20040728016569A

Accident · Substantial damage

FAA accident report · Robsin R44RAVENII · Walnut Creek, NC · July 28, 2004

Date
July 28, 2004 · 09:00 local
Place
Walnut Creek, NC
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N442RD
NTSB investigation
NTSBATL04LA155
Reported as
Robsin R44RAVENII
Reported engine
Lycoming IO540*
People aboard
1
Fatal injuries
0

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) Pilot was executing an approach into a confined area behind his house. Pilot stated that he landed the aircraft on the edge of a concrete helipad causing the aircraft to rock backwards when the tail rotor "came off." The helipad was elevated approximately four inches and the pilot stated that the aircraft had been moved up onto the helipad after the accident. On site investigation revealed the 90 degree gearbox and tailrotor completely separated from the aircraft with extensive damage to the tailrotor blades and assembly. Additionally, the vertical stabilizer was bent severely to the left indicating a nose left yaw. Fuselage inspection showed evidence of internal damage to the tail and engine mount structures. There were no noticeable ground marks indicating the tailrotor had struck the ground. The entire area around the helipad had been raked and smoothed recently.

As the FAA filed it

(-23) PILOT WAS EXECUTING AN APPROACH INTO A CONFINED AREA BEHIND HIS HOUSE. PILOT STATED THAT HE LANDED THE AIRCRAFT ON THE EDGE OF A CONCRETE HELIPAD CAUSING THE AIRCRAFT TO ROCK BACKWARDS WHEN THE TAIL ROTOR "CAME OFF." THE HELIPAD WAS ELEVATED APPROXIMATELY FOUR INCHES AND THE PILOT STATED THAT THE AIRCRAFT HAD BEEN MOVED UP ONTO THE HELIPAD AFTER THE ACCIDENT. ON SITE INVESTIGATION REVEALED THE 90 DEGREE GEARBOX AND TAILROTOR COMPLETELY SEPARATED FROM THE AIRCRAFT WITH EXTENSIVE DAMAGE TO THE TAILROTOR BLADES AND ASSEMBLY. ADDITIONALLY, THE VERTICAL STABILIZER WAS BENT SEVERELY TO THE LEFT INDICATING A NOSE LEFT YAW. FUSELAGE INSPECTION SHOWED EVIDENCE OF INTERNAL DAMAGE TO THE TAIL AND ENGINE MOUNT STRUCTURES. THERE WERE NO NOTICEABLE GROUND MARKS INDICATING THE TAILROTOR HAD STRUCK THE GROUND. THE ENTIRE AREA AROUND THE HELIPAD HAD BEEN RAKED AND SMOOTHED RECENTLY.

NTSB investigation

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