Safety record in brief:1 NTSB accident (substantial damage, Sep 2025)11 ADs may apply3 service difficulty reports
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The pilot’s failure to maintain directional control during the departure roll resulting in a collision with a tractor/loader.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC25LA110)
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.
ANTENNA, PN 110-773 APPEARS TO BE BROKEN INTERNALLY. THE TOP PORTION OF THE ANTENNA, INCLUDING THE WIRE WHIP, CAN BE EASILY LIFTED OFF THE BASE. VISUAL INSP ALONE WILL NOT REVEAL THIS DISCONNECT. THIS ANTENNA IS PART OF THE ME406 ELT SYSTEM. THIS IS THE 4TH INCIDENT OF THIS CONDITION ON VARIOUS…
From FAA Service Difficulty Reports; matched by N-number and serial number.FELT SEALING STRIP APPROXIMATELY .5 INCH X 7 INCHES WAS COMING LOOSE FROM INSIDE THE ENGINE INDUCTION AIR PLENUM. OFFENDING FELT STRIP WAS REMOVED AS IT SERVES NO PURPOSE. THIS STRIP WAS LOCATED AT ABOUT 4 O’CLOCK ON THE INSIDE SURFACE ACROSS THE RT END OF THE LOWER PLENUM PANEL PN 2658039-19.…
From FAA Service Difficulty Reports; matched by N-number and serial number.LOWER SURFACE OF LT AND RT FORWARD WING SPARS AND LIFT STRUT ATTACH FITTINGS HAVE BEEN CHAFED BECAUSE OF CONTACT WITH THE LIFT STRUT UPPER FAIRING/COVER. WORST DAMAGE WAS LESS THEN .005 INCH IN DEPTH AND WAS EASILY BLENDED OUT. APPLIED VINYL CHAFE TAPE TO SPAR AND STRUT FITTINGS TO PREVENT…
From FAA Service Difficulty Reports; matched by N-number and serial number.