This N-number isn't registered right now. Below is its last known registration, canceled Mar 22, 2012.
Safety record in brief:1 NTSB accident (substantial damage, Sep 2009)3 ADs may apply12 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 inability to maintain control due to the mechanic's inadvertent switching of two cyclic control tubes of different lengths during maintenance.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN09LA571)
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.
BROKEN STUDS ON SCROLL. OVERHAUL, INSPECTED, WELD REPAIRED CRACK, INSTALLED (24) EACH NEW STUDS, STRESS RELIEVED, REPLACED (2) EACH INSERTS, AND APPLIED.
From FAA Service Difficulty Reports; matched by N-number and serial number.PERFORMED 6 MONTH INSPECTION. FLOAT HAS TORN END CAP, AND LEAK IN NR 2 CELL. PERFORMED 6 MONTH INSPECTION, REPLACED END CAP, & REPAIRED LEAK.
From FAA Service Difficulty Reports; matched by N-number and serial number.ALUMINUM DAMAGED BY IMPELLER. REMOVED AND RE-APPLIED PLASMA SPRAY ON CONTOUR. (OVERHAULED).
From FAA Service Difficulty Reports; matched by N-number and serial number.STIFF THROTTLE SHAFT. ROUGH/ DRY INTERNAL BEARINGS. ACTION TAKEN: SENT TO ACRO FOR REPAIR. REPAIRED AND TESTED IAW HONEYWELL OHM FORM 15-1095A.
From FAA Service Difficulty Reports; matched by N-number and serial number.NEW TIE BOLTS FROM STOCK THAT COULD NOT BE USED ON AIRCRAFT DUE TO PLATING FLAKING OFF ON MUTE.
From FAA Service Difficulty Reports; matched by N-number and serial number.TRANSMISSION MAKING METAL. LEFT PINION AND BEVEL GEAR BREAKING DOWN, LEFT INT SHAFT TEETH PITTED, LEFT FREEWHEEL WORN BEYOND LIMITS.
From FAA Service Difficulty Reports; matched by N-number and serial number.SCROLL COULD NOT BE INSTALLED DUE TO PLATING FLAKING OFF INSIDE RIGHT TURNING VANE.
From FAA Service Difficulty Reports; matched by N-number and serial number.ALTIMETER IS UNRELIABLE.
From FAA Service Difficulty Reports; matched by N-number and serial number.NEW METER SET ISSUED TO 131EH, BUT COULD NOT BE USED DUE TO DENT ON ORIFICE RIM; STREAKS.
From FAA Service Difficulty Reports; matched by N-number and serial number.NEW ALTIMETER WILL NOT TEST, COULD NOT BE INSTALLED ON AIRCRAFT.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 12 reports.