Safety record in brief:1 NTSB accident (substantial damage, Aug 2008)4 ADs may apply5 service difficulty reports
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The pilot's decision to attempt to takeoff on a short, wet runway with a heavily loaded airplane, and his failure to abort the takeoff before it became impracticable.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC08LA111)
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 |
|---|---|---|---|
| 2023-05-16 | Reciprocating Engine Power Section | Mar 15, 2023 | Engine (IO-520-L) |
| 2022-04-04 | Reciprocating Engine Oil System | Mar 29, 2022 | Engine (IO-520-L)Only with: F&M Enterprises, Inc. or Stratus Tool Technologies, LLC oil filter adapter installed per STC SE8409SW, SE09356SC, or SE10348SC. |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (207A) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO-520-L)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P 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.
BRAKES NO BRAKING ACTION-CORRECTIVE ACTION REPLACED BRAKE LININGS IAW C207MM 5-58. PERFORMED BRAKE BURN-IN IAW C207MM 5-59A. OPS CHECK GOOD. NO DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.AIRCRAFT ON GROUND AND PILOT REPORTS NO LEFT RUDDER AND NO LEFT BRAKE. MAINTENANCE INSPECTED AIRCRAFT AND DETERMINED THAT THE LEFT SIDE MASTER CYLINDER WAS SHEARED. MAINTENANCE REPLACED DEFECTIVE MASTER CYLINDER AS REQUIRED. NO OTHER DEFECTS WERE NOTED. TIME ON PART IS UNKNOWN.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTS FUEL LEAKING FROM REAR OF ENGINE COMPARTMENT. MAINTENANCE TIGHTENED LOOSE FUEL LINE BETWEEN ENGINE DRIVE FUEL PUMP AND FUEL CONTROL. GROUND RUN REVEALED NO FURTHER LEAKS.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING A PHASE INSPECTION, THE COPILOT LOWER OUTER DOOR SILL WAS FOUND CRACKED. REPLACED WITH A NEW.
From FAA Service Difficulty Reports; matched by N-number and serial number.EXHAUST VALVE APPARENTLY STUCK OPEN, WAS STRUCK BY PISTON AND IN TURN SLIGHTLY BENT AT THE STEM. THIS INADVERTENTLY CAUSE THE VALVE TO STICK IN A CLOSED POSITION THERE BY BENDING THE EXHAUST PUSHROD SLIGHTLY.
From FAA Service Difficulty Reports; matched by N-number and serial number.