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 engine_model_key = 'CF343B1' 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 engine_model_key = 'CF343B1' 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 A6WA200740693Nut Clip · crackedFS 484.0 RT SIDE, CLIP FOUND CRACKED ON FLOOR SUPPORT STRUCTURE AT RBL 27.0, FS 484.00, RBL 27.00, FLOOR SUPPORT CLIP REPLACED IAW SRM 51-42-16, 51-21-16 AND SRM 51-42-06. (K)SDR CA071217010Fcu · faulted(CAN) FLAP FAIL ON APPROACH WHEN FLAPS SELECTED TO 20 FROM 8. SYS RESET AND CHECKED SERVICEABLE, MAINT EMPLOYEE ON SITE GOT FAULT CODES FROM FECU. SKEW BITE RESET AND FLAP CONTROL AND POWER DRIVE UNIT RESETS CARRIED OUT. FLAP FAULT CLEARED. FLAPS CYCLED SEVSDR A6WA200740698Diaphragm · crackedDIAPHRAGM CRACK UNDER FWD UPPER PAX DOOR CORNER COVER. (K) BRACKET CRACKED UNDER FWD UPPER PAX DOOR CORNER COVER REPLACED IAW SRM 51-42-06.SDR CA071217008Drive Assy · faulty(CAN) FLAPS FAILED AT 30 DEG WHEN 45 DEG SELECTED. FLAP ACTUATORS, PDU AND FECU REPLACED TEST FLIGHT CARRIED OUT CHECKED SUSPECT POWER FLAP DRIVE AT FAULT DUE TO HISTORY. (TC NR 20071217008)SDR A6WA200740689Bracket · crackedBRACKET CRACK ON LOWER PAX DOOR EDGE (LOCK MECHANISM AREA) AFT STA 334.00. CRACKED BRACKET ON PAX DOOR BTW FS 329.5 TO FS 338.0 IS REPLACED IAW SRM 51-41-04. (K)SDR CHQA200700094Shaft · failedIAH TO HRL - ON APPROACH TO HRL, THE FLAPS FAILED AT 20 DEGREES WHEN SELECTED TO 30 DEGREES. THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE WAS ABLE TO RESET THE FLAP SYSTEM AND OPERATE THE FLAPS IN ORDER TO FERRY THE AIRCRAFT TO SDR A6WA200740694Intercostal · crackedCRACK FOUND ON INTERCOSTAL FS 484, LBL 27 AND LBL 36, WL 72.00. INTERCOSTAL AT FS 484, LBL 27 AND LBL 36 AT WL 72.00. REPAIRED IAW REO 601R-53-41-059 REV A AND SRM 51-24-16, 51-21-16 AND SRM 51-42-06. (K)SDR A6WA200740695Drag Angle · crackedCRACK FOUND ON AFT ATTACH ANGLE OF PAX DOOR (DRAG ANGLE). AFT ATTACH ANGLE OF PAX DOOR REPAIRED IAW REO 61R-52-11-513 REV A. (K)SDR A6WA200740696Intercostal · crackedLT INTERCOSTAL CLIP AT FS 621.0 TO FS 625.0 IS CRACKED. INTERCOSTAL CLIP AT FS 621.0 TO FS 625.0 LT REPLACED IAW SRM 51-42-20. (K)SDR A6WA200740697Support Bracket · crackedRT HYDRAULIC SUPPORT BRACKET AT FS 718 IS CRACKED. RT HYDRAULIC SUPPORT BRACKET AF FS 718 IS CRACKED. (K)SDR A6WA200740699Floor Panel · corrodedCORROSION EXIST ON FLOOR STRUCTURE FS 280, LBL 9 TO RBL 9. PERFORMED ON FLOOR STRUCTURE FS 280, LBL 9 TO RBL 9 IAW REO 601R-53-11-926. (K)SDR A6WA200740685Structure · crackedEDGE MEMBER CRACK ON PAX DOOR AT FOLDING STEP HINGE. (K) PAX DOOR EDGE MEMBER FABRICATED IAW SRM 51-24-26 AND INSTALL IAW SRM 51-42-13.SDR A6WA200740686Structure · gougedFWD PAX DOOR PULL IN LEVEL