C A S A C-212-CD

Service difficulty reports · 37

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duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR JTAA202308231003Attach Fitting · crackedPERFORMED 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 A0473-0001Aug 21, 2023 · N309HG · Casa C212CD · Fuselage Main, Attach FittingsSDR JTAA202308231002Attach Fitting · crackedPERFORMED 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 212-24154-02.2Aug 21, 2023 · N309HG · Casa C212CD · Fuselage Main, Attach FittingsSDR JTAA202308231001Attach Fitting · crackedPERFORMED 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 212-24103-02.1Aug 21, 2023 · N309HG · Casa C212CD · Fuselage Main, Attach FittingsSDR 2016FA0000220Hinge Bracket · corrodedRT 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.May 10, 2016 · N217BH · Casa C212CD · Wing, Control Surface Attach FittingsSDR 2016F00121Bearing · migratedCOPILOT 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 PLAMay 10, 2016 · N217B · Casa C212CD · Aileron Control SystemSDR 39LA20150404133Nut · out of positionTHE 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 LApr 4, 2015 · N606AR · Casa C212CD · Propeller Controlling SystemSDR 39LA2014022860Connector · damagedDURING 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 LOOFeb 28, 2014 · N607AR · Casa C212CD · Ice/Rain Protection System WiringSDR 39LA2014022459Unknown · fumesDURING 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 FUMEFeb 24, 2014 · N607AR · Casa C212CD · Air Distribution SystemSDR 8EKA201309130002Escape Hatch · departedAFTER 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 SHAFTAug 23, 2013 · N502FS · Casa C212CD · Emergency ExitsSDR 8EKA201309130001Escape Hatch · departedAFTER 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 HANAug 23, 2013 · N502FS · Casa C212CD · Emergency ExitsSDR 39LA2013072400164Bracket · corrodedFOUND 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.Jul 24, 2013 · N606AR · Casa C212CD · Wing, Control Surface Attach FittingsSDR 39LA2013072400154Skin · dentedTWO 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.Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/SkinSDR 39LA2013072400144Skin · dentedTWO 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.Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/SkinSDR 39LA2013072400134Skin · corrodedWHILE 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 WJul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/SkinSDR 39LA2013072400124Skin · corrodedFOUND 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.Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/SkinSDR 39LA2013072400114Skin · corrodedWHILE 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"Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/SkinSDR 39LA2013072400104Bracket · corrodedFOUND 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.Jul 24, 2013 · N606AR · Casa C212CD · Wing, Control Surface Attach FittingsSDR 39LA2013072400094Web · chafedFOUND 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.Jul 24, 2013 · N606AR · Casa C212CD · Fuel StorageSDR 39LA2013072400084Window Frame · corrodedDURING 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.Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, StructureSDR 39LA2013072400074Attach Fitting · crackedWHILE 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 BUSHJul 24, 2013 · N606AR · Casa C212CD · Fuselage, Stabilizer Attach FittingsSDR 39LA2013072400064Frame · gougedFOUND DEEP GOUGE RT SIDE IN FRAME 1F. REPAIRED IAW EO 2021032-309 AND EO2012032-424, AND AIRLIFT DWG NR 2012032-2030.Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, FrameSDR 39LA2013072400054Skin · crackedWHILE 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.Jul 24, 2013 · N606AR · Casa C212CD · Wing, Plate/SkinSDR 39LA2013072400044Skin · puncturedLOWER 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.Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/SkinSDR 39LA2013072400034Frame · crackedFOUND 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.Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, FrameSDR 39LA2013072400024Skin · dentedFORWARD FUSELAGE LT SIDE, 1 DEEP DENT AT FS 3538, WL 33.0. REPAIRED IAW EO 2021032-309 AND EO2012032-424.Jul 24, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/SkinSDR 39LA2013071900014Fitting · damagedBS 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.Jul 19, 2013 · N606AR · Casa C212CD · Fuselage, Wing Attach FittingsSDR 39LA2013071900004Skin · dentedBELLY SKIN DENTED BEYOND LIMITS. REPLACED BELLY SKINS IAW EO 2021032-309 AND EO2012032-424.Jul 19, 2013 · N606AR · Casa C212CD · Fuselage Main, Plate/SkinSDR EHAA20130211002Engine · power lossFIFTEEN 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 Feb 11, 2013 · N502FS · Casa C212CD · Engine (Turbine/Turboprop)SDR 39LA2013020600014Engine · power lossDURING 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.Feb 5, 2013 · N607AR · Casa C212CD · Engine (Turbine/Turboprop)SDR 39LA2013011800001Indicator · malfunctionedAFTER 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.Jan 16, 2013 · N607AR · Casa C212CD · Navigation SystemSDR 3PRA201109070001Switch · burnedWHILE 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 SWITCSep 7, 2011 · N967BW · Casa C212CD · Fuel System WiringSDR P4YA2010031600001Skin · crackedDURING 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 Apr 14, 2010 · N967BW · Casa C212CD · Wing, Center BoxSDR RRI2001F00000Propeller · separatedPROP 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 OSep 23, 2001 · N7241E · Casa C212CD · Propeller AssemblySDR 2000ZZZX659Spar · damagedDURING 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)Jan 27, 2000 · N203PA · Casa C212CD · Horizontal Stabilizer, Spar/RibSDR 99ZZZX4495Gear · failedTHE 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.Nov 15, 1999 · N204PA · Casa C212CD · Turbine Engine Accessory DriveSDR 2000ZZZX658Gear · failedTHE 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.Nov 15, 1999 · N204PA · Casa C212CD · Turbine Engine Accessory DriveSDR 99ZZZX1994Pump · crackedSIGNS OF DEFECT: LOW OIL PSI, HIGH TEMPERATURE, AND OIL TANK SPEWING OUT OIL (IT WAS BEING PRESSURIZED). INSPECTION (DISASSEMBLY) REVEALED SCAVENGE PUMP WAS CRACKED.Apr 13, 1999 · N7241E · Casa C212CD · Turbine Engine Oil System
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