19990925029699A

Accident · Substantial damage

FAA accident report · Amtr DOMINATOR · Auburn-Lewiston, ME · September 25, 1999

Date
September 25, 1999 · 16:54 local
Place
Auburn-Lewiston, ME
Airport
Auburn-Lewiston Municipal
Phase of flight
Practice Training Manuevers
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N4449N
NTSB investigation
NTSBNYC99LA237
Reported as
Amtr Dominator
Reported engine
ROTAX ROTAX503
People aboard
1
Fatal injuries
0
Pilot’s flight hours
129 total23 in this make and model26 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(.4) 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. (-23) pilot was practicing pedal turns. On his 3rd time at approx 200' AGL he completed a pedal turn with too slow an airspeed. He completed the turn and the aircraft immediately began to descend. Pilot added power but could not stop the descent rate. He was able to bring the rotors parallel with the ground in preparation for impact.

As the FAA filed it

(.4) 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. (-23) PILOT WAS PRACTICING PEDAL TURNS. ON HIS 3RD TIME AT APPROX 200' AGL HE COMPLETED A PEDAL TURN WITH TOO SLOW AN AIRSPEED. HE COMPLETED THE TURN AND THE AIRCRAFT IMMEDIATELY BEGAN TO DESCEND. PILOT ADDED POWER BUT COULD NOT STOP THE DESCENT RATE. HE WAS ABLE TO BRING THE ROTORS PARALLEL WITH THE GROUND IN PREPARATION FOR IMPACT.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.