20081230853599A

Accident · Substantial damage

FAA accident report · Cotton HELICYCLE · Spring, TX · December 30, 2008

Date
December 30, 2008 · 12:55 local
Place
Spring, TX
Airport
David Wayne Hooks Memorial
Phase of flight
Hovering
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N555CX
NTSB investigation
NTSBCEN09LA113
Reported as
Cotton Helicycle
Reported engine
SOLAR T62
People aboard
1
Fatal injuries
0
Pilot’s flight hours
3,700 total140 in this make and model30 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.

On 12-30-2008 @ 12:55 hours local, the pilot stated that he was in transition from hover taxi to forward flight when the engine quit producing power. During landing attempt, the right landing gear skid contacted the ground in a nose low attitude. The right landing gear skid collapsed upward into the right side of the aircraft fuselage. In turn, the aircraft rolled onto its right side causing irreparable damage to both main rotor blades and one (1) main rotor grip. Other obvious damage was to the lower vertical fin and right side fuselage. Post examination of the aircraft fuel sump, fuel lines to the fuel control and fuel selector valve revealed no anomalies. There were no injuries.

As the FAA filed it

ON 12-30-2008 @ 12:55 HOURS LOCAL, THE PILOT STATED THAT HE WAS IN TRANSITION FROM HOVER TAXI TO FORWARD FLIGHT WHEN THE ENGINE QUIT PRODUCING POWER. DURING LANDING ATTEMPT, THE RIGHT LANDING GEAR SKID CONTACTED THE GROUND IN A NOSE LOW ATTITUDE. THE RIGHT LANDING GEAR SKID COLLAPSED UPWARD INTO THE RIGHT SIDE OF THE AIRCRAFT FUSELAGE. IN TURN, THE AIRCRAFT ROLLED ONTO ITS RIGHT SIDE CAUSING IRREPARABLE DAMAGE TO BOTH MAIN ROTOR BLADES AND ONE (1) MAIN ROTOR GRIP. OTHER OBVIOUS DAMAGE WAS TO THE LOWER VERTICAL FIN AND RIGHT SIDE FUSELAGE. POST EXAMINATION OF THE AIRCRAFT FUEL SUMP, FUEL LINES TO THE FUEL CONTROL AND FUEL SELECTOR VALVE REVEALED NO ANOMALIES. THERE WERE NO INJURIES.

NTSB investigation

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