This N-number isn't registered right now. Below is its last known registration, canceled Jul 15, 2013.
Safety record in brief:1 NTSB accident (substantial damage, Apr 2007)3 ADs may apply5 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.
Fatigue cracking of the oil line from the engine gearbox to the oil pressure gauge, which resulted in loss of engine lubricating oil, leading to seizure of the power turbine.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA07LA108)
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 |
|---|---|---|---|
| 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.
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.
DURING REMOVAL OF M/R BLADES, FOUND ONE OF THE LEAD LAG/LINK BUSHINGS LOOSENED FROM LINK. PART REJECTED BY MDHS FIELD SERVICE REP. REPLACED DEFECTIVE LINK ASSY W/SERVICEABLE UNIT.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING ROUTINE INSPECTION OF AD 94-24-04, THE DUPLEX BEARING WAS LOOSE (AXIALLY) INSIDE OF PITCH CONTROL HOUSING (369A1802) - THE ENTIRE BEARING INCLUDING THE OUTER HOUSING OF THE BEARING. THIS COULD ALLOW THE BEARING TO SPIN INSIDE THE HOUSING. SUBMITTER STATED SHOULD BE PRESSURE FIT.
From FAA Service Difficulty Reports; matched by N-number and serial number.POWER CHECK RESULTS - LOW POWER. COMPRESSOR ASSY REPLACED, DISCREPANCY CLEARED. (ALLISON MODEL 250 REPORT NR A 134718).
From FAA Service Difficulty Reports; matched by N-number and serial number.MAIN ROTOR BLADE L/E ABRASION STRIP ERODED AT THE OUTBOARD END OF M/R BLADE NEAR THE TIP. CAUSE OF EROSION - OPERATING IN AND AROUND SAND AND DIRT DURING OFF-AIRPORT LANDINGS. REPAIR MADE TO AREA PER APPROVED ENG. DATA - 8110-3. M/R BLADE RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING ROUTINE/RECOMMENDED 1,000-HOUR INSPECTION OF THE OUTLET STRAINER ASSEMBLY, THE SCREEN WAS NOT INSTALLED, RATHER AN INLET FITTING, PN 1740235, WAS INSTALLED. THIS UNIT IS APPROXIMATELY 980 HOURS TSN. SUBMITTER RECOMMENDS COMPLETE INSPECTION OF ASSY (FILTER, SCREEN, PACKINGS, ETC.) PRIOR TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.