20090627011229A

Accident · Substantial damage

FAA accident report · Amtr ROTORWAY 162F · Midlothian/Wax, TX · June 27, 2009

Date
June 27, 2009 · 12:02 local
Place
Midlothian/Wax, TX
Airport
Mid-Way Regional
Phase of flight
Hovering
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1934
NTSB investigation
NTSBCEN09CA394
Reported as
Amtr ROTORWAY162F
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
100 total90 in this make and model0 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.

(-23) The pilot stated that he was approaching the south side of taxiway where he planned to hover at 10 feet and fly to his hangar. During transition, he lost tail rotor effectiveness, and the aircraft impacted the taxiway, bounced, and spun. He was unsure of all that happened during the sequence. The aircraft landed upright, with substantial damage. The tail rotor and main rotor blades impacted the ground. The main rotor blades impacted the tail boom. The landing gear collapsed at the left rear attach point. The fuselage bent behind the cabin area. The pilot/builder indicated that the aircraft could be rebuilt. The tail rotor and main rotor blades indicate that they were not a full speed when the aircraft impacted. Further information from the pilot indicated that he was performing an autorotation.

As the FAA filed it

(-23) THE PILOT STATED THAT HE WAS APPROACHING THE SOUTH SIDE OF TAXIWAY WHERE HE PLANNED TO HOVER AT 10 FEET AND FLY TO HIS HANGAR. DURING TRANSITION, HE LOST TAIL ROTOR EFFECTIVENESS, AND THE AIRCRAFT IMPACTED THE TAXIWAY, BOUNCED, AND SPUN. HE WAS UNSURE OF ALL THAT HAPPENED DURING THE SEQUENCE. THE AIRCRAFT LANDED UPRIGHT, WITH SUBSTANTIAL DAMAGE. THE TAIL ROTOR AND MAIN ROTOR BLADES IMPACTED THE GROUND. THE MAIN ROTOR BLADES IMPACTED THE TAIL BOOM. THE LANDING GEAR COLLAPSED AT THE LEFT REAR ATTACH POINT. THE FUSELAGE BENT BEHIND THE CABIN AREA. THE PILOT/BUILDER INDICATED THAT THE AIRCRAFT COULD BE REBUILT. THE TAIL ROTOR AND MAIN ROTOR BLADES INDICATE THAT THEY WERE NOT A FULL SPEED WHEN THE AIRCRAFT IMPACTED. FURTHER INFORMATION FROM THE PILOT INDICATED THAT HE WAS PERFORMING AN AUTOROTATION.

NTSB investigation

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