20260512005529A

Accident · Substantial damage

FAA accident report · Stinson 108-3 · Quilcene, WA · May 12, 2026

Date
May 12, 2026 · 10:50 local
Place
Quilcene, WA
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N588C
NTSB investigation
NTSBWPR26LA183
Reported as
Stinson 108-3
Reported engine
Franklin 6A4-165-B3
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
977 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.

At approximately 10:35 aircraft was southbound at 4000 feet AGL. While cruising at 2600 RPM pilot experienced sudden engine vibration and consequent engine power loss. Noise and vibration increased, smoke visible from engine, oil appeared on windshield, smoke entered cockpit. Pilot identified potential landing site as an open field and initiated approach to left pattern for southbound landing. Pilot lost sight of landing area on final due to oil on the windshield. Pilot maintained descent until flare, touchdown, applied brakes, and continued to decrease speed until the main tires decended into a shallow ditch and the plane came to rest causing damage to the empennage. Upon engine tear down inspection with NTSB, discovered holes in top of engine case and case cover. Number 3 piston missing from cylinder and found in pieces inside oil pan. Exhaust valve stem for #3 cylinder inside exhaust valve guide and majority of exhaust valve head found in oil pan.

As the FAA filed it

AT APPROXIMATELY 10:35 AIRCRAFT WAS SOUTHBOUND AT 4000 FEET AGL. WHILE CRUISING AT 2600 RPM PILOT EXPERIENCED SUDDEN ENGINE VIBRATION AND CONSEQUENT ENGINE POWER LOSS. NOISE AND VIBRATION INCREASED, SMOKE VISIBLE FROM ENGINE, OIL APPEARED ON WINDSHIELD, SMOKE ENTERED COCKPIT. PILOT IDENTIFIED POTENTIAL LANDING SITE AS AN OPEN FIELD AND INITIATED APPROACH TO LEFT PATTERN FOR SOUTHBOUND LANDING. PILOT LOST SIGHT OF LANDING AREA ON FINAL DUE TO OIL ON THE WINDSHIELD. PILOT MAINTAINED DESCENT UNTIL FLARE, TOUCHDOWN, APPLIED BRAKES, AND CONTINUED TO DECREASE SPEED UNTIL THE MAIN TIRES DECENDED INTO A SHALLOW DITCH AND THE PLANE CAME TO REST CAUSING DAMAGE TO THE EMPENNAGE. UPON ENGINE TEAR DOWN INSPECTION WITH NTSB, DISCOVERED HOLES IN TOP OF ENGINE CASE AND CASE COVER. NUMBER 3 PISTON MISSING FROM CYLINDER AND FOUND IN PIECES INSIDE OIL PAN. EXHAUST VALVE STEM FOR #3 CYLINDER INSIDE EXHAUST VALVE GUIDE AND MAJORITY OF EXHAUST VALVE HEAD FOUND IN OIL PAN.

NTSB investigation

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