# Service difficulty reports: Construcciones Aeronauticas C-212-200

A list on [Construcciones Aeronauticas C-212-200](https://openairdocs.org/model/construcciones-aeronauticas-c-212-200.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 83 reports

- [SDR JTAA20260821001](https://openairdocs.org/sdr/JTAA20260821001.md): Engine · making metal · Aug 21, 2026 · N309HG · Casa C212200 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILED IN FLIGHT. ON INSPECTION FOUND METAL PARTICLES IN OIL FILTER BOWL.
- [SDR UATA2420714265701](https://openairdocs.org/sdr/UATA2420714265701.md): Rib · buckled · Jul 8, 2026 · N424CA · Casa C212200 · Wing, Rib/Bulkhead
  > LEFT WING HAS BUCKLED RIB AND WRINKLED SKIN AT WING STATION 6500. CAUSE/TIMEFRAME OF DAMAGE UNKNOWN. WING APPEARS TO HAVE ENDURED IMPACT ON BOTTOM OF WING TIP AREA. SFP APPROVED BY ANC FSDO FOR RELOCATION TO GREYBULL, WY FOR REPAIRS.
- [SDR UATA2870513265701](https://openairdocs.org/sdr/UATA2870513265701.md): Stiffener · cracked · May 6, 2026 · N439RA · Casa C212200 · Wing Main, Frame Structure
  > FOUND A CRACK IN STIFFENER ON THE LH WING FALSE SPAR AT W.S. 4900. THE CRACKED STIFFENER WAS R&R WITH NEW, FABRICATED STIFFENER MADE FROM 2024-T3 ALUMINUM.032" THICK, THE PRE-EXISTING SPACER HAD NO DAMAGE AND WAS REUSED. THE NEW STIFFENER WAS PRIMED WITH SUPE
- [SDR UATA2420127265305](https://openairdocs.org/sdr/UATA2420127265305.md): Floorbeam · collapsed · Jan 27, 2026 · N424CA · Casa C212200 · Fuselage Main, Floor Beam
  > - F15 WEB SAGGING UNDERFLOOR - REMOVED FRAME15 TOP CAP AND FABRICATED A NEW CAP FROM 2024 T351 ALUMINUM "T" ANGLE, 0.084 THICK, 38.5 INCHES LONG. STRAIGHTENED OUT THE WEB ON FRAME 15. FABRICATED A DOUBLER FROM 2024 T3, 0.032" THICK MEASURING 38.5" LONG X 3 1/4
- [SDR UATA2420127265304](https://openairdocs.org/sdr/UATA2420127265304.md): Floorbeam · corroded · Jan 27, 2026 · N424CA · Casa C212200 · Fuselage Main, Floor Beam
  > F16 TOP CAP CORRODED AT NUT PLATES. REMOVED FRAME 16 TOP CAP AND FABRICATED A NEW CAP FROM 2024 T351 ALUMINUM "T" ANGLE, 0.100 THICK. ETCHED AND ALODINED THE "T" ANGLE AND PRIMED WITH SUPER KOROPON EPOXY PRIMER. INSTALLED THE "T" ANGLE USING MS20470AD-4 AND MS
- [SDR UATA2420127265303](https://openairdocs.org/sdr/UATA2420127265303.md): Floorbeam · buckled · Jan 27, 2026 · N424CA · Casa C212200 · Fuselage Main, Floor Beam
  > F12 BUCKLED UNDER FLOOR. F12 UNDERFLOOR T ANGLE CENTER CAP - REMOVED DAMAGED T ANGLE. FABRICATED NEW T ANGLE FROM 2024T3.085" X 1 5/8" X 1" TO SAME SIZE, DESIGN, AND HOLE PATTERN AS PREVIOUSLY INSTALLED. FABRICATED REPAIR DOUBLER 4 1/2"X 39 1/2" ALL NEW PARTS
- [SDR UATA2420127265302](https://openairdocs.org/sdr/UATA2420127265302.md): Floorbeam · corroded · Jan 27, 2026 · N424CA · Casa C212200 · Fuselage Main, Floor Beam
  > F11 CAP CORRODED BETWEEN SEAT RAILS. FL 1 UNDERFLOOR T ANGLE CENTER CAP - REMOVED FRAME 11 CAP SPLICE SECTION. FABRICATED NEW CAP SPLICE SECTION FROM 2024T351 0.125" X 1 5/8" X 1" ALUMINUM TO SAME SIZE, DESIGN, AND HOLE PATERN AS PREVIOUSLY INSTALLED. PARTS WE
