# Service difficulty reports: C A S A C-212-CD

A list on [C A S A C-212-CD](https://openairdocs.org/model/c-a-s-a-c-212-cd.md).

Newest first. General aviation reporting is voluntary.

- [SDR JTAA202308231003](https://openairdocs.org/sdr/JTAA202308231003.md): Attach Fitting · cracked · Aug 21, 2023 · N309HG · Casa C212CD · Fuselage Main, Attach Fittings
  > PERFORMED EDDY CURRENT INSPECTION OF ACCESSIBLE AREAS OF FRAME NO.29, 31, L/H, R/H UPPER & LOWER ATTACH FITTINGS (QTY:8) AND FRAME NO.31 SHOWS REJECTABLE INDICATIONS ON LWR L/H FITTING. 1 EA, P/N A0473-0001
- [SDR JTAA202308231002](https://openairdocs.org/sdr/JTAA202308231002.md): Attach Fitting · cracked · Aug 21, 2023 · N309HG · Casa C212CD · Fuselage Main, Attach Fittings
  > PERFORMED EDDY CURRENT INSPECTION OF ACCESSIBLE AREAS OF FRAME NO.29, 31, L/H, R/H UPPER & LOWER ATTACH FITTINGS (QTY:8) AND FRAME NO.31 SHOWS REJECTABLE INDICATIONS ON UPPER R/H FITTING. 1 EA, P/N 212-24154-02.2
- [SDR JTAA202308231001](https://openairdocs.org/sdr/JTAA202308231001.md): Attach Fitting · cracked · Aug 21, 2023 · N309HG · Casa C212CD · Fuselage Main, Attach Fittings
  > PERFORMED EDDY CURRENT INSPECTION OF ACCESSIBLE AREAS OF FRAME NO.29, 31, L/H, R/H UPPER & LOWER ATTACH FITTINGS (QTY:8) AND FRAME NO.29 SHOWS REJECTABLE INDICATIONS ON UPPER R/H FITTING & LWR L/H FITTING. 2 EA, P/N 212-24103-02.1
- [SDR 2016FA0000220](https://openairdocs.org/sdr/2016FA0000220.md): Hinge Bracket · corroded · May 10, 2016 · N217BH · Casa C212CD · Wing, Control Surface Attach Fittings
  > RT INBD AILERON HINGE BRACKET FOUND TO HAVE EXFOLIATION CORROSION AT AIRFRAME ATTACH POINT, REQUIRING REPLACEMENT OF PART. OTHER CONTROL SURFACE HINGES/ATTACH BRACKETS INSPECTED WITH NO DEFECTS.
- [SDR 2016F00121](https://openairdocs.org/sdr/2016F00121.md): Bearing · migrated · May 10, 2016 · N217B · Casa C212CD · Aileron Control System
  > COPILOT AILERON CONTROL ROD FOUND DISCONNECTED FROM INTERCONNECT BELLCRANK, DUE TO BEARING MIGRATION FROM ROD END. INSTALLATION DID NOT HAVE LARGE DIAMETER WASHER INSTALLED, WHICH ACTS AS A FAIL-SAFE TO THIS OCCURRENCE. OPPOSITE SIDE WAS INSPECTED & SOME PLA
- [SDR 39LA20150404133](https://openairdocs.org/sdr/39LA20150404133.md): Nut · out of position · Apr 4, 2015 · N606AR · Casa C212CD · Propeller Controlling System
  > THE 2 ENG POWER LEVER HAD NO CONTROL OVER THE ENG DURING CRUISE FLIGHT. THE NR 2 ENG WAS SHUTDOWN IN FLIGHT & AN EMER WAS DECLARED. THE ACFT LANDED WITHOUT INCIDENT. INSPECTED NR 2 ENG CONTROL SYS & FOUND THAT THE NUT FOR THE PROPELLER PITCH CONTROL INPUT L
- [SDR 39LA2014022860](https://openairdocs.org/sdr/39LA2014022860.md): Connector · damaged · Feb 28, 2014 · N607AR · Casa C212CD · Ice/Rain Protection System Wiring
