# Service difficulty reports: Construcciones Aeronauticas C-212-CC

A list on [Construcciones Aeronauticas C-212-CC](https://openairdocs.org/model/construcciones-aeronauticas-c-212-cc.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 5 · 201 reports

- [SDR UATA2650916265301](https://openairdocs.org/sdr/UATA2650916265301.md): Skin · damaged · Sep 16, 2026 · N1331C · Casa C212CC · Fuselage Main, Plate/Skin
  > FS 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
- [SDR UATA2026072835701](https://openairdocs.org/sdr/UATA2026072835701.md): Hinge Fitting · corroded · Jul 23, 2026 · N440RA · Casa C212CC · Wing, Control Surface Attach Fittings
  > 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 IN
- [SDR UATA20264105702](https://openairdocs.org/sdr/UATA20264105702.md): Skin · corroded · Apr 8, 2026 · N352CA · Casa C212CC · Trailing Edge Flaps
  > RH 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 FITTING
- [SDR UATA1900410265701](https://openairdocs.org/sdr/UATA1900410265701.md): Hinge · corroded · Apr 8, 2026 · N352CA · Casa C212CC · Trailing Edge Flaps
  > RH 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 N
- [SDR UATA2650406267901](https://openairdocs.org/sdr/UATA2650406267901.md): Oil Cooler · failed · Apr 6, 2026 · N1331C · Casa C212CC · Engine Oil Temperature
  > LEFT ENGINE OIL TEMPERATURE INCREASED TO REDLINE, PERFORMED PRECAUTIONARY SHUTDOWN. REMOVED AND REPLACED #1 OIL COOLER REF CASA MM 79-20-00 LEAK CHECK GOOD.
- [SDR UATA202603275702](https://openairdocs.org/sdr/UATA202603275702.md): Skin · cracked · Mar 20, 2026 · N440RA · Casa C212CC · Wing, Plate/Skin
  > 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 OUTBOAR
- [SDR UATA1740327265701](https://openairdocs.org/sdr/UATA1740327265701.md): Skin · cracked · Mar 20, 2026 · N440RA · Casa C212CC · Wing, Plate/Skin
  > 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 RIV
- [SDR UATA202603275304](https://openairdocs.org/sdr/UATA202603275304.md): Channel · worn · Mar 18, 2026 · N440RA · Casa C212CC · Fuselage Miscellaneous Structure
  > 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
- [SDR UATA1740327265303](https://openairdocs.org/sdr/UATA1740327265303.md): Doubler · cracked · Mar 18, 2026 · N440RA · Casa C212CC · Fuselage Main, Plate/Skin
  > 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
- [SDR UATA1740327265301](https://openairdocs.org/sdr/UATA1740327265301.md): Gusset · corroded · Mar 16, 2026 · N440RA · Casa C212CC · Fuselage Miscellaneous Structure
  > 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, ALOD
- [SDR UATA1750227265701](https://openairdocs.org/sdr/UATA1750227265701.md): Skin · cracked · Feb 27, 2026 · N348CA · Casa C212CC · Wing, Plate/Skin
  > TWO 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.
- [SDR UATA2025100605301](https://openairdocs.org/sdr/UATA2025100605301.md): Fairing · cracked · Sep 25, 2025 · N352CA · Casa C212CC · Wing Main, Frame Structure
  > FOUND 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.