- [SDR UATA2026012765301](https://openairdocs.org/sdr/UATA2026012765301.md): Fitting · corroded · Jan 27, 2026 · N424CA · Casa C212200 · Fuselage Miscellaneous Structure
  > L F11 REAR UNDER FLOOR FITTING CORRODED BEYOND LIMITS, F11 & F6 UNDERFLOOR FITTING HAVE CORROSION AT NUT PLATES. F6 & F11 JUNCTION BAR FITTINGS FOUND CORRODED. JUNCTION BAR FITTINGS. REMOVED ALL JUNCTION BAR FITTINGS FROM F6 & F11. REMOVED CORROSION UNDER & A
- [SDR UATA2420127265701](https://openairdocs.org/sdr/UATA2420127265701.md): Hinge Bracket · corroded · Jan 27, 2026 · N424CA · Casa C212200 · Trailing Edge Flaps
  > RT INBD. FLAP, THE OUTBD. PYLON AIRFRAME SIDE, BOTH OF THE HINGE PLATES HAVE PITTING CORROSION THAT IS BEYOND LIMITS. DRILLED BOTH HINGE PLATES AND THE INBD. AND OUTBD. PYLON SIDE SKINS OFF. FITTED AND INSTALLED NEW SIDE SKINS P/N 212-13202-05-1 (INBD.) AND P/
- [SDR UATA2025121100501](https://openairdocs.org/sdr/UATA2025121100501.md): Skin · cracked · Nov 29, 2025 · N439RA · Casa C212200 · Horizontal Stabilizer, Plate/Skin
  > RIGHT HORIZONTAL STAB TOP SKIN CRACKED JUST OTBD OF AFT ATTACH FITTING HSS 740. REMOVED TOP REAR SKIN FROM STAB ROOT TO WS 1200. ELEVATOR COVE SKIN WAS DE-RIVITED TO WS 1500 FOR ACCESS. FABRICATED NEW SKIN AND PATTER AS ORIGINAL INSTALLATION. ACID ETCHED, AL
- [SDR UATA2870815255301](https://openairdocs.org/sdr/UATA2870815255301.md): Frame · buckled · Aug 13, 2025 · N439RA · Casa C212200 · Fuselage Main, Structure
  > LH FWD FRAME OF THE LOWER RAMP OPENING (P/N 212-23201-03-1) IS BUCKLED BETWEEN FRAME 17+18. REPLACED DAMAGED C CHANNEL 212-23201-03-1 WITH NEW. SEE 337 DATED 08/13/2025 FOR FURTHER INFORMATION. IMPACT DAMAGE FOUND IN C CHANNEL 212-23201-03-1 FWD OF F18. REMOVE
- [SDR UATA2024092400001](https://openairdocs.org/sdr/UATA2024092400001.md): Frame · buckled · Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Main, Frame
  > FRAME 16 IS BUCKLED UNDER THE FLOOR JUST LEFT OF CENTER. REMOVED BUCKLED SECTION OF FRAME 16 WEB AND SPLICED IN A NEW PIECE OF MATERIAL. WORK WAS DONE REFERENCING THE CASA 212 STRUCTURAL REPAIR MANUAL APPENDIX II FIGURE B25. DETAILS OF THE REPAIR ARE AVAILAB
- [SDR UATA2024092402709](https://openairdocs.org/sdr/UATA2024092402709.md): Attach Fitting · corroded · Sep 10, 2024 · N439RA · Casa C212200 · Horizontal Stabilizer Structure
  > LH HORIZONTAL STABILIZER FORWARD ATTACH FITTING HAS CORROSION AT THE GUIDE PIN HOLE FOR THE TRIANGLE LEADING EDGE. (LOCATED INSIDE THE STABILIZER). REMOVED THE HORIZONTAL STABILIZER. DRESSED OUT THE CORROSION AND TREATED (ETCHED AND ALODYNED) PER THE CASA CORR
- [SDR UATA2024092405308](https://openairdocs.org/sdr/UATA2024092405308.md): Fitting · corroded · Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous Structure
  > THE EXTRUSION ON THE AFT SIDE OF FRAME 11 (RIGHT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 1 RH AFT FITTING 212-22406-06-2 WITH NEW RA-212-22406-06-2 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.
