MCDONNELL DOUGLAS HELI CO 369FF near Fossil, OR — 2009-10-12
- Date
- 2009-10-12
- Location
- Fossil, OR, USA
- Aircraft
- MCDONNELL DOUGLAS HELI CO 369FF
- Registration
- N527SH
- Category
- Helicopter
- Highest injury
- Fatal
- Fatalities
- 1
- Phase of flight
- Maneuvering
Probable cause
The pilot's failure to maintain clearance from a power pole to which he was connecting wire-pulling ropes.
NTSB narrative
The pilot of the helicopter was pulling a rope along a line of wood power poles, and placing the rope within the lowest traveler (pulley) attached to each power pole. The placement of the rope into the traveler required maneuvering the helicopter in close proximity to the pole, while the rope was attached to a long-line that was shorter than the distance from the top of the pole to the traveler that the rope was being placed in. The pilot had already placed the rope in the traveler on the first pole of the line, and had just completed the placement of the rope into the traveler on the second pole, when he began to maneuver the helicopter in order to proceed to the next pole. At the beginning of that maneuver, the pilot inadvertently allowed the helicopter to come close enough to the pole that he had just finished working on for its main rotor blades to come in contact with the pole. Immediately thereafter, all five of the main rotor blades separated from the helicopter, whereupon the helicopter's tail boom separated from its fuselage. The helicopter then fell to the down-sloping terrain near the base of the pole. No pre-accident anomalies were found with the helicopter's airframe, engine, or flight control system.
Analysis
- Primary failure mode
- Loss of control
- First missed decision gate
- Pilot could have maintained a safer distance from the power pole.
NTSB coding
Evidence available
- Photos
- 27 docket documents
Docket documents27
- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1form
- Release of Aircraft Wreckage, NTSB Form 6120.15form
- Statement of Party Representatives to NTSB Investigationinterview
- Witness Statement - David Bilboainterview
- Witness Statements Given to FAAinterview
- MD Helicopter Field Notesother
- Record of Conversationsother
- Image 1. View of top of helicopter laying on right side down-slope from power pole.photos
- Image 10. View of main rotor hub, with root of red blade still attached.photos
- Image 11. View of blue, red, and white main rotor blades (green and yellow blades partially shown on right).photos
- Image 12. View of green and yellow main rotor blades (partial view of blue, red, and white blades on left).photos
- Image 13. View of tail boom in three sections (forward, aft, and horizontal stabilizer).photos
- Image 14. View of left cyclic handle, showing cargo hook release button and cargo hook emergency release lever.photos
- Image 15. View of left collective handle, showing separated electrical switch unit.photos
- Image 16. View of right side of turbo-shaft engine prior to removal.photos
- Image 17. View of in-flight metallic foreign object damage (FOD) to compressor blades.photos
- Image 18. View of side-mounted cargo hook being used with power pole long-line.photos
- Image 2. View of front of helicopter lying behind stump down-slope from power pole, showing long-line running from near pole to helicopter.photos
- Image 3. View of forward portion of tail boom lying against fence down-slope from helicopter.photos
- Image 4. View of aft portion of tail boom lying beyond fence down-slope of helicopter.photos
- Image 5. View of ball-hook lying near power pole with long-line running down-slope to point near helicopter.photos
- Image 6. View of entire power pole, with neutral wire traveler (with rope attached) seen on right side below wood cross member.photos
- Image 7. View of top of power pole showing where it was severed by main rotor blade impact.photos
- Image 8. Front view of helicopter at teardown (cyclic stick lying on floor near center of photo).photos
- Image 9. View of right side of helicopter at teardown.photos
- Rolls-Royce Engine Teardown Report (Narrative Section)report
- Toxicological Reportreport
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