  > DURING CRUISE FLIGHT FROM OASH TO OAIX THE FLIGHT CREW COULD SMELL HOT ELECTRICAL FUMES IN THE FLIGHT DECK. THE QRH WAS COMPLIED WITH, & THE SOURCE OF THE ELECTRICAL SMELL COULD NOT BE DETERMINED. THE FLIGHT WAS COMPLETED WITHOUT FURTHER INCIDENT. FOUND LOO
- [SDR 39LA2014022459](https://openairdocs.org/sdr/39LA2014022459.md): Unknown · fumes · Feb 24, 2014 · N607AR · Casa C212CD · Air Distribution System
  > DURING CRUISE FLIGHT FROM OAMS TO OAIX THE FLIGHT CREW EXPERIENCED FUMES IN THE FLIGHT DECK. O2 MASKS WERE DONNED BY THE CREW & THE QRH WAS COMPLIED WITH. THE ELECTRICAL SYSTEMS WERE CHECKED WITH NO DISCREPANCIES NOTED. ENG BLEED VLVS WERE CLOSED & THE FUME
- [SDR 8EKA201309130002](https://openairdocs.org/sdr/8EKA201309130002.md): Escape Hatch · departed · Aug 23, 2013 · N502FS · Casa C212CD · Emergency Exits
  > AFTER NORMAL REFUELING OPERATION, REMOVE HATCH AND FUELED FROM TOP OF AIRPLANE, WENT TOPSIDE TO INSPECT THE FUEL CAPS. ON RETURNING TO CABIN, REINSTALLED HATCH. ROTATED THE HANDLE TO "LOCKED" POSITION AND HANDLE CAME OFF. NOTICED ROLL PIN FOR HANDLE TO SHAFT
- [SDR 8EKA201309130001](https://openairdocs.org/sdr/8EKA201309130001.md): Escape Hatch · departed · Aug 23, 2013 · N502FS · Casa C212CD · Emergency Exits
  > AFTER THE NORMAL REFUELING, REMOVED HATCH AND FUELED FROM THE TOP OF AIRPLANE, WENT TOPSIDE TO INSPECT THE FUEL CAPS. ON RETURNING TO THE CABIN, REINSTALLED THE HATCH. ROTATED THE HANDLE TO THE "LOCKED" POSITION, THERE WAS A POP AND THE HANDLE CAME OFF IN HAN
- [SDR 39LA2013072400164](https://openairdocs.org/sdr/39LA2013072400164.md): Bracket · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Control Surface Attach Fittings
  > FOUND CENTER WING RT OTBD FLAP BRACKET, INBD AND OTBD SKIN CORRODED BEYOND LIMITS. REPLACED WITH NEW SKINS PN'S 212-13202-05-1 AND 212-13202-05-2. REPAIR PREFORMED IAW EO2012032-309 AND EO2021032-424, AND DWG NR 2012032-2032.
- [SDR 39LA2013072400154](https://openairdocs.org/sdr/39LA2013072400154.md): Skin · dented · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin
  > TWO DENTS FOUND ON LOWER SURFACE OF RT WING AT APPROX WING STATION 9350. REPLACED WING SKIN IAW EO 2021032-309 AND EO2012032-424, AND AIRLIFT DWG N R 2012032-2033.
- [SDR 39LA2013072400144](https://openairdocs.org/sdr/39LA2013072400144.md): Skin · dented · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/Skin
  > TWO UPPER FUSELAGE SKINS REQUIRE REPLACEMENT DUE TO DENTED AREAS BEYOND LIMITS, SEVERAL ELONGATED RIVET HOLES. REPLACED 2 EA UPPER FUSELAGE SKINS IAW EO 2021032-309 AND EO2012032-424.
