20040126000489A

Accident · Substantial damage

FAA accident report · Bell 206B · Turner, OR · January 26, 2004

Date
January 26, 2004 · 15:45 local
Place
Turner, OR
Phase of flight
Pwr Off Vert Land/Autorotate
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N92CA
NTSB investigation
NTSBSEA04LA036
Reported as
Bell 206B
Reported engine
Allison 250C20B
People aboard
1
Fatal injuries
0
Pilot’s flight hours
11,500 total6,000 in this make and model60 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) On 1/26/2004, while practicing long line vertical accuracy maneuvers for an upcoming o.a.s. checkride, under 14 CFR, part 91 operating rules, Mr. Mcdaniel experienced rapid deceleration of the engine. The aircraft was in an uncontrolled hover at approximately 110 feet AGL. Mr. Mcdaniels executed an autorotation into the field he was hovering above. During the touchdown phase of the maneuver, it appears that the tail skid contacted the ground prior to the aircraft main skids. This appears to have caused the main rotor blades to flex down an abnormal amount, striking the tail boom and severing it from the aircraft. The aircraft came to rest approximately 40 feet from the initial touchdown spot and slid to an upright stop. The field consisted of wet grass approximately 3 inches tall with intermixed soft mud. Mr. Mcdaniels was uninjured. The aircraft was recovered and transported to reforestation services, inc. maintenance facility at salem, Oregon (sle). A complete aircraft inspection was performed with emphasis on the engine, specifically the fuel and engine pneumatic systems.

As the FAA filed it

(-23) ON 1/26/2004, WHILE PRACTICING LONG LINE VERTICAL ACCURACY MANEUVERS FOR AN UPCOMING O.A.S. CHECKRIDE, UNDER 14 CFR, PART 91 OPERATING RULES, MR. MCDANIEL EXPERIENCED RAPID DECELERATION OF THE ENGINE. THE AIRCRAFT WAS IN AN UNCONTROLLED HOVER AT APPROXIMATELY 110 FEET AGL. MR. MCDANIELS EXECUTED AN AUTOROTATION INTO THE FIELD HE WAS HOVERING ABOVE. DURING THE TOUCHDOWN PHASE OF THE MANEUVER, IT APPEARS THAT THE TAIL SKID CONTACTED THE GROUND PRIOR TO THE AIRCRAFT MAIN SKIDS. THIS APPEARS TO HAVE CAUSED THE MAIN ROTOR BLADES TO FLEX DOWN AN ABNORMAL AMOUNT, STRIKING THE TAIL BOOM AND SEVERING IT FROM THE AIRCRAFT. THE AIRCRAFT CAME TO REST APPROXIMATELY 40 FEET FROM THE INITIAL TOUCHDOWN SPOT AND SLID TO AN UPRIGHT STOP. THE FIELD CONSISTED OF WET GRASS APPROXIMATELY 3 INCHES TALL WITH INTERMIXED SOFT MUD. MR. MCDANIELS WAS UNINJURED. THE AIRCRAFT WAS RECOVERED AND TRANSPORTED TO REFORESTATION SERVICES, INC. MAINTENANCE FACILITY AT SALEM, OREGON (SLE). A COMPLETE AIRCRAFT INSPECTION WAS PERFORMED WITH EMPHASIS ON THE ENGINE, SPECIFICALLY THE FUEL AND ENGINE PNEUMATIC SYSTEMS.

NTSB investigation

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