20030813019959A

Accident · Substantial damage

FAA accident report · Snias AS350D · Lewiston, ID · August 13, 2003

Date
August 13, 2003 · 14:35 local
Place
Lewiston, ID
Phase of flight
To Vertical (Helicopter Only)
Operating rules
Rotorcraft external load (Part 133)
Operator
X5HL
Damage
Substantial damage
Aircraft
N57731
NTSB investigation
NTSBSEA03FA169
Reported as
Snias AS350D
Reported engine
Allison 250C30
Fatal injuries
0
Pilot’s flight hours
4,000 total100 in this make and model50 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 aircraft was on a mission dropping water from a bambi bucket withlong line in use. The pilot had picked up a load of water and had reached an altitude of approximately 150' when the pilot heard a loud bang, engine out warning light illuminated, engine out horn sounded and there was an immediate power loss. He entered autorotation and impacted the ground without releasing the bambi bucket which was full of water. The aircraft impacted the ground on a heading of 130 degrees and slid for approximately 60 feet, coming to a stop on a heading of 060 degrees. Two witnesses on the ground stated they heard a popping sound from the engine followed with visible smoke and flame coming from the engine exhaust. On scene investigation revealed extensive accumulation of ferrous particles on the engine gearbox chip plug. The engine sump chip plug showed no abnormal accumulation of metal particles. The airframe mounted engine oil filter was examined and found to have an extensive amount of metal particles in the filter and filter housing. A small amount of engine oil was examined from the external filter and small, suspended metal particles were visible in the oil. The power turbine wheel was seized and could not be rotated by hand. When the main rotor blades were rotated backwards to engage the power train, scraping and metal rattling could be heard inside the power section of the engine.

As the FAA filed it

(-23) THE AIRCRAFT WAS ON A MISSION DROPPING WATER FROM A BAMBI BUCKET WITHLONG LINE IN USE. THE PILOT HAD PICKED UP A LOAD OF WATER AND HAD REACHED AN ALTITUDE OF APPROXIMATELY 150' WHEN THE PILOT HEARD A LOUD BANG, ENGINE OUT WARNING LIGHT ILLUMINATED, ENGINE OUT HORN SOUNDED AND THERE WAS AN IMMEDIATE POWER LOSS. HE ENTERED AUTOROTATION AND IMPACTED THE GROUND WITHOUT RELEASING THE BAMBI BUCKET WHICH WAS FULL OF WATER. THE AIRCRAFT IMPACTED THE GROUND ON A HEADING OF 130 DEGREES AND SLID FOR APPROXIMATELY 60 FEET, COMING TO A STOP ON A HEADING OF 060 DEGREES. TWO WITNESSES ON THE GROUND STATED THEY HEARD A POPPING SOUND FROM THE ENGINE FOLLOWED WITH VISIBLE SMOKE AND FLAME COMING FROM THE ENGINE EXHAUST. ON SCENE INVESTIGATION REVEALED EXTENSIVE ACCUMULATION OF FERROUS PARTICLES ON THE ENGINE GEARBOX CHIP PLUG. THE ENGINE SUMP CHIP PLUG SHOWED NO ABNORMAL ACCUMULATION OF METAL PARTICLES. THE AIRFRAME MOUNTED ENGINE OIL FILTER WAS EXAMINED AND FOUND TO HAVE AN EXTENSIVE AMOUNT OF METAL PARTICLES IN THE FILTER AND FILTER HOUSING. A SMALL AMOUNT OF ENGINE OIL WAS EXAMINED FROM THE EXTERNAL FILTER AND SMALL, SUSPENDED METAL PARTICLES WERE VISIBLE IN THE OIL. THE POWER TURBINE WHEEL WAS SEIZED AND COULD NOT BE ROTATED BY HAND. WHEN THE MAIN ROTOR BLADES WERE ROTATED BACKWARDS TO ENGAGE THE POWER TRAIN, SCRAPING AND METAL RATTLING COULD BE HEARD INSIDE THE POWER SECTION OF THE ENGINE.

NTSB investigation

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