N478WT

Substantial
None

PIPER PA-24-260S/N: 24-4634

Accident Details

Date
Monday, July 11, 2022
NTSB Number
CEN22LA313
Location
Rapid City, SD
Event ID
20220711105449
Coordinates
44.044227, -103.078790
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A total loss of engine power for reasons that could not be determined because the airplane was unavailable for examination.

Aircraft Information

Registration
Make
PIPER
Serial Number
24-4634
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
PA-24-260PA24
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
PA-24-260

Registered Owner (Current)

Name
BAS PART SALES LLC
Address
575 ED BEEGLES LN
City
GREELEY
State / Zip Code
CO 80631
Country
United States

Analysis

On July 10, 2022, about 1810 mountain daylight time, a Piper PA-24-260 airplane, N478WT, sustained substantial damage when it was involved in an accident near Rapid City, South Dakota. The pilot was uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he departed for an estimated 30-minute flight. When the airplane was about 6,000 ft above mean sea level, the engine lost all power. The pilot declared an emergency with air traffic control and stated that he needed to return to the airport. He subsequently switched fuel tanks and attempted multiple engine restarts, but power could not be restored. Unable to reach the runway, he performed a forced landing to a field, during which the airplane bounced, the right main landing gear collapsed, and the airplane slid until it came to rest upright, which resulted in substantial damage to the elevator. The pilot stated that, following the accident, he turned off the fuel selector to prevent a fire.

The pilot stated that the airplane had undergone an annual inspection about 2 days before the accident flight. Following the inspection, the pilot flew the airplane in the traffic pattern and then added 30 gallons of fuel to each main fuel tank for a total of 68 gallons of fuel on board the airplane. He said that it was his habit to start the flight with the left main fuel tank selected. When the engine lost power, he switched to the right main fuel tank for the restart attempts. He said that he did not use the auxiliary fuel tanks.

During a postaccident examination by the Federal Aviation Administration, fuel was drained from the left and right main fuel tanks as well as the right auxiliary fuel tank. When the left auxiliary fuel tank was checked, no fuel was present. No contaminants were found in any of the fuel samples.

A detailed engine examination could not be accomplished because the insurance company sold the wreckage before it was released by the National Transportation Safety Board.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN22LA313