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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

June 9, 2000 · Stewart S-51 · N51FY

Forty Fort, PA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 9, 2000
Injury Outcomes
1 injury (1 minor injury)
Location
Forty Fort, PA
Aircraft
Stewart S-51
Tail Number
N51FY
Operator
Frank Yamrick
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
NYC00LA156

During takeoff, approximately 150 above the ground, the propeller reduction gearbox input shaft failed, and the airplane lost all power. The pilot performed a forced landing to a field where the airplane struck a fence. After reviewing the wreckage, the pilot stated that he machined his own shaft for the home built airplane. He stated that he machined the shaft too thin, and after about 150 hours of operation, it failed at its weakest point. The kit manufacturer stated that the production model shafts are larger, and used aviation splines, whereas the accident airplane had a smaller shaft that used automotive splines.

NTSB Probable Cause

The owner/builder's inadequate design, resulting in total failure of the reduction gear assembly accessory drive shaft.

Full Narrative

On June 9, 2000, about 0850 Eastern Daylight Time, a homebuilt S-51, N51FY, was substantially damaged a force landing to a field at Forty Fort, Pennsylvania. The airplane departed from Wilkes-Barre Wyoming Valley Airport (WBW), Wilkes-Barre, Pennsylvania. The certificated commercial pilot sustained minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight conducted under 14 CFR Part 91. The pilot stated that during the initial climb, about 150 feet above the ground, the engine lost all power. The pilot performed a forced landing to a field. During the landing, the airplane struck a fence and sustained damage to the right wing. Examination of the wreckage by a Federal Aviation Administration inspector revealed that the propeller reduction gear box input shaft had sheared. When asked about the shaft, the pilot stated that it failed "at the weakest point." He added that the failed area was too thin, and needed to be re-machined. He believed that over an approximate 150 hours of operation, stress caused the component to fail. According to the kit manufacturers, the failure was limited to the pilot's airplane. A machine shop had provided the reduction gearbox input shaft for the production models. The pilot decided to machine his own parts for his particular airplane. The pilot obtained some rough castings from the machine shop, but that was the only similarity between the failed shaft and the production shafts. The manufacturer added that the shafts in the production models are larger, and use aviation splines, whereas the pilot used automotive splines.

Flight

Event TypeAccident
Event Time08:50 EDT
Nearest AirportWyoming Valley Airport (0nm)
Runway25
Runway Length3376 ft
Runway Width75 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftStewart S-51
Tail NumberN51FY
Aircraft CategoryAir
DamageSubstantial
OperatorFrank Yamrick
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsGeneral Motors · GM 350 · Reciprocating · 427
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury)
Fatal0
Serious0
Minor1
Uninjured0
Total1
Crew 1Age 55 · Second Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind220° @ 10 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point57
Altimeter30.04 inHg
Observation Time12:54
Weather SourceWFAC

Appendix: Source Data