Construcciones Aeronauticas C-212-CC

Service difficulty reports · 201

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'C212CC'
  ORDER BY difficulty_date DESC"

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SDR UATA2650916265301Skin · damagedFS 27 LOWER BEAM & LOWER SKINS DAMAGED. REMOVED F27 LOWER BEAM. PREVIOUSLY REPAIRED RT LOWER SKIN SECTION, LT & RT FS27 TO C CHANNEL BRACKETS/CVR BOX MOUNTING STRUCTURE. CUT MIDDLE/LH LOWER SKINS JUST AHEAD OF F28 FLANGE REMOVING FWD ~13" OF BOTH SKINS. FAB'D Sep 16, 2026 · N1331C · Casa C212CC · Fuselage Main, Plate/SkinSDR UATA2026072835701Hinge Fitting · corrodedRT & 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 INJul 23, 2026 · N440RA · Casa C212CC · Wing, Control Surface Attach FittingsSDR UATA20264105702Skin · corrodedRH INNER FLAP, OUTBOARD PYLON, OUTBOARD SKIN CORRODED. RH INNER FLAP, OUTBOARD PYLON, HINGE FITTINGS AND OUTBOARD SKIN FOUND CORRODED. APPROXIMATE WING STATION 2900. REMOVED DAMAGED FITTINGS AND SKIN. COPIED EXISTING RIVET PATTERNS AND HOLE SIZE TO NEW FITTINGApr 8, 2026 · N352CA · Casa C212CC · Trailing Edge FlapsSDR UATA1900410265701Hinge · corrodedRH INBOARD FLAP, OUTBOARD PYLON BOTH FLAP HINGE PLATES CORRODED. RH INNER FLAP, OUTBOARD PYLON, HINGE FITTINGS AND OUTBOARD SKIN FOUND CORRODED. APPROXIMATE WING STATION 2900. REMOVED DAMAGED FITTINGS AND SKIN. COPIED EXISTING RIVET PATTERNS AND HOLE SIZE TO NApr 8, 2026 · N352CA · Casa C212CC · Trailing Edge FlapsSDR UATA2650406267901Oil Cooler · failedLEFT ENGINE OIL TEMPERATURE INCREASED TO REDLINE, PERFORMED PRECAUTIONARY SHUTDOWN. REMOVED AND REPLACED #1 OIL COOLER REF CASA MM 79-20-00 LEAK CHECK GOOD.Apr 6, 2026 · N1331C · Casa C212CC · Engine Oil TemperatureSDR UATA202603275702Skin · crackedRIGHT 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 OUTBOARMar 20, 2026 · N440RA · Casa C212CC · Wing, Plate/SkinSDR UATA1740327265701Skin · crackedRH 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 RIVMar 20, 2026 · N440RA · Casa C212CC · Wing, Plate/SkinSDR UATA202603275304Channel · wornWEAR 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 Mar 18, 2026 · N440RA · Casa C212CC · Fuselage Miscellaneous StructureSDR UATA1740327265303Doubler · crackedREPAIR 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 Mar 18, 2026 · N440RA · Casa C212CC · Fuselage Main, Plate/SkinSDR UATA1740327265301Gusset · corrodedRH 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, ALODMar 16, 2026 · N440RA · Casa C212CC · Fuselage Miscellaneous StructureSDR UATA1750227265701Skin · crackedTWO CRACKS FOUND IN TRAILING EDGE OF LT LOWER INNER FLAP COVE AT APPROXIMATE WS 1800 & 2800. REMOVED 6 1/4 X 2 3/8 SECTION FROM OTBD CRACKED AREA & 4 1/4 X 2 3/8 SECTION FROM INBD CRACKED AREA. REMOVED RIVETS AS REQUIRED FROM UPPER FLAP COVE SKIN FOR ACCESS. Feb 27, 2026 · N348CA · Casa C212CC · Wing, Plate/SkinSDR UATA2025100605301Fairing · crackedFOUND CRACK IN RH WING TO FUSELAGE FAIRING AT FRAME F5. (SEE AOT-C212-53-0001 