- [SDR UATA2024092405307](https://openairdocs.org/sdr/UATA2024092405307.md): Fitting · corroded · Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous Structure
  > THE EXTRUSION ON THE AFT SIDE OF FRAME 6 (RIGHT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 6 RH AFT FITTING 212-22406-07-1 WITH NEW RA-212-22406-07-1 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.
- [SDR UATA2024092405306](https://openairdocs.org/sdr/UATA2024092405306.md): Fitting · corroded · Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous Structure
  > THE EXTRUSION ON THE FWD. SIDE OF FRAME 6 (RIGHT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 6 RH FWD FITTING 212-22406-06-1 WITH NEW RA-212-22406-06-1 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.
- [SDR UATA2024092405305](https://openairdocs.org/sdr/UATA2024092405305.md): Fitting · corroded · Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous Structure
  > THE EXTRUSION ON THE FWD. SIDE OF FRAME 6 (LEFT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 6 LH FWD FITTING 212-22406-06-2 WITH NEW RA-212-22406-06-2 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.
- [SDR UATA2024092405304](https://openairdocs.org/sdr/UATA2024092405304.md): Fitting · corroded · Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Miscellaneous Structure
  > THE EXTRUSION ON THE AFT SIDE OF FRAME 6 (LEFT SIDE UNDER FLOOR) HAS INTERGRANULAR CORROSION. REPLACED ORIGINAL FRAME 6 LH AFT FITTING 212-22406-07-2 WITH NEW RA-212-22406-07-2 FITTING. SEE 337 DATED 07-24-2024 FOR FURTHER DETAIL.
- [SDR UATA202409245303](https://openairdocs.org/sdr/UATA202409245303.md): Frame · buckled · Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Main, Frame
  > FRAME 16 IS BUCKLED UNDER THE FLOOR JUST LEFT OF CENTER. REMOVED BUCKLED SECTION OF FRAME 16 WEB AND SPLICED IN A NEW PIECE OF MATERIAL. WORK WAS DONE REFERENCING THE CASA 212 STRUCTURAL REPAIR MANUAL APPENDIX II FIGURE B25. DETAILS OF THE REPAIR ARE AVAILABL
- [SDR UATA202409245302](https://openairdocs.org/sdr/UATA202409245302.md): Frame · cracked · Sep 10, 2024 · N439RA · Casa C212200 · Fuselage Main, Frame
  > ONE PROFILE AT FRAME 10 IS CRACKED AT THE TOP END AND THE FRAME IS BUCKLED (UNDER FLOOR). REPLACED PROFILE, STRAIGHTENED FRAME, AND INSTALLED FRAME DOUBLER. FAA FORM 337 WAS COMPLETED.
- [SDR UATA2024092405701](https://openairdocs.org/sdr/UATA2024092405701.md): Profile · cracked · Sep 10, 2024 · N439RA · Casa C212200 · Wing Main, Frame Structure
  > L/H OUTBOARD WING HAS ONE CRACKED PROFILE ON THE FALSE SPAR AT WING STATION 4900. REPLACED CRACKED PROFILE WITH ONE OF LOCAL MANUFACTURE.
