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 = '408' 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 = '408' 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 COEA2024052917708Longeron · crackedWO 257747 NR 6 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, THE L/H NACELLE INBOARD SIDE LONGERON UNDER THE ICE VANE ATTACH POINT SHOWS SIGNS OF CRACKED STARTING. REPLACED THE L/H LOWER AFT COWLING AND FORWARD INTAKE COWLING REF. MM 71-10-05 AND SDR COEA2024052916708Longeron · crackedWO 257747 NR 5 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, THE R/H NACELLE OUTBOARD SIDE LONGERON IS CRACKED IN BEND RADIUS UNDER THE ICE VANE ACTUATOR ATTACH POINTS. REPLACED THE R/H LOWER AFT COWLING AND FORWARD INTAKE COWLING REF. C408 MM 71-1SDR COEA2024051415759Access Panel · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE DISCOVERED ON THE L/H ENGINE AFT INBOARD ACCESSORY PANEL 421CR. A TEMPORARY REPAIR WAS PERFORMED ON THE L/H ENGINE AFT INBOARD ACCESSORY PANEL PER TEXTRON REF: DQ44226M1. REPLACED THE L/H ENGINE AFT INBOASDR COEA2024041214757Skin · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS FOUND ON THE L/H ENGINE LOWER FWD COWL INBOARD UNDER EXHAUST. A TEMPORARY REPAIR WAS PERFORMED ON THE L/H ENGINE LOWER FWD COWL PER DOCUMENT REF: DQ428170M2. A NEW TEMPORARY REPAIR WAS PERFORMED PER DQ438SDR COEA2024041213759Panel · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS FOUND ON THE R/H ENGINE AFT OUTBOARD ACCESSORY PANEL. A TEMPORARY REPAIR WAS PERFORMED ON THE R/H ENGINE AFT OUTBOARD ACCESSORY PANEL PER TEXTRON DOCUMENT REF: DQ428170M2. REPLACED THE R/H ENGINE AFT OUTBSDR WUXA202403260101Cowling · crackedCOWLING CRACKING IN MULTIPLE LOCATIONS BOTH #1 AND #2 ENGINES. INTERNAL CRACKING AROUND RIVETS AND NUT-PLATES. CRACKING IN ROOT OF BEND RADIUS ON ANGLE BRACKETS. CRACKS ADJACENT TO CAMLOCKS ON COWLING PANELS. CRACKS PROTRUDING DIRECTLY FROM CAMLOCKS ON COWLINGSDR COEA2024032610767Skin · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS DISCOVERED IN THE #2 ENGINE R/H OUTBOARD ACCESSORY PANEL SKIN AROUND 1/4 TURN FASTENER. #2 R/H OUTBOARD ACCESSORY PANEL SKIN REPAIRED VIA REPLACEMENT AS NEEDED IAW C408 SPM 20-50-00 AND C408 IPC 54-10-00 SDR FXGA2024040800001Mount · crackedLEFT AND RIGHT ENGINE INERTIAL SEPARATOR MOUNTING STRUCTURE, NS 41 TO NS 50 CRACKED.SDR FXTA20240312001Cylinder · leakingRUDDER BIAS SYSTEM ALLOWING RUDDER TO FAVOR ONE SIDE INSTEAD OF BALANCING AS DESIGNED. MORE PILOT RUDDER INPUT REQUIRE TO COUNTER ACT.SDR MTNA20240308001Mount · crackedPERFORMED INSPECTION OF THE ICE VANE ACTUATOR MOUNT STRUCTURE FOR CRACKING. CRACK WAS FOUND ON THE #2 ICE VANE ACTUATOR STRUCTURE. PERMANENT REPAIR TO BE COMPLETED. PERFORMED MARKING OF THE CRACK ENDS AS INSTRUCTED IN THE ENGINEERING LETTER. REINSPECTION TO BSDR COEA2024031209734Longeron · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS DISCOVERED ON THE L/H ENGINE LONGERON UNDER THE PLENUM PANEL (LOWER AREA). REPAIR ACCOMPLISHED