- [SDR UATA1750815255701](https://openairdocs.org/sdr/UATA1750815255701.md): Hinge · cracked · Aug 13, 2025 · N348CA · Casa C212CC · Ailerons
  > LH 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 INST
- [SDR UATA1750702255301](https://openairdocs.org/sdr/UATA1750702255301.md): Channel · damaged · Jul 2, 2025 · N348CA · Casa C212CC · Fuselage Miscellaneous Structure
  > IMPACT 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 P
- [SDR UATA20205095701](https://openairdocs.org/sdr/UATA20205095701.md): Skin · corroded · May 8, 2025 · N348CA · Casa C212CC · Wing, Plate/Skin
  > CORROSION 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 0
- [SDR UATA1740327265302](https://openairdocs.org/sdr/UATA1740327265302.md): Seat Track · corroded · Mar 16, 2025 · N440RA · Casa C212CC · Fuselage, Seat/Cargo Attach Fittings
  > 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 SE
- [SDR UATA2025031915701](https://openairdocs.org/sdr/UATA2025031915701.md): Stiffener · cracked · Mar 11, 2025 · N348CA · Casa C212CC · Wing Miscellaneous Structure
  > CRACKED 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 STIFF
- [SDR UATA2650214255303](https://openairdocs.org/sdr/UATA2650214255303.md): Web · crushed · Feb 14, 2025 · N1331C · Casa C212CC · Fuselage Miscellaneous Structure
  > RH 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 PLAT
- [SDR UATA2650214255302](https://openairdocs.org/sdr/UATA2650214255302.md): Web · crushed · Feb 14, 2025 · N1331C · Casa C212CC · Fuselage Miscellaneous Structure
  > LH 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 SPLICE
- [SDR UATA2650214255301](https://openairdocs.org/sdr/UATA2650214255301.md): Frame · punctured · Feb 14, 2025 · N1331C · Casa C212CC · Fuselage Main, Frame
  > FOUND 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 INDICA
- [SDR UATA2024101045310](https://openairdocs.org/sdr/UATA2024101045310.md): Door Frame · cracked · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Structure (General)
  > LOWER 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.
- [SDR UATA202410100001](https://openairdocs.org/sdr/UATA202410100001.md): Door Frame · chafed · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Structure
  > LOWER 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.
- [SDR UATA202410105308](https://openairdocs.org/sdr/UATA202410105308.md): Frame · mechanic error · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Frame
  > MECHANIC 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. INSTA
- [SDR UATA202410105307](https://openairdocs.org/sdr/UATA202410105307.md): Fitting · corroded · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Miscellaneous Structure
  > LH 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.
- [SDR UATA202410105306](https://openairdocs.org/sdr/UATA202410105306.md): Fitting · corroded · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Miscellaneous Structure
  > RH 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.
- [SDR UATA2024101045305](https://openairdocs.org/sdr/UATA2024101045305.md): Skin · corroded · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Plate/Skin
  > LOWER 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.
- [SDR UATA2024101045304](https://openairdocs.org/sdr/UATA2024101045304.md): Frame · cracked · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Frame
  > FRAME 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 P
- [SDR UATA2024101045303](https://openairdocs.org/sdr/UATA2024101045303.md): Frame · cracked · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Frame
  > FRAME 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 DETAIL
- [SDR UATA1901010245302](https://openairdocs.org/sdr/UATA1901010245302.md): Floorbeam · corroded · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Floor Beam
  > UNDER 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
- [SDR UATA1901010245301](https://openairdocs.org/sdr/UATA1901010245301.md): Skin · damaged · Oct 10, 2024 · N352CA · Casa C212CC · Fuselage Main, Plate/Skin
  > LOWER 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 DETAIL
- [SDR UATA202408024531](https://openairdocs.org/sdr/UATA202408024531.md): Fairing · cracked · Jul 15, 2024 · N440RA · Casa C212CC · Aerodynamic Fairings
  > 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
- [SDR UATA202406105702](https://openairdocs.org/sdr/UATA202406105702.md): Profile · cracked · May 3, 2024 · N439RA · Casa C212CC · Wing Miscellaneous Structure
  > FOUND 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 REP
- [SDR UATA202406105301](https://openairdocs.org/sdr/UATA202406105301.md): Fitting · cracked · May 3, 2024 · N439RA · Casa C212CC · Fuselage Miscellaneous Structure
  > FOUND FLOOR BEAM TO SIDEWALL EXTRUDED FITTINGS TO BE CORRODED AND CRACKED AT FRAME 6 AND 11, BOTH RH AND LH. REPLACING FITTINGS WITH NEW.
