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NTSB Report

June 15, 1998 · Bellanca 17-31A · N39853

Millry, AL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 15, 1998
Injury Outcomes
No injuries (1 uninjured)
Location
Millry, AL
Aircraft
Bellanca 17-31A
Tail Number
N39853
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ATL98LA084

While in cruise flight, the airplane engine's #2 cylinder connecting rod suffered a fracture. This resulted in the #2 piston becoming jammed in the cylinder and bending of the #2 cylinder intake valve pushrod. These events resulted in partial loss of engine power and a forced reduction in power setting. The pilot performed an emergency landing whereon the landing roll, the airplane skidded and turned in efforts to avoid a collision with a tree/fence row. The turn resulted in a collapse of the right main landing gear and right wing collision with the terrain. The landing gear broke off the aircraft, punctured the right main fuel cell, broke the main right wing wood spar and bent the right fuselage stringers. The outboard 36' of main right wing was severed from the airframe.

NTSB Probable Cause

The fracture of the #2 cylinder connecting rod which resulted in partial loss of engine power and subsequent forced landing. A factor in the accident was the rough terrain.

Full Narrative

On June 15, 1998, about 1755 Central Daylight Time, a Bellanca BL-17-31A, N39853, collided with terrain during a forced landing near Millry, Alabama. The airplane was operated by the pilot under the provisions of Title 14 CFR Part 91, and visual flight rules. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight. The private pilot and sole occupant was not injured, and the airplane sustained substantial damage. The flight originated from Dekalb-Peachtree Airport in Atlanta, Georgia at 1645 Eastern Daylight Time for Corpus Christi, Texas. According to the pilot, while in cruise flight, the engine noise changed as the engine appeared to lose 15 to 30 percent of its power. According to the pilot, a moderate vibration began a few seconds later causing him to reduce power to idle and execute a forced landing. Upon landing, the pilot stated, "the field had lots of washboard effect." According to Federal Aviation Administration (FAA) inspectors who examined the wreckage, the airplane skidded approximately 300-320 yards upon landing. In an attempt to avoid a collision with a tree/fence row, the pilot attempted to turn the aircraft to the left. Inspector's noted the right main landing gear collapsed, the right main fuel cell punctured, main right wing wood spar broken at the fuselage attachment point, bending of the right fuselage stringers and 36" of the right wingtip was torn from the airframe. Examination of the aircraft engine revealed a fractured #2 cylinder connecting rod, #2 piston jammed in the cylinder and a bent #2 cylinder intake valve pushrod.

Flight

Event TypeAccident
Event Time17:55 CDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBellanca 17-31A
Tail NumberN39853
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · IO-540-K1E5 · Reciprocating · 300
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 54 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind210° @ 14 kt, gusting 20 kt
Visibility10 sm
CeilingNone
Altimeter29.00 inHg
Observation Time22:56
Weather SourceWFAC

Appendix: Source Data