N9645A

Substantial
Serious

BELL UH-1B S/N: 303

Accident Details

Date
Sunday, July 17, 1994
NTSB Number
SEA94LA183
Location
PILOT ROCK, OR
Event ID
20001206X01881
Coordinates
45.390983, -118.779571
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

DIRECTIONAL CONTROL WAS NOT MAINTAINED FOR UNDETERMINED REASONS.

Aircraft Information

Registration
N9645A
Make
BELL
Serial Number
303
Engine Type
Turbo-shaft
Model / ICAO
UH-1B UH1
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
PACIFIC AEROMOTIVE CORP
Address
PO BOX 450
Status
Deregistered
City
ERIE
State / Zip Code
CO 80516-0450
Country
United States

Analysis

On July 17, 1994, at 1030 Pacific daylight time, a Bell UH-1B, N9645A, sustained substantial damage when it collided with terrain while conducting helicopter logging operations near Pilot Rock, Oregon. The pilot, who was the sole occupant, was seriously injured. No flight plan was filed for the flight, and there was no report of an ELT activation. A small fire was set by the exhaust at the crash site.

The pilot had pickled a load of logs prior to the accident, when he lost directional control of the aircraft. The helicopter descended to impact near the bottom of a draw or canyon. The pilot had little recollection of the events after the accident. As his medical condition improved, he stated that he recalled that the pedals would not move, and the aircraft rotated around its vertical axis counter-clockwise.

During other interviews with the pilot, his recollection of the occurrence varied, including the apparent direction of rotation, and the recollection that the left pedal was stuck. He recalled attempting to "airstream" the aircraft, but found that to be unsuccessful. He then said he recalled attempting to maneuver back near his logging crew to crash, so that he wouldn't be far from rescue. The aircraft continued to rotate until impact.

The wreckage was inspected after it was moved to a salvage yard. Tail rotor control continuity was established from the tail rotor through the tail boom. The nose was crushed, precluding establishing control continuity in the cabin section of the fuselage. The tail rotor drive components were shipped to Bell for testing and disassembly. No evidence of a mechanical malfunction was found during component disassembly and inspection.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# SEA94LA183