N6356X

Substantial
None

CONTINENTAL COPTERS INC 47GS/N: CCI-563

Accident Details

Date
Saturday, August 31, 2013
NTSB Number
ERA13LA390
Location
Sandy Hook, KY
Event ID
20130831X85235
Coordinates
38.085556, -83.130279
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The in-flight disengagement of the tail rotor extension shaft from the tail rotor gearbox, resulting in a loss of tail rotor control.

Aircraft Information

Registration
Make
CONTINENTAL COPTERS INC
Serial Number
CCI-563
Engine Type
Reciprocating
Year Built
1963
Model / ICAO
47G
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
2
FAA Model
47G

Registered Owner (Current)

Name
PLEASANT AVIATION LLC
Address
PO BOX 287
City
MOUNT PLEASANT
State / Zip Code
TX 75456-0287
Country
United States

Analysis

On August 31, 2013, about 0950 eastern daylight time, Continental Copters, Inc. 47G, N6356X, was substantially damaged during a forced landing near Sandy Hook, Kentucky. The commercial pilot and one passenger were not injured. The helicopter was registered to Sierra Aeronautics LLC and was operated by the pilot under the provisions of 14 Code of Regulations Part 91 as a positioning flight. Day, visual meteorological conditions prevailed and no flight plan was filed. The flight originated at Morehead, Kentucky (M97) about 0930.

As the helicopter was established in the traffic pattern for landing at a pre-established landing zone, at 300 feet above ground level (AGL), the pilot turned onto final and made a power reduction. The helicopter began to yaw to the right, and then back to the left. The pilot raised the collective and the helicopter yawed again to the right and the pilot felt unusual vibrations. The pilot then attempted an autorotation. He avoided a tree and a parked car and the helicopter landed hard on a gravel road.

An inspector with the Federal Aviation Administration responded to the accident site and inspected the wreckage. There was evidence of main rotor contact with the aft section of the tail boom. The tail boom and main rotor blades sustained structural damage. The most aft section of the tail rotor drive shaft was missing; a search of the area failed to locate the missing component. Manipulation of the tail rotor shaft input at the tail rotor gearbox revealed a lack of continuity to the tail rotor hub and blades. When the universal joint, located at the forward end of the extension housing tube, was turned, the tail rotor did not rotate.

Disassembly of the tail rotor gear box revealed that the internal gears were normal in appearance and well lubricated. The tail rotor extension shaft was found disconnected from the input coupling to the tail rotor gear box. The splined end on the aft section of the shaft exhibited signatures of overheating and rotation while out of the input coupling. There were scoring marks inside the extension housing tube, indicative of excessive play in the shaft and center bearing housing.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA13LA390