N731FL

Substantial
Serious

PITTS S-1TS/N: 1061

Accident Details

Date
Thursday, February 17, 2022
NTSB Number
CEN22LA123
Location
Spring, TX
Event ID
20220217104664
Coordinates
30.053099, -95.551847
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The failure of maintenance personnel to properly connect the throttle cable, which led to the pilot’s inability to control engine power during the initial climb. Contributing to the accident was the pilot’s misjudgment of the headwind during the forced landing, which resulted in the airplane’s touchdown short of the runway and its impact with airport structures.

Aircraft Information

Registration
Make
PITTS
Serial Number
1061
Engine Type
Reciprocating
Year Built
2007
Model / ICAO
S-1TPTMS
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
S-1T

Registered Owner (Current)

Name
LIBRINO FILIPPO
Address
17502 FOREST VINE CT
City
TOMBALL
State / Zip Code
TX 77377-8139
Country
United States

Analysis

On February 17, 2022, about 1448 central standard time, a Pitt S-1T, N731FL, was substantially damaged when it was involved in an accident at David Wayne Hooks Memorial Airport (DWH), Spring, Texas. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that, after departure from DWH, he noticed that engine power was not responding to throttle movements. The pilot turned back toward DWH and entered a left downwind leg to runway 35L. During the base turn and after turning off the engine ignition switch, the pilot executed a forced landing. Due to a higher-than-anticipated headwind, the pilot misjudged the flight profile, and the airplane landed before reaching runway 35L. The airplane impacted instrument landing system structures, which substantially damaged both wings, the fuselage, and the empennage.

Postaccident examination revealed that the throttle cable was disconnected from the throttle lever arm at the fuel injector/control, and a loose washer was found at the bottom of the engine cowling. Proper installation of the throttle lever included a bolt, two washers, a castellated nut, and a cotter pin. The bolt, castellated nut, and cotter pin were not located.

During the airplane’s last annual inspection, the engine fuel nozzles, fuel injector, and flow divider were removed for overhaul and were then reinstalled. During this maintenance, the throttle cable would have been disconnected, and it should have been reconnected once the maintenance was completed. After the annual inspection, no maintenance actions were recorded or reported that would have required the throttle cable to be disconnected.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA123