N54MC

Substantial
None

PIPER PA-28-161S/N: 28-7816208

Accident Details

Date
Thursday, May 6, 2021
NTSB Number
CEN21LA211
Location
Spring, TX
Event ID
20210510103051
Coordinates
30.061779, -95.552788
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

An engine fire that resulted from a fuel leak into the carburetor air box due to the electric fuel pump over-pressurizing the carburetor needle/seat assembly. Contributing to the severity of the fire was the flight instructor’s failure to turn off the electric fuel pump before exiting the airplane.

Aircraft Information

Registration
N54MC
Make
PIPER
Serial Number
28-7816208
Engine Type
Reciprocating
Year Built
1977
Model / ICAO
PA-28-161P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HOFFMAN AVIATION SERVICES LLC
Address
38110 DONIGAN RD
Status
Deregistered
City
BROOKSHIRE
State / Zip Code
TX 77423-8784
Country
United States

Analysis

On May 6, 2021, about 1707 central daylight time, a Piper PA-28 airplane, N54MC, was

substantially damaged when it was involved in an accident at David Wayne Hooks Memorial Airport (DWH), Spring, 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.

During landing rollout, the flight instructor noticed a loss of engine power. After exiting the runway, the flight instructor was able to restart the engine on the second attempt. The flight instructor and student pilot subsequently noticed a fire that produced smoke and extreme heat in the cabin compartment. The flight crew shut the engine off and egressed the airplane. The electric fuel pump was turned on before landing, which is normal operating procedure, and remained on after the fire was observed and when the flight crew egressed the airplane. Per the emergency procedures checklist, it should have been turned off. The fire substantially damaged the engine mount and firewall before airport fire department personnel were able to extinguish it.

Postaccident examination revealed that fuel leaked from the carburetor into the air box when the electric fuel pump was turned on. Carburetor disassembly by a carburetor repair station revealed no anomalies with the needle/seat assembly, mixture control shaft, nozzle, idle tube, accelerator pump, or throttle lever. Repair station personnel noted that if the electric fuel pump pressure is greater than 6 pounds per square inch, the carburetor needle/seat assembly will allow fuel to enter the carburetor bowl and overflow into the air box.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21LA211