GOUGED PULL IN LEVEL GOUGED .070 INCH AND ALLOWABLE MAXIMUM .050 INCH IAW REO 601R-52-11-524. (K) FWD PAX DOOR PULL IN LEVER REPAIRED IAW REO 601R-52-11-524.SDR A6WA200740687Structure · crackedFWD UPPER CORNER COVER CRACK ON PAX DOOR. (K) FWD UPPER CORNER COVER OF PAX DOOR REPLACED IAW SRM 51-42-13.SDR A6WA200740688Cover · crackedAFT UPPER CORNER COVER CRACK ON PAX DOOR. (K) AFT UPPER CORNER COVER REPLACED IAW SRM 51-42-13. (K)SDR A6WA200740705Intercostal · crackedCRACK SUSPECTED ON AC CONNECTOR BOX. CRACK CONFIRMED BY EDDY CURRENT INSPECTION. INTERCOSTAL AND RECEPTACLE SUPPORT REPLACED IAW SRM 51-42-06. (K)SDR A6WA200740657Drive Unit · malfunctionedFLAP FAIL CAUTION MESSAGE INFLIGHT. LANDED WITH FLAPS AT 8 DEGREES. LANDING WEIGHT 40,300 LBS. SPEED 150 KNOTS VERTICAL SPEED LESS THAN 400 FT MINUTE MAX BTMS READING =3. REMOVED AND REPLACED FLAPS POWER DRIVE UNIT IAW AMM 27-52-01. PERFORMED OPS CHECK IASDR A6WA200740658Charger · inoperativeENTRY-WAY EMERGENCY FLOODLIGHT INOPERATIVE. REMOVED AND REPLACED CHARGER ASSY NR 2 IAW 33-51-05, OPS CHECK GOOD. (K)SDR A6WA200740674Hinge · crackedPAX DOOR UPPER FOLDING STEP, LOWER HINGE IS CRACKED. PAX DOOR UPPER FOLDING STEP, LOWER HINGE REPLACED IAW SRM 51-41-00. (K)SDR CA071211004Pdu · failed(CAN) AFTER LANDING WITH FLAPS AT 45 DEGREES, FLAPS SELECTED TO 0 DEGREES. CREW RECEIVED A FLAP FAIL AMBER MESSAGE AT FLAPS 41 DEGREES. MAINTENANCE TROUBLESHOOTING REVEILED FECU FAULT CODES FOR ASYMMETRY, BINDNG AND FLAPS NOT IN POSITION LEADING TO REPLACEMENTSDR CA071211005Flex Drive · twisted(CAN) AFTER LANDING WITH FLAPS AT 45 DEGREES, FLAPS SELECTED TO 0 DEGREES. CREW RECEIVED A FLAP FAIL AMBER MESSAGE AT FLAPS 41 DEGREES. DURING MAINTENANCE TROUBLESHOOTING OF FLAPS THE NR 2 RT FLEX DRIVE SHAFT ASSY WAS FOUND TWISTED. UPON REMOVAL PART LENGHTH WSDR CHQA200700085Sensor · malfunctionedSDF TO IAH - DURING DESCENT TO IAH. THE CREW RECEIVED A FLAP FAIL MESSAGE. THE APPROACH WAS ABORTED AND THE CREW RAN THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU AND FOUND CODES FOR THE LEFT BRAKE POSITION SENSING UNIT. THE BRAKE PSDR CHQA200700086Flex Drive · damagedIAH TO MAF - AFTER TAKEOFF, THE FLAP LEVER WAS MOVED TO 0 AND THE FLAPS STOPPED RETRACTING AT 6. THE QRH WAS FOLLOWED AND SUFFICIENT FUEL WAS BURNED OFF TO ALLOW FOR A LANDING BELOW STRUCTURAL LANDING WEIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT WITH THE FLASDR MASA200700836Fan · damagedFOUND INDICATION OF ARC OUT AT THE 12 O'CLOCK POSITION IN AREA 8. REMOVED AND REPLACED FAN DISK, ALL OPS CHECK GOOD.SDR A6WA200840002Terminal · burnedGENERATOR NR 1 CAUTION RECEIVED AT CRUISE, COMPLIED WITH QRH. FOUND AC GENEATOR BURNED UP AT TERMINALS. REMOVED AND REPLACED GENERATOR NR 