialized tooling, no further examination or testing were accomplished.

Flight

Event TypeAccident
Event Time11:06 MDT
Nearest AirportWest Fork Lodge Airport (0.5nm NNE)
Runway2 /
Runway Length2600 ft
Runway Width65 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftStoddard Hamilton Glasair II FT
Tail NumberN8176J
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsEggenfellner · E6 3.6 Liter · Reciprocating · 250
Seats2

People & Injuries

Injury Summary2 injuries (2 serious injuries)
Fatal0
Serious2
Minor0
Uninjured0
Total2
Crew 1Age 63 · Third Class · Serious
Crew 2Serious

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility10 sm
CeilingNone
Temperature / Dew Point57 F / 36 F
Altimeter30.20 inHg
Observation Time11:53
Weather SourcePILO

Appendix: Source Data