- [SDR 2020F00439](https://openairdocs.org/sdr/2020F00439.md): Frame Angle · corroded · Nov 4, 2020 · N117BH · Casa C212200 · Fuselage Main, Frame
  > DURING ROUTINE INSPECTION, ON FRAME 6 UNDER THE FLOORBOARDS AT APPROXIMATELY BL 700(LT), THE FRAME ANGLE WAS FOUND CORRODED WITH A SUBSEQUENT CRACK IN THE SUPPORTING ANGLE UNDERNEATH IT.
- [SDR BIGA20200701003](https://openairdocs.org/sdr/BIGA20200701003.md): Terminal · loose · Jun 29, 2020 · N217BH · Casa C212200 · Windshield/Door Rain/Ice Removal
  > DURING FLIGHT INTO ICING CONDITIONS THE WINDSHIELD HEAT WAS SELECTED ON AND THE POWER TERMINAL OF THE COPILOT’S WINDSHIELD EXHIBITED ARCING. WINDSHIELD HEAT WAS DE-SELECTED AND THE APPROPRIATE CIRCUIT BREAKERS WERE PULLED. DURING GROUND SYSTEM TROUBLESHOOTIN
- [SDR UATA2421209495701](https://openairdocs.org/sdr/UATA2421209495701.md): Profile · cracked · Dec 4, 2019 · N424CA · Casa C212200 · Wing Miscellaneous Structure
  > IN COMPLYING WITH AD98-12-28, FOUND ONE FALSE SPAR PROFILE TO BE CRACKED. REPLACED PROFILE WITH A NEW FABRICATED PROFILE.
- [SDR BIGA20190821001](https://openairdocs.org/sdr/BIGA20190821001.md): Line · leaking · Aug 18, 2019 · N107BH · Casa C212200 · Hydraulic System, Main
  > INITIAL REPORTS WERE OF AN SMOKE IN THE COCKPIT, NOTICED HYDRAULIC FLUID ON THE WINDOWS INTERNALLY AND EXTERNALLY AND HYDRAULIC FLUID FROM THE RADOME TO THE RAMP DOOR DRIPPING OFF THE BELLY. HYDRAULIC FLUID SEEMED TO BE CONCENTRATED ON THE RIGHT (CO-PILOT)
- [SDR 39LA20190611184](https://openairdocs.org/sdr/39LA20190611184.md): Skin · corroded · Jun 11, 2019 · Casa C212200 · Wing, Plate/Skin
  > DURING SCHEDULED INSPECTIONS, A CORROSION WAS FOUND ON THE CENTER WING UPPER SKIN, R/H WS1175 TO WS3500. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, SUPPLEMENTAL INFORMATION MAY BE ADDED TO THIS SDR.
- [SDR 39LA20190611183](https://openairdocs.org/sdr/39LA20190611183.md): Skin · corroded · Jun 11, 2019 · Casa C212200 · Wing, Plate/Skin
  > DURING SCHEDULED INSPECTIONS, A CORROSION WAS FOUND ON THE CENTER WING UPPER SKIN, L/H WS1175 TO WS3500. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, SUPPLEMENTAL INFORMATION MAY BE ADDED TO THIS SDR.