1 ASSY IAW AMM 24. (K)SDR A6WA200840003Terminal · burnedGENERATOR NR 1 CAUTION RECEIVED AT CRUISE, COMPLIED WITH QRH. FOUND AC GENERATOR BURNED UP AT TERMINALS. REMOVED AND REPLACED GENERATOR NR 1 ASSY IAW AMM 24. (K)SDR A6WA200740668Angle · crackedLT AND RT ANGLES CRACKED ON REAR PRESSURE BULKHEAD AFT SURFACE. (M) LT AND RT ANGLES ON AFT PRESSURE BULKHEAD (AFT FACE) AT FS 622, WL 73 TO 75, BTW STR 16 AND 17 INSTALLED AS IAW SRM 51-42-20. (K)SDR A6WA200740673Drag Angle · crackedPAX DOOR STAIR ASSY, AFT DRAG ANGLE IS CRACKED. REPAIRED IAW CRJ200, REO 601R-52-11-513 REV (A). (K)SDR A6WA200740676Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT FS 589 TO 621, LBL 27. JOB PERFORMED ON FLOOR SUPPORT FS 589 TO 621, LBL 27 IAW REO 601R-53-61-2439. (K)SDR A6WA200740677Floor Support · crackedCRACK FOUND ON FLOOR STRUCTURE FS 621, LBL 45 CRACK LENGTH IS .500 INCH. FLOOR SUPPORT AT FS 621.00 LBL 45 REPAIRED IAW REO 601R-53-61-117, REV C. (K)SDR A6WA200740675Bulkhead · crackedCRACK FOUND ON T FWD PRESSURE BULKHEAD PARKING BRAKE CABLE HOLE APPROX .650 INCH LONG. FWD PRESSURE BULKHEAD AT FS 202.00, LBL 23.71. REPAIRED IAW REO 601R-53-11-563. (K)SDR A6WA200740670Structure · crackedON PAX DOOR, CRACK FOUND ON PASSENGER EDGE MEMBER. (M) PAX DOOR ON PASSENGER EDGE MEMBER REPAIRED IAW REO 601R-52-11-279. (K)SDR VNAA0711012Inlet · damagedCREW REPORTED MULTIPLE BIRD STRIKES TO THE FUSELAGE, WING AND BOTH ENGINES. MAINTENANCE INSPECTED FOUND DAMAGE TO THE LEFT ENGINE INLET, FORWARD EQUIPMENT BAY DOOR AND BULKHEAD, AND THE RIGHT WING LEADING EDGE. MAINTENANCE REMOVED AND REPLACED THE DAMAGED LESDR A6WA200740650Pump · inoperativeHYD NR 1 LOW PRESS CAUTION MESSAGE IN FLIGH, HYD 1 QUANTITY READ ZERO FOR 35 MINUTES. PERFORMED PRECAUTIONARY SHUTDOWN OF NR 1 ENGINE AFTER LANDING. FOUND NR 1 SUCTION LINE CHAFED THROUGH AND PRESSURE FLEX PERMASWEDGE REPAIR, REMOVED AND REPLACED PRESSURE LISDR CHQA200700083Actuator · bindingIAH TO AMA - DURING APPROACH TO AMA, THE FLAPS FAILED AT ZERO DEGREES WHEN SELECTED TO 8 DEGREES. ATC WAS NOTIFIED AND THE QRH WAS FOLLOWED. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS INSPECTED BY EMERGENCY PERSONNEL BEFORE TAXING TO THE GATE. MAINTENANCESDR VNAA0711010Tire · failedCREW REPORTED THE RIGHT NOSE TIRE SHREDDED UPON LANDING IN CLT. MAINTENANCE INSPECTED AND FOUND THE TIRE SHREDDED, DAMAGE TO THE NLG FOLLOW UP DOOR AND A DENT IN THE FUSELAGE. