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NTSB Report

September 25, 1999 · Pratt Dominator · N4449N

Auburn, ME

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
September 25, 1999
Injury Outcomes
No injuries (1 uninjured)
Location
Auburn, ME
Aircraft
Pratt Dominator
Tail Number
N4449N
Injuries
None
Aircraft Damage
Substantial
NTSB Number
NYC99LA237

The pilot was practicing a 180 degree turn with 0 airspeed to a downwind condition at 100 feet agl in his homebuilt gyroplane. He had successfully completed the maneuver once, and was attempting it for a second time. During the second attempt, the pilot slowed the gyroplane until reaching approximately 0 airspeed, then applied pedal to execute the turn. The gyroplane entered a rapid descent. The pilot advanced the throttle, and lowered the nose of the gyroplane to gain airspeed. Recognizing the impending impact, the pilot leveled the rotor's tip-path-plane, and the gyroplane impacted the ground level with forward airspeed. The landing gear collapsed, and the rotor contacted the ground on both sides. In addition, the rotor contacted the engine driven propeller, shearing off all three blades. The gyroplane bounced back into the air, and then impacted the ground for a second time. During the second impact, the gyroplane was level, but rolled right after ground contact, and slid 20 to 30 feet on its side before coming to a stop. According to the kit manufacturer, at 0 airspeed the gyroplane would descend at 1,000 to 1,500 feet per minute.

NTSB Probable Cause

The pilot's improper decision to execute a 0 airspeed pedal turn at 100 feet agl.

Full Narrative

On September 25, 1999, at 1654 eastern daylight time, a Dominator homebuilt gyroplane, N4449N, was substantially damaged when it impacted terrain while maneuvering at the Auburn Municipal Airport, Auburn, Maine. The certificated private pilot was not injured, and visual meteorological conditions prevailed. A visual flight rules flight plan was not filed, and the personal local flight was conducted under 14 CFR Part 91. According to the pilot, he was practicing a 180 degree turn with 0 airspeed to a downwind condition at 100 feet agl when the accident happened. The pilot added that he had just successfully completed the maneuver once, and was attempting it for a second time. During the second attempt, the pilot slowed the gyroplane until reaching approximately 0 airspeed then applied pedal to execute the turn. After completing the turn, the gyroplane entered a rapid descent. The pilot advanced the throttle, and lowered the nose of the gyroplane to gain airspeed. Recognizing the impending impact, the pilot leveled the rotor's tip-path-plane, and the gyroplane impacted the ground level with forward airspeed. The landing gear collapsed, and the rotor contacted the ground on both sides. In addition, the rotor contacted the engine driven propeller, shearing off all three blades. The gyroplane bounced back into the air, and then impacted the ground for a second time. During the second impact, the gyroplane was level, but rolled right after ground contact, and slid 20 to 30 feet on its side before coming to a stop. The pilot reported the winds were approximately 10 knots. He made no mention of any preimpact failures or malfunctions that may have contributed to the accident. According to the manufacture of the kit, the gyroplane would develop a 1,000 to 1,500 foot per minute descent at 0 airspeed.

Flight

Event TypeAccident
Event Time16:54 EDT
Nearest AirportAuburn Municipal (0nm)
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftPratt Dominator
Tail NumberN4449N
Aircraft CategoryGyro
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsRotax · 503 · Reciprocating · 65
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 45 · Third Class

Conditions

ConditionsVMC
LightDaylight
Wind310° @ 6 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point64 F / 45 C
Altimeter29.00 inHg
Observation Time20:55
Weather SourceWFAC

Appendix: Source Data