MIA02LA147

NTSB accident investigation · Bellanca 17-31A · Gainesboro, TN · August 10, 2002

Accident · Minor injuriesLimited investigationFinal report
Date
August 10, 2002, 11:08 local (16:08 UTC)
Place
Gainesboro, TN
Injuries
2 minor
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N39835Bellanca 17-31A
Weather
Visual (VMC) · Day
Status
Completed · report July 23, 2003
Report
Approved by Office Director
Parties
FAA
FAA report
20020810023559A
Case key
55445

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

On this page

Probable cause

a total loss of engine power due to the failure of the main bearing, a loss of oil pressure and the seizure of a connecting rod, resulting in damage to the airplane during the subsequent forced landing.

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
Engine assembly,bearing - failureCause
Lubricating system - no pressure
Engine assembly,connecting rod - seized
Engine assembly,cylinder - separation
Forced landingEmergency descent/landing
In flight collision with objectEmergency descent/landing
Object - fence
Object - fence post

Analysis

At an altitude of 3,500 feet, the airplane's engine began vibrating. The pilot said he was unable to maintain altitude and at about 1,800 feet the engine stopped operating. On approach to an open field the landing gear impacted a barbwire fence, collapsed, and the right wing hit a post, causing the airplane to veer to the right before coming to rest. Examination of the wreckage revealed that the number 3 cylinder was pushed away from the case. The cylinder studs were stripped as though the nuts had been force off without rotating. An engine teardown revealed that a main bearing on the crankshaft journal had spun; causing a reduction in forced oil lubrication, and seized the connecting rod, which forced the cylinder away for the case. The cause of the spun main bearing, which forced the cylinder displacement, was not determined.

Factual narrative

On August 10, 2002, about 1108 central daylight time, a Bellanca 17-31A, N39835, operated by a private individual as a Title 14 CFR Part 91 personal flight, struck a fence during a forced landing near Gainesboro, Tennessee. Visual meteorological conditions prevailed. No flight plan was filed. The airplane was substantially damaged. The private-rated pilot and one passenger received minor injuries. The flight had originated from the Jackson County Airport, near Gainesboro, Tennessee, about 1040, en route to Somerset, Kentucky.

The pilot stated that he was cruising at about 3,500 feet when the airplane's engine began vibrating. He said he looked at the engine instruments but found no abnormal indications. He further stated that he attempted to return to the Jackson County Airport, but was unable to maintain altitude and at about 1,800 feet the engine stopped operating. He said he approached an open field, and was about to land when the landing gear impacted a barbwire fence and collapsed. The right wing then hit a post and the airplane veered to the right before coming to rest. The accident site was about ten miles west north west of the airport.

According to the FAA inspector's statement, examination of the wreckage revealed that the airplane was lying on its belly with the landing gear torn loose. The fuel caps were removed, the fuel tanks all showed "fuel was available," and the fuel appeared blue. The fuel selector was checked and it indicated that fuel was being drawn from the left wing. The primary fuel valve was found "on main." The engine cowling was removed and number 3 cylinder was pushed away from the case. The cylinder studs were stripped as though the nuts had been "force off without rotating." Oil had blown through the cowling area. The oil filter and oil filler cap was in place and no other catastrophic damage noted. The propeller was slightly bent aft on two blades. Atlanta Air Salvage. Inc., Griffin, Georgia, conducted an engine teardown, which revealed that a main bearing on the crankshaft journal had spun; causing a reduction in forced oil lubrication, and seized the connecting rod, which forced the cylinder away for the case. The cause of the spun main bearing, which forced the cylinder displacement, was not determined.

Aircraft

Registration
N39835
Reported as
Bellanca 17-31A
Category
Airplane
Serial number
73-32-96
Airframe hours
2,029
Engine
Lycoming IO-540-K1E5, 300 hp, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Robert C. Perry
Airworthiness certificate
Standard, Normal
Last inspection
Annual · February 1, 2002 · 79 hours before
Departed
1A7 · Gainesboro, TN
Destination
SME · Somerset, 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
53
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
May 20, 2001
Seat
Left
Flight hours
139 total · 48 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
230° at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
82 °F, dew point 66 °F
Altimeter
30.06 inHg
Observed at
SME, 52 nm away

Docket · 7

The files NTSB released with the investigation on June 3, 2003, on NTSB’s docket system: statements, records, photos and specialists’ reports. 999 KB in all.

FAA reports on this event · 1

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