20210506009299A

Accident · Substantial damage

FAA accident report · Piper PA-28-161 · Houston, TX · May 6, 2021

Date
May 6, 2021 · 17:07 local
Place
Houston, TX
Airport
David Wayne Hooks Memorial Air
Phase of flight
Landing: Rollout
Damage
Substantial damage
Aircraft
N54MC
NTSB investigation
NTSBCEN21LA211
Reported as
Piper PA-28-161
Reported engine
Lycoming O-320-D3G
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Flight instructor
Pilot’s flight hours
728 total45 in this make and model14 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On 5/06/2021 at around 4:30 local CST N54MC entered kdwh airspace for work in the traffic pattern. After the 3rd lap around they landed with the intent of going back to "the flight school".

After touchdown they started slowing down to exit the runway. As soon as they started slowing down, the engine shutdown. But they still had momentum to exit runway 35L on taxiway e. they exited the runway and came to a full stop and advised tower that their engine quit after landing and that they were going to attempt the restart.

During the restart, CFI was handling the restart due to the student being at low time and low experience. CFI treated the restart like a normal restart at first, but after the engine would not start, CFI attempted the vapor lock starting procedure. The engine began to start like normal and that is when CFI introduced fuel. Once he moved the mixture to rich, the aircraft cabin got extremely hot, and they began to see the flames.

At that moment, the student and CFI began evacuating the aircraft due to the smoke entering the cabin and the extreme heat they felt.

After evacuating they got to a safe distance from the aircraft and CFI called the flight school to get some help. Airport rescue and fire fighting was dispatched to extinguish fire. The electric fuel pump was left on after the fire began. The engine compartment was substantially damaged by the fire to include bottom engine cowling and surrounding areas. The engine mount and dampers were substantially damaged. The engine firewall was buckled from heat damage.

As the FAA filed it

ON 5/06/2021 AT AROUND 4:30 LOCAL CST N54MC ENTERED KDWH AIRSPACE FOR WORK IN THE TRAFFIC PATTERN. AFTER THE 3RD LAP AROUND THEY LANDED WITH THE INTENT OF GOING BACK TO "THE FLIGHT SCHOOL".

AFTER TOUCHDOWN THEY STARTED SLOWING DOWN TO EXIT THE RUNWAY. AS SOON AS THEY STARTED SLOWING DOWN, THE ENGINE SHUTDOWN. BUT THEY STILL HAD MOMENTUM TO EXIT RUNWAY 35L ON TAXIWAY E. THEY EXITED THE RUNWAY AND CAME TO A FULL STOP AND ADVISED TOWER THAT THEIR ENGINE QUIT AFTER LANDING AND THAT THEY WERE GOING TO ATTEMPT THE RESTART.

DURING THE RESTART, CFI WAS HANDLING THE RESTART DUE TO THE STUDENT BEING AT LOW TIME AND LOW EXPERIENCE. CFI TREATED THE RESTART LIKE A NORMAL RESTART AT FIRST, BUT AFTER THE ENGINE WOULD NOT START, CFI ATTEMPTED THE VAPOR LOCK STARTING PROCEDURE. THE ENGINE BEGAN TO START LIKE NORMAL AND THAT IS WHEN CFI INTRODUCED FUEL. ONCE HE MOVED THE MIXTURE TO RICH, THE AIRCRAFT CABIN GOT EXTREMELY HOT, AND THEY BEGAN TO SEE THE FLAMES.

AT THAT MOMENT, THE STUDENT AND CFI BEGAN EVACUATING THE AIRCRAFT DUE TO THE SMOKE ENTERING THE CABIN AND THE EXTREME HEAT THEY FELT.

AFTER EVACUATING THEY GOT TO A SAFE DISTANCE FROM THE AIRCRAFT AND CFI CALLED THE FLIGHT SCHOOL TO GET SOME HELP. AIRPORT RESCUE AND FIRE FIGHTING WAS DISPATCHED TO EXTINGUISH FIRE. THE ELECTRIC FUEL PUMP WAS LEFT ON AFTER THE FIRE BEGAN. THE ENGINE COMPARTMENT WAS SUBSTANTIALLY DAMAGED BY THE FIRE TO INCLUDE BOTTOM ENGINE COWLING AND SURROUNDING AREAS. THE ENGINE MOUNT AND DAMPERS WERE SUBSTANTIALLY DAMAGED. THE ENGINE FIREWALL WAS BUCKLED FROM HEAT DAMAGE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.