N8176J

Substantial
Serious

STODDARD HAMILTON GLASAIR IIS/N: 2123

Accident Details

Date
Saturday, May 29, 2021
NTSB Number
WPR21LA219
Location
Darby, MT
Event ID
20210602103195
Coordinates
45.953056, -114.142220
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
2
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

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.

Aircraft Information

Registration
Make
STODDARD HAMILTON
Serial Number
2123
Engine Type
Reciprocating
Year Built
1999
Model / ICAO
GLASAIR IIMI2
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
GLASAIR II S FT

Registered Owner (Current)

Name
BURRUSS ALLEN C
Address
1375 CHAFFIN LN
City
CORVALLIS
State / Zip Code
MT 59828-9502
Country
United States

Analysis

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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR21LA219