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NTSB Report

August 7, 2005 · O Connor Air Command Elite · N2416P

Cincinnati, OH

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 7, 2005
Injury Outcomes
1 injury (1 minor injury), 1 uninjured
Location
Cincinnati, OH
Aircraft
O Connor Air Command Elite
Tail Number
N2416P
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
IAD05LA116

Shortly after takeoff, about three-quarters down the runway and at an altitude of 50 feet, the gyrocopter's engine surged, then experienced a "partial, but significant loss of power." The pilot reduced the power to idle and attempted to land on the remaining runway. He flared too high, the main landing gear hit the runway "hard," and the gyrocopter's nose pitched down, collapsing the nose wheel and shearing it off. The gyrocopter then rolled about 90 degrees onto its right side, and skidded to a stop just before reaching the end of the runway. The gyrocopter was powered by a non-certified engine, and the reason for the partial loss of engine power was not determined. The pilot reported a total of 76 hours of flight time, of which, 72 hours were in gyrocopters.

NTSB Probable Cause

The pilot's improper flare following a partial loss of engine power, which resulted in a hard landing. A factor was the partial loss of engine power for unknown reasons.

Full Narrative

On August 7, 2005, about 1455 eastern daylight time, a homebuilt Air Command Elite gyrocopter, N2416P, was substantially damaged during a forced landing at Cincinnati-Blue Ash Airport (ISZ), Cincinnati, Ohio. The certificated private pilot was not injured, and the passenger incurred minor injuries. Visual meteorological conditions prevailed, and no flight plan had been filed for the local personal flight, conducted under 14 CFR Part 91. The pilot reported to a Federal Aviation Administration (FAA) inspector that shortly after takeoff, about three-quarters down runway 24 and at an altitude of 50 feet, the engine "surged," then experienced a "partial, but significant loss of power." The pilot reduced the power to idle and attempted to land on the remaining runway. He flared too high, the main landing gear hit the runway "hard," and the gyrocopter's nose pitched down, "collapsing the nose wheel and shearing it off." The gyrocopter then rolled about 90 degrees onto its right side, and skidded to a stop just before reaching the end of the runway. The gyrocopter was powered by a non-certified Subaru 1522 engine. The post-accident examination of the wreckage did not reveal the reason for the partial power loss. The pilot reported a total of 76 hours of flight time, of which, 72 hours were in gyrocopters. Weather, reported at an airport about 12 nautical miles to the southeast, at 1453, included winds from 050 degrees true at 5 knots, temperature 88 degrees Fahrenheit, and dew point 73 degrees Fahrenheit.

Flight

Event TypeAccident
Event Time14:55 EDT
Nearest AirportBlue Ash Airport (0nm)
Runway24
Runway Length3499 ft
Runway Width75 ft
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftO Connor Air Command Elite
Tail NumberN2416P
Aircraft CategoryGyro
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsSubaru · 1522 · Reciprocating · 130
Seats2

People & Injuries

Injury Summary1 injury (1 minor injury), 1 uninjured
Fatal0
Serious0
Minor1
Uninjured1
Total2
Crew 1Age 37 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind50° @ 5 kt
Visibility6 sm
CeilingNone
Altimeter30.10 inHg
Observation Time18:53
Weather SourceWFAC

Appendix: Source Data