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 A6WA200740096Anchor Fitting · crackedPAX DOOR ANCHOR FITTING (AFT) PN 601R3807413 IS CRACKED. MAINTENANCE REPLACED PAX DOOR ANCHOR FITTING (AFT) PN 601R3807413 IAW AMM 52-11-17-400-803. (K)SDR A6WA200740097Anchor Fitting · crackedPAX DOOR ANCHOR FITTING (FWD) PN 601R380742-3 IS CRACKED. MAINTENANCE REPLACED PAX DOOR ANCHOR FITTING (FWD) PN 601R3807423 IAW AMM 52-11-17-400-803. (K)SDR A6WA200740099Floorbeam · crackedFLOOR SUPPORT ANGLE AT FS621.0 IS CRACKED (LT) MAINTENANCE REPAIRED LT FS621 FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K)SDR A6WA200740100Floor Support · crackedFLOOR SUPPORT ANGLE AT FS 621 IS CRACKED (RT). MAINTENANCE REPAIRED RT FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117, REV C. (K)SDR A6WA200740101Intercostal · crackedINTERCOSTAL CRACKED AT FS484.0, RBL 36.0. MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW BSC SR 601-53-0030A AND REO 601R-53-41-059, REV A. (K)SDR A6WA200740102Intercostal · crackedINTERCOSTAL CRACKED AT FS484.0, LBL 36.0. MAINTENANCE CUT AWAY DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW BSC SR 601R-53-0030A AND REO 601R-53-41-059, REV A. (K)SDR A6WA200740088Intercostal · crackedRT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.2 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K)SDR A6WA200740089Intercostal · crackedLT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.2 INCH LONG. MAINTENANCE REMOVED AND REPLACED LT INTERCOSTAL PN 601-35012-51 IAW SRM 51-42-06. (K)SDR A6WA200740087Intercostal · crackedFS 484 INTERCOSTAL CRACKED AT RBL 36. MAINTENANCE DAMAGED FLANGE AND INSTALLED REPAIR ANGLE IAW REO 601R-53-41-059 REV A AND BSC STANDARD REPAIR 601R-53-0030A. (K)SDR VNAA0702014Anti-Ice Valve · failedCREW REPORTED A NR 2 COWL ANTI-ICE CAS MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ANTI-ICING VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FORSDR A6WA200740085Angle · crackedAFT EQUIPMENT COMPARTMENT FS 625.00 OBLIQUE ANGLE LT CRACKED 2 INCHES LONG IN AFT RADIUS. MAINTENANCE REMOVED OLD CRACKED 625 OBLIQUE ANGLE, INSTALLED NEW SERVICEABLE ANGLE PN 601-35012-51 IAW SRM 51-42-06. (K)SDR A6WA200740086Angle · crackedAFT EQUIPMENT COMPARTMENT FS 625.00 OBLIQUE ANGLE. RT IS CRACKED 2 INCH LONG IN AFT RADIUS MAINTENANCE REMOVED OLD CRACKED 625 OBLIQUE ANGLE, INSTALLED NEW SERVICEABLE ANGLE, PN 601-35012-52 IAW SRM 51-42-06. (K)SDR A6WA200740084Cowling · departedTOP OF LT ENGINE COWLING DETACHED FROM ENGINE IN FLIGHT STRIKING VERTICAL AND HORIZONTAL STABILIZERS. REMOVED AND REPLACED UPPER NOSE COWL IAW AMM 71. (K)SDR CA070302002Cowling · departed(CAN) FLIGHT 3808, REPORTED A LOUD NOISE SHORTLY AFTER DEPARTURE, ON LANDING DISCOVERED COWLING MISSING AND UNKNOWN DAMAGE TO HORIZONTAL STABILIZER, NO REPORTED INJURIES, SN 7849 (REG N456ZW). WHAT COLLATERAL