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 n_number = 'N968FD' 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 n_number = 'N968FD' 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 FDEA202610061486Bulb · failedFOUND L1 EMERGENCY EXIT SIGN DIM DURING MX PRE-FLIGHT AMM: 33-51-01-2 REMOVED AND REPLACED 11 FAULTY BULBS AT THE L1 EMERGENCY EXIT SIGN AS PER ABOVE REF. (P/N 0L3071BPEGPL). OPS CHECK GOOD. A/C OK FOR SERVICE.SDR FDEA202606030667Pressure Switch · failedJUST STARTING THE TAKEOFF ROLL GOT C HYD SYS PRESS CAUTION MESSAGE. ABORTED TAKEOFF AND RAN QRH PVD AMM: 29-11-19-4 REMOVED AND REPLACED CTR HYD SYSTEM PRESSURE SWITCH AT CANNON PLUG S10002. OP'S CHECK GOOD. NO LEAKS OR FAULTS NOTED. AC OK FOR SERVICE. ALSDR FDEA202604160456Control Cable · out of adjustEXPERIENCED EXTREME UNCOMMANDED PITCH OSCILLATIONS ON CLIMB OUT BETWEEN 3 AND 4 THOUSAND FEET. OSCILLATIONS LASTED 10 TO 15 SECONDS. AIR CRAFT CLEAN CONFIGURATION ACCELERATING TO 250 KNOTS. ENGAGED CENTER AUTOPILOT AND OSCILLATIONS CEASED. MULTIPLE HAND FSDR FDEA202508021357Floorbeam · corrodedAFT CARGO COMPT. FLOORBEAM AT BS 1681 LBL 5.0 WITH CORROSION.SDR FDEA202508021356Floorbeam · corrodedAFT CARGO COMPT. FLOOR BEAM AT BS 1681 LBL 5.0 WITH CORROSION. THIS REPAIR WAS ACCOMPLISHED FOLLOWING EA # F-5310-T0384258 REV A P1. PROCEDURES.COPY ATTACHED.TITLE: FUSELAGE - REPAIR OF STA 1681 FLOOR BEAM UPPER CHORD CORROSION AT LBL 5. THIS IS A MAJOR RESDR FDEA202507301342Skin · dentedRIGHT HORIZONTAL STAB. UPPER SKIN WITH DENT BETWEEN STAB STA 104.248 AND STA 152.248 AND BETWEEN FRONT . SPAR AND AUX SPAR. EVALUATED DENT ON RH HORIZONTAL STAB UPPER SKIN BETWEEN STAB STA 104.248 - 152.248 AND BETWEEN FRONT SPAR & AUX SPAR FOUND THE FOLLWSDR FDEA202507251319Skin · bentL4 DOOR FWD / LWR CORNER SKIN BENT. REPAIRED L4 DOOR FWD, LWR CORNER SKIN, INSTALLED DOUBLER, FILLER IAW SRM 52-10-01-2R AND EA F - 5210-T0384238 P1. THIS IS MAJOR REPAIR.SDR FDEA202507181263Seat Track · corrodedFLIGHT COMPT SEAT TRACK BETWEEN BS 345.0 TO 365.0 LBL 7.0 WITH CORROSION.SDR FDEA202507181262Seat Track · corrodedFLIGHT COMPART SEAT TRACK BETWEEN BS 345.0 TO BS 365.0 RBL 14.5 WITH CORROSION.SDR FDEA202503110355Battery Pack · failedDURING PREFLIGHT CENTER GALLEY EXIT LIGHT AND L1 DOOR SLIDE LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS POWER SUPPLY BATTERY REF757MM 33-51-07-2.L1 DOOR SLIDE LIGHT AND GALLEY CENTER EXIT LIGHT AND ALL EXIT LIGHTS OPS CHECK GOOSDR FDEA202410031419Bolt · brokenPDIS 968 52-10-0118 03OCT24 13:43 MIA