19970717018729A

Accident · Substantial damage

FAA accident report · Bell 206L-1 · Amelia, LA · July 17, 1997

Date
July 17, 1997 · 06:30 local
Place
Amelia, LA
Airport
Lake Palourde Base Heliport
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3892R
NTSB investigation
NTSBFTW97LA270
Reported as
Bell 206L1
Fatal injuries
0

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.

Helicopter lost power after takeoff, executed an auto rotation. Landed hard and rolled over on its side. (-23) the pilot stated that shortly after takeoff, at approximately 60-feet above ground level, a loud bang occurred. The aircraft yawed to the left and the rotor speed began to decay. The pilot initiated an autorotation and made a hard right turn to land in a suitable area. The aircraft landed hard on the right skid and came to rest on the right side. Subsequent examination of the engine and its systems did not reveal any mechanical malfunctions. The engine did show evidence of ingestion of a foreign matter. The engine bleed air scroll was stained with what is assumed to be remnants of a ground frog. It is believed that a ground frog was ingested into the engine compressor and caused a momentary stall. Due to the low altitude, the pilot assumed it was a total failure of the engine and executed an emergency landing. The operator of the aircraft has experienced other incidents which it attributes to ingestion of a frog into the engine. Since this latest occurrence, the operator has established procedures to cover the engine intake area when the aircraft are parked overnight at this location. The operator has also consulted with environmental professionals to attempt to further eliminate the problem.

As the FAA filed it

HELICOPTER LOST POWER AFTER TAKEOFF, EXECUTED AN AUTO ROTATION. LANDED HARD AND ROLLED OVER ON ITS SIDE. (-23) THE PILOT STATED THAT SHORTLY AFTER TAKEOFF, AT APPROXIMATELY 60-FEET ABOVE GROUND LEVEL, A LOUD BANG OCCURRED. THE AIRCRAFT YAWED TO THE LEFT AND THE ROTOR SPEED BEGAN TO DECAY. THE PILOT INITIATED AN AUTOROTATION AND MADE A HARD RIGHT TURN TO LAND IN A SUITABLE AREA. THE AIRCRAFT LANDED HARD ON THE RIGHT SKID AND CAME TO REST ON THE RIGHT SIDE. SUBSEQUENT EXAMINATION OF THE ENGINE AND ITS SYSTEMS DID NOT REVEAL ANY MECHANICAL MALFUNCTIONS. THE ENGINE DID SHOW EVIDENCE OF INGESTION OF A FOREIGN MATTER. THE ENGINE BLEED AIR SCROLL WAS STAINED WITH WHAT IS ASSUMED TO BE REMNANTS OF A GROUND FROG. IT IS BELIEVED THAT A GROUND FROG WAS INGESTED INTO THE ENGINE COMPRESSOR AND CAUSED A MOMENTARY STALL. DUE TO THE LOW ALTITUDE, THE PILOT ASSUMED IT WAS A TOTAL FAILURE OF THE ENGINE AND EXECUTED AN EMERGENCY LANDING. THE OPERATOR OF THE AIRCRAFT HAS EXPERIENCED OTHER INCIDENTS WHICH IT ATTRIBUTES TO INGESTION OF A FROG INTO THE ENGINE. SINCE THIS LATEST OCCURRENCE, THE OPERATOR HAS ESTABLISHED PROCEDURES TO COVER THE ENGINE INTAKE AREA WHEN THE AIRCRAFT ARE PARKED OVERNIGHT AT THIS LOCATION. THE OPERATOR HAS ALSO CONSULTED WITH ENVIRONMENTAL PROFESSIONALS TO ATTEMPT TO FURTHER ELIMINATE THE PROBLEM.

NTSB investigation

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