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November 11, 2005 · Rehler Gyrocopter · N100KR

New Braunfels, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
November 11, 2005
Injury Outcomes
1 injury (1 fatality)
Location
New Braunfels, TX
Aircraft
Rehler Gyrocopter
Tail Number
N100KR
Injuries
Fatal
Aircraft Damage
Substantial
NTSB Number
DFW06LA028

The 700-hour private pilot/builder/owner was approaching Runway 13 when a gust of wind turned the gyrocopter sideways. The gyrocopter subsequently flipped inverted and impacted the runway. Examination of the gyrocopter did not reveal any mechanical deficiencies. The winds at the airport were reported from 150 degrees at 12 knots near the time of the accident.

NTSB Probable Cause

The pilot's failure to maintain control while landing. A contributing factor was the high winds.

Full Narrative

On November 11, 2005, about 1705 central standard time, an experimental Rehler gyrocopter, N100KR, was substantially damaged following a loss of control while on approach to Runway 13 at the New Braunfels Municipal Airport, near New Braunfels, Texas. The private pilot/builder/owner, sole occupant of the gyroplane, was fatally injured. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight conducted under 14 Code of Federal Regulations Part 91. The local flight originated at the New Braunfels Airport at an undetermined time. Several witnesses observed the gyrocopter as it descended and approached the runway. When the gyrocopter was about 30 feet above the ground, a gust of wind turned the aircraft sideways, and the gyrocopter "flipped inverted and impacted the runway on its main rotor system." Some of the witnesses reported hearing the engine make a power change before ground impact. A Federal Aviation Administration (FAA) inspector performed an on-scene examination of the wreckage. The inspector established flight and engine control continuity and found fuel in the fuel tank. No mechanical deficiencies or anomalies were noted. The pilot designed and constructed the gyrocopter. According to his website, he described his gyrocopter as a single-place, experimental aircraft powered by a 100 HP, four-cylinder, four- cycle Rotax engine. The gyrocopter featured a 27-foot-diameter main rotor system, with a three-bladed, 68-inch-diameter propeller installed in the pusher configuration. The gyrocopter was reported to be capable to cruise between 35 and 95 miles per hour. The pilot's last FAA third class medical was issued on June 9, 2004. At that time, the pilot reported a total of 700 flight hours. Toxicological testing was performed by the FAA's Accident Research Laboratory, Oklahoma City, Oklahoma. Weather reported at the airport at 1751 was wind from 150 degrees at 12 knots, visibility 10 statute miles, broken clouds at 6,000 feet, overcast clouds at 7,000 feet, temperature 81 degrees Fahrenheit, dew point 62 degrees Fahrenheit, and a barometric pressure setting of 29.97 inches of Mercury.

Flight

Event TypeAccident
Event Time17:05 CST
Nearest AirportNew Braunfels Municipal (0nm)
Runway13
Runway Length5352 ft
Runway Width100 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftRehler Gyrocopter
Tail NumberN100KR
Aircraft CategoryGyro
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotax · 912S · Reciprocating · 100
Seats1

People & Injuries

Injury Summary1 injury (1 fatality)
Fatal1
Serious0
Minor0
Uninjured0
Total1
Crew 1Age 63 · Third Class · Fatal

Conditions

ConditionsVMC
LightDaylight
Wind150° @ 12 kt
Visibility10 sm
CeilingBroken clouds 6000 ft
Temperature / Dew Point63 F
Altimeter29.96 inHg
Observation Time23:51
Weather SourceWFAC

Appendix: Source Data