- [SDR UATA202406105701](https://openairdocs.org/sdr/UATA202406105701.md): Fairing · loose · Apr 24, 2024 · N352CA · Casa C212CC · Wing Miscellaneous Structure
  > OB 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 24E3
- [SDR UATA202403183483](https://openairdocs.org/sdr/UATA202403183483.md): Skin · cracked · Feb 9, 2024 · N348CA · Casa C212CC · Fuselage Main, Plate/Skin
  > WHILE 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 PROV
- [SDR UATA202402023312](https://openairdocs.org/sdr/UATA202402023312.md): Skin · cracked · Jan 23, 2024 · N1331C · Casa C212CC · Fuselage Main, Plate/Skin
  > WHILE 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 REQUEST
- [SDR UATA202401043521](https://openairdocs.org/sdr/UATA202401043521.md): Skin · cracked · Jan 3, 2024 · N352CA · Casa C212CC · Fuselage Main, Plate/Skin
  > WHILE 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 REQUES
- [SDR UATA202312214394](https://openairdocs.org/sdr/UATA202312214394.md): Frame · cracked · Dec 21, 2023 · N439RA · Casa C212CC · Fuselage Main, Frame
  > WHILE 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.
- [SDR UATA202312013483](https://openairdocs.org/sdr/UATA202312013483.md): Skin · corroded · Nov 22, 2023 · N348CA · Casa C212CC · Wing, Plate/Skin
  > DURING 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.
- [SDR 2023F00302](https://openairdocs.org/sdr/2023F00302.md): Fitting · cracked · Oct 10, 2023 · N604AR · Casa C212CC · Horizontal Stabilizer, Attach Fittings
  > WHILE 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 212-3
- [SDR JTAA20230803001](https://openairdocs.org/sdr/JTAA20230803001.md): Fitting · cracked · Aug 3, 2023 · N604AR · Casa C212CC · Horizontal Stabilizer, Attach Fittings
  > DURING 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.
- [SDR JTAA20230803003](https://openairdocs.org/sdr/JTAA20230803003.md): Fitting · cracked · Aug 3, 2023 · N604AR · Casa C212CC · Fuselage, Stabilizer Attach Fittings
  > DURING 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.
- [SDR JTAA20230803002](https://openairdocs.org/sdr/JTAA20230803002.md): Fitting · cracked · Aug 3, 2023 · N604AR · Casa C212CC · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR UATA202309124392](https://openairdocs.org/sdr/UATA202309124392.md): Casting · cracked · Jul 18, 2023 · N439RA · Casa C212CC · Fuselage, Landing Gear Attach Fittings
  > DURING 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)
- [SDR UATA202306013481](https://openairdocs.org/sdr/UATA202306013481.md): Fairing · loose · Mar 23, 2023 · N348CA · Casa C212CC · Trailing Edge Flaps
  > UPON SCHEDULED MAINTENANCE INSPECTION, FOUND FIBERGLASS FLAP HINGE FAIRING LOOSENED, AND SUBSEQUENTLY CHAFED THE FLAP ATTACH PYLON BEYOND LIMITS.
- [SDR 2022F00329](https://openairdocs.org/sdr/2022F00329.md): Engine · failed · Aug 11, 2022 · N109BH · Casa C212CC · Engine (Turbine/Turboprop)
  > UNCOMMANDED RH ENGINE SHUTDOWN.
- [SDR UATA202203243311](https://openairdocs.org/sdr/UATA202203243311.md): Skin · gouged · Mar 24, 2022 · N1331C · Casa C212CC · Cargo/Baggage Doors
  > A 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
- [SDR UATA202203243482](https://openairdocs.org/sdr/UATA202203243482.md): Attach Fitting · cracked · Feb 23, 2022 · N348CA · Casa C212CC · Wing, Attach Fittings
  > DURING SCHEDULED MAINTENANCE, FOUND A CRACK IN THE R/H WING LOWER OUTBOARD ATTACH FITTING USING X-RAY METHOD.
- [SDR UATA2021122242416](https://openairdocs.org/sdr/UATA2021122242416.md): Skin · corroded · Nov 15, 2021 · N424CA · Casa C212CC · Wing, Plate/Skin
  > LOWER 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 2.26
- [SDR UATA2021111142415](https://openairdocs.org/sdr/UATA2021111142415.md): Spar Cap · cracked · Nov 11, 2021 · N424RA · Casa C212CC · Wing Spar
  > CRACK FOUND WHILE PERFORMING SID INSPECTIONS VIA X-RAY ON R/H WING BOTTOM FWD WING SPAR STRUCTURE CLOSE TO THE WING ROOT.

Next page: https://openairdocs.org/model/construcciones-aeronauticas-c-212-cc/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = 'C212CC'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/construcciones-aeronauticas-c-212-cc/reports

---
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