N1488

Substantial
None

THORP T 18S/N: 303

Accident Details

Date
Friday, November 6, 2015
NTSB Number
WPR16LA023
Location
Independence, OR
Event ID
20151107X72135
Coordinates
44.836666, -123.200836
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A separation of the canopy mechanism during flight, which resulted in the pilot’s precautionary landing and the airplane’s subsequent collision with a fence post.

Aircraft Information

Registration
Make
THORP
Serial Number
303
Engine Type
Reciprocating
Model / ICAO
T 18T18
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
T-18

Registered Owner (Current)

Name
BOOTH MAC E
Address
835 AIRPORT RD
City
INDEPENDENCE
State / Zip Code
OR 97351-9632
Country
United States

Analysis

On November 6, 2015, at 1530 Pacific standard time, an experimental Thorp T-18, N1488, was substantially damaged during a precautionary landing in a field near Independence State Airport, Independence, Oregon. The pilot was operating the airplane under the provisions of 14 Code of Federal Regulations Part 91. The private pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed and no flight plan was filed.

In a phone interview following the accident, the pilot stated that the airplane was climbing after takeoff when the canopy partially disconnected from the airplane and the airplane violently vibrated. The pilot landed in a cow pasture and the right wing impacted a fence post during the landing roll. He further reported that the airplane was serial number 303 and his father had built the airplane. The airplane had an early canopy design that had been modified in later designs. The canopy ran on a track. On each side of the canopy there are two fiberglass rollers and the back was secured through a track. The rear track separated and allowed airflow underneath to lift up and vibrate the canopy. The pilot believed that the separation occurred due to repeated use over time.

A Federal Aviation Administration (FAA) inspector examined the airplane following the accident. The canopy mechanism allowed the canopy to move fore and aft, as well as retain the aft portion of the canopy during flight. The rear portion of the mechanism separated at a weld.

The Thorp T-18 type club was contacted regarding the canopy mechanism design. The mechanism was reported as a unique design and uncommon to the fleet.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR16LA023