- [SDR 39LA2013072400134](https://openairdocs.org/sdr/39LA2013072400134.md): Skin · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin
  > WHILE PERFORMING GENERAL VISUAL INSPECTION OF WING (TASK 57.02, ITEM 11 OF 1 YEAR INSPECTION UNDER COMPANY CAMP, WO 124890-5), FOUND FLAP COVE BEHIND NR 2 ENGINE CORRODED. NON ROUTINE DISCREPANCY GENERATED UNDER WO 125651-603. REPLACED FLAP COVE SKINS FROM W
- [SDR 39LA2013072400124](https://openairdocs.org/sdr/39LA2013072400124.md): Skin · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin
  > FOUND CORROSION UNDER LT CENTER SECTION EXHAUST FAIRING DURING INSPECTION. CORROSION FOUND TO BE BEYOND MFG LIMITS. REPAIRED IAW EADS TECH INSTRUCTION NR 17 DATED OCTOBER 1992, EO2012032-309 AND EO2021032-424.
- [SDR 39LA2013072400114](https://openairdocs.org/sdr/39LA2013072400114.md): Skin · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin
  > WHILE PERFORMING GENERAL VISUAL INSPECTION OF WING (TASK 57.02, ITEM 11 OF 1 YEAR INSPECTION UNDER COMPANY CAMP, WO 124890-5), FOUND WING SKIN BEHIND NR 2 ENGINE CORRODED. REPLACED WING T/E SKIN FROM WING STATION 1266 TO WING STATION 3500 WITH 2024-T3, 0.025"
- [SDR 39LA2013072400104](https://openairdocs.org/sdr/39LA2013072400104.md): Bracket · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Control Surface Attach Fittings
  > FOUND CENTER WING LT OTBD FLAP BRACKET, INBD SKIN CORRODED BEYOND LIMITS. REPLACED WITH NEW SKIN, PN 212-13202-05-2, IAW EO 2012032-309 AND EO 2012032-424, AND DWG NR 2012032-2032, SUPPORTED BY FAA FORM 8110-3 DATED 31 MAY 2013.
- [SDR 39LA2013072400094](https://openairdocs.org/sdr/39LA2013072400094.md): Web · chafed · Jul 24, 2013 · N606AR · Casa C212CD · Fuel Storage
  > FOUND CHAFE DAMAGE TO LT WING FUEL TANK COLLECTOR BOX FORWARD WEB. PERFORMED REPAIR IAW EO2012032-309 AND EO2012032-424, AND DWG NR 12032-2038, SUPPORTED BY FAA FORM 8110-3 DATED 31 MAY 2013.
- [SDR 39LA2013072400084](https://openairdocs.org/sdr/39LA2013072400084.md): Window Frame · corroded · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Structure
  > DURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE CO-PILOT'S WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO2012032-309 AND EO2021032-424, AND AIRLIFT DWG 2012032-2036, SUPPORTED BY FAA FORM 8110-3, DATED 31 MAY 2013.
- [SDR 39LA2013072400074](https://openairdocs.org/sdr/39LA2013072400074.md): Attach Fitting · cracked · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage, Stabilizer Attach Fittings
  > WHILE PERFORMING EDDY CURRENT INSPECTION, SUPPLEMENTAL INSPECTION DOCUMENT 20,000 /2,800 FLIGHT SUPPLEMENTAL INSPECTION OF HORIZONTAL STABILIZER, FOUND THAT LT HORIZONTAL STABILIZER UPPER AAFT ATTACH FITTING HAS CORROSION AND CRACK INDICATION AROUND MOUNT BUSH
- [SDR 39LA2013072400064](https://openairdocs.org/sdr/39LA2013072400064.md): Frame · gouged · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Frame
  > FOUND DEEP GOUGE RT SIDE IN FRAME 1F. REPAIRED IAW EO 2021032-309 AND EO2012032-424, AND AIRLIFT DWG NR 2012032-2030.
- [SDR 39LA2013072400054](https://openairdocs.org/sdr/39LA2013072400054.md): Skin · cracked · Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/Skin
  > WHILE PERFORMING GENERAL VISUAL INSPECTION OF WING. FOUND FLAP COVE BEHIND NR 1 ENGINE EXHAUST CRACKED IN 2 PLACES. REPAIRED IAW EO2012032-309 AND EO2012032-424.
