Oom Fanus
13th Mar 2006, 11:59
Heard SANParks EC120 recently had a governor failure. Anyone with more info? Was it a once off, or is it going to be something to watch for in the EC120?:confused:
B Sousa
13th Mar 2006, 13:42
Had a major fatal in the U.S. a few months ago with something in that area. Think it was a problem was found to be in the Fuel Control.
NTSB Identification: LAX05GA231
14 CFR Public Use
Accident occurred Wednesday, July 13, 2005 in Fair Oaks, CA
Aircraft: Eurocopter France EC120B, registration: N266SD
Injuries: 2 Fatal, 1 Serious.
This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed.
On July 13, 2005, about 1910 Pacific daylight time, an Eurocopter EC120B, N266SD, experienced a loss of engine power and collided with terrain near Fair Oaks, California. The Sacramento County Sheriff's Department was operating the public-use helicopter under the provisions of 14 CFR Part 91. The commercial pilot and the student pilot rated observer sustained fatal injuries, and the observer trainee sustained serious injuries. The helicopter sustained substantial damage. The local flight departed Mather, California. Visual meteorological conditions prevailed, and no flight plan had been filed. The approximate global positioning system (GPS) coordinates of the primary wreckage were 38 degrees 38 minutes north latitude and 121 degrees 13 minutes west longitude.
About 1910, the pilot transmitted "Mayday, mayday, mayday, we're going down." Within minutes of the mayday call, several people reported that they had just witnessed a possible helicopter crash. Witnesses reported hearing a "popping" noise and observed flames and smoke emitting from the exhaust of the helicopter just prior to impact. A grass fire consumed the hillside just above the accident site.
The helicopter was reported to be flying over steep, hilly, terrain. It impacted near the bottom of a 60-degree sloped hillside and rolled on its side after coming to rest at the base of the hill.
Post accident examination revealed a total loss of the free turbine blades. The main rotor blades revealed low rotational energy at the time of impact.