N138CT

Substantial
Minor

FLIGHT DESIGN CTSWS/N: 07-09-25

Accident Details

Date
Sunday, December 13, 2020
NTSB Number
ERA21LA073
Location
Marion , NC
Event ID
20201213102411
Coordinates
35.720300, -82.014100
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
0
Total Aboard
2

Probable Cause and Findings

The pilot’s failure to maintain airplane control during takeoff, resulting in a rejected takeoff and runway excursion.

Aircraft Information

Registration
N138CT
Make
FLIGHT DESIGN
Serial Number
07-09-25
Engine Type
Reciprocating
Year Built
2007
Model / ICAO
CTSWFDCT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
GAHAGAN EDWARD L
Address
3383 HWY 63
Status
Deregistered
City
HOT SPRINGS
State / Zip Code
NC 28743
Country
United States

Analysis

On December 13, 2020, about 1045 eastern standard time, a Flight Design CTSW, N138CT, was substantially damaged when it was involved in an accident near Marion, North Carolina. The airline transport pilot and one passenger sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that all preflight operations were routine for the cross-country flight to Frankfort, Kentucky. Shortly after liftoff at an airspeed of about 46 knots, the airplane suddenly yawed to the right and came back down on the runway. The pilot elected to reject the takeoff, but the airplane continued to veer to the right. The airplane then departed the runway and entered an area of soft terrain. The nosewheel collapsed, and the airplane nosed over.

The pilot also reported that the takeoff gross weight was 1,310 pounds, which was 10 pounds below maximum gross weight for the airplane. He also reported that “something failed in the rudder.”

Postaccident examination of the airplane found that the nose gear had collapsed and was crushed into the lower fuselage. The vertical stabilizer and rudder were structurally damaged. Flight control continuity was established from the rudder to the cockpit rudder pedals. The pedals were jammed and would not move. Further examination revealed that the collapsed nose gear bent the rod between the rudder pedal assembly and the nose gear steering linkage. Otherwise, the rudder was free and clear with full travel available. Flight control continuity was also confirmed from the elevator and ailerons to the cockpit controls.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA21LA073