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NTSB Report

June 26, 1999 · Gillmore Benson B&M · N2152G

Greencastle, IN

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 26, 1999
Injury Outcomes
1 injury (1 serious injury)
Location
Greencastle, IN
Aircraft
Gillmore Benson B&M
Tail Number
N2152G
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
CHI99LA200

The pilot said that the roll control was lost and while attempting to maneuver for a landing. He said that on approach '... about 200 ft and 400 yards from the threshold of the runway the first violent left bank occurred.' He said he applied controls to counter the bank and the gyroplane '... sluggishly started turning back to the right...' He said that he then began to nose the gyroplane down to gain some airspeed and at that point the engine suffered a loss of power. He said that about 50 feet above ground level, '... the machine made another violent roll to the left and nosed toward the ground.' He said opposite controls did not arrest the roll and the gyroplane impacted the terrain just left of the runway. An examination of the gyroplane subsequent to the accident found that the right cyclic control rod was fractured. The fracture was discolored with corrosion through 90% of the material All other mechanical anomalies were consistent with impact damage.

NTSB Probable Cause

the failure of the cyclic control rod. Factors were aircraft control not possible for the pilot.

Full Narrative

On June 26, 1999, at 0830 eastern standard time, a Gillmore Benson B&M (amateur built gyroplane), N2152G, departed controlled flight and impacted the terrain near Greencastle, Indiana. The gyroplane sustained substantial damage, while the pilot received serious injuries. The personal 14 CFR part 91 flight was operating in visual meteorological conditions. No flight plan was on file. The local flight departed about 0715. The pilot said that the roll control was lost and while attempting to maneuver for a landing on runway 18. He said that on approach "... about 200 ft and 400 yards from the threshold of the runway the first violent left bank occurred." He said he applied controls to counter the bank, and the gyroplane "... sluggishly started turning back to the right..." He said that he then began to nose the gyroplane down to gain some airspeed and at that point the engine suffered a loss of power. He said that about 50 feet above ground level, "... the machine made another violent roll to the left and nosed toward the ground." He said that opposite controls did not arrest the roll and the gyroplane impacted the terrain just left of the runway. An examination of the gyroplane subsequent to the accident found that the right cyclic control rod was fractured. The Federal Aviation Administration inspector found the fracture discolored with corrosion through 90% of the material. He said the rod was necessary to maintain the roll control of the gyroplane. All other mechanical anomalies found were consistent with impact damage, according to the inspector.

Flight

Event TypeAccident
Event Time09:30 EDT
Nearest AirportPutnam County (0nm)
Runway18
Runway Length5000 ft
Runway Width100 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftGillmore Benson B&M
Tail NumberN2152G
Aircraft CategoryGyro
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsSubaru · EA81-TURBO · Reciprocating · 107
Seats1

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 40 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind230° @ 5 kt
CeilingNone
Temperature / Dew Point0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data