N720TX

Substantial
None

CIRRUS DESIGN CORP SR20S/N: 1564

Accident Details

Date
Friday, November 6, 2020
NTSB Number
CEN21LA108
Location
Fort Worth, TX
Event ID
20210104102489
Coordinates
32.985303, -97.318095
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A failure of the nose wheel landing strut for reasons that could not be determined based on available information.

Aircraft Information

Registration
Make
CIRRUS DESIGN CORP
Serial Number
1564
Engine Type
Reciprocating
Year Built
2005
Model / ICAO
SR20SR20
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
SR20

Registered Owner (Current)

Name
C A ROB CO LLC
Address
15841 ADDISON RD
City
ADDISON
State / Zip Code
TX 75501
Country
United States

Analysis

On November 5, 2020, at 2233 central standard time, a Cirrus SR20 airplane, N720TX, was substantially damaged when it was involved in an accident near Fort Worth, Texas. The flight instructor and student pilot were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

The flight instructor and the student pilot were conducting touch-and-go takeoffs and landings to runway 16R. After the airplane touched down, the nose of the airplane came down and the nose landing gear collapsed. The airplane came to rest on the runway.

Examination of the airplane by a Federal Aviation Administration (FAA) inspector revealed substantial damage to the firewall and lower composite structure. The nose landing gear tire was flat, and the nose landing gear strut was separated at the top of the assembly.

A video provided by the flight instructor, which recorded the landing, showed that the accident landing was not a hard landing. The airplane touched down and as the nose of the airplane came down and contacted the runway, a sound consistent with a flat tire could be heard, followed by the subsequent nose landing gear collapse.

According to the FAA inspector, the airplane had experienced a hard landing about 2 months before the accident landing. The operator completed the Cirrus Hard/Overweight Landing maintenance checklist and subsequently returned the airplane to service. The accident landing was the fourth landing following the return to service.

The nose landing gear strut assembly was not retained by the operator and submitted for metallurgical examination. Pictures of the fracture surface were inconclusive.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21LA108