20220213001889I

Incident · Minor damage

FAA incident report · Piper PA-25-235 · Tuscon, AZ · February 13, 2022

Date
February 13, 2022 · 12:45 local
Place
Tuscon, AZ
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N9815P
Reported as
Piper PA-25-235
Reported engine
Lycoming 0-540 series
People aboard
1
Fatal injuries
0
Other injuries
0

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.

The pilot said he had a normal acceleration and lift off . At approximately 150' AGL the engine lost power, and dropped RPM to approximately 200-300 RPM. No prior warning or rough running engine or any indications prior to that moment. Once identified, the pilot verified throttle and mixture controls full forward, aux fuel pump on, and realized that there was not going to be a restoration of power, the aircraft impacted a burm and a ditch, and the airplane came forward on the nose and then to a stop. The engine was sputtering at time of impact.

As the FAA filed it

THE PILOT SAID HE HAD A NORMAL ACCELERATION AND LIFT OFF . AT APPROXIMATELY 150' AGL THE ENGINE LOST POWER, AND DROPPED RPM TO APPROXIMATELY 200-300 RPM. NO PRIOR WARNING OR ROUGH RUNNING ENGINE OR ANY INDICATIONS PRIOR TO THAT MOMENT. ONCE IDENTIFIED, THE PILOT VERIFIED THROTTLE AND MIXTURE CONTROLS FULL FORWARD, AUX FUEL PUMP ON, AND REALIZED THAT THERE WAS NOT GOING TO BE A RESTORATION OF POWER, THE AIRCRAFT IMPACTED A BURM AND A DITCH, AND THE AIRPLANE CAME FORWARD ON THE NOSE AND THEN TO A STOP. THE ENGINE WAS SPUTTERING AT TIME OF IMPACT.