CHI89LA063

NTSB accident investigation · Beech 95-B-55 · Crothersville, IN · March 26, 1989

Accident · Minor injuriesLimited investigationFinal report
Date
March 26, 1989, 15:30 local (21:30 UTC)
Place
Crothersville, IN
Injuries
2 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N27WFBeech 95-B-55
Weather
Visual (VMC) · Dawn
Status
Completed · report July 11, 1990
Report
Approved by Office Director
FAA report
19890326004529A
Case key
14332

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

A failure of the engine due to a crankshaft counterweight failure. The pilot performed emergency procedures and executed a forced landing in an open field, where the aircraft encountered a large muddy area, bogged down and nosed over.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine power(total) - mech failure/malfCruise - normal
Eng assembly,crankshaft counterweights/vib damper - failure,totalCause
Maintenance,recordkeeping - poorPilot in command
Powerplant - failure,totalCause
Emergency procedure - performedPilot in command
Forced landingDescent - emergency
Nose overLanding - roll
Terrain condition - open fieldFactor
Terrain condition - wetFactor
Landing gear,nose gear - overload

Analysis

During a local pleasure flight, while in normal cruise, the right engine failed totally. The pilot reduced power on the left (operating) engine to 'curtail the violent vibration of the aircraft' and executed a forced landing in an open field. As the aircraft was rolling out after touchdown, it encountered a muddy area. The nose gear bogged down, then collapsed, and the aircraft nosed over. Post-accident examination of the right engine revealed that the pin retaining plate cut through the crankshaft counterweight, releasing it. Further examination revealed that the counterweights had not been 'tuftrided', a surface hardening process which prevents the pin retaining plate from cutting/wearing through the counterweight. This process has been required on new engines since 1968, and on rebuilt engines since 1973-74. The accident engine was rebuilt by the manufacturer in 1971. Logbook/maintenance information provided by the pilot was incomplete.

Aircraft

Registration
N27WF
Reported as
Beech 95-B-55
Category
Airplane
Serial number
TC-694
Airframe hours
4,645
Engine
Continental IO-470-L, 260 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Casebolt, Fon
Registered owner
Casebolt, Fon
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 18, 1988 · 50 hours before
Departed
BQM · Louisville, KY
Destination
BQM · Louisville, KY

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
52
Certificate
Private
Airplane ratings
Multi-engine land, Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
474 total · 137 in this make and model · 332 as pilot in command · 10 in the last 90 days · 2 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Dawn
Wind
160° at 10 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 52 °F
Altimeter
30.00 inHg
Observed at
LOU, 32 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.