On December 5, 2007, at 1600 mountain standard time, a Bell UH-1B, N46969, impacted terrain approximately 33 miles southwest of Ennis, Montana. R & R Conner Aviation LLC was operating the helicopter under the provisions of 14 Code of Federal Regulations Part 91. The pilot was not injured; the helicopter sustained substantial damage. Visual meteorological conditions prevailed and no flight plan was filed for the local positioning flight. Use your browsers 'back' function to return to synopsisReturn to Query Page
According to the pilot, he had flown the helicopter for five cycles throughout the day (about 1.3 to 1.5 hours per cycle) and landed at the landing zone to remove the long line. The pilot was asked by ground personnel to reposition the helicopter from the landing zone to a nearby road, in order for a snowplow to access the landing zone. Once the snowplow was finished, the pilot began to reposition the helicopter to the landing zone. As the helicopter was lifting from the ground, it began to vibrate, that turned into a severe "hop or a bounce." The pilot climbed the helicopter to about 15 feet; however, it continued to vibrate. The helicopter then began to nose over and become uncontrollable. The pilot then decided to force land the helicopter. The helicopter landed hard in two feet of snow and sustained structural damage to the doorframe.
The Federal Aviation Administration inspector stated that following the accident, the minimum collective control friction was measured at 8 pounds, and the maintenance manual specified a friction between 14 to 16 pounds. The maintenance manual noted that if the friction is not set properly, a collective bounce (vertical oscillation) could be induced. No other mechanical anomalies were identified and the reason for the loss of friction could not be determined.
According to the Operator's Manual for the UH-1B helicopter, "Collective bounce is a pilot induced vertical oscillation that may be encountered in any flight condition by a rapid buildup of vertical bounce at approximately three cycles per second. The severity of this oscillation is such that effective control of the aircraft may become difficult to maintain."