- [SDR 39LA2019061105182](https://openairdocs.org/sdr/39LA2019061105182.md): Skin · punctured · Jun 5, 2019 · N602AR · Casa C212200 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED INSPECTIONS, A PUNCTURE WAS FOUND IN THE FUSELAGE SKIN JUST FORWARD OF THE TAIL STAND MOUNT. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE THE REPAIR IS COMPLETED, OPEN
- [SDR 39LA2019060311801](https://openairdocs.org/sdr/39LA2019060311801.md): Floorbeam · corroded · May 31, 2019 · N602AR · Casa C212200 · Fuselage Main, Floor Beam
  > DURING SCHEDULED INSPECTIONS, THE FLOOR BEAM AT LANDING GEAR FRAME 9 WAS FOUND TO HAVE CORROSION AT A FLOORBOARD NUTPLATE. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. OPEN
- [SDR 39LA20181030178](https://openairdocs.org/sdr/39LA20181030178.md): Channel · corroded · Oct 30, 2018 · N602AR · Casa C212200 · Trailing Edge Flaps
  > DURING REPAIR ACTIONS TO THE RT INBD FLAP PIVOT CONTROL POINT, THE CHANNEL ATTACHED TO THE SUPPORT BOX WAS FOUND TO BE CORRODED. REF SRM FIG 2-24 POS 3 DWG 212-11157 NHA LINK BRACKET I AND II. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE T
- [SDR 39LA20181030177](https://openairdocs.org/sdr/39LA20181030177.md): Fitting · worn · Oct 30, 2018 · N602AR · Casa C212200 · Trailing Edge Flaps
  > DURING INSPECTION, DANAGE WAS NOTED TO THE RT INBD FLAP PIVOT CONTROL POINT. THE LT AND RT FITTING PLATES WERE FOUND WORN BEYOND LIMITS AT THE BOLT HOLES. REF SRM FIG 2-24 POS 7 DWG 212-11157 NHA LINK BRACKET I AND II. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS
- [SDR KGBR201809240001](https://openairdocs.org/sdr/KGBR201809240001.md): Screw · loose · Sep 24, 2018 · N349TA · Casa C212200 · Fuel Storage
  > DURING PANEL REMOVAL FOR INSPECTION. PANEL HOLDING PRESSURE RELIEF VALVE PN:1604270 DISCOVERED ONE ADJUSTING SCREW LOOSE, SECOND ADJUSTING SCREW MISSING AND LAYING ON BOTTOM OF TANK.
- [SDR 39LA20151004145](https://openairdocs.org/sdr/39LA20151004145.md): Blade · cracked · Oct 4, 2015 · N602AR · Casa C212200 · Propeller Blade Section
  > DURING POST FLIGHT WALK AROUND, THE FLIGHT CREW DISCOVERED ON THE LT PROPELLER ONE OF THE BLADES WAS CRACKED.
- [SDR 39LA20150902142](https://openairdocs.org/sdr/39LA20150902142.md): Unknown · fumes · Sep 2, 2015 · N602AR · Casa C212200 · Air Distribution System
  > DURING CRUISE, WHEN HEATER VLV OPENED, THE FLIGHT CREW NOTICED FUMES IN BOTH THE FLIGHT DECK & CABIN. TESTED GEARBOX FOR POSITIVE PRESS & FOUND NORMAL NEGATIVE PRESS. HEATING SYS CHECKED GOOD ON GND IAW AMM 21-40-00.
- [SDR 8EKA20150630001](https://openairdocs.org/sdr/8EKA20150630001.md): Governor · sticks · Jun 11, 2015 · N502FS · Casa C212200 · Propeller Governor
  > PROP GOVERNOR STUCK IN FLIGHT. ACFT RETURNED TO BASE. GOVERNOR FOUND TO BE STICKY.
- [SDR 39LA20150326110](https://openairdocs.org/sdr/39LA20150326110.md): Cap · corroded · Mar 26, 2015 · N602AR · Casa C212200 · Ailerons
  > RIGHT AILERON END CAP FOUND CORRODED THROUGH, AT COUNTERWEIGHT. REPAIRED IAW COMPANY ENGINEERING ORDER 14022-300.
- [SDR 8EKA20150309001](https://openairdocs.org/sdr/8EKA20150309001.md): Attach Bracket · cracked · Mar 6, 2015 · N437CA · Casa C212200 · Horizontal Stabilizer Miscellaneous Structure
  > DURING PERIODIC SCHEDULED INSPECTION FOUND CRACK IN FWD ATTACHMENT BRACKET FOR THE RT HORIZONTAL STABILIZER INBD LE.