- [SDR 39LA2013072400044](https://openairdocs.org/sdr/39LA2013072400044.md): Skin · punctured · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN AT BS 5390 - 6966, LBL 20.0 - RBL 20.0 HAS PIERCED SKIN. REPAIRED EO 2021032-309 AND EO2012032-424, AND AIRLIFT DWG NR 2012032-2031.
- [SDR 39LA2013072400034](https://openairdocs.org/sdr/39LA2013072400034.md): Frame · cracked · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Frame
  > FOUND CRACKED FRAME AT BS 9650 LT SIDE RAMP AREA FUSELAGE 5TH STRINGER FROM BOTTOM. REPAIRED IAW EO 2021032-309 AND EO2012032-424, AND DWG NR 2012032-2029.
- [SDR 39LA2013072400024](https://openairdocs.org/sdr/39LA2013072400024.md): Skin · dented · Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/Skin
  > FORWARD FUSELAGE LT SIDE, 1 DEEP DENT AT FS 3538, WL 33.0. REPAIRED IAW EO 2021032-309 AND EO2012032-424.
- [SDR 39LA2013071900014](https://openairdocs.org/sdr/39LA2013071900014.md): Fitting · damaged · Jul 19, 2013 · N606AR · Casa C212CD · Fuselage, Wing Attach Fittings
  > BS 5744.3 RT SIDE FWD WING MOUNT INSIDE CABIN HAS ONE HOLE DRILLED ACROSS MOUNTING BRACKET. REPAIRED IAW EO 2021032-309 AND EO2012032-424, AND DWG NR 2012032-2032.
- [SDR 39LA2013071900004](https://openairdocs.org/sdr/39LA2013071900004.md): Skin · dented · Jul 19, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/Skin
  > BELLY SKIN DENTED BEYOND LIMITS. REPLACED BELLY SKINS IAW EO 2021032-309 AND EO2012032-424.
- [SDR EHAA20130211002](https://openairdocs.org/sdr/EHAA20130211002.md): Engine · power loss · Feb 11, 2013 · N502FS · Casa C212CD · Engine (Turbine/Turboprop)
  > FIFTEEN MINUTES INTO THE FLIGHT, THE NR 1 ENGINE EXPERIENCED A MOMENTARY POWER LOSS OF ABOUT TEN PERCENT TORQUE. ALL THE GAUGES INDICATED THE SAME AND THE ACFT YAWED IN THAT DIRECTION. THIS LASTED ONLY A SECOND OR TWO, BUT A FEW MINUTES LATER THE SAME THING
- [SDR 39LA2013020600014](https://openairdocs.org/sdr/39LA2013020600014.md): Engine · power loss · Feb 5, 2013 · N607AR · Casa C212CD · Engine (Turbine/Turboprop)
  > DURING THE TAKEOFF ROLL, IT WAS DETERMINED THAT THE RT ENGINE WAS NOT MAKING THE PREDICTED POWER. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT AND ACFT WAS TAXIED BACK TO THE RAMP FOR MX.
- [SDR 39LA2013011800001](https://openairdocs.org/sdr/39LA2013011800001.md): Indicator · malfunctioned · Jan 16, 2013 · N607AR · Casa C212CD · Navigation System
  > AFTER DEPARTING, ENROUTE, THE TAWS FAILED. ACFT RETURNED BACK TO DEPARTURE. INSPECTED WIRING AND CONNECTIONS, NO DEFECTS NOTED. PERFORMED GPS AND TWAS SYS OPS AND FUNCTIONAL CHECKS WITH NO DEFECTS NOTED IAW TAWS ST3400 MANUAL 82002-IM, REVISION J1.