DAMAGE TO HZ STAB AND OTHER AREAS? HZ STAB LEADINSDR CA070312005Housing · cracked(CAN) CREW ESCAPE HATCH HANDLE HOUSING FOUND CRACKED AND OUTER HANDLE WAS CORRODED. THE PART OF THE HOUSING THAT FITS INSIDE OF THE INNER HANDLE WAS CRACKED COMPLETELY OFF. (TC NR 20070312005)SDR A6WA200740081Duct · crackedINSPECTED APU AND FOUND UPPER AND LOWER INTAKE DUCTS CRACKED BEYOND LIMITS IAW AMM 49-14-01. REMOVED AND REPLACED UPPER AND LOWER APU INTAKE DUCTS. OPERATIONAL CHECK GOOD IAW 49-52-01. UPPER DUCT TSN = 7728, LOWER DUCT TSN = 11740.SDR A6WA200740083Potentiometer · out of adjustFLAPS FAIL CAS MSG AT ZERO DEGREES, LANDING WEIGHT 40,000 LBS, TOUCHDOWN SPEED 160 KNOTS, MAX BRAKE TEMP = 6.0 FLAP LANDING PERFORMED RIG CHECK OF BPSU`S, IAW AMM 27-51-10, FOUND NR 6 AND NR 7 POTENTIOMETERS OUT OF ADJUSTMENT. ADJUSTED POTENTIOMETERS AND PERSDR A6WA200740080Wire Harness · defectiveAPPROXIMATELY 17,000 AGL (STEERING INOP) CAS MESSAGE ILLUMINATED MOMENTS LATER (WOW INPUT) MESSAGE ILLUMINATED. COMPLIED WITH QRH. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED MLG WOW NR 1 ELECTRICAL HARNESS. OPS CHECK GOOD AT THIS TIME, IAW AMM 32-61-05.SDR VNAA0702013Flap System · inoperativeCREW REPORTED A FLAP FAIL MESSAGE DISPLAYED AFTER TAKEOFF. CREW ELECTED TO CONTINUE FLIGHT AND LAND IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED CIRCUIT BREAKERS IN ACCORDANCE WITH THE AIRCRAFT SERVICE LETTER. AIRCRAFT WAS RELEASED FOR SERVICE.SDR A6WA200740071Structure · damagedFOUND NR 15 HOLE AT WS 148 LHS IS ELONGATED TO .230 INCH. (M) MAINTENANCE REPAIRED BY CLEANING UP HOLE AND INSTALLING FREEZE PLUG IAW EO 601R57-10925A. (K)SDR A6WA200740069Angle · crackedFOUND FS 484 ANGLE IS CRACKED AT LBL 36. (M) MAINTENANCE REPLACED ANGLE IAW REO 601R-53-41-059. (K)SDR A6WA200740070Angle · crackedFOUND FS 484 ANGLE IS CRACKED AT RBL 36. (M) MAINTENANCE REPLACED ANGLE IAW REO 601R-53-41-059. (K)SDR A6WA200740067Fitting · crackedIB AND OB CLIPS AT FS 280, RBL 9.0, FLOOR SUPPORT BEAM ARE CRACKED IN RADIUS APPROX .30 INCHES LONG EACH. (K) MAINTENANCE REMOVED AND REPLACED IB AND OB CLIPS PN 601R31113-58 IAW SRM 51-42-06, SRM 51-42-20 AND BSC STANDARD REPAIR 601R-53-0057A. (K)SDR A6WA200740068Fitting · crackedIB AND OB CLIPS AT FS 280, LBL 9.0, FLOOR SUPPORT BEAM ARE CRACKED IN RADIUS APPROX .30 INCH LON EACH. (K) MAINTENANCE REMOVED AND REPLACED IB AND OB CLIPS PN 601R31113-57 IAW SRM 51-42-06, SRM 51-42-20 AND BSC STANDARD REPAIR 601R-53-0057A. (K)SDR A6WA200740064Fitting · crackedFS 280.00 CLIPS ARE CRACKED .2500 INCH IN UPPER RADIUS IB AND OB OF LBL 9. (K) MAINTENANCE REMOVED AND REPLACED FS 280 CLIPS IB AND OB OF LBL 9 IAW MFG STANDARD REPAIR NR 601R-53-0057A STEPS 1 THRU 4. (K)SDR A6WA200740065Fitting · crackedFS 280.00 CLIPS ARE CRACKED .2500 INCH IN UPPER RADIUS IB AND OB RBL 9. (K) MAINTENANCE REMOVED AND REPLACED FS 