C A S A C-212-DF
Service difficulty reports · 44
Newest first. General aviation reporting is voluntary.
Query with SQL
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 = 'C212DF' 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.
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 = 'C212DF' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 8TNC202601220054Floorbeam · bentDURING ROUTINE OPERATIONS IN ANCHORAGE, AK (ANC), MAINTENANCE DISCOVERED DAMAGE TO THE ENDS OF LOWER FRAME 13 & 16 INNER FRAME T-CHORD FLANGES AT LBL19 & RBL19, NEAR THE SEAT TRACK SUPPORTS. THE T-CHORD FLANGE CORNERS WERE LOCALLY BENT DOWN WITH GOUGING ON THESDR 8TNC202601220001Skin · crackedDURING ROUTINE MAINTENANCE IN ANCHORAGE, AK (ANC), MAINTENANCE NOTED THAT (2EA.) FASTENERS COMMON TO THE HORIZONTAL STABILIZER LOWER SKIN & SPAR CHORD HAVE CRACKED OUT. THE CRACKS MEASURE .204” AND .242” LONG, RESPECTIVELY, AND THEY EMANATE IN THE OUTBOARD DIRSDR 2024F00264Motor · failedMOTOR INOPERATIVE - RETRACTABLE LANDING/TAXI LAMP ASSY - BURNT ELECTRICAL SMELL IN COCKPITSDR 39LA20151117147Landing Light · shortedON DEPARTURE, SMOKE NOTICED IN THE COCKPIT. DECLARED EMER & RETURNED. R & R LT LANDING LIGHT IAW MM 33-40-10.SDR 39LA20151015146Unknown · smokeDURING APPROACH, THE FLIGHT CREW SMELLED & OBSERVED A PUFF OF SMOKE THAT CAME FROM THE BOTTOM LT SIDE OF THE INSTRUMENT PANEL. NO ACTION WAS TAKEN AS LANDING WAS IMMINENT & A NORMAL LANDING WAS PERFORMED WITHOUT INCIDENT.SDR 39LA20150501135Escape Hatch · departedDURING TAKEOFF ROLL, THE TOP ESCAPE HATCH DEPARTED THE ACFT. THE TAKEOFF WAS ABORTED WITHOUT INCIDENT & RETURNED TO PARKING.SDR 39LA20150115105Unknown · smokeDURING CLIMB OUT AT APPROX 10,000 FT MSL THE FLIGHT CREW REPORTED A STRONG SMOKE SMELL IN THE FLIGHT DECK FOLLOWED BY A PLUME OF SMOKE RISING FROM THE FLOOR BENEATH THE FIRST OFFICER`S RUDDER PEDALS. THE FLIGHT CREW ACCOMPLISHED THE EMER CHECKLIST FOR SMOKE ESDR 39LA20140917102Mount Fitting · corrodedDURING NDT OF LT ENG MOUNT FITTING INSPECTION, FOUND AFT UPPER LT ENG MOUNT FITTING TO BE CORRODED. REMOVED UPPER ENG MOUNT FITTING PN 212-13116-01.2 & SENT OUT TO BE LOCALLY FABRICATED. WORK DONE IAW DWG 14019-2026.SDR 39LA20140917101Frame · damagedDURING INSPECTION FOUND NR 11 LT & NR 11 RT FRAMES DAMAGED. LOCALLY FABRICATED FRAMES. WORK PERFORMED IAW DWG 14019-2018 & 14019-2019 INSTRUCTIONS.SDR 39LA20140917100Frame · damagedDURING INSPECTION FOUND NR 6 LT & NR 6 RT FRAMES DAMAGED. LOCALLY FABRICATED FRAMES. WORK PERFORMED IAW DWG 14019-2013 & 14019-2014 INSTRUCTIONS.SDR 39LA2014090599Mount Fitting · corrodedFOUND CRACK INDICATION ON NR 1 ENG UPPER MOUNT FITTING ON LT WING FWD SPAR NEAR GROUNDING LUG. FURTHER INSPECTION FOUND TO BE LEVEL 2 CORROSION. PART TO BE REPLACED WITH SERVICEABLE.SDR 39LA2014082798Skin · crackedCRACK FOUND AT STATION 3950 LT SIDE OF FUSELAGE. LOCALLY MANUFACTURED FILLER USING .032 X 2024-T3 & DOUBLER USING .040 X 2024-T3. ALL WORK DONE FOLLOWING DWG 14019-2049 REV V1. NO FURTHER ACTION REQUIRED AT THIS TIME.SDR 39LA2014082797Skin · crackedCRACK FOUND AT STATION 3950 RT SIDE OF FUSELAGE. LOCALLY MANUFACTURED FILLER USING .032 X 2024-T3 & DOUBLER USING .040 X 2024-T3. ALL WORK DONE FOLLOWING DWG 14019-2049 REV V1. NO FURTHER ACTION REQUIRED AT THIS TIME.SDR 39LA2014082696Rib · corrodedTOP INNER RIB OF LT HORIZONTAL STABILIZER AT INBD ATTACH FITTING FOUND CORRODED BEYOND LIMITS. REPLACED INNER RIB AS REQUIRED.SDR 39LA2014082695Skin · corrodedRIGHT WING LOWER SURFACE IN AREA OF ENG EXHAUST TRAIL HAS CORROSION DAMAGE FROM ENG EXHAUST PRODUCT. MILITARY TECHNICAL INSTRUCTION 17 TO BE PERFORMED REPAIR OF EXHAUST AREA THROUGH SKIN REPLACEMENT & DOUBLER PATCH.SDR 39LA2014082694Skin · corrodedLEFT WING LOWER SURFACE IN AREA OF ENG EXHAUST TRAIL HAS CORROSION DAMAGE FROM ENG EXHAUST PRODUCT. MILITARY TECHNICAL INSTRUCTION 17 TO BE PERFORMED, REPAIR OF EXHAUST AREA THROUGH SKIN REPLACEMENT & DOUBLER PATCH.SDR 39LA2014082693Channel · corrodedRIGHT SEAT TRACK HAT CHANNEL SUPPORT & SEAT TRACK FROM FS 2400 TO 3950 FOUND CORRODED BEYOND LIMITS & IN NEED OF REPLACEMENT.SDR 39LA2014082692Channel · corrodedLEFT SEAT TRACK SUPPORT HAT CHANNEL & SEAT TRACK FROM FS 3150 TO 3950 FOUND CORRODED BEYOND LIMITS & IN NEED OF REPLACEMENT.SDR 39LA2014082691Skin · dentedDURING INSPECTION FOUND RT HORIZONTAL STABILIZER UPPER OTBD SKIN TO HAVE A DENT BEYOND LIMITS. FABRICATED SECTION OF SKIN USING ORIGINAL SKIN AS SAMPLE. MATERIAL USED .025 X 2024-T3 LOT 267230. ALL WORK DONE IAW EO 14019-300, REV V8 PAR 8 112. NO FURTHER ASDR 39LA2014082690Mount Bracket · corrodedDURING REMOVAL OF HORIZONTAL STABILIZER FOUND LT LOWER MOUNT BAR CORRODED. LOCALLY MANUFACTURED IAW EO 14019-2028 REV 1R. NO FURTHER ACTION REQUIRED AT THIS TIME.SDR 39LA2014082689Mount Bracket · corrodedDURING REMOVAL OF HORIZONTAL STABILIZER FOUND LT UPPER MOUNT BAR CORRODED. LOCALLY MANUFACTURED IAW EO 14019-2027 REV 1R. NO FURTHER ACTION REQUIRED AT THIS TIME.SDR 39LA2014082087Window Frame · corrodedDURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME INBD VERTICAL SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.SDR 39LA2014082086Window Frame · corrodedDURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME INBD VERTICAL SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.SDR 39LA2014082085Window Frame · corrodedDURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.SDR 39LA2014082084Window Frame · corrodedDURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT’S WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.SDR 8EKA20140801Panel · corrodedDURING INSPECTION FOUND CORROSION IN AFT CARGO DOOR. REMOVED CORROSION DAMAGED PANELS. FABRICATED & INSTALLED TWO REPAIR PANELS. ALL REPAIRS PERFORMED IAW SRM.SDR 8EKA201402060002Profile · crackedDURING 1200 HR FALSE SPAR RECURRING AD INSPECTION, IAW AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE LT WING. REMOVED LT WING AUXILIARY SPAR PROFILE ANGLE, WS 5700. INSTALLED REINFORCED LT WING AUXILIARY SPAR PROFILE ANGLE. ALL RESDR 8EKA2014020600001Profile · crackedDURING 1200 HR FALSE SPAR RECURRING INSPECTION, & AD INSPECTION AD 98-12-28. FOUND CRACKS IN THE PROFILE OF FALSE SPAR LOCATED IN THE RT WING. REMOVED RT WING AUXILIARY SPAR PROFILE ANGLE. INSTALLED REINFORCED RT WING AUXILIARY SPAR PROFILE ANGLE. ALL REMOSDR 39LA2013122642Skin · corrodedDURING CPCP INSPECTION, FOUND CORROSION ON LT WING TE AT CTR OF INBD