19951025034459A

Accident · Substantial damage

FAA accident report · Cessna 170B · Oconomowoc, WI · October 25, 1995

Date
October 25, 1995 · 09:00 local
Place
Oconomowoc, WI
Airport
Oconomowoc Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4555C
NTSB investigation
NTSBCHI96LA016
Reported as
Cessna 170B
Reported engine
Continental O300A
Fatal injuries
0

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.

Lost power on climb from touch and go. Landed straight ahead into corn and nosed over. Cause power loss unknown. (-23) while performing a touch and go landing the pilot stated he applied throttle and became airborne. He stated the engine only developed 1000 RPM. The aircraft loss altitude and airspeed, landed in a corn field and flipped over on its back, 1/4 mile from the end of the runway. Investigation did not reveal any discrepancies with the engine or its related systems. Engine was run on the aircraft and developed 1950-2000 RPM at full throttle even though accident damage ignition leads were intermittently shorting out.

As the FAA filed it

LOST POWER ON CLIMB FROM TOUCH AND GO. LANDED STRAIGHT AHEAD INTO CORN AND NOSED OVER. CAUSE POWER LOSS UNKNOWN. (-23) WHILE PERFORMING A TOUCH AND GO LANDING THE PILOT STATED HE APPLIED THROTTLE AND BECAME AIRBORNE. HE STATED THE ENGINE ONLY DEVELOPED 1000 RPM. THE AIRCRAFT LOSS ALTITUDE AND AIRSPEED, LANDED IN A CORN FIELD AND FLIPPED OVER ON ITS BACK, 1/4 MILE FROM THE END OF THE RUNWAY. INVESTIGATION DID NOT REVEAL ANY DISCREPANCIES WITH THE ENGINE OR ITS RELATED SYSTEMS. ENGINE WAS RUN ON THE AIRCRAFT AND DEVELOPED 1950-2000 RPM AT FULL THROTTLE EVEN THOUGH ACCIDENT DAMAGE IGNITION LEADS WERE INTERMITTENTLY SHORTING OUT.

NTSB investigation

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