L1 DOOR HINGE S BROKEN RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 06OCT24 "MEL 52-11-01-A: L1 DSDR FDEA202410031418Hinge · failedL1 DOOR HINGE S BROKEN INITIAL INSPECTION APPEARS THAT LOWER ARM ASSY - GUIDE-HINGE MECH" DETACHED FROM THE DOOR, THE 4 BOLTS THAT HELD THE SERRADED PLATE ATTACHED TO THE ARM BACKED OUT. RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B. L1 DOOR - SDR FDEA202409261375Bottle · emptyR1 DOOR EMERGENCY POWER RESERVOIR DEFLATED. RELEASED FOR SERVICE PER MEL : 52-11-01-A CATEGORY : B EXPIRATION : 29SEP24 "MEL 52-11-01-A: _R1____ (IDENTIFY L1 OR R1 DOOR OR SLIDE) - DOOR EMERGENCY POWER RESERVOIR DEFLATED. REMOVED AND REPLACED R1 DOOR EMSDR FDEA202307181241Fan · failedAT CRUISE FL370 WE EXPERIENCED AN ACRID ODOR ELECTRICAL IN NATURE. WE DONNED THE O2 MASKS INITIATED AN EMERGENCY DESCENT AND RAN QRH 8.1.14. WE STOPPED THE CHECKLIST AT STEP 9 DUE TO THE DECREASE IN ODOR. UPON LANDING IN STL WE NOTICED AN EQPT OVHT EICAS SDR FDEA202206281614Lamp · inoperativeON POSTFLIGHT NOTICED LH SIDE EXTERNAL EMERGENCY LIGHT INOP. RELAMPED 917 AS PER AMM TASK 33-51-06-962-001-001 REV 129.22 OPS CHECK GOOD.SDR FDEA202205181256Spacer · crackedMDIS 968 32-41 8125 18MAY22 OPO FACT U DURING DAILY CHECK FOUND THE NLG WHEEL LH SPACER WITH A CRACK WITH 2 INCH. SPACER OF NOSE LANDING GEAR WHEEL LH REPLACED / INSTALLED AS PER AMM 32-45-02-4 REV 129.SDR FDEA202203020401None · nonePDIS 968 27-50 7913 02MAR22 HEL FACT U DURING FINAL LANDING CONFIGURATION, UPON SELECTING FLAPS 25, WE RECEIVED A TE FLAPS DISAGREE. THE FLAP HANDLE WAS 25 (CHECKED IN THE DETENT) AND THE FLAPS INDICATED 20. THE TE FLAPS DISAGREE MESSAGE WENT SDR FDEA202201190103Transmission · trippedTRAILING EDGE FLAP DISAGREE LIGHT AT FLAPS 20 SELECTING 25. RAN QRH & LANDED. TROUBLEHOT IAW FIM 27-51 FAULT TREE 805, NO FAULT FOUND ON FSEU 1, 2 OR 3. FOUND INTMT FAULT CODE 305 ON FSEU 1, LEG-0, NO FAULT HISTORY ON FSEU 2 & 3. LOAD INDICATOR POPPEDSDR FDEA202110182646Crease Beam · corrodedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CREASE BEAM INBD CHORD CORRODED, BETWEEN STA1400 AND STA1620, RBL64.4 COMPLIED WITH FEDEX EA: F-5321-T0364905 PT1, EA TITLE: FUSELAGE - CARGO COMP FLOORS - CREASE BEAM INNER CHORD, STA1400-STA1620, RH SIDE, EXTSDR FDEA202110082601None · noneFUSELAGE - MAINFRAME - STATION 1640 FUSELAGE FRAME WEB OPEN HOLE HFEC INSPECTION FOUND INBD 2EA HOLES WITH CRACK SIGNAL, AT STGR14RH COMPLIED WITH FEDEX EA: F-5310-T0364784 PT1, EA TITLE: FUSELAGE - MAINFRAME - CRACK INDICATIONS AT