20230118001569A

Accident · Substantial damage

FAA accident report · Piper PA-31-350 · Middlefield, OH · January 18, 2023

Date
January 18, 2023 · 09:30 local
Place
Middlefield, OH
Airport
Geauga County Airport
Phase of flight
Takeoff: Climb Out
Operating rules
Air taxi and commuter (Part 135)
Operator
EZ9A
Damage
Substantial damage
Aircraft
N101MA
NTSB investigation
NTSBERA23LA112
Reported as
Piper PA-31-350
Reported engine
Lycoming TI0-540 series
People aboard
6
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
9,275 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.

privacy data omitted Departed kyng (youngstown/ warren regional airport) enroute to kyip (willow run airport). During the climb around 6000 feet the pilot noticed oil coming out of the right engine cowling. At around 7000 feet the right engine began to run rough. Pilot elected to shut down and secure the engine. The pilot then declared an emergency and asked ATC for vectors to the nearest airport. ATC vectored the aircraft for the rnav/gps runway 11 at Geauga County Airport (7G8). The pilot performed the approach with the gear down and flaps up to ensure the aircraft was under control. Pilot states that the approach speed was around 120 knots. Normal blue line speed is approximately 108 knots until short final then slowing to around 90 knots. With the right engine propeller feathered and zero flaps the increased airspeed caused the aircraft to touch down hard and likely long. The aircraft was unable to stop on the remaining portion of the 3500 foot runway. Aircraft left the paved runway surface and traveled about 700 feet past the end into a farm field. The landing gear collapsed and damage occurred to the left wing, nose and left engine propeller. The right engine cowling had oil covering a good portion of the cowling from the front to at least mid way back. Visual inspection through the oil dipstick door oil was covering the top of the engine case. Closer inspection after the aircraft was recovered revealed a crack in the engine case just above the number 5 cylinder. The r/h engine was disassmebled and the determining factor was that the number 5 cylinder was experiencing detonation which burned a hole in the pistion. The hole in the piston allowed compressed cylinder gases to enter the engine case which cause the front seal to blow out and created the oil leak. The number 5 connecting rod siezed and broke due to oil starvation. When the connecting rod broke it cracked the engine case above the number 5 cylinder. The pilot and 5 passengers were uninjured.

As the FAA filed it

^PRIVACY DATA OMITTED^ DEPARTED KYNG (YOUNGSTOWN/ WARREN REGIONAL AIRPORT) ENROUTE TO KYIP (WILLOW RUN AIRPORT). DURING THE CLIMB AROUND 6000 FEET THE PILOT NOTICED OIL COMING OUT OF THE RIGHT ENGINE COWLING. AT AROUND 7000 FEET THE RIGHT ENGINE BEGAN TO RUN ROUGH. PILOT ELECTED TO SHUT DOWN AND SECURE THE ENGINE. THE PILOT THEN DECLARED AN EMERGENCY AND ASKED ATC FOR VECTORS TO THE NEAREST AIRPORT. ATC VECTORED THE AIRCRAFT FOR THE RNAV/GPS RUNWAY 11 AT GEAUGA COUNTY AIRPORT (7G8). THE PILOT PERFORMED THE APPROACH WITH THE GEAR DOWN AND FLAPS UP TO ENSURE THE AIRCRAFT WAS UNDER CONTROL. PILOT STATES THAT THE APPROACH SPEED WAS AROUND 120 KNOTS. NORMAL BLUE LINE SPEED IS APPROXIMATELY 108 KNOTS UNTIL SHORT FINAL THEN SLOWING TO AROUND 90 KNOTS. WITH THE RIGHT ENGINE PROPELLER FEATHERED AND ZERO FLAPS THE INCREASED AIRSPEED CAUSED THE AIRCRAFT TO TOUCH DOWN HARD AND LIKELY LONG. THE AIRCRAFT WAS UNABLE TO STOP ON THE REMAINING PORTION OF THE 3500 FOOT RUNWAY. AIRCRAFT LEFT THE PAVED RUNWAY SURFACE AND TRAVELED ABOUT 700 FEET PAST THE END INTO A FARM FIELD. THE LANDING GEAR COLLAPSED AND DAMAGE OCCURRED TO THE LEFT WING, NOSE AND LEFT ENGINE PROPELLER. THE RIGHT ENGINE COWLING HAD OIL COVERING A GOOD PORTION OF THE COWLING FROM THE FRONT TO AT LEAST MID WAY BACK. VISUAL INSPECTION THROUGH THE OIL DIPSTICK DOOR OIL WAS COVERING THE TOP OF THE ENGINE CASE. CLOSER INSPECTION AFTER THE AIRCRAFT WAS RECOVERED REVEALED A CRACK IN THE ENGINE CASE JUST ABOVE THE NUMBER 5 CYLINDER. THE R/H ENGINE WAS DISASSMEBLED AND THE DETERMINING FACTOR WAS THAT THE NUMBER 5 CYLINDER WAS EXPERIENCING DETONATION WHICH BURNED A HOLE IN THE PISTION. THE HOLE IN THE PISTON ALLOWED COMPRESSED CYLINDER GASES TO ENTER THE ENGINE CASE WHICH CAUSE THE FRONT SEAL TO BLOW OUT AND CREATED THE OIL LEAK. THE NUMBER 5 CONNECTING ROD SIEZED AND BROKE DUE TO OIL STARVATION. WHEN THE CONNECTING ROD BROKE IT CRACKED THE ENGINE CASE ABOVE THE NUMBER 5 CYLINDER. THE PILOT AND 5 PASSENGERS WERE UNINJURED.

NTSB investigation

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

Other reports on N101MA · 1

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