PER MANUFACTURER AVIATION SERVICES ICT WO 206698 DATED 4/22/2024.SDR FXTA2024032105001Cylinder · leakingRUDDER PEDAL HARDER TO PUSH WITH RUDDER BIAS ON. FOUND THE RUDDER BIAS AIR CYLINDER LEAKING AIR FROM ONE SIDE CAUSING THE RUDDER TO BIAS THE NON LEAKING SIDE.SDR COEA2024030508738Panel · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS FOUND ON THE L/H ENGINE INBOARD PLENUM PANEL AFT SIDE MIDDLE STIFFENER. A TEMPORARY REPAIR WAS PERFORMED ON THE L/H ENGINE INBOARD PLENUM PANEL PER TEXTRON DOCUMENT REF: DQ43349M1. REPLACED THE PANEL IAW SDR COEA2024030507734Panel · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE DISCOVERED ON THE L/H ENGINE INBOARD PLENUM PANEL AFT SIDE BY THE UPPER MIDDLE STIFFENER. THIS IS THE SUPPLEMENTAL SDR FOR CORRECTIVE ACTION: WO 256404 NR 22, L/H ENGINE INBOARD PLENUM PANEL WAS REPLACED ISDR MTNA2024032623001Mount · crackedICE VANE ACTUATOR MOUNT AND STRUCTURES ON #2 ENGINE INSPECTION PERFORMED. FOUND CRACKS UNDER THE RH ENGINE ACTUATOR MOUNT. PERFORMED MARKING OF CRACK ENDS AS INSTRUCTED IN TEXTRON ENGINEERING LETTER REF DQ43241M1 DATED 2/27/2024. REINSPECTION TO BE PERFORMED ESDR COEA2024022106738Skin · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS DISCOVERED IN THE #2 ENGINE LOWER FWD COWL OUTBOARD UNDER THE EXHAUST. CORRECTIVE ACTION: A TEMPORARY REPAIR WAS PERFORMED PER FXTB DOCUMENT #01/30/2024. REPLACED THE LOWER FWD COWL MID SKIN AND INLET FRASDR COEA2024032612708Skin · chafedL/H FLAP LE CHAFING FROM INBOARD FLAP ACTUATOR ACCESS PANEL. L/H PANEL FIT INSTALLED PER C408 SRM 51-00-00 AND C408 IPC 57-20-25. L/H FLAP ACTUATOR PANELS MODIFIED AND INSTALLED IAW SR-408-ATA57-43632 REV A PARA 4.3.3 AND 4.4. OPS CHECK GOOD. NO CONTACT WITH SDR COEA2024032611708Access Panel · chafedR/H FLAP LE CHAFING FROM INBOARD FLAP ACTUATOR ACCESS PANEL. R/H PANEL FIT INSTALLED PER C408 SRM 51-00-00 AND C408 IPC 57-20-25. R/H FLAP ACTUATOR PANELS MODIFIED AND INSTALLED IAW SR-408-ATA57-43632 REV A PARA. 4.3.3 AND 4.4. OPS CHECK GOOD. NO CONTACT WITHSDR COEA2024013005767Longeron · crackedWO 254814 NR 6 DISCREPANCY: DURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED ON THE L/H NACELLE UNDER THE INERTIAL SEPERATOR MOUNTING POINT, INBOARD SIDE. (LONGERON). REPAIRED COWLING WAS REINSTALLED IAW C408 MM 71-10-15.SDR COEA2024013004767Support Bracket · crackedWO 254814 NR 6 DISCREPANCY: DURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED ON THE L/H NACELLE UNDER THE INERTIAL SEPERATOR MOUNTING POINT, INBOARD SIDE. LONGERON SUPPORT BRACKET. REPAIRED COWLING REINSTALLED IAW C408 MM 71-10-15.SDR COEA2024012603757Support · crackedWO 254213 NR 5 DISCREPANCY: DURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED IN THE L/H ENGINE COWL AT THE LOWER SUPPORT STRINGER UNDER THE ICE VAIN ACTUATOR MACHINED BRACKET. REPLACED THE L/H ENGINE COWL SUPPORT IAW CESSNA 408 SRM 51-40-05.SDR COEA2024012602757Support Bracket · crackedDURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED IN THE R/H