RH STA 1640 FUSELAGE FRASDR FDEA202109172322Drive Assy · trippedON APPROACH SELECTED FLAPS 25 AND GOT TE FLAP DISAGREE. QRH AND LANDED FLAPS 20. FIM 27-51 FT 808 REV 127.2 APPLIED, FOUND RH INB FLAPDRIVE OVERLOAD POPOUT ACTUATED. FOUND SPINDEL DIRTY AND DRY. CLEANED AND LUBRICATED. FLAPS CYCLED , NO FAULTS. OK FOR SESDR FDEA202011262978Lamp · inoperativeFLIGHT COMPARTMENT EMERGENCY LIGHT IS NOT WORKING. ENT BY: 624027 RPT BY: 624027 FACT 26NOV20 08:22 MUC U 944, S/N NONE. ACC AMM: 33-51-09-3 COCKPIT EMERGENCY LIGHT LAMP REMOVED AND REPLACED, FUNCTION OK. LAMP MANUFACTURER GE, MPN 1317, CPN 0032.SDR FDEA202011262977Light · inoperativeEMERGENCY SLIDE LIGHT AT DOOR 1 LT IS INOPERABLE. ACC AMM: 33-51-06-2-1 L1 SLIDE EMERGENCY LIGHT LAMP REMOVED AND REPLACED, FUNCTION OK.SDR FDEA202011262975Lamp · burned outMDIS 968 33-50 6639 26NOV20 MUC FACT U. FLIGHT COMPARTMENT EMERGENCY LIGHT IS NOT WORKING. FACT 26NOV20 08:22 MUC U ACC AMM: 33-51-09-3. COCKPIT EMERGENCY LIGHT LAMP REMOVED AND REPLACED, FUNCTION OK. LAMP MANUFACTURER GE, MPN 1317, CPN 0032944, SN NONE.SDR FDEA202011262974Lamp · burned outMDIS 968 33-50 6638 26NOV20 MUC FACT U. EMERGENCY SLIDE LIGHT AT DOOR 1 L IS INOPERABLE. FACT 26NOV20 08:12 MUC U. ACC AMM: 33-51-06-2-1 L1 SLIDE EMERGENCY LIGHT LAMP. REMOVED AND REPLACED, FUNCTION OK. LAMP MANUFACTURER GE, MPN 767, CPN 3313380. SN NONESDR FDEA202009252329Transmission · trippedTRAILING EDGE FLAP DISAGREE EICAS MESSAGE WHEN SELECTING FLAP 20 TO 25. BITE DONE ON ESCU NR 1. FOUND ON EXT FAULTS MSG 221 RIGHT FLAP XNT. TRAILING EDGE FLAP TRANSMISSION POP OUT TRIPPED. TRANSMISSION FLUID CHECK DONE AND LUBRICATION DONE. ALSO POPOUT RESDR FDEA2020081861918Battery Pack · inoperativeEXTERIOR EMERGENCY LIGHTING AT L1 DOOR NOT WORKING. BATTERY PACK M731 REPLACED AND TESTED IAW AMM 33-51-07-2,SDR FDEA2020081861917Battery · inoperativeINTERIOR EMERGENCY LIGHT ABOVE L1 DOOR NOT WORKING. BATTERY PACK M731 REPLACED AND TESTED IAW AMM 33-51-07-2.SDR FDEA201911263098Tee Fitting · corrodedFORWARD CARGO DOOR LOWER INTERCOSTAL OUTER TEE #4 FROM FWD SIDE IS CORRODED EVALUATED CORROSION ON FWD CARGO DOOR LWR. INTERCOSTAL OUTER TEE #4 FROM FWD SIDE FOUND TO BE 100% OUT OF LIMITS IAW B757 SRM 53-30-02-1A FIG. 101 DET. IV, REMOVED OUTER SUPPORT TSDR FDEA201911263097Tee Fitting · corrodedFWD CARGO DOOR LOWER INTERCOSTAL OUTER TEE #2 FROM THE FWD SIDE IS CORRODED EVALUATED CORROSION ON FWD CARGO DOOR LWR. INTERCOSTAL OUTER TEE #2 FROM THE FWD SIDE FOUND TO BE 100% OUT OF LIMITS IAW B757 SRM 53-30-02-1A