This N-number isn't registered right now. Below is its last known registration, canceled Feb 26, 2008.
Safety record in brief:1 NTSB accident (destroyed damage, Aug 2004)3 ADs may apply6 service difficulty reports
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 maintain adequate terrain clearance during cruise, which resulted in the in-flight collision with mountainous terrain. Dark night conditions and mountainous terrain were contributing factors.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for SEA04FA166)
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 |
|---|---|---|---|
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (99)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; … |
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (99) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
OVERHAULED STARTER/GENERATOR. INSTALLED ON AIRCRAFT, WAS FOUND DEFECTIVE. ITEM WAS REMOVED FROM AIRCRAFT AND RETURNED. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.PRE-FLIGHT INSPECTION REVEALED A SMALL PORTION OF THE AILERON SKIN CRACKED AT THE INBOARD SECTION, TOP SKIN, TRAILING EDGE ADJACENT TO THE MOVABLE TRIM. FURTHER INSPECTION REVEALED EXTENSIVE CORROSION RELATED CRACKING MOSTLY ALONG THE TRAILING EDGE. REMOVED STATIC WICKS AND FOUND FURTHER…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING REPLACEMENT OF FLAP ACTUATORS, LEFT INBOARD FLAP MOVED IN THE OPPOSITE DIRECTION OF FLAP SELECTOR POSITION. REMOVED FLAP ACTUATOR AND DETERMINED THAT DRIVE ASSEMBLY WAS INCORRECT FOR INBOARD ACTUATOR. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK IN LEFT ELEVATOR TORQUE TUBE FOUND DURING 100-HOUR INSPECTION. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.UPON REMOVAL OF COMPRESSOR SECTION FROM RT SIDE, LOWER ENGINE MOUNT TUBE ASSY FOUND CHAFED ON TORSION TUBE BEYOND SERVICEABLE LIMITS. REPLACED ENTIRE MOUNT TUBE ASSY WITH SERVICEABLE MOUNT TUBE ASSY. CHAFE AREA DETERMINED TO BE IN VICINITY OF STAINLESS STEEL FIRESHIELD, LOWER SIDE. REPOSITIONED…
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOTS REPORTED VERY WEAK NAVIGATION RECEPTION, EVEN AFTER NUMEROUS CHECKS FROM AVIONICS SHOP EQUIPMENT. A DIFFERENT SET OF ANTENNAS WERE INSTALLED, BUT DID NOT RESOLVE PROBLEM. ONLY AFTER A NEW SET OF ANTENNAS WERE INSTALLED, DID THE PROBLEM DISAPPEAR.
From FAA Service Difficulty Reports; matched by N-number and serial number.