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES. MAINTENANCE REMOVED AND REPLACESDR MASA200700821Access Panel · departedASH 7160 - BHM-ORD, REPORTED AN UPPER FAN COWL ACCESS PANEL MISSING/DEPARTED ON THE RUNWAY. MX REPLACED THE COWL AND DID NOT FIND ANY SUBSEQUENT AIRCRAFT DAMAGE.SDR CA071126009Cowling · broken(CAN) UPON LANDING, DURING THE OPERATION OF NR1 THRUST REVERSER THE NR 1 ENGINE UPPER FAN COWL DEPARTED THE AC. THE PILOTS DID NOT NOTICE THAT THE COWLING WAS MISSING UNTIL THEY DID THEIR POST FLIGHT WALK-AROUND. THE COWLING WAS LATER FOUND BY AIRPORT OPERATISDR CHQA200700080Flap · malfunctionedCLE TO MSP - ON APPROACH FLAPS FAILED AT ZERO DEGREES. CREW RAN QRH WHILE RECEIVING VECTORS FROM ATC AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU FOR MESSAGES, FOUND NONE, AND RESET THE FLAP SYSTEM. AFTER RESETTING, THE FLAP SSDR CHQA200700081Unknown · odorDFW TO IAH - AFTER TAKEOFF, WHILE CLIMBING THROUGH 6,000FT, CREW RECEIVED "SMOKE TOILET" MESSAGE. THE FLIGHT ATTENDANT CHECKED THE LAV AND SMELLED SMOKE AND HEARD THE ALARM GOING OFF. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. EMERGENCY CRESDR A6WA200740638Connector · dirtyINFLIGHT, RT N2 GAUGE READS ZERO APPROXIMATELY 30 MINUTES INTO FLIGHT. CLEANED BLUE HARNESS CONNECTOR W8P2 AT RT ALTERNATOR IAW 73-21-13 AND AWAC SUPP 06-003, OPS CHECK GOOD. (K)SDR CA071127008Windshield · cracked(CAN) F/O WINDSHIELD SHATTERED OUTSIDE LAYERS AT FL340. (TC NR 20071127008)SDR CA071127009Windshield · cracked(CAN) CLIMBING THROUGH 32,400 ON OUR WAY TO 34,000 WE HEARD A POP AND SAW THE PILOTS WINDSHIELD CRACK/ SPLINTER. FOLLOWED QRH AND CONTINUED TO DESTINATION. (TC NR 20071127009)SDR A6WA200740664Hinge · crackedRT SIDE BUTE DOOR 694JB PIANO HINGE CRACKED. HINGE REPLACED ON BUTE DOOR 694JB IAW CRJ 200, SRM 51-42-06 AND PAINTED IAW CRJ 200, SRM 51-25-01. (K)SDR A6WA200740636Flap System · failedAFTER TAKEOFF FLAPS FAILED AT 13 DEGREES OAT +6 DEGREES CELCIUS, WHEN FLAPS BEING RETRACTED FROM 20 DEGREES TO 8 DEGREES. RESET FLAPS IAW AWAC SUPPLEMENT 98-018B STEPS 1.3 AND 1.4 FLAPS RESET, AIRCRAFT RELEASED FOR SERVICE. (K)SDR A6WA200740631Skin · gougedRT MLG DOOR L/E INNER SKIN GOUGE RT MLG DOOR REPAIRED IAW REO 601R-52-82-034. (K)SDR A6WA200740641Floorbeam · crackedCRACK EXIST ON BRACKET OF FLOORBEAM, FS 280, LBL 9 AND RBL 9 CRACK ON BRACKET IS 1 INCH. NEW SERVICEABLE BRACKETS INSTALL AT FS 280.00, LBL 9.0 AND RBL 9.0 IAW SRM 51-42-06. (K)SDR A6WA200740642Exhaust Duct · corrodedAPU EXHAUST LIPS CRACKED AT 5 O`CLOCK AND 6 O`CLOCK. APU EXHAUST REPLACED IAW AMM 49-81-01-400-801. (K)SDR A6WA200740659Intake Duct · crackedAPU INTAKE DUCT CRACKED. APU INTAKE DUCT REPLACED IAW AMM. (K)SDR A6WA200740661Intercostal · crackedCRACK EXIST ON INTERCOSTAL AND BRACKET FS 484, RBL 27 AND RBL 36 CRACK DIMENTION OF INTERCOSTAL 1 INCH AND BRACKET .500 INCH. INTERCOSTAL AT FS 484, RBL 36 REPAIRED IAW REO 601R-53-41-059 BRACKET AT FS 484, RBL 27, REPLACED IAW REO 601R-53-41-059. (K)
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