Sikorsky CH-54A accident near Ketchikan, AK

On July 13, 1996, a Sikorsky CH-54A (helicopter) was involved in an accident near Ketchikan, AK. 1 person died. Damage to the aircraft: destroyed.

Date
July 13, 1996
Place
Ketchikan, AK
Aircraft
Sikorsky CH-54A · Helicopter
Injuries
1 fatal, 1 serious, 0 minor
Damage
Destroyed
Position
55.611°N, 131.580°W
NTSB ID
20001208X06129

Official records · ANC96FA098

NTSB summary

History of the Flight On July 13, 1996, about 1325 Alaska daylight time, a Sikorsky CH-54A helicopter, N541SB, crashed during aero logging operations, about 16 miles north-northeast of Ketchikan, Alaska. The helicopter was being operated as a visual flight rules (VFR) local area flight under Title 14 CFR Part 133 when the accident occurred. The helicopter, registered to and operated by Silver Bay Logging Company, Juneau, Alaska, was destroyed. The certificated commercial pilot received serious injuries. The copilot, holder of a commercial helicopter certificate, received fatal injuries. Visual meteorological conditions prevailed. The flight originated at a nearby logging camp about 1308. The operator reported that logging operations were being conducted near Shelter Cove, located in the Tongass National Forest. The helicopter, a surplus military aircraft certificated in the restricted category, was using a 200 foot long external cable to retrieve logs. The helicopter was operating on its 4th cycle of the day and was hovering above nearby trees over an area of cut logs. Ground personnel, communicating with the pilot by radio, hooked the helicopter's cable to a metal choker cable that was cinched around 2 large logs with an estimated total weight of 18,000 pounds. The helicopter lifted the logs about 60 feet above the ground when a popping sound was heard coming from the helicopter and the tailrotor began to slow down. The helicopter was observed to spin counter-clockwise about 5 complete turns. The pilot released the load of logs from the end of the cable and commented over

Probable cause

failure of the number 5 tailrotor bearing. A factor relating to the accident was: the uneven/steep sloping terrain, where the pilot was forced to land. Possible factors were: inadequate handling/labeling of the 'relubed' bearing by intermediate supplyier(s), and/or insufficient shelf life/service limits for military surplus parts.

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