N319RC

Substantial
None

Cooke Rotorway ExecS/N: 3195

Accident Details

Date
Saturday, May 15, 2004
NTSB Number
FTW04LA131
Location
Willis, TX
Event ID
20040525X00665
Coordinates
30.351943, -95.414443
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The partial loss of engine power due to the failure of the #1 cylinder valve retainer clip. A contributing factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N319RC
Make
COOKE
Serial Number
3195
Engine Type
Reciprocating
Year Built
1985
Model / ICAO
Rotorway ExecSA02
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
COOKE RONALD W
Address
12344 LAKE VISTA DR
Status
Deregistered
City
WILLIS
State / Zip Code
TX 77318-5235
Country
United States

Analysis

On May 15, 2004, at 1622 central daylight time, a Cooke Rotorway Exec amateur-built helicopter, N319RC, was substantially damaged following a partial loss of engine power while hovering in preparation for takeoff from a boat dock located on Lake Conroe, near Willis, Texas. The helicopter was registered to and operated by the pilot. The commercial pilot/builder, sole occupant of the helicopter, was not injured. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight conducted under 14 Code of Federal Regulations Part 91. The local flight was originating at the time of the accident.

The 3,200-hour pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that after running the engine up to operating temperatures, he completed his pre-takeoff checklist. He lifted off from the boat dock to a 3-foot hover for about 20 to 30 seconds, and then started to move the helicopter over the water. Subsequently, he heard a ratcheting sound followed by a loss of engine power. He attempted to land back on the boat dock, but the helicopter descended quickly and the right landing skid and the main rotor blades contacted the dock. The helicopter came to rest upright in a boat slip in about 4-feet of water, adjacent to the dock.

Two Federal Aviation Administration (FAA) inspectors performed an on-scene examination of the helicopter. According to one of the inspectors, the helicopter had been recovered from the water and the main rotor blades were already removed. The aft portion of the tail boom, the main rotor blades, and the main rotor system were damaged.

Examination of the engine revealed that the #1 cylinder exhaust valve keeper retaining clip was disengaged.

The pilot reported to one of the FAA inspectors that he had recently sent the #1 cylinder to Rotorway for repair. The cylinder was reinstalled the helicopter approximately 10 flight hours prior to the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW04LA131