20251011020609I

Incident · Minor damage

FAA incident report · Cessna 150M · Windsor Locks, CT · October 11, 2025

Date
October 11, 2025 · 11:51 local
Place
Windsor Locks, CT
Airport
Bradley International Arport
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N63079
Reported as
Cessna 150M
Reported engine
Continental 17020
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
790 total

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 mishap aircraft was on the second leg of a cross country flight with a single occupant. Afer taking on fuel at baf, the aircraft departed for 47N. While climbing out through 2500 MSL, the aircraft engine suffered catastrophic failure of cylinder number 4. The upper section of the cylinder barrel seperated from the lower section approximately four inches above the cylinder flange. This also caused catastrophic destruction of the number four piston and bending of the number four pushrod. The severe vibration caused the pilot to shut down the engine within gliding distance of bdl. The pilot declared an emergency and completed a successful engine out landing. There were no injuries reported.

As the FAA filed it

THE MISHAP AIRCRAFT WAS ON THE SECOND LEG OF A CROSS COUNTRY FLIGHT WITH A SINGLE OCCUPANT. AFER TAKING ON FUEL AT BAF, THE AIRCRAFT DEPARTED FOR 47N. WHILE CLIMBING OUT THROUGH 2500 MSL, THE AIRCRAFT ENGINE SUFFERED CATASTROPHIC FAILURE OF CYLINDER NUMBER 4. THE UPPER SECTION OF THE CYLINDER BARREL SEPERATED FROM THE LOWER SECTION APPROXIMATELY FOUR INCHES ABOVE THE CYLINDER FLANGE. THIS ALSO CAUSED CATASTROPHIC DESTRUCTION OF THE NUMBER FOUR PISTON AND BENDING OF THE NUMBER FOUR PUSHROD. THE SEVERE VIBRATION CAUSED THE PILOT TO SHUT DOWN THE ENGINE WITHIN GLIDING DISTANCE OF BDL. THE PILOT DECLARED AN EMERGENCY AND COMPLETED A SUCCESSFUL ENGINE OUT LANDING. THERE WERE NO INJURIES REPORTED.

Other reports on N63079 · 1

Matched to the same aircraft by N-number and date.