Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Mar 2022)11 ADs may apply3 service difficulty reports
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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 failure of the pilot of the second aircraft to maintain a safe distance from the lead airplane while taxiing, which resulted in a ground collision.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN22LA149)
The pilot's inadequate pre-flight inspection, which resulted in a decrease in airplane performance due to ice, and a subsequent hard landing.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC04LA050)
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 |
|---|---|---|---|
| 2021-04-10 | Textron Aviation, Inc. Airplanes | Apr 12, 2021 | Airframe (208B)Certain serial numbers: 208 20800564–20800594; 208 20800603–20800605; 208B 208B5141–208B5285; 208B 208B5287–208B5305; 208B 208B5307–208B5312; 208B 208B5314; … |
| 2009-15-05 | Cessna Aircraft Company Models 208 and 208B Airplanes | Jul 27, 2009 | Airframe (208B)Certain serial numbers: 208 20800500–20800504; 208B 208B1216; 208B 208B2001; 208B 208B2003–208B2023; 208B 208B2025–208B2029; 208B 208B2031–208B2037; … |
| 2009-05-12 | Cessna Aircraft Company Models 208 and 208B Airplanes | Apr 15, 2009 | Airframe (208B)Certain serial numbers: 208 20800001–20800415; 208 20800417–20800419; 208B 208B0001–208B1081; 208B 208B1083–208B1215; 208B 208B1217–208B1257; 208B 208B1259–208B1305; … |
| 2008-13-06 | Cessna Aircraft Company Models 208 and 208B Airplanes | Jul 30, 2008 | Airframe (208B)Certain serial numbers: 208 20800001–20800415; 208B 208B0001–208B1299 |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (208B)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2007-10-15 | Cessna Aircraft Company Models 208 and 208B Airplanes | Jun 21, 2007 | Airframe (208B) |
| 2006-01-11 R1 | The Cessna Aircraft Company Models 208 and 208B Airplanes | Feb 22, 2006 | Airframe (208B) |
| 2004-08-17 | Cessna Aircraft Company Models 208 and 208B Airplanes | May 17, 2004 | Airframe (208B)Certain serial numbers: 208 20800370; 208 20800371; 208B 208B1034–208B1043; 208B 208B1045; 208B 208B1046; 208B 208B1048 |
| 2003-21-04 | Cessna Aircraft Company Models 208 and 208B Airplanes | Oct 21, 2003 | Airframe (208B)Certain serial numbers: 208 20800001–20800369; 208B 208B0001–208B1014; 208B 208B1017; 208B 208B1018; 208B 208B1020–208B1024; 208B 208B1026; … |
| 2002-22-17 | Cessna Aircraft Company Models 208 and 208B Airplanes | Dec 31, 2002 | Airframe (208B) |
| 97-25-04 | Cessna Aircraft Company Models 208, 208A, 208B, 425, and 441 Airplanes | Jan 21, 1998 | Airframe (208B) |
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 THE LAST PHASE INSPECTION A CRACK WAS DISCOVERED IN THE LEFT ELEVATOR TORQUE TUBE.
From FAA Service Difficulty Reports; matched by N-number and serial number.AFTER ENGINE INSTALLATION FROM OVERHAUL, THE PERFORMANCE RUN PRODUCED THE "AUX FUEL PUMP" AND "FUEL PRESSURE LOW" LIGHTS ON THE ANNUNCIATOR PANEL CYCLING ON AND OFF TOGETHER. THIS HAPPENS WHEN THE FUEL PRESSURE IN THE HOPPER TANK DROPS BELOW 4.75 PSI. (FUEL PUMP 0.00) (K)
From FAA Service Difficulty Reports; matched by N-number and serial number.AUTOPILOT WOULD NOT DISENGAGE IN PITCH CONTROL DUE TO SHORTED Q-211 (PITCH ENGAGE TRANSISTOR) SUPPLYING CONTINUOUS POWER TO PITCH SERVO-CLUTCH. AUTOPILOT WAS ABLE TO BE DISENGAGED BY HOLDING DOWN AUTOPILOT DISCONNECT BUTTON AND PULLING AUTOPILOT CIRCUIT BREAKER.
From FAA Service Difficulty Reports; matched by N-number and serial number.