ENGINE COWL AT THE LOWER SUPPORT STRINGER UNDER THE ICE VAIN ACTUATOR MACHINED BRACKET. REPLACED R/H COWL SUPPORT AND LONGERON IAW CESSNA 408 SRM 51-40-05. PN# 7852122-28 SUPPORT & 7852121-88 LSDR FXTA2040321119002Duct · chafedLH AND RH AFT ICE VANE DOOR FOUND TO BE CHAFING ON EXIT DUCT CAUSING A GROOVE TO BE WORN INTO THE SKIN WHEN ICE VANE SYSTEM IN THE NORMAL CONFIGURATION.SDR FXTA2040321119001Longeron · crackedBOTH LH AND RH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ATTACHMENT OF THE ICE VANE DOOR LINKAGE CASTINGS. CRACKING WAS NOTICED COMING OUT FROM UNDER THE CASTINGS AND WHEN THE INSPECTION PANELS WERE OPENED TO LOOK AT THE STRUCTURE UNDER THE CASTINSDR FXTA202403210095Longeron · crackedBOTH LH AND RH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ATTACHMENT OF THE ICE VANE DOOR LINKAGE CASTINGS. CRACKING WAS NOTICED COMING OUT FROM UNDER THE CASTINGS AND WHEN THE INSPECTION PANELS WERE OPENED TO LOOK AT THE STRUCTURE UNDER THE CASTINSDR MTNA20240117001Mount · crackedPERFORMED INSPECTION OF THE ICE VANE ACTUATOR MOUNT STRUCTURE FOR CRACKING. CRACK WAS FOUND ON THE #2 NACELLE UNDER THE RIGHT HAND SIDE OF THE ICE VANE ACTUATOR MOUNT. REMOVED THE #2 AFT LOWER COWLING AND WAS SENT FOR REPAIR. RECEIVED SERVICEABLE COWLING AND ISDR COEA2024011201734Doubler · crackedWO 254211 NR 5 DISCREPANCY: DURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED IN THE R/H ENGINE COWL AT THE LOWER SUPPORT STRINGER UNDER THE VAIN ACTUATOR MACHINED BRACKET. REPAIRS COMPLETED IAW SR-408-ATA54-42396 TO R/H ENGINE COWL AND INCORPORATED SDR FXTA2024032129001Support · crackedLH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ICE VANE DOOR LINKAGE CASTING ATTACHMENTS. P/N: 7852122-28 & 7852122-27 CRACKEDSDR MTNA202403265002Mount · crackedICE VANE ACTUATOR MOUNT AND STRUCTURES ON #2 ENGINE INSPECTION PERFORMED. FOUND CRACKS ON THE IBOARD ACTUATOR MOUNTING PLATE LOWER SIDE. FOUND CRACK ON #1 ENGINE NACELLE AS WELL, REMOVED BOTH #1 AND #2 AFT LOWER COWLINGS AND GAVE TO TEXTRON GO TEAM FOR REPAIRSSDR MTNA2024032615001Mount · crackedICE VANE ACTUATOR MOUNT AND STRUCTURES ON #1 ENGINE INSPECTION PERFORMED. FOUND CRACKS ON THE INBOARD ACTUATOR MOUNTING STRUCTURE LOWER SIDE. ASSISTED TEXTRON GO TEAM IN REPAIRS BY REMOVING AFT LOWER COWLING. AFT LOWER ENGINE COWLING REPAIRED UNDER TEXTRON WORSDR COEA2023112902708Unknown · unknownWO 252637/NR 6 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, IT WAS DISCOVERED THAT THE R/H INTAKE INTERIOR LOWER SURFACE PANEL IS CRACKED. REPLACED THE R/H ENGINE LOWER COWL SKIN IAW 408 SRM CH 51-00-00 AND IPC 71-10-10.SDR FXTA2024032110001Duct · chafedLH & RH AFT ICE VANE DOOR FOUND CHAFING ON EXIT DUCT CAUSING A GROOVE TO BE WORN INTO THE SKIN WHEN THE ICE VANES WERE IN THE NORMAL CONFIGURATION.SDR MTNA20231012001Panel · crackedFOUND CRACKS ON THE BOAT TAIL PANEL 422CR. NO CRACKS FOUND ON THE ICE VANE ACTUATOR STRUCTURE. CORRECTIVE ACTION IN WORK.
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