- [SDR 3PRA201109070001](https://openairdocs.org/sdr/3PRA201109070001.md): Switch · burned · Sep 7, 2011 · N967BW · Casa C212CD · Fuel System Wiring
  > WHILE PERFORMING "BEFORE START" CHECKS WITH GPU CONNECTED AND POWERING SYS, A HEAVY ELECTRICAL BURNING ODOR AND SMOKE CAME FROM OVERHEAD ELECTRICAL PANEL. CREW THEN SHUTDOWN SYSTEMS IAW COMPANY SOP'S AND ALERTED MX. MX FOUND RT AUXILLIARY FUEL PUMP QA8 SWITC
- [SDR P4YA2010031600001](https://openairdocs.org/sdr/P4YA2010031600001.md): Skin · cracked · Apr 14, 2010 · N967BW · Casa C212CD · Wing, Center Box
  > DURING CENTER WING NDI DRIVEN BY THE REPETITIVE INSPECTION REQUIREMENT OF AD 2008-06-03 THROUGH THE INSP REQUIREMENTS OF AOL 212-018 REV2, EDDY CURRENT REVEALED A 50 PERCENT INDICATION AT STA YN=1037 BETWEEN LONGERONS 3 & 4. VISUAL INSP CONFIRMED AND REVEALED
- [SDR RRI2001F00000](https://openairdocs.org/sdr/RRI2001F00000.md): Propeller · separated · Sep 23, 2001 · N7241E · Casa C212CD · Propeller Assembly
  > PROP HUB SEPARATED AT BOLTS, LEAVING JUST THE AREA OF THE HUB THAT THE BOLTS ATTACH TO. THE HUB WAS NEW AT THE OVERHAUL. THERE WAS NO VIBRATION AT ALL DURING THE FLIGHTS AND STARTS THAT LOOK PLACE EARLY THAT DAY OR THE DAY BEFORE. THERE WAS NO EVIDENCE OF O
- [SDR 2000ZZZX659](https://openairdocs.org/sdr/2000ZZZX659.md): Spar · damaged · Jan 27, 2000 · N203PA · Casa C212CD · Horizontal Stabilizer, Spar/Rib
  > DURING SCHEDULED MAINTENANCE CHECK, THE RIGHT HORIZONTAL STABILIZER AFT SPAR BEAM WAS FOUND CRACKED. CAUSE OF FAILURE IS UNKNOWN AT THIS TIME. REPLACED AFT BEAM ASSEMBLY. CASA TECHNICAL SUPPORT WAS NOTIFIED. AIRCRAFT TC: 18,394. (X)
- [SDR 99ZZZX4495](https://openairdocs.org/sdr/99ZZZX4495.md): Gear · failed · Nov 15, 1999 · N204PA · Casa C212CD · Turbine Engine Accessory Drive
  > THE NUT SECURING BEARING TO IDLER GEAR PN 896806-1 LOOSENED CAUSING GEAR TO BIND IN GEARCASE. THIS BINDING CAUSED THE NR 1 IDLER IN THE TORQUE SENSOR TO SHEER WHICH RESULTED IN ENGINE SHUT DOWN.
- [SDR 2000ZZZX658](https://openairdocs.org/sdr/2000ZZZX658.md): Gear · failed · Nov 15, 1999 · N204PA · Casa C212CD · Turbine Engine Accessory Drive
  > THE NUT SECURING BEARING TO IDLER GEAR, P/N 896806-1, LOOSENED CAUSING GEAR TO BIND IN GEARCASE. THIS BINDING CAUSED TNE NR 1 IDLER IN THE TORQUE SENSOR TO SHEER WHICH RESULTED IN ENGINE SHUT-DOWN.
- [SDR 99ZZZX1994](https://openairdocs.org/sdr/99ZZZX1994.md): Pump · cracked · Apr 13, 1999 · N7241E · Casa C212CD · Turbine Engine Oil System
  > SIGNS OF DEFECT: LOW OIL PSI, HIGH TEMPERATURE, AND OIL TANK SPEWING OUT OIL (IT WAS BEING PRESSURIZED). INSPECTION (DISASSEMBLY) REVEALED SCAVENGE PUMP WAS CRACKED.

## 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 = 'C212CD'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/c-a-s-a-c-212-cd/reports

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