N9396F

Substantial
None

Hughes 269BS/N: 840126

Accident Details

Date
Monday, December 11, 2006
NTSB Number
DFW07CA037
Location
Houma, LA
Event ID
20070130X00110
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

A partial loss of engine power as a result of a cracked engine cylinder and broken spark plug which resulted in a hard landing. A factor was that it was not possible to attain proper rotor RPM.

Aircraft Information

Registration
N9396F
Make
HUGHES
Serial Number
840126
Year Built
1964
Model / ICAO
269B

Registered Owner (Historical)

Name
JOHNSTON FLYING SERVICES LLC
Address
217 AVIATION RD
Status
Deregistered
City
HOUMA
State / Zip Code
LA 70363-5492
Country
United States

Analysis

The 2,873-hour flight instructor, who reported having accumulated 550-hours in the same make and model helicopter, reported that during a training flight, while practicing touchdown autorotations, the helicopter shuttered with a slight vibration through the airframe on climb out. The flight instructor added that the vibration stopped and he elected to continue the climb turning toward a downwind leg for the next autorotation. The helicopter shuttered again, this time much more violently, while on the downwind leg. The pilot stated on the NTSB Form 6120.1, Pilot/Operator Accident/Incident Report, that "I felt like the gearbox was locking up or something." The rated student pilot who was flying the helicopter at the time then declared "you've got the controls" to the instructor. The flight instructor immediately entered autorotation and the shutter stopped. In an attempt to regain powered flight the instructor then reapplied throttle which immediately created a violent vibration again and he decided to roll throttle completely off and continue with the emergency landing. The altitude at the onset was approximately 400 feet above ground level (agl). The flight instructor initiated a 180-degree turn autorotation to align the helicopter into the prevailing wind. The flight instructor also stated that the transfer of controls and attempt to regain powered flight, followed by the delay in entering the autorational turn, created a low airspeed and low rotor RPM situation that made the successful landing not possible. The flight instructor stated that he "waited until the last second and pulled the collective up to the stops and prayed." The helicopter landed hard and managed to remain in the upright position. The flight instructor and the rated student pilot were not injured. An FAA inspector, who traveled to the site, noted that the spark plug and helicoil was broken out on the number two cylinder. Further inspection of the number two cylinder revealed three separate cracks in the cylinder wall.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW07CA037