- [SDR 39LA20150224109](https://openairdocs.org/sdr/39LA20150224109.md): Shaft · sheared · Feb 24, 2015 · N607AR · Casa C212200 · Elevator Control System
  > DURING THE WALK AROUND INSPECTION PRIOR TO FLIGHT, MX OBSERVED THAT THE LT & RT ELEVATORS WERE DEFLECTED IN OPPOSITE DIRECTIONS. FURTHER INVESTIGATION REVEALED THAT THE LT ELEVATOR INTERCONNECT SHAFT HAD SHEARED. THERE WERE REPORTS OF HIGH WIND CONDITIONS IN
- [SDR 39LA20150203106](https://openairdocs.org/sdr/39LA20150203106.md): Light · malfunctioned · Feb 3, 2015 · N604AR · Casa C212200 · Flight Compartment Lighting
  > AT CRUISE FLIGHT DURING NIGHT VISION GOGGLE TRAINING THERE WAS AN ORDER OF SMOKE IN THE FLIGHT DECK. THE COPILOTS SIDE OF THE OVERHEAD PANEL WAS HOT TO THE TOUCH IN THE VICINITY OF THE LIGHT SWITCHES & RHEOSTATS. FLIGHT DECK LIGHTING WAS EXTINGUISHED & THE O
- [SDR 39LA2014060900005](https://openairdocs.org/sdr/39LA2014060900005.md): Propeller · split · Jun 9, 2014 · N969BW · Casa C212200 · Propeller Blade Section
  > IN CRUISE FLIGHT HEARD A LOUD BANG. SCANNED THE ENG INSTRUMENTS, THE LT TORQUE GAUGE WAS AT 120%, THE LT EGT HAD DROPPED BY APPROXIMATELY 100 DEGREES & THE LT FUEL FLOW HAD DROPPED TO 215 PPH FROM 300PPH. THERE WAS NO OTHER INDICATIONS OF A PROBLEM. PULLED
- [SDR 3RAA20140520001](https://openairdocs.org/sdr/3RAA20140520001.md): Gear · failed · May 19, 2014 · N467CS · Casa C212200 · Turbine Engine Reduction Gear
  > DURING A JUMP RUN, WHILE IN CRUISE, THE LT ENGINE CHIP LIGHT FLICKERED MOMENTARILY & THEN THE ENGINE SHUT DOWN. RETURNED TO THE DEPARTURE & LANDED WITHOUT FURTHER INCIDENT. SUSPECT CATASTROPHIC FAILURE OF THE LT ENGINE. R & R ENGINE. ACFT RETURNED TO SERV
- [SDR 39LA2013011800003](https://openairdocs.org/sdr/39LA2013011800003.md): Indication Sys · malfunctioned · Jan 17, 2013 · N969BW · Casa C212200 · Engine Indicating System
  > ON CLIMB OUT, RT ENGINE EGT BEGAN TO FLUCTUATE BETWEEN 200- 400 DEGREES. CLIMB POWER WAS SET PRIOR TO FLUCTUATION, EGT READING WAS ERRONEOUS. POWER REDUCED TO PRECLUDE AN INADVERTENT EGT OVER TEMP. SHORTLY AFTER, EGT FLUCTUATIONS BECAME LARGER CAUSING THE E
- [SDR 39LA2013011500013](https://openairdocs.org/sdr/39LA2013011500013.md): Sensor · dirty · Jan 15, 2013 · N605AR · Casa C212200 · Engine (Turbine/Turboprop)
  > ON CLIMB OUT, ABOUT 8 MILES FROM DPRATURE, RT ENGINE STARTED TO SURGE BETWEEN 95 -60 PERCENT TORQUE, AND 650- 250 EGT. RETURNED TO DEPARTURE. AS ACFT LEVELED OFF AND STARTED TO DESCEND THE ENGINE RAN NORMALLY. NO OTHER ABNORMALITIES WERE NOTED AND LANDING
- [SDR P4YA2012091200001](https://openairdocs.org/sdr/P4YA2012091200001.md): Cable · separated · Aug 24, 2012 · N962BW · Casa C212200 · Engine Controls
  > DURING HEAVY CHECK, FOUND NR 1 ENGINE TELEFLEX CABLE DAMAGED/PULLED APART AT THE SWAGE HOUSING.
