Safety record in brief:1 NTSB accident (substantial damage, Feb 2009)No ADs since 1998 matched12 service difficulty reports
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The flight crew's decision to continue flight into adverse weather. Contributing to the accident was blowing snow which limited their visibility during final approach to land.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC09LA019)
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.
No ADs published since 1998 matched this airframe or engine model.
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.
RT & LT INNER FLAP, OTBD PYLON, OTBD HINGE FITTINGS FOUND CORRODED. APPROXIMATE WS 2900. REMOVED DAMAGED FITTINGS. COPIED EXISTING RIVET PATTERNS AND HOLE SIZE TO NEW FITTINGS. 5 RIVETS IN LT PYLON FITTING INSTALLATION OVERSIZED BY 1 SIZE FOR HOLE DAMAGE OR INSTALLATION OF BLIND FASTENERS. ALL…
From FAA Service Difficulty Reports; matched by N-number and serial number.RH WING HAS CRACK ON TRAILING EDGE UNDERSIDE ABOVE OUTBOARD FLAP ASSEMBLY AT WS4800 AS MARKED. REPAIRED CRACKED SECTION OF RT FLAP COVE SKIN. REMOVED 75MM X 25MM SECTION FROM INBOARD CRACKED AREA AND 90MM X 25MM SECTION FROM OUTBOARD CRACKED AREA. REMOVED RIVETS AS REQUIRED FROM UPPER FLAP COVE…
From FAA Service Difficulty Reports; matched by N-number and serial number.RIGHT WING HAS CRACK ON TRAILING EDGE UNDERSIDE ABOVE OUTBOARD FLAP ASSEMBLY AT WS5000 AS MARKED. REPAIRED CRACKED SECTION OF RH FLAP COVE SKIN. SEE 337 DATED 3/20/2026. REMOVED 75MM X 25MM SECTION FROM INBOARD CRACKED AREA AND 90MM X 25MM SECTION FROM OUTBOARD CRACKED AREA. REMOVED RIVETS AS…
From FAA Service Difficulty Reports; matched by N-number and serial number.REPAIR DOUBLER AT LOWER END OF FRAME 19 CRACKED (LH SIDE). REPLACED DOUBLER SEE 337 DATED 3/18/2026. CRACK FOUND AT DOUBLER FOR L/H FRAME 19. R&R WITH 2 DOUBLERS (ONE FWD AND ONE AFT OF FRAME) WITH .032IN 2024 T-3 ALUMINUM IRW CASA 212 SRM SECTION IV FIG 4.28 PAGES OA-02 AND CASA 212 SRM APPENDIX…
From FAA Service Difficulty Reports; matched by N-number and serial number.WEAR MARK ON C CHANNEL SECTION BETWEEN L/H FRAMES 17-20. R&R WITH P/N: 212-23201-03-1 IRW CASA 212 SRM SECTION IV FIGURE 4.28 PAGES 0A-02 & INSTALLED WITH FASTENERS AN470E5, AN470E6, AN426E4, AN426E5, HL18-5, HL18-6, HL70-5, & HL70-6. IRW AC-43.13-1 B SECTION 4-57 PAGES 4-14 TO 4-17 & SECTION 4-57…
From FAA Service Difficulty Reports; matched by N-number and serial number.RH SIDE FR 6 & FR 11 FLOOR SUPPORT GUSSETS NUT PLATES CORRODED. REPLACED F6/F11 JUNCTION BARS. FOUND 4 FUSELAGE JUNCTION FITTINGS CORRODED ON RH AT FRAME 6 & 11 UNDERFLOOR. FOUND RH WALL SEAT RAIL MIDDLE SECTION CORRODED. F6 & ALL NEW PARTS ACID ETCHED, ALODINED, AND PRIMED W/ 511K011 EPOXY…
From FAA Service Difficulty Reports; matched by N-number and serial number.RH SIDE WALL SEAT RAIL IS CORRODED AT FRAME 5F. REPLACED RH WALL MIDDLE SEAT RAIL SECTION. RH WALL SEAT RAIL SECTION. REMOVED SEAT RAIL. FABRICATED NEW SEAT RAIL FROM 206196-1 :2024-T3511 SEAT RAIL STOCK TO SAME DIMENSIONS AS PREVIOUSLY INSTALLED. INSTALLED SEAT RAIL USING CR3242 RIVETS, NAS1670…
From FAA Service Difficulty Reports; matched by N-number and serial number.THE FUSELAGE TO WING FILLET FAIRING, WHERE IT WRAPS AROUND THE FUSELAGE TO ATTACH AT FRAME 5 WAS FOUND CRACKED. THIS IS THE THIRD AIRCRAFT IN OUR FLEET THIS YEAR WITH A SIMILAR CRACK. THERE IS AN AD NOTE ON THE FRAME 5 AND FUSELAGE SKIN CRACKING IN THIS AREA, BUT THE ONLY CRACK WAS IN THE FAIRING…
From FAA Service Difficulty Reports; matched by N-number and serial number.UPON SCHEDULED UNDERFLOOR INSPECTION, FOUND FRAME 16F RIB WEBBING AT BL 0.0 SLIGHTLY BUCKLED OR DEFORMED. A DOUBLER WAS FABRICATED, USING 2024 T3 MATERIAL OF 0.040" THICKNESS, APPROXIMATELY 39.5" LONG BY 3.75" WIDE. DOUBLER WAS INSTALLED USING UNIVERSAL MS20470 RIVETS. CRITERIA FOR ACCOMPLISHING…
From FAA Service Difficulty Reports; matched by N-number and serial number.UPON SCHEDULED INSPECTION FOUND FRAME 14F SLIGHTLY BUCKLED. TECHNICIANS WERE ABLE TO STRAIGHTEN THE BUCKLE, AND FABRICATE A DOUBLER OF ONE GAUGE THICKER THAN ORIGINAL MATERIAL, 4.25" BY 10" IN SIZE. THE DOUBLER WAS INSTALLED USING AN470AD4 RIVETS. A FAA FORM 337 WAS FILED.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 12 reports.