FOR DETAILS). REPAIRED CRACK DAMAGE AND REINFORCED F5 RH BY INSTALLATION OF SB KIT SB212530055K01. SEE 337 DATED 09/25/2025. FOR FURTHER DETAILS.Sep 25, 2025 · N352CA · Casa C212CC · Wing Main, Frame StructureSDR UATA1750815255701Hinge · crackedLH AILERON CENTER HINGE STRUCTURE, A PREVIOUS REPAIR PATCH IS CRACKED. REPAIR WAS ACCOMPLISHED AS FOLLOWS: REMOVED THE PREVIOUS CRACKED REPAIR ANGLE. USING THE ORIGINAL ANGLE AS A PATTERN A NEW ANGLE WAS FABRICATED FROM 301 STAINLESS STEEL 0.040 THICK AND INSTAug 13, 2025 · N348CA · Casa C212CC · AileronsSDR UATA1750702255301Channel · damagedIMPACT DAMAGE FOUND IN C CHANNEL AFT OF F19. REMOVED DAMAGED C CHANNEL AND INTERCOSTALS AT F18 AND F19 THAT WERE MODIFIED TO ACCEPT A PREVIOUS REPAIR TO OLD C CHANNEL. FABRICATED NEW INTERCOSTALS FOR F18 AND F19. ALL NEW PARTS WERE ACID ETCHED, ALODINED AND PJul 2, 2025 · N348CA · Casa C212CC · Fuselage Miscellaneous StructureSDR UATA20205095701Skin · corrodedCORROSION FOUND ON LOWER SURFACE OF LH WING AT W.S. 3450. REMOVED BRACE STRUT AT APPROXIMATE W.S. 3200 AND SPLICE PLATE AT APPROX. W.S. 3060 FOR ACCESS TO REPAIR AREA. REMOVED DAMAGED SKIN, REMOVED SEALANT FROM PREVIOUS INSTALLATION. FABRICATED NEW SKIN FROM 0May 8, 2025 · N348CA · Casa C212CC · Wing, Plate/SkinSDR UATA1740327265302Seat Track · corrodedRH 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 SEMar 16, 2025 · N440RA · Casa C212CC · Fuselage, Seat/Cargo Attach FittingsSDR UATA2025031915701Stiffener · crackedCRACKED U CHANNEL IN AFT LH CENTER WING SECTION STATION 2380, AS FLAGGED. REPLACED CRACKED STIFFENER WITH NEW. SEE 337 DATED 03/11/2025 FOR FURTHER INFO. FAA FORM 337 STATES: FOUND CRACK IN STIFFENER ON THE LEFT CENTER WING AFT BEAM AT W.S. 2380. CRACKED STIFFMar 11, 2025 · N348CA · Casa C212CC · Wing Miscellaneous StructureSDR UATA2650214255303Web · crushedRH SEAT RAIL LONGITUDINAL WEB CRUSHED AT F17. REPAIRED IAW C212 SRM B26. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED SECTION OF WEB ~4.5 X 9". FABRICATED REPLACEMENT WEB SECTION TO SAME DIMENSIONS AS REMOVED FROM 2024T3 0.025", AND SPLICE PLATFeb 14, 2025 · N1331C · Casa C212CC · Fuselage Miscellaneous StructureSDR UATA2650214255302Web · crushedLH SEAT RAIL LONGITUDINAL WEB CRUSHED AT F17. REPAIRED IAW C212 SRM B26. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED SECTION OF WEB ~ 5.5" X 9.5". FABRICATED REPLACEMENT WEB SECTION TO SAME DIMENSIONS AS REMOVED FROM 2024T3 0.025", AND SPLICEFeb 14, 2025 · N1331C · Casa C212CC · Fuselage Miscellaneous StructureSDR UATA2650214255301Frame · puncturedFOUND A SMALL PUNCTURE IN THE AFT SIDE OF THE RH WEB OF FRAME 11, 2 INCHES ABOVE FLOOR LEVEL. REPAIRED PER CASA ENGINEERING DOC 252EA-00020 REV A. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED MATERIAL. DAMAGED AREA INSPECTED BY HFEC, NO INDICAFeb 14, 2025 · N1331C · Casa C212CC · Fuselage Main, FrameSDR UATA2024101045310Door Frame · crackedLOWER CARGO DOOR CUTOUT FRAME, LH SIDE "C" CHANNEL HAS A CRACK IN THE UPPER FLANGE JUST AFT OF FRAME 19. INSTALLED AN INTERNAL REINFORCING DOUBLER BEHIND THE CRACK.. SEE FORM 337 FOR DETAILS OF THE REPAIR.Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Structure (General)SDR UATA202410100001Door Frame · chafedLOWER CARGO DOOR CUTOUT FRAME, RH SIDE "C" CHANNEL HAS 2 CHAFE MARKS IN THE UPPER RADIUS, JUST FWD. OF FRAME 19. BLENDED CHAFFED AREAS AND INSTALLED AN INTERNAL REINFORCING DOUBLER BEHIND THE CHAFFED AREAS. SEE FORM 337 FOR DETAILS OF THE REPAIR.Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, StructureSDR UATA202410105308Frame · mechanic errorMECHANIC INDUCED DAMAGE TO FRAME 11 WEB, UNDER THE FLOOR, 5 INCHES LEFT OF CENTER. DRESSED OUT THE DAMAGED AREA & FABRICATED A DOUBLER 2 1/4 INCH BY 3 INCHES OF 2024 T3 ALUMINUM 0.040 THICK. ETCHED & ALODINED THAN PRIMED WITH SUPPER KOROPON EPOXY PRIMER. INSTAOct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, FrameSDR UATA202410105307Fitting · corrodedLH SIDE EXTRUSION ON AFT SIDE OF FRAME 11, UNDER FLOOR HAS EXFOLIATION CORROSION. REPLACED EXTRUSION WITH NEW 212-22406-07-2. SEE FORM 337 DATED 9/20/2024 FOR FURTHER DETAIL.Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Miscellaneous StructureSDR UATA202410105306Fitting · corrodedRH SIDE EXTRUSION ON FWD. SIDE OF FRAME 11, UNDER FLOOR IS CRACKED. (BOUNDARY LAYER CORROSION). REPLACED EXTRUSION WITH NEW 212-22406-06-1. SEE FORM 337 DATED 9/20/2024 FOR FURTHER DETAIL.Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Miscellaneous StructureSDR UATA2024101045305Skin · corrodedLOWER LH SKIN BETWEEN FRAME 17 AND 18 CORRODED. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN AND INSTALLED. SEE FORM 337 DATED 9/20/2024 FOR FURTHER DETAIL.Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Plate/SkinSDR UATA2024101045304Frame · crackedFRAME 19 RH CRACKED BEHIND ACTUATOR ATTACH POINT. REMOVED THE OLD REINFORCEMENT DOUBLER REPAIR. FABRICATED A NEW DOUBLER FROM 2024 T3 ALCLAD ALUMINUM 0.050 THICK, 6 INCHES TALLER THAN THE PREVIOUS DOUBLER (10 INCHES TOTAL). ETCHED AND ALODINE THE DOUBLER AND POct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, FrameSDR UATA2024101045303Frame · crackedFRAME 19 CRACKED BEHIND LH ACTUATOR ATTACH POINT. FABRICATED AND INSTALLED NEW LOWER FRAME 19 AND ACTUATOR ATTACH POINT DOUBLER. SEE FORM 337 DATED 9/20/2024 FOR FURTHER DETAILOct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, FrameSDR UATA1901010245302Floorbeam · corrodedUNDER SIDE OF THE UPPER "T" FLANGE AT FRAME 11, THERE IS EXFOLIATION CORROSION UNDER THREE DIFFERENT NUT PLATES (CENTER AREA). REMOVED A 21 INCH SECTION OF THE CENTER "T" FLANGE BETWEEN THE TWO FLOOR SEAT TRACKS. FABRICATED A NEW LENGTH OF "T" FLANGE FROM THE Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Floor BeamSDR UATA1901010245301Skin · damagedLOWER RH SIDE SKIN BETWEEN FRAME 17 AND 18 CORRODED. REMOVED DAMAGED SKIN, FABRICATED NEW SKIN AND INSTALLED. SEE FORM 337 DATED 9/20/2024 FOR FURTHER