20040709026469A

Accident · Substantial damage

FAA accident report · Beech N35 · Austin, MN · July 9, 2004

Date
July 9, 2004 · 13:00 local
Place
Austin, MN
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N80HL
NTSB investigation
NTSBCHI04LA181
Reported as
Beech N35
Reported engine
Continental IO470*
People aboard
4
Fatal injuries
0
Pilot’s flight hours
875 total450 in this make and model41 in the last 90 days

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.

(-23) Aircraft in cruise flight when engine suddenly oversped. Pilot was unable to control RPM with the propeller control. Prop RPM stabilized at 2500 RPM with throttle reduction to 15 inches map. Pilot noted an oil pressure indication of zero. Approximately 30 seconds later, aircraft began to shake; white smoke entered the cabin, and oil appeared on the windshield. After onset of airframe shaking, the pilot sensed that all power was lost. He subsequently secured the engined by pulling the mixture control to idle cutoff. Unable to make it to an airport, the pilot chose a field and maneuvered for an emergency landing. The field was muddy. Pilot landed gear-up.

As the FAA filed it

(-23) AIRCRAFT IN CRUISE FLIGHT WHEN ENGINE SUDDENLY OVERSPED. PILOT WAS UNABLE TO CONTROL RPM WITH THE PROPELLER CONTROL. PROP RPM STABILIZED AT 2500 RPM WITH THROTTLE REDUCTION TO 15 INCHES MAP. PILOT NOTED AN OIL PRESSURE INDICATION OF ZERO. APPROXIMATELY 30 SECONDS LATER, AIRCRAFT BEGAN TO SHAKE; WHITE SMOKE ENTERED THE CABIN, AND OIL APPEARED ON THE WINDSHIELD. AFTER ONSET OF AIRFRAME SHAKING, THE PILOT SENSED THAT ALL POWER WAS LOST. HE SUBSEQUENTLY SECURED THE ENGINED BY PULLING THE MIXTURE CONTROL TO IDLE CUTOFF. UNABLE TO MAKE IT TO AN AIRPORT, THE PILOT CHOSE A FIELD AND MANEUVERED FOR AN EMERGENCY LANDING. THE FIELD WAS MUDDY. PILOT LANDED GEAR-UP.

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 N80HL · 2

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