280 CLIPS IB AND OB OF RBL 9 MFG STANDARD REPAIR NR 601R-53-0057A, STEPS 1 THRU 4. (K)SDR A6WA200740066Angle · crackedLT AND RT FS 625.00 OBLIQUE ANGLES ARE CRACKED .5 INCH LONG ON AFT RADIUS. (K) MAINTENANCE DRILLED OFF, REMOVED CRACKED OBLIQUE ANGLES LT AND RT FS 625 DRILLED UP, ALODINED AND INSTALLED ANGLES PN 601-35012-51 (LT AND 601-35012-529 (RT). OBLIQUE ANGLES INSTSDR CA070219011Connector · corroded(CAN) CREW REPORTED PASSENGER ADDRESS CIRCUIT BREAKER 1Q5 POPPED , NON PA/CHIMES/CALL FUNCTION. MAINTENANCE INSPECTION FOUND STOWED CONNECTOR P1RU CORRODED AND SHORTING , CONNECTOR IS FOR AFT CABIN PA HANDSET ( NOT INSTALLED ON THIS TAIL) , CONNECTOR HAD BEEN SDR A6WA200740062Bracket · crackedHYDRAULIC TRANSDUCER HAT CHANNEL APPROX .1 INCH LONG RT MLG WHEEL WELL CEILING. (K) MAINTENANCE INSTALLED NEW HAT CHANNEL IAW SRM 51-42-06. (K)SDR A6WA200740063Bracket · crackedHYDRAULIC TRANSDUCER HAT CHANNEL CRACKED APPROX .1 INCH LONG LT MLG WHEEL WELL CEILING. (K) MAINTENANCE INSTALLED NEW HAT CHANNEL IAW SRM 51-42-06. (K)SDR CA070219009Flap System · failed(CAN) DURING APPROACH WHEN FLAP SELECTED TO 8 DEG, CREW RECEIVED (FLAP FAIL) CAUTION MESSAGE ON EICAS, CONTROL POSITION DISPLAY SHOWED 2DEG ON LT FLAP AND 0 DEG ON RT FLAP. ZERO DEG FLAP LANDING CARRIED OUT. AFTER LANDING CREW PERFORMED VISUAL INSPECTION OF TSDR CA070214001Flap System · jammed(CAN) ON APPROACH, WHEN THE CREW SELECTED FLAP 8, THE FLAPS DID NOT MOVE AND THEY STAYED AT 0. CREW LANDED FLAPLESS WITHOUT INCIDENT. NO MORE DETAILS. INFORMATION WILL BE UPDATED AS SOON AS IS AVAILABLE. (TC NR 20070214001)SDR VNAA0702009Unknown · unknownCREW REPORTED A LOUD NOISE COMING FROM THE F/O'S SIDE AFTER TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT HAND FORWARD FUSELAGE AREA. SUSPECT COMM DOOR LEFT OPEN BUT WAS NOT OPEN UPON ARRIVAL TO AIRCRAFT. NO DEFSDR CA070213001Fcu · malfunctioned(CAN) FLAP FAIL MESSAGE RECEIVED IN-FLIGHT. AIRCRAFT LANDED UNEVENTFUL WITH FLAPS ZERO (FLAPS WOULD NOT MOVE). (TC NR 20070213001)SDR CA070225001Windshield · broken(CAN) INNER CORE OF CAPTAINS WINDSHIELD SHATTERED AT FL 330. MX REPLACED CAPTAINS WINSHIELD IAW 56-11-01. (TC NR 20070225001)SDR VNAA0702008Unknown · unknownCREW REPORTED PITOT BASE HEAT/ L AOA HEAT/ L STATIC HEAT/ L PITOT HEAT CAS MESSAGES AFTER TAKEOFF. CREW DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED CIRCUIT BREAKER RESETS PER BBD SERVICE LETTER. MAINTENANCE ALSO PERFORMESDR A6WA200740059Support Angle · crackedCARGO DOOR SUPPORT BEAM ANGLE THAT ATTACHES TO REAR PRESSURE BULKHEAD FS 621. CRACKED APPROX 1 INCH LONG (ANGLE PN 601R35050-109). MAINTENANCE DRILLED OFF, REMOVED CRACKED BRACKET, INSTALLED NEW SUPPORT ANGLE PN 601R35050-109 USING HST10AG-6 AND HST110AG-6 HSDR A6WA200740060Rib · crackedLT MLG BATT RIB CRACKED 1 INCH LONG UPPER AFT CORNER MAINTENANCE REPAIRED BATT RIB IWA REO 