ATL92LA010

NTSB accident investigation · Beech A36 · Selma, AL · October 17, 1991

Accident · Minor injuriesLimited investigationFinal report
Date
October 17, 1991, 16:45 local (21:45 UTC)
Place
Selma, AL
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N3735YBeech A36
Weather
Visual (VMC) · Day
Status
Completed · report July 14, 1993
Report
Approved by Office Director
FAA report
19911017046849A
Case key
8537

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

The fatigue failure of the engine crankshaft counterweight blade, which resulted from excessive wear of the counterweight pin bushings, due to corrosion from an unknown source.

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/malfApproach - vfr pattern - final approach
Eng assembly,crankshaft counterweights/vib damper - corrodedCause
Eng assembly,crankshaft counterweights/vib damper - fatigueCause
Eng assembly,crankshaft counterweights/vib damper - previous damageCause
Forced landingCruise
Planned approach - improperPilot in commandFactor
On ground/water encounter with terrain/waterLanding - roll

Analysis

During cruise flight, the engine RPM decreased, momentarily. The pilot landed and a mechanic checked the engine. No anomalies were found. A post maintenance flight, in the landing pattern, was flown to verify engine operation. On final approach, the engine quit, and the airplane was landed in rough terrain short of the runway. Examination of the engine revealed that the number 2 check counterweight blade was fractured. Metallurgical examination discovered corrosion pitting on the inner diameter of the counterweight pin bushings, as well as excessive inner diameter wear. The counterweight blade fracture exhibited evidence of fatigue. A log book entry indicated that the engine had been previously disassembled for examination following a lightning strike. There was no record of an engine overhaul. The safety board believes that the counterweight failed in fatigue, because of previous pitting damage to the bushings, from an unknown source.

Aircraft

Registration
N3735Y
Reported as
Beech A36
Category
Airplane
Serial number
E-1767
Airframe hours
3,070
Engine
Continental IO-520-BB, 285 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Gray, Thomas L.
Registered owner
Gray, Thomas L.
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 17, 1991 · 68 hours before
Airport
SEM · Craig Field, runway 14, 8,002 × 150 ft, asphalt

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
31
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
358 total · 155 in this make and model · 271 as pilot in command · 52 in the last 90 days · 24 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
10 statute miles
Lowest ceiling
None
Temperature
75 °F
Altimeter
30.00 inHg

FAA reports on this event · 1

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

Other investigations on N3735Y · 1

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