Safety record in brief:1 NTSB accident (substantial damage, Sep 2007)4 ADs may apply66 service difficulty reports
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The pilot's failure to maintain directional control during the landing roll. Factors include a ditch located between the runway and the taxiway.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA07CA261)
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 |
|---|---|---|---|
| 2020-16-06 | Horizontal Stabilizer Structure | Sep 1, 2020 | Airframe (A-1B) |
| 2006-10-21 | Engine Components Incorporated (ECi) Reciprocating Engine Connecting Rods | Jun 22, 2006 | Engine (O-360-A1P)Only with: ECi connecting rods P/N AEL11750 (forging P/N AEL11488) installed, rod serial numbers 54/6 and below, produced between January 2002 and January 2004. |
| 2006-06-16 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and… | Apr 27, 2006 | Engine (O-360-A1P)Only with: Engines manufactured new or rebuilt, overhauled, or that had a crankshaft installed after March 1, 1999. |
| 2005-19-11 | Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360… | Oct 21, 2005 | Engine (O-360-A1P)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999. |
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 TAKEOFF ROLL THE PITCH ASSYMETRIC WARNING CAME ON. REMOVED AND REPLACED THE CREW ALERTING COMPUTER.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING TAKEOFF THE RT ENGINE ITT WENT TO 765 DEGREES. CREW ABORTED THE TAKEOFF AND RETURNED TO BLOCK. REMOVED AND REPLACED THE ITT INDICATOR FOR THE RT ENGINE.
From FAA Service Difficulty Reports; matched by N-number and serial number.MIA - FLT 5069 - FOUND EMERGENCY LIGHTS DON'T WORK WHEN AIRCRAFT IS NOT POWERED UP. LIGHT DON NOT WORK WHEN POWER IS ON IE, OR EXTERNAL POWER RAI ALL 6 BATTERY PACKS (S/N 6506, 6498, 6406, 6635, 6399, 269). (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.SAW - DURING CPCP2 FOUND RIGHT FRAME 37 CORRODED ON AFT SIDE JUST ABOVE SILL PLATE CORRODED. REMOVED AND REPLACED FRAME 37 RIGHT IAW SRM 51-25-02 AND 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.SAW - DURING CPCP2 FOUND RIGHT FLOOR SUPPORT FROM FRAME 36 TO 38 CORRODED. REMOVED AND REPLACED RIGHT FLOOR SUPPORT IAW ATR42 SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.SAW - DURING CPCP2 FOUND RIGHT FLOOR SUPPORT FROM FRAME 38 TO 39 CORRODED. REMOVED AND REPLACED AND REPLACED RIGHT FLOOR SUPPORT IAW ATR 42 SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.SAW - DURING CPCP2 FOUND SERVICE DOOR SILL DRAIN TRACK CORRODED. REMOVED AND REPLACED SILL PLATE DRAIN TRACK IAW SRM 51-25-01 AND 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING CPCP4 INSPECTION, FOUND ALL PAX DOOR TREAD SUPPORTS HAVE CORROSION. REPLACED ALL PAX DOOR TREAD SUPPORTS IAW SRM 51-25-02. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP FORWARD BEAM ATTACH POINT CORRODED. REPLACED LEFT OUTBOARD FLAP ASSY IAW JIC 57-53-00-RAI-10000-006. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.SAW - DURING INSPECTION, FOUND LEFT OUTBOARD FLAP AFT BEAM ATTACH FITTING CORRODED. REPLACED LEFT OUTBOARD FLAP ASSEMBLY IAW JIC 57-53-00-RAI-10000-006. (M)
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 66 reports.