601R-57-51-046. (K)SDR A6WA200740061Rib · crackedRT MLG BATT RIB CRACKED 1 INCH LONG AT UPPER AFT CORNER.. MAINTENANCE REPAIRED BATT RIB IAW REO 601R-57-51-046. (K)SDR REXA200700044Smoke Warning · activatedTOILET SMOKE MESSAGE AFTER TAKEOFF, PILOT DELCARED EMERGENCY, PERFORMED QRH, LANDING UNEVENTFULL. DEFERRED APU IAW MEL.SDR VNAA0702006Strut · dischargedCREW REPORTED A GEAR DISAGREE MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT IN DAY. MAINTENANCE INSPECTED AND SERVICED THE NOSE LANDING GEAR SHOCK STRUT OIL AND NITROGEN IAW THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO PERFORSDR CA070208001Control Lever · damaged(CAN) AFTER LANDING WITH FLAPS SELECTED TO 45 DEGREES, THE CREW SELECTED FLAPS FROM 45 TO 20 DEGREES AND THE FLAPS DID NOT MOVE. CAPTAIN PUT THE FLAPS BACK TO 45 DEGREES. FECU (FLAPS ELECTRONIC CONTROL UNIT) CODES RETRIEVED BY MAINTENANCE POINTED OUT TO THE FLSDR CA070503001Actuator · unserviceable(CAN) SHORTLY AFTER DEPARTURE, RUNWAY 27L, AT APPROXIMATELY 3000 FEET, THE AC ROLLED TO 45 DEGREES, AND PITCHED UP > 18 DEGREES. THE CREW RECOVERED THE AIRCRAFT AT AN ALTITUDE OF 4500 FEET. POST INCIDENT INVESTIGATION FOUND NO ANOMALIES WITH THE AILERON CONTSDR A6WA200740054Beam · crackedVERTICLE BEAM AT FS 559.0, RBL 9 CRACKED APPROX .300 INCH LONG AT LOWER OB FLANGE. MAINTENANCE REPAIRED FS 559.0 BULKHEAD POST AT RBL 9, LOWER OB FLANGE IAW REO 601R53-41-057 (A). (K)SDR A6WA200740055Intercostal · crackedFS 484.0 INTERCOSTAL CRACKED AT RBL 36 APPROX .4 INCH IN UPPER RADIUS. MAINTENANCE REPAIRED INTERCOSTAL IAW REO 601R-53-41-059 REV (A) AND BSC STANDARD REPAIR 601R-53-0030A. (K)SDR A6WA200740056Skin · corrodedRT WING LOWER PLANK FUEL ACCESS PANEL 640AB HOLE NR 4 AT WS 54.681 HAS MINOR CORROSION ON AFT FLANGE APPROX .003 INCH DEEP AND 3 INCHES LONG IN CRITICAL AREA. MAINTENANCE REPAIRED FUEL WING PLANK CUTOUT HOLE NR 4 (640AB) IAW REO 601R-57-21-030 REV (F).SDR VNAA0702003Flap System · unknownCREW REPORTED A FLAPS FAIL MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED CIRCUIT BREAKERS IAW THE SERVICE LETTER. AIRCRAFT WAS RELEASED FOR SERVICE.SDR A6WA200740052Intercostal · crackedRT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STRINGER 14R IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL PN 601-35012-52 IAW SRM 51-42-06. (K)SDR A6WA200740053Intercostal · crackedLT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STRINGER 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL PN 6013501251 IAW SRM 51-42-06. (K)SDR CA070206003Cover · dislodged(CAN) APPROX 10 MINS INTO THEIR DESCENT, THE NR 1 OIL PRESSURE WARNING LIGHT ILLUMINATED. THE NR 1 OIL PRESSURE READ 0. THE CREW REFERENCED THEIR CHECKLIST AND SHUTDOWN THE ENGINE. THE CREW ANNOUNCED TO THE PAX THAT DUE TO LOW OIL PRESSURE THEY WERE GOING TO
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