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December 11, 2006 · Hughes 269B · N9396F

Houma, LA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 11, 2006
Injury Outcomes
No injuries (2 uninjured)
Location
Houma, LA
Aircraft
Hughes 269B
Tail Number
N9396F
Operator
Johnston Flying Service
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DFW07CA037

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 autorotational 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. At the time of the accident, the winds were reported from 070 degrees at 10 knots, gusting to 15 knots.

NTSB Probable Cause

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.

Full Narrative

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.

Flight

Event TypeAccident
Event Time15:45 CST
Nearest AirportHouma-Terrebonne Airport (0nm)
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo

Aircraft

AircraftHughes 269B
Tail NumberN9396F
Aircraft CategoryHeli
DamageSubstantial
OperatorJohnston Flying Service
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · HIO360A1D · Reciprocating · 180
Seats2

People & Injuries

Injury SummaryNo injuries (2 uninjured)
Fatal0
Serious0
Minor0
Uninjured2
Total2
Crew 1Age 45 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind90° @ 12 kt
Visibility7 sm
CeilingBroken clouds 3500 ft
Temperature / Dew Point63 F
Altimeter30.22 inHg
Observation Time21:55
Weather SourceWFAC

Appendix: Source Data