20040306010969A

Accident · Destroyed

FAA accident report · Bell 206L-3 · March 6, 2004

Date
March 6, 2004 · 16:23 local
Phase of flight
Forced/Precautionary Landing
Operating rules
Air taxi and commuter (Part 135)
Operator
HEEA
Damage
Destroyed
Aircraft
N81SP
NTSB investigation
NTSBFTW04LA088
Reported as
Bell 206L3
Reported engine
Allison 250C30P
People aboard
3
Fatal injuries
0
Pilot’s flight hours
3,299 total206 in this make and model112 in the last 90 days

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) The pilot stated that he heard a loud bang and felt a shudder in the airframe shortly after takeoff from an offshore platform. The pilot immediately entered an autorotation with the intent of landing on the water. The pilot was not able to deploy the emergency floats before contacting the water. The aircraft rolled over and became submerged upside down. The pilot and two passengers exited the aircraft without injury. The investigation revealed that the engine compressor had sustained minor foreign object damage (FOD). It could not be determined whether the FOD occurred before the accident or during the impact sequence. The source of the loud bang and shudder is suspected to be a compressor stall. It was also discovered that the emergency float system inflation mechanism was not rigged properly.

As the FAA filed it

(-23) THE PILOT STATED THAT HE HEARD A LOUD BANG AND FELT A SHUDDER IN THE AIRFRAME SHORTLY AFTER TAKEOFF FROM AN OFFSHORE PLATFORM. THE PILOT IMMEDIATELY ENTERED AN AUTOROTATION WITH THE INTENT OF LANDING ON THE WATER. THE PILOT WAS NOT ABLE TO DEPLOY THE EMERGENCY FLOATS BEFORE CONTACTING THE WATER. THE AIRCRAFT ROLLED OVER AND BECAME SUBMERGED UPSIDE DOWN. THE PILOT AND TWO PASSENGERS EXITED THE AIRCRAFT WITHOUT INJURY. THE INVESTIGATION REVEALED THAT THE ENGINE COMPRESSOR HAD SUSTAINED MINOR FOREIGN OBJECT DAMAGE (FOD). IT COULD NOT BE DETERMINED WHETHER THE FOD OCCURRED BEFORE THE ACCIDENT OR DURING THE IMPACT SEQUENCE. THE SOURCE OF THE LOUD BANG AND SHUDDER IS SUSPECTED TO BE A COMPRESSOR STALL. IT WAS ALSO DISCOVERED THAT THE EMERGENCY FLOAT SYSTEM INFLATION MECHANISM WAS NOT RIGGED PROPERLY.

NTSB investigation

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