This N-number isn't registered right now. Below is its last known registration, canceled Aug 10, 2009.
Safety record in brief:3 NTSB accidents (substantial damage at worst, latest Dec 1994)4 ADs may apply
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
THE PILOT'S FAILURE TO FOLLOW THE INFORMATION IN THE FLIGHT MANUAL CONCERNING THE USE OF THE PARTICLE SEPARATOR KIT AND DEFLECTOR KIT WHEN OPERATING IN FALLING SNOW. FACTORS WERE THE ROUGH TERRAIN IN THE FORCED LANDING AREA AND NO INSTALLATION OF THE DEFLECTOR KIT.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC95LA014)
WHILE ON A LOCAL FLT, THE PLT DESCENDED TO APRX 500 FT AGL AND FLEW THE HELICOPTER ALONG A COASTAL AREA. HE REPORTED THE HELICOPTER SUDDENLY LOST POWER AND HE INITIATED AN AUTOROTATIVE LANDING TO THE BEACH WHERE THE HELICOPTER 'HAD A HARD LANDING.' AN EXAM REVEALED A CRACKED AND BROKEN PNEUMATIC LINE AT THE FUEL CONTROLLER.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX86LA091)
THE PILOT REPORTED THAT THE ENGINE FAILED AT AN ALTITUDE OF 800 FEET MSL DURING THE CLIMB TO CRUISE PHASE OF A SIGHTSEEING FLIGHT WITH 3 PASSENGERS ON BOARD. THE ACFT LANDED IN THE SURF OF THE PACIFIC OCEAN AND DAMAGED THE TAIL ROTOR. THE PILOT AND PASSENGERS RECEIVED NO INJURIES. AN EXAMINATION OF THE FUEL SYSTEM DISCLOSED AN EXESS OF 3 GALLONS OF FRESH WATER IN THE TANK.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX85LA282)
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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2009-07-52 | 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. |
| 2006-16-04 | Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division… | Sep 7, 2006 | Engine (250-C20 SER) |
| 2006-13-06 | Rolls-Royce Corporation (Formerly Allison Engine Company, Allison Gas Turbine Division… | Jul 26, 2006 | Engine (250-C20 SER)Only with: Engines with gas producer rotor assembly tie bolt P/Ns A23008020, E23008020 (EXTEX), 23008020, 6843388, 6876991 (RRC), A23008020 (SAP), or 23008020P (Pacific Sky Supply) installed. |
| 2005-10-13 | Rolls-Royce Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E… | Jun 22, 2005 | Engine (250-C20 SER)Only with: Engines that do not have turbine energy absorbing ring RRC P/N 23035175, or an equivalent FAA-approved serviceable ring, installed. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
No Service Difficulty Reports found for this airframe since 1995.