- [SDR EHAA20120824007](https://openairdocs.org/sdr/EHAA20120824007.md): Gearbox · inoperative · Aug 24, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop)
  > DURING CRUISE AT FL 85, THE NR 2 ENGINE RAPIDLY STARTED TO LOSE POWER AND DISPLAYED INDICATIONS OF FAILURE. THE COPILOT AND I NOTICED A CHANGE IN ACFT AND ENGINE PERFORMANCE, VERIFIED BY ENGINE TORQUE, RPM, FUEL FLOW, EGT AND SUBSEQUENT LOSS OF OIL PRESSURE D
- [SDR EHAA20120731006](https://openairdocs.org/sdr/EHAA20120731006.md): Engine · power loss · Jul 31, 2012 · N348CA · Casa C212200 · Engine (Turbine/Turboprop)
  > DURING CLIMB, NR 2 ENGINE EGT DROPPED TO ZERO AND ENGINE LOST POWER.
- [SDR KGBR2012070600001](https://openairdocs.org/sdr/KGBR2012070600001.md): Spar · corroded · Jul 6, 2012 · N602AR · Casa C212200 · Wing Spar
  > LT WING, UPPER FWD SPAR AFT HORIZONTAL LEG, EXFOLIATED AT APPROX WS 3496, ALSO PROBABLE EXFOLIATION AT WS 2130 TO 2450 AND POSSIBLE EXFOLIATION AT WS 2900 TO 3000.
- [SDR 3RAA2012212001](https://openairdocs.org/sdr/3RAA2012212001.md): Mount Bracket · broken · Mar 29, 2012 · N467CS · Casa C212200 · Rudder Control System
  > DURING CLIMB AFTER TAKEOFF, THE PILOTS RUDDER PEDALS MOVED ALL THE WAY FORWARD. THE COPILOT TOOK OVER AND SAFELY LANDED THE AIRCRAFT. MAINTENANCE INVESTIGATED AND DISCOVED THE PILOTS RUDDER PEDAL ADJUSTMENT MOUNT BRACKET HAD BROKEN OFF IT'S MOUNT ALLOWING TH
- [SDR STZA2011F00151](https://openairdocs.org/sdr/STZA2011F00151.md): Wire Harness · corroded · Jun 23, 2011 · N502FS · Casa C212200 · Fuel Boost Pump
  > PRIMARY LT FUEL BOOST PUMP LOST POWER. ACFT SAFELY RETURNED TO ORIGINATING AIRPORT. FOUND THAT THE PUMP WIRE HARNESS (THE INTEGRAL WIRES FROM THE PUMP TO THE CONNECTOR) WAS CORRODED.
- [SDR BIGASDR1103](https://openairdocs.org/sdr/BIGASDR1103.md): Plate · cracked · May 2, 2011 · N117BH · Casa C212200 · Landing Gear Brake System
  > AFTER START UP AND ATTEMPTING TO TAXI THE LT AND RT BRAKES WOULD NOT RELEASE PROPERLY AFTER HAVING THE PARKING BRAKE SET. BOTH BRAKE ASSEMBLIES (PN 5006484-3) WERE SENT OUT FOR OVERHAUL. THE BACKING PLATE (PN 5006180) FOR BRAKE ASSY SN APR84-161 WAS FOUND CR

Next page: https://openairdocs.org/model/construcciones-aeronauticas-c-212-200/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 = 'C212200'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/construcciones-aeronauticas-c-212-200/reports

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