FIG.101 DET. 1V, REMOVED OUTER TEE SUPSDR FDEA2019111542955Acoustic Panel · puncturedAPU LH SIDE ABOVE OIL COOLING DUCT HAS A PUCTURE HOLE ON ACCUSTIC PANEL. ACCOMPLISHED REPAIR ON APU L/H SIDE ABOVE OIL COOLING DUCT ON ACCUSTIC PANEL (INTERNAL FUSELAGE SKIN) IAW B757 SRM 51-80-01-2R FIG 201 AND IAW B757 SRM 51-70-10-2R REPAIR 2.SDR FDEA201908201954Flap System · malfunctionedON APPROACH (ABOUT 1500') CALLED FOR FLAPS 25 DEGREES AND THE TRAILING EDGE FLAPS DISAGREE LGT ILLUMINATED. BROKE OFF THE APPROACH, RAN THE QRH AND LANDED FLAPS 20 DEGREES WITHOUT FURTHER INCIDENT. FIM 27-51 FT 803 CARRIED OUT, NO FAULTS EVIDENT, ON EITHSDR FDEA2019061751308Control Rod · out of adjustTHE SLIDE PLACARD DOES NOT COME INTO VIEW WHEN THE LEFT FORWARD DOOR IS ARMED, ADJUSTED AND LUBRICATED L1 DOOR EMERGENCY MECHANISM RETRACTABLE DOOR CONTROL ROD , SYSTEM TESTED SATISFACTORY IAW AMM 52-11-20-5, MEL CLOSED, PLACARD REMOVED, A/C OK FOR SERVSDR FDEA2019060391194Ballscrew · damagedWHILE COMPLYING WITH TSI 27-50/5006 FOUND OVERLOAD INDICATOR POPPED ON R/H INBOARD TRANSMISSION ASSY ON INBD FLAP INPECTED BALLSCREW WITH A CHEESECLOTH FOR SHARP EDGES AND FOUND UNSATISFACTORY ON TRANSMISSION #5. INSPECTED ALL OTHER TRANSMISSION ASSY'S SDR FDEA201905291180Warning System · false activationON FINAL APP. ATH. EICAS DISPLAYED TE FLAP DISAGREE (WITH FLAPS 20). RAN QRH. PERFORMED FIM 27-51 FAULT 811. UNABLE TO DUPLICATE THE FAULT FLAP SLAT ELEX UNIT 1 2 3 WITH NO EXIST FAULTS. IN FAULT HISTORY "0" - MSG 30S FLAP DISAGREE INTERM. OPERATIONAL TEST OFSDR FDEA201903150644Transducer · out of adjustA/P ON IN VNAV, BELOW PATH, THROTTLES IDLE AIRCRAFT NOSE PITCHES DOWN RESULTING IN 6000' FPM DESCENT WITH AIRSPEED INCREASING AND SPEED BRAKES OUT. AIRCRAFT DOES NOT HONOR AIRSPEED, VNAV PATH, OR VERTICAL SPEED. AUTOPILOT DISENGAGED WITH VERY HEAVY NOSE DOWINSDR FDEA201902150417Computer · malfunctionedWITH R A/P ON, A/C WENT FROM A 2000 FPM TO A 4500 FPM RATE OF DESCENT. APPROACHING LEVEL OFF ALT PF CLCK IS OFF A/P AND HAND FLEW REMAINDER OF ARRIVAL AND APPROACH REPEAT GRIPE ON A/P SYSTEM. IDENTIFIED PARTS FLT MGMT COMPUTER MPN: 4052506-955 CPN: 3414772 QTSDR FDEA201902150416Autoland Sys · malfunctionedPDIS 968 22-20 4737 14FEB19 TLV FACT U LOGPAGES:3011346 3011350 REPEAT EVENT: IN VNAV PATH @ 350, DECENDING TO 210, ACT WENT FROM VNAV PATH TO VNAV SPEED AND PITCHED DOWN AGRESSIVLEY TO 10 DEG NOSE LOW AND OVER 7000FPM DESCENT. DURING DESCENSDR FDEA2018092102640Pump · malfunctionedRT HYD ENG PUMP EICAS DURING FLIGHT