DETAILOct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Plate/SkinSDR UATA202408024531Fairing · crackedTHE 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 AREAJul 15, 2024 · N440RA · Casa C212CC · Aerodynamic FairingsSDR UATA202406105702Profile · crackedFOUND A CRACKED PROFILE ON THE AFT FALSE SPAR OF THE LH WING AT STA 2820. PROFILES AT FURTHER OUT STATIONS HAVE INSPECTIONS REQUIRED BY AN AD NOTE 98-12-28 WHICH DIDN'T COVER THIS PROFILE. THE CRACKED PROFILE WAS REMOVED AND ANOTHER PROFILE FABRICATED TO REPMay 3, 2024 · N439RA · Casa C212CC · Wing Miscellaneous StructureSDR UATA202406105301Fitting · crackedFOUND FLOOR BEAM TO SIDEWALL EXTRUDED FITTINGS TO BE CORRODED AND CRACKED AT FRAME 6 AND 11, BOTH RH AND LH. REPLACING FITTINGS WITH NEW.May 3, 2024 · N439RA · Casa C212CC · Fuselage Miscellaneous StructureSDR UATA202406105701Fairing · looseOB FLAP, IB HINGE FWD FAIRING BECAME LOOSE AND CHAFED INTO THE BOTTOM SKIN OF THE RH WING, JUST FORWARD OF THE HINGE. THE DAMAGE SPECIFICATIONS WERE SENT TO AIRBUS ENGINEERING AND THEY PRODUCED REPAIR INSTRUCTIONS ON ENGINEERING AUTHORIZATION (EA) NUMBER 24E3Apr 24, 2024 · N352CA · Casa C212CC · Wing Miscellaneous StructureSDR UATA202403183483Skin · crackedWHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.5" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE INSPECTED BY THE AOT. THE OEM HAS BEEN CONTACTED, THE SITUATION REPORTED, AND A REPAIR SCHEME WAS PROVFeb 9, 2024 · N348CA · Casa C212CC · Fuselage Main, Plate/SkinSDR UATA202402023312Skin · crackedWHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.070" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE INSPECTED BY THE AOT. THE OEM HAS BEEN CONTACTED, HE SITUATION REPORTED, AND A REPAIR SCHEME REQUESTJan 23, 2024 · N1331C · Casa C212CC · Fuselage Main, Plate/SkinSDR UATA202401043521Skin · crackedWHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.719" WAS FOUND ON THE FUSELAGE SKIN IN THE AREA OUTLINED TO BE INSPECTED BY THE AOT. THE OEM HAS BEEN CONTACTED, THE SITUATION REPORTED, AND A REPAIR SCHEME REQUESJan 3, 2024 · N352CA · Casa C212CC · Fuselage Main, Plate/SkinSDR UATA202312214394Frame · crackedWHILE INSPECTING THE AIRFRAME PER AD2022-17-06, AOT C212-53-0001 AND SB212-53-0055, A CRACK OF 0.75" WAS FOUND IN THE AREA OUTLINED. THE AIRCRAFT WAS REPAIRED BY PARTIALLY APPLYING THE SB ALREADY MENTIONED, AND AN EA FROM THE MANUFACTURER.Dec 21, 2023 · N439RA · Casa C212CC · Fuselage Main, FrameSDR UATA202312013483Skin · corrodedDURING MAINTENANCE, SEVERE CORROSION WAS FOUND IN THE UPPER SKIN OF THE R/H WING BETWEEN STA. 2380 AND STA. 2900, CENTERED OVER STRINGER #1. UNDER THE ENGINE NACELLE FAIRING/SCALLOP.Nov 22, 2023 · N348CA · Casa C212CC · Wing, Plate/SkinSDR 2023F00302Fitting · crackedWHILE INVESTIGATING HORIZONTAL FITTINGS ON FUSELAGE SIDE DUE TO CRACKS IN FITTINGS, FOUND MATING FITTINGS ATTACHED TO HORIZONTAL STABILIZERS CRACKED AS WELL WHEN INSPECTED POST STABILIZER REMOVAL FROM EMPENNAGE. R/H STABILIZER AFT SPAR