20230418008769I

Incident · Minor damage

FAA incident report · Piper PA-28-140 · Annada, MO · April 18, 2023

Date
April 18, 2023 · 17:45 local
Place
Annada, MO
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N9530W
Reported as
Piper PA-28-140
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
86 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.

Pilot flying one passenger experienced an engine failure. Pilot successfully completed a forced landing in a field. Aircraft rolled to a stop where both pilot and passenger exited the aircraft safely.

The incident investigation revealed minor airframe damage consisting of scratches to the inboard right wing, lower skin panels. The engine #3 cylinder seperated from the engine case and was slammed into the right-side engine cowling. The right-side cowling was bowed outward from the impact of the cylinder. All 4 cylinder retainer boltes were sheared. The case aft of the #3 cylinder was fractured and broken out. The pistion was found at the bottom of the engine cowling with the piston pin broken out and missing.

As the FAA filed it

PILOT FLYING ONE PASSENGER EXPERIENCED AN ENGINE FAILURE. PILOT SUCCESSFULLY COMPLETED A FORCED LANDING IN A FIELD. AIRCRAFT ROLLED TO A STOP WHERE BOTH PILOT AND PASSENGER EXITED THE AIRCRAFT SAFELY.

THE INCIDENT INVESTIGATION REVEALED MINOR AIRFRAME DAMAGE CONSISTING OF SCRATCHES TO THE INBOARD RIGHT WING, LOWER SKIN PANELS. THE ENGINE #3 CYLINDER SEPERATED FROM THE ENGINE CASE AND WAS SLAMMED INTO THE RIGHT-SIDE ENGINE COWLING. THE RIGHT-SIDE COWLING WAS BOWED OUTWARD FROM THE IMPACT OF THE CYLINDER. ALL 4 CYLINDER RETAINER BOLTES WERE SHEARED. THE CASE AFT OF THE #3 CYLINDER WAS FRACTURED AND BROKEN OUT. THE PISTION WAS FOUND AT THE BOTTOM OF THE ENGINE COWLING WITH THE PISTON PIN BROKEN OUT AND MISSING.