N952W

Substantial
None

Saint Glasair II SFTS/N: 2117

Accident Details

Date
Friday, October 11, 2024
NTSB Number
ERA25LA011
Location
Forest, VA
Event ID
20241015195308
Coordinates
37.278100, -79.388500
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The installation of a non-failsafe coupler that resulted in the separation of the throttle cable from the throttle arm and a subsequent partial loss of engine power.

Aircraft Information

Registration
Make
SAINT
Serial Number
2117
Engine Type
Reciprocating
Year Built
1997
Model / ICAO
Glasair II SFTRAZM
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
GLASAIR II SFT

Registered Owner (Current)

Name
ACE PDR LLC
Address
810 N STEMMONS FWY
City
LEWISVILLE
State / Zip Code
TX 75067-2529
Country
United States

Analysis

On October 11, 2024, about 1647 eastern daylight time, an experimental amateur-built Glasair II SFT, N952W, was substantially damaged when it was involved in an accident near Forest, Virginia. The private pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he departed on a cross-country flight with 46 gallons of fuel. About 45 minutes later, upon nearing the destination airport, he entered the traffic pattern to land on runway 18. The pilot reported he had to make a left turn to avoid other inbound traffic, and he ended up circling the airport and reentering the traffic pattern on crosswind. The airplane was high during the landing approach and the pilot performed a go-around. While on the crosswind leg of the traffic pattern for a second approach, the airplane exhibited a partial loss of engine power. The pilot attempted to glide to runway 36 but overshot the runway and landed in a field. The airplane’s nose landing gear collapsed, resulting in substantial damage to the left wing and forward fuselage.

Examination of the wreckage by an FAA inspector revealed that a threaded coupler between the throttle rod end and throttle cable had loosened and disconnected the cable from the throttle arm, which would allow the arm to freely move toward idle position. The inspector added that he had never seen such a coupler before on certificated aircraft. Although it provided a means to adjust the throttle cable, it also proved to be a single point of failure. Additionally, there was no means to secure the coupler, such as a cotter pin or safety wire.

The inspector further stated that the airplane had accrued about 50 hours of operation since its most recent condition inspection was completed on February 1, 2024.

According to the owner of the kit manufacturer, the make and model kit does not include throttle cables, and builders usually source engine controls from other companies. The owner added that he had never seen a throttle cable coupler used for aircraft. He believed it must have been a custom installation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA25LA011