AUTO EVENT RECORDED IN FLIGHT SHOWING RIGHT SYSTEM HYDRAULIC PRESSURE AT 1070 PSI, WHILE LEFT SYSTEM WAS AT 2980 PSI, AND CENTER SYSTEM AT 3120 PSI. CRANKED NR 2 ENGINE AT THE GATE AS PER JET RUN-UP HANDBOOK, AND PRESSURE ROSDR FDEA2018090502338Sensor · dirtyR1 CREW DOOR SLIDE ARMED LIGHT INOP. CLEANED SENSOR AND PERFORMED INSPECTION AND TEST IAW AMM 52-11-25-5-0 SYSTEM OK ACFT RELEASED FOR FLIGHT.SDR FDEA2018082312151Control Panel · malfunctionedWITH VERTICAL SPEED SELECTED, RIGHT AUTO PILOT, AND -500FT/MIN SELECTED AT 10,000FT, ACTUAL VERTICAL SPEED WENT TO -2500FT/MIN UNTIL AUTOPILOT WAS DESESECTED IS 0. SIMILAR TO PREVIOUS WRITEUP. THE FOLLOWING MCDP GROUND TEST 30 CURRENT FAULT REPORT AND TESSDR FDEA2018081752046Servo Valve · failedDURING DESCENT FROM 15,000 TO 11,000 IN VERT SPEED WITH -1 300 FPM SELECTED, ON THE LEFT AUTOPILOT, THE AIRCRAFT PUSHED OVER TO -3 000FPM. DISCONNECTED THE AUTOPILOT TO PULL OUT OF THE DIVE AND THERE WAS VERY HEAVY PRESSURE ON THE YOKE. HAD TO TRIM NOSE UP FORSDR FDEA201806151499Wheel · looseNOSEWHEEL STEERING HAD TO BE STEERED TO THE LEFT TO MAINTAIN STRAIGHT COURSE. R&R RT NOSE WHEEL PER MM 32-45-02-4.SDR FDEA201711123237Beam · crackedSTUB BEAM AT STA 580 IS CRACKED CUTOUT & REMOVED DAMAGE AREA FROM FLOOR SUPPORT BEAM STA 580 LBL 45 UPPER FLANGE AFT IAW SRM 51-10-02 & EA F5310-T0336463 P1. FABRICATED NEW REPAIR ANGLE AND REPAIR RADIUS STRAP IAW EA NR F5310-T0336463 P1 & INSTALLED REPAIR ANGSDR FDEA201711023131Frame · crackedMAIN CABIN, FRAME BS 1640 CRACKED APROXIMATELY 5/16 INCH LONG, BELOW STRINGER 14L. REPAIRED THE FRAME IAW EA F-5310-T0336394, P1.SDR FDEA201707212016Strap · out of positionR1 DOOR WOULD NOT ARM FOUND SLIDE STRAP IN THE WAY OF THE GIRT BAR, STOWED STRAP, OPS CHECKED GOOD IAW MM 25-66-11-2.SDR FDEA201707191994Lamp · inoperativeR1 SLIDE LIGHT INOPERATIVE. REPLACED THE LAMPS IAW SMP, OPS CHECKED GOOD.SDR FDEA201610283756Reservoir · low pressureFOUND L1 EMERGENCY POWER DOOR RESERVOIR PSI BELOW LIMITS. R & R THE RESERVOIR IAW MM 52-11-30-4, ACFT OK FOR SERVICE.SDR FDEA201610273704Cover · missingDURING POST FLIGHT, FOUND EMERGENCY ESCAPE ROPE COVER MISSING ONE LATCH . INSTALLED NEW COVER IAW 25-61-00-4-0. OK FOR SERVICESDR FDEA201607312695Proximity Sensor · dirtyL1 DOOR SLIDE LIGHT INOPERATIVE WITH DOOR CLOSED AND SLIDE ARMED. CLEANED SMALL AMOUNT OF DEBRIS FROM GIRT BAR PROXIMITY SWITCHES, CYCLED DOOR ARMING LEVER MANY TIMES, L1 LIGHT OPS CHECKED NORMAL IAW MM 25-66-00-0-0.
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