NTSB CAROL · Event
Event BFO94LA026
Registry · N41826
FAA Aircraft Registry record.
Make / Model
VELOCITY VELOCITY STANDARD RG
Year of manufacture
2005
Engine
LYCOMING HIO-360 SER (205 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20220414
ADS-B equipped
Yes — Mode-S A4F495
Registrant of record
TRULL STEPHEN G
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A FROZEN OIL LINE RESULTING IN THE STARVATION OF OIL TO THE ENGINE AND SUBSEQUENT LOSS OF ENGINE POWER. A RELATED FACTOR WAS THE UNSUITABLE TERRAIN FOR A FORCED LANDING.
Factual narrative
On Sunday, January 16, 1994, at 1215 eastern standard time, a Bellanca 8KCAB, N41826, collided with the ground while on final approach during a power-off forced landing at Middletown, Ohio. The certificated airline transport pilot, the sole occupant was not injured, while the airplane sustained substantial damage. The personal flight was being operated under 14 CFR 91, and originated in Moraine, Ohio. Visual meteorological conditions prevailed at the time and a flight plan was not filed. According to the pilot, during cruise flight at 2000 feet MSL he noticed both the oil temperature and oil pressure gages were indicating zero. He stated that he looked out of the airplane to see if there was any evidence of oil, but there was none. The pilot stated that he decided to return to the airport and not land sooner as he thought it "appeared to be only an indication problem. Within approximately 2 minutes engine rpm started decreasing slowly then engine started shaking violently. At that time I pulled mixture and picked the only field I thought I could make...The field was short with trees at both ends and plowed north/south. I attempted landing south but due to the shortness of the field I could not stop without hitting trees." The engine was removed to Moraine Aircraft in Moraine, Ohio, for further examination. The examination included removing the oil sump and accessory case. When the oil sump was removed and the oil was drained out of the oil hoses, there was evidence of water in the oil. The interior of the sump contained pieces of bearing material. The connecting rod on the number one cylinder separated at the large end resulting in the piston being jammed in the cylinder. When the accessory case was removed there was evidence of aluminum melting in the area of the bearing around the oil pump. According to the FAA aviation safety inspector, there was starvation of oil in the engine. DURING CRUISE FLIGHT AT 2000 FEET MSL, THE PILOT REPORTED THAT THE OIL TEMPERATURE AND PRESSURE GAGES SUDDENLY INDICATED ZERO. HE STATED THAT HE LOOKED ALONG THE SIDES OF THE AIRPLANE FOR ANY EVIDENCE OF OIL, BUT THERE WAS NONE. THE PILOT STATED THAT HE THOUGHT THIS MAY HAVE BEEN AN INDICATION PROBLEM, SO HE ELECTED TO RETURN TO THE AIRPORT. HE STATED THAT WITHIN TWO MINUTES OF THE ZERO INDICATION THE ENGINE STARTED TO VIBRATE VIOLENTLY. THE PILOT STATED THAT THERE WAS NO SUITABLE PLACE FOR A FORCED LANDING, SO HE LANDED IN A PLOWED FIELD AND COLLIDED WITH TREES DURING THE LANDING. THE ENGINE WAS REMOVED FOR FURTHER EXAMINATION. THE EXAMINATION INCLUDED THE REMOVAL OF THE OIL SUMP AND ACCESSORY CASE. WHEN THE OIL SUMP WAS REMOVED THERE WAS EVIDENCE OF BEARING MATERIAL IN THE SUMP AND ALSO THERE WAS WATER IN THE OIL THAT WAS DRAINED OUT OF THE OIL HOSES. THE CONNECTING ROD ON THE NUMBER ONE CYLINDER SEPARATED AT THE LARGE END RESULTING IN THE PISTON BEING JAMMED IN THE CYLINDER. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_BFO94LA026.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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