This N-number isn't registered right now. Below is its last known registration, canceled Aug 27, 2024.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Jun 2012)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 inadvertently taxied the airplane into a ditch.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC12CA048)
The pilot's selection of an unsuitable, rough, runway. Factors were the crosswind, the pilot's inexperience, the company's inadequate surveillance of their operation, and dispatch of an inexperienced pilot to the unsuitable airport.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC00LA115)
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-F) |
| 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-F)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.
ALTERNATOR INOPERATIVE.
From FAA Service Difficulty Reports; matched by N-number and serial number.VERY LOW RIPPLE VOLTAGE PRODUCED BY UNIT, DROPS OFFLINE UNDER LOAD.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED LOSS OF POWER AND VIBRATION ON LANDING. MAINTENANCE DISCOVERED THE NR 3 CYLINDER HEAD CRACKED.
From FAA Service Difficulty Reports; matched by N-number and serial number.PILOT REPORTED POWER LOSS AND VIBRATION - RE-ROUTED AND MADE A SAFE LANDING. MAINTENANCE DISCOVERED THE NR 2 CYLINDER HAD 100 PERCENT HEAD SEPARATION AT THE HEAD TO BARREL INTERFACE IN LINE WITH THE TOP OF THE STEEL BARREL.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOLLOWING REPAIR FROM LANDING ACCIDENT, ON FIRST FLIGHT AFTER REPAIRS, PILOT REPORTED AIRSPEED APPEARED TO INDICATE 30 KNOTS LOW. POST FLIGHT MAINTENANCE REVELED A CHAFE HOLE IN PITOT LINE IN LEFT WING AT A NOSE RIB.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOLLOWING REPAIR FROM LANDING ACCIDENT, ON FIRST FLIGHT AFTER REPAIRS, PILOT REPORTED AIRSPEED APPEARED TO INDIDCATE 30 KNOTS LOW. POST FLIGHT MAINTENANCE REVELED A CHAFE HOLE IN PITOT LINE IN LT WING AT A NOSE RIB.
From FAA Service Difficulty Reports; matched by N-number and serial number.