FLAP, BETWEEN WING STATION 1266 & 2620.SDR 39LA2013121941Rib · damagedRIGHT HAND OTBD WING RIB AT WS 9500 FOUND DAMAGED WITH MULTIPLE CRACKS & DENTED FORMERS. R & R RT HAND WING RIB IAW EO2013047-311 PARA 8.42 REV B.SDR 39LA2013121940Skin · corrodedRIGHT WING EXHAUST TRAIL SKIN SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED RT WING EXHAUST TRAIL SKIN IAW EO 2013047-311 PARA 8.22 REV B.SDR 39LA2013121939Channel · corrodedLEFT WING INBD FLAP TRACK U CHANNEL SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED LT WING INBD FLAP TRACK U CHANNEL IAW EO 20130417-311 PARA 8.25 & PARA 8.31 REV B.SDR 39LA2013121938Skin · corrodedLEFT WING EXHAUST TRAIL SKIN SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED LT WING EXHAUST TRAIL SKIN IAW EO 2013047-311 PARA 8.21 REV B.SDR 39LA2013121937Channel · corrodedLEFT WING INBD FLAP TRACK U CHANNEL SHOWS SIGNS OF HEAT EROSION & CORROSION. REPLACED LT WING INBD FLAP TRACK U CHANNEL IAW EO 20130417-311 PARA 8.25 & PARA 8.31 REV B.SDR 39LA2013121936Skin · dentedLEFT WING LOWER SKIN DENTED OTBD OF EXISTING REPAIR. R & R REPAIR IAW EO 2013047-311 PARA 8 40 REV B.SDR 39LA2013121935Support Channel · corrodedRIGHT SEAT TRACK SUPPORT CHANNEL BETWEEN FS 2400 & FS 2960 HAS HEAVY CORROSION AROUND ATTACHMENTS. REPLACED SEAT TRACK SUPPORT CHANNEL BETWEEN FS 2400 & 2960 IAW EO 2013047-311 PARA 8 33 REV B.SDR 39LA2013121934Skin · dentedDENT ON LOWER SKIN OF LT HORIZONTAL STABILIZER STATION HSS3620. REPAIRED DAMAGED AREA ON LOWER SKIN OF LT HORIZONTAL STABILIZER BY INSTALLING A DOUBLER STATION HSS3620, IAW AAR DRAWING 13047-2043 REV IR.SDR 39LA2013121933Skin · dentedLEFT SIDE FUSELAGE SKIN HAS A DENT BETWEEN FS 3950 - 4310, BELOW STRINGER 18L. R & R SKIN AT FS 3550 & FS 3950 BELOW STRINGER 18L IAW EO 2013047-311 PARA 8 19 REV B.SDR 39LA2013121932Skin · dentedRIGHT SIDE FUSELAGE SKIN DENTED SEVERAL PLACES BETWEEN FS 3550 - 3950 ABOVE & BELOW STRINGER 7R. R & R RT SIDE FUSELAGE SKIN AT FS 3550 - 3950 ABOVE & BELOW STRINGER 7 RT, FABRICATED NEW REPAIR PARTS IAW DRAWING 13047-2048 REV V MATERIAL SPEC 040 INCHES 2024-TSDR 39LA2013121931Skin · dentedMULTIPLE DENTS IN FUSELAGE CTR BELLY SKIN AROUND FS 4670. FABRICATED REPAIR DOUBLER & INSTALLED IAW CASA 212-300SRM APPENDIX II, FIG B7 & EO 2013047-311 PARA 8 39 REV B.SDR 39LA2013121930Frame · crackedFRAME 27F, STATION 12615 BETWEEN STRINGER 1L & 1R IS CRACKED IN RADIUS BEYOND LIMITS. REPLACED FRAME 27F AT STATION 12615 IAW AIRLIFT EO 2013047-311 PARA 8 41 REV B.SDR 39LA201310100001Light · failedDETECTED FUMES IN COCKPIT DURING FLIGHT. FOUND LT TAXI-LANDING LIGHT CIRCUIT BREAKER TRIPPED. GAINED ACCESS TO LT LANDING LIGHT, FOUND ODOR EMINATING FROM LIGHT ASSY. R & R LT TAXI-LANDING LIGHT ASSY. OPS TESTED GOOD ON GROUND, WORK COMPLETED IAW AMM 33-40SDR EHAA20130412004Terminal Block · burnedDURING FLIGHT LT WINDOW HEAT SHORTED.SDR SROM2011011Wire Harness · chafedMULTIPLE CIRCUIT BREAKERS ON OVERHEAD PANEL POPPED IN FLIGHT. FLIGHT CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. BREAKERS THAT TRIPPED INSTRUMENT LIGHT, ANTI SKID AND TEST, RADIO POWER AND NR 2 INVERTER OUTPUT 26 VAC AND 115 VAC. DETERMINED T
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