20190906012739A

Accident · Destroyed

FAA accident report · Piper PA-18-150 · Hood River, OR · September 6, 2019

Date
September 6, 2019 · 10:10 local
Place
Hood River, OR
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N14365
NTSB investigation
NTSBWPR19FA251
Reported as
Piper PA-18-150
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor

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.

PIC was departing runway 25 at 4S2 on a VFR instructional flight in N14365, a PA-18-150, on 09-06-2019 at 1010 local time. Witnesses report that this was the second time around the pattern. PIC was seated in the rear seat, and the other pilot was seated in the front seat undergoing a flight review. Shortly after departure at approximately 100 feet AGL, aircraft lost power and entered a stall / spin impacting the ground between the runway extended centerline and parallel taxiway. Both occupants were killed and the aircraft was destroyed. Post-accident investigation indicated no abnormalities with the airframe or engine. The fuel shutoff valve was in one of two ?off? Positions at the time of impact, and no fuel was present in the carburetor.

As the FAA filed it

PIC WAS DEPARTING RUNWAY 25 AT 4S2 ON A VFR INSTRUCTIONAL FLIGHT IN N14365, A PA-18-150, ON 09-06-2019 AT 1010 LOCAL TIME. WITNESSES REPORT THAT THIS WAS THE SECOND TIME AROUND THE PATTERN. PIC WAS SEATED IN THE REAR SEAT, AND THE OTHER PILOT WAS SEATED IN THE FRONT SEAT UNDERGOING A FLIGHT REVIEW. SHORTLY AFTER DEPARTURE AT APPROXIMATELY 100 FEET AGL, AIRCRAFT LOST POWER AND ENTERED A STALL / SPIN IMPACTING THE GROUND BETWEEN THE RUNWAY EXTENDED CENTERLINE AND PARALLEL TAXIWAY. BOTH OCCUPANTS WERE KILLED AND THE AIRCRAFT WAS DESTROYED. POST-ACCIDENT INVESTIGATION INDICATED NO ABNORMALITIES WITH THE AIRFRAME OR ENGINE. THE FUEL SHUTOFF VALVE WAS IN ONE OF TWO ?OFF? POSITIONS AT THE TIME OF IMPACT, AND NO FUEL WAS PRESENT IN THE CARBURETOR.

NTSB investigation

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