ATTACH FITTING P/N 212-3Oct 10, 2023 · N604AR · Casa C212CC · Horizontal Stabilizer, Attach FittingsSDR JTAA20230803001Fitting · crackedDURING A 1Y, 2Y, 4Y CPCP INSPECTION OF THE EMPENNAGE OF S/N 289 IT WAS FOUND 6 OUT OF 8 OF THE HORIZONTAL STABILIZER FITTINGS CRACKED. THE CRACKS WERE FOUND IN THE RADIUS OF ONE OF THE FITTINGS & FROM FASTNER TO FASTNER ON OTHERS.Aug 3, 2023 · N604AR · Casa C212CC · Horizontal Stabilizer, Attach FittingsSDR JTAA20230803003Fitting · crackedDURING A 1Y, 2Y, 4Y CPCP INSPECTION OF THE EMPENNAGE OF S/N 289 IT WAS FOUND 6 OUT OF 8 OF THE HORIZONTAL STABILIZER FITTINGS CRACKED. THE CRACKS WERE FOUND IN THE RADIUS OF ONE OF THE FITTINGS & FROM FASTNER TO FASTNER ON OTHERS.Aug 3, 2023 · N604AR · Casa C212CC · Fuselage, Stabilizer Attach FittingsSDR JTAA20230803002Fitting · crackedDURING A 1Y, 2Y, 4Y CPCP INSPECTION OF THE EMPENNAGE OF S/N 289 IT WAS FOUND 6 OUT OF 8 OF THE HORIZONTAL STABILIZER FITTINGS CRACKED. THE CRACKS WERE FOUND IN THE RADIUS OF ONE OF THE FITTINGS & FROM FASTNER TO FASTNER ON OTHERS.Aug 3, 2023 · N604AR · Casa C212CC · Fuselage Miscellaneous StructureSDR UATA202309124392Casting · crackedDURING ROUTINE SCHEDULED MAINTENANCE FOUND A CRACK IN THE R/H MLG UPPER FORWARD LANDING GEAR ATTACH POINT CASTING. REMOVED AND REPLACED CASTING. THIS SCHEDULED INSPECTION IS PART OF AN INSPECTION PROGRAM THAT WAS BROUGHT ON BY AD96-07-14. (PSE53-20-08)Jul 18, 2023 · N439RA · Casa C212CC · Fuselage, Landing Gear Attach FittingsSDR UATA202306013481Fairing · looseUPON SCHEDULED MAINTENANCE INSPECTION, FOUND FIBERGLASS FLAP HINGE FAIRING LOOSENED, AND SUBSEQUENTLY CHAFED THE FLAP ATTACH PYLON BEYOND LIMITS.Mar 23, 2023 · N348CA · Casa C212CC · Trailing Edge FlapsSDR 2022F00329Engine · failedUNCOMMANDED RH ENGINE SHUTDOWN.Aug 11, 2022 · N109BH · Casa C212CC · Engine (Turbine/Turboprop)SDR UATA202203243311Skin · gougedA FORKLIFT LOADING THE AIRCRAFT SLIPPED ON ICE, AND HIT THE AFT UPPER CARGO DOOR AS WELL AS THE AIRCRAFT STRUCTURE DIRECTLY AFT OF THE DOOR, CAUSING GOUGING, AS WELL AS BUCKLING OF THE ASSOCIATED FRAMES. DAMAGE WAS REPAIRED IAW THE SRM, AND A FAA FORM 337 WAS Mar 24, 2022 · N1331C · Casa C212CC · Cargo/Baggage DoorsSDR UATA202203243482Attach Fitting · crackedDURING SCHEDULED MAINTENANCE, FOUND A CRACK IN THE R/H WING LOWER OUTBOARD ATTACH FITTING USING X-RAY METHOD.Feb 23, 2022 · N348CA · Casa C212CC · Wing, Attach FittingsSDR UATA2021122242416Skin · corrodedLOWER WING SKIN SECTION @ WING STATION 2800 UNDER FLAP PYLON WAS FOUND TO HAVE SEVERE PITTING CORROSION. FABRICATED NEW SKIN AS PER ORIGINAL, AND REPLACED PER AC43.13-1B, PAR 4-53, 4-55, 4-57 AND CASA 212 SRM SECT. II, FIG 2.26Nov 15, 2021 · N424CA · Casa C212CC · Wing, Plate/SkinSDR UATA2021111142415Spar Cap · crackedCRACK FOUND WHILE PERFORMING SID INSPECTIONS VIA X-RAY ON R/H WING BOTTOM FWD WING SPAR STRUCTURE CLOSE TO THE WING ROOT.Nov 11, 2021 · N424RA · Casa C212CC · Wing Spar
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