THE DELAYED FLARE AND THE IMPROPER TOUCHDOWN BY THE PILOT IN COMMAND. FACTORS WERE THE OPERATION OF THE AIRCRAFT WITH KNOWN DEFICIENCIES BY THE OPERATOR AND THE PILOT, DELAYED MAINTENANCE, AND, AN ENGINE COMPRESSOR ASSEMBLY STALL, COMBINED WITH EROSION AND CORROSION OF THE STATOR VANES WHICH RESULTED IN A COMPLETE LOSS OF POWER.
THE HELICOPTER WAS BEING USED ON AN AERIAL RIGHT-OF-WAY-BURNING FLT. THE PLT REPORTED THAT DUE TO THE TERRAIN & OBSTACLES, HIS ATTENTION WAS TO THE OUTSIDE OF THE HELICOPTER DURING THE BURNING OPERATION. AFTER COMPLETING THE BURNING OPERATION FOR THAT FLT, HE CHECKED THE ACFT FUEL QUANTITY & NOTED AN INDICATION OF 2 TO 3 GAL REMAINING. THE PLT IMMEDIATELY HEADED TOWARD THE LANDING AREA. APRX 1/4…
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
Bell Helicopter Textron Canada Limited Model 206A Series, 206B Series, 206L Series, 407…
May 1, 2009
Airframe (206B-III)Only with: Model 206A/206B/206L series with cyclic control lever assembly P/N 206-001-401-111, 206-001-400-115, or 206-001-400-111, and Model 407/427 with lever assembly P/N 407-001-320-105 or 407-001-320-109, with less than 50 hours TIS.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (0)
No Service Difficulty Reports found for this airframe since 1995.