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 = 'A310' 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 = 'A310' 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 05FDEA04086Data Plate · missingDISCREPANCY (N0633 AND N0634): UNABLE TO VALIDATE MFG P/N AND S/N OF INSTALLED AIRFRAME LIFE LIMITED PARTS LT AND RT MLG RETRACT CYLINDERS DUE TO MISSING DATA PLATES. NSTALLED NEW DATA PLATE PER FEDEX DRWG. Z-20-001 REV. A AND AMM 11-22-32SDR 05FDEA04041Shear Pin · failedAFTER TAKEOFF FROM KMIA,WHEN THE MLG RETRACTED THE LT MLG DOOR SHOWED UNLOCKED ON FWD PANEL, OVERHEAD PNL,AND ECAM.WHILE GERAR HANDLE WAS IN THE UP POSITION THE AMBER DOOR LIGHT WAS ON AND THE RED GEAR UNLK LIGHT WAS ON.WHEN LDG GEAR HANDLE WAS MOVED TO NEUSDR 05FDEA04016Regulator · malfunctionedNR 2 ENGINE INDICATED HIGH OIL PRESSURE, THEN FOLLOWED QRH & MONITORED PARAMETERS. OIL PRESS. WENT TO 20-32 PSI (LOW) FOLLOWED QRH AND SHUTDOWN ENGINE. DECLARED EMERGENCY AND LANDED RWY 32L. HIGH OIL PRESS. WAS 100, LOW OIL PRESS. WAS 22. PRESSURE VARIED SDR 05FDEA03996Skin · damaged2 GOUGES IN UPPER EXTERIOR FUSELAGE SKIN AT FR61 BETWEEN RT STRINGERS 3-4. CUT OUT DAMAGED AREA OF SKIN IAW A310-200 SRM 53-27-00. PERFORMED HFEC IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED DOUBLER REPAIR IAW A310-200 SRM 53-10-12 FIG. 228.SDR 05FDEA03995Skin · damagedPUNCTURE, DENT, AND GOUGES IN SKIN AT FR 46 RT STRINGERS 7-9. DAMAGE AREA APPROX 11.5 INCH X 7 INCH. CUT OUT DAMAGED AREA TO SKING ANS STRINGER IAW A310-200 SRM 53-10-12 AND 53-10-14. PERFORMED HFEC IAW NTM 51-10-08. NO CRACKS NOTED. SPLICED STRINGERSDR 05FDEA03994Skin · puncturedPUNCTURE AND DENT IN SKIN APPROX FR 44 RT STRINGERS 6-7. DAMAGE APPROX 5.00 IN X 3.2 IN. CUT OUT DAMAGE IAW A310-200 SRM 53-27-00. NDT FOR CRACKS IAW NTM 51-10-08. NO CRACKS NOTED. INSTALLED REPAIR DOUBLER IAW A310-200 SRM 53-10-12 FIG. 228. WORK DOCUMSDR 05FDEA03596Skin · gougedRT WING NR 2 SLAT IB TE HAS DENT AND GOUGE APPROX 4.7" LONG UPPER END (HURRICANE RITA NR 31) REF N00081. COMPLIED WITH EA 6-5750-93420SDR 05FDEA03505Door · malfunctionedSOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FO R AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICATIOSDR 05FDEA02977Seat Track · corrodedMDCC - SEAT TRACK BETWEEN FS 75-77 LBL HAS SPOTS OF CORROSION.SDR 05FDEA02976Seat Track · damagedMDC - SEAT TRACK AT RBL 58 BETWEEN FS 62-63 HAS SEVERAL DAMAGED LUGS.SDR 05FDEA02975Control Unit · malfunctionedON CLIMB-OUT JUST ABV FL190, MAIN DECK CARGO SMOKE WARNING ANNUNCIATED FOR MID 2. PRIOR TO MAIN DECK WARNING LOOP A MID 2 FAULTED. COMMENCED AIR TURN-BACK TO KGRR, RAN MDC SMOKE PROC IAW QRH. ECAM REQUEST TO NORM ON DESCENT THROUGH APPROX 15000'MSL. NO SMOSDR 05FDEA02916Floor Panel · delaminatedMDCC FLOOR PANEL 232EG IS DELAMINATED. FABED NEW FLOOR PANEL.SDR 05FDEA02915Floor Panel · crackedMDCC FLOOR PANEL 241WH IS CRACKED. FABED NEW FLOOR PANEL.SDR 05FDEA02914Floor Panel · delaminatedMDCC FLOOR PANEL 232NG DELAMINATED. FABED NEW FLOOR PANEL.SDR 05FDEA02913Floor Panel · crackedMDCC FLOOR PANEL 231JG IS CRACKED. FABED NEW FLOOR PANEL.SDR 05FDEA02912Floor Panel · crackedMDCC FLOOR PANEL 231JH CRACKED. FABED NEW FLOOR PANEL.SDR 05FDEA02911Floor Panel · crackedMDCC FLOOR PANEL 231KH IS CRACKED. FABED NEW FLOOR PANEL.SDR 05FDEA02910Floor Panel · crackedMDCC FLOOR PANEL 231TG CRACKED. FABED NEW FLOOR PANEL.SDR 05FDEA02909Floor Panel · puncturedMDCC FLOOR PANEL 231VG IS PUNCTURED. FABED NEW FLOOR PANEL.SDR 05FDEA02908Floor Panel · delaminatedMDCC FLOOR PANEL 242UJ DELAMINATED. FABED NEW PANEL.SDR 05FDEA02907Floor Panel · crackedMDCC FLOOR PANEL 231VG-2 IS CRACKED. FABED NEW FLOOR PANEL.SDR 05FDEA02906Floor Panel · crackedMDCC FLOOR PANEL 232TG IS CRACKED. FABED NEW FLOOR PANEL.SDR 05FDEA02905Floor Panel · delaminatedMDCC FLOOR PANEL 242EK IS DELAMINATED. FABED NEW FLOOR PANEL.SDR 05FDEA02904Floor Panel · crackedMDCC - FLOOR PANEL 231NH IS CRACKED. FAB`D NEW PANEL.SDR 05FDEA02903Seat Track · corrodedMDCC - SEAT TRACK FR 79 LBL 56 CORRODED. REMOVED CORROSION, REMOVED SEAT TRACK, DRILLED NEW TRACK, INSTALLED TRACK IAW SRM 53-10-16, 51-40-21, 51-40-44, AND 51-40-21.SDR 05FDEA02902Seat Track · corrodedMAIN DECK SEAT TRACK FR 58 TO 72 CORRODED. REMOVED CORROSION, REMOVED TRACKS, FAB REPAIR PARTS INSTALLED REPAIR PARTS IAW SRM 51-23-10, 51-40-21, AND 53-10-16.SDR 05FDEA02901Spar · corrodedLT HORIZ STAB UPPER REAR SPAR T-CAP LOWER SIDE CORRODED AT NUTPLATES 51 TO 57 IN FROM FUSELAGE. REMOVED NUTPLATES, REMOVED CORROSION, MODIFIED RIB SUPPORT FABED REPAIRS, AND INSTALLED REPAIRS IAW SRM 51-40-21, 55-11-21, AND 51-74-10.SDR 05FDEA02900Seat Track · crackedMCD SEAT TRACK BET FR 61 AND FR 62 BL 0 HAS CRACK. REPAIRED SEAT TRACK IAW SRM 53-10-16.SDR 05FDEA02928Engine · malfunctionedON TAKEOFF ROLL AT 40 PERCENT N1 WHEN TOGA BUTTONS DEPRESSED NR 1 ENG ADVANCED, NR 2 ENG DID NOT. REJECT AT LESS THAN 20 KNOTS. RELEASED FOR SERVICE PER MEL/CDL: 22-30-01-A. R AND I TCC PER MM 22-36-34-4 AND PERFORMED ADJUSTMENT AND TEST PER MM 22-30-00-5SDR 05FDEA02920Seat Track · corrodedMDCC SEAT TRACK BETWEEN FR. 51 ,52 LBL 56 HAS CORROSION . REMOVED AND REPLACED SEAT TRACK DUE TO OUT OF LIMITS CORROSION IAW SRM 53-10-16 AND 51-40-21.SDR 05FDEA02919Seat Track · damagedMDCC SEAT TRACK HAS DAMAGED LUGS. REMOVED DAMAGED TRACK AND INSTALLED NEW TRACK IAW SRM 51-40-21, 51-21-10, AND 53-10-16.SDR 05FDEA02918Seat Track · nickedMDCC SEAT TRACK HAS NICKS. REMOVED NICKED SEAT TRACK AND INSTALLED NEW TRACK IAW SRM 53-10-16, 51-27-00,51-40- 40,AND 51-21-00.SDR 05FDEA02917Seat Track · corrodedMDCC SEAT TRACK IS CORRODED. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK IAW SRM53-10-16, 51-40-21, AND51- 23-10.SDR 05FDEA02225Coalescer Bag · contaminatedON TAXI OUT MEM, SMELLED A STRONG SMELL THEN A FULL MAIN DECK SMOKE WARNING WHICH LASTED FOR SEVERAL MINUTES. DECLARED EMERGENCY. DETECTION CLEARED ITSELF. RETURNED TO GATE. REPLACED NR 1 AND 2 PACK WATER SEPARATOR BAGS AS PRECAUTIONARY REF A310 AMM 21-51-SDR 05FDEA02008Proximity Sensor · failedTAT HEAT FAULT. TAT FAULT & ALL THREE PITOT HEAT FAULT ILLUMINATED ON OVERHEAD. REMOVED PROXIMITY SENSOR UNIT AND INSTALLED LANDING GEAR RELAY SIMULATOR SET IAW A310-200 MM 32-00-00-5. LANDING GEAR HANDLE WOULD GO TO FULL UP WITHOUT INTERLOCK AS IT SHSDR 05FDEA02042Fire Loop · damagedAFTER T/O AT 15000FT, RECEIVED FIRE WARNING ON ENGINE NR 2. DID PROCEDURES AND RETURNED TO LLBG. TLV U-INSPECTION & T/S PERFORMED ON MTSI 26-10/9536. FIXED DIFFERED LOOP-B, FOUND TWO PLUGS ON LOOP-A SENSING ELEMENTS IN BAD CONDITION (ONE WITH RUBBER ISOLSDR 05FDEA01996Wire Harness · chafedENG NR 2 EGT ANALOG INDICATION CONSTANTLY SWINGS BETWEEN 440 DEG C TO 460 DEG C IN CRZ. NR 1 EGT STABLE AT 450 DEG C. ENG NR 2 EGT INDICATION ERRATIC AS WELL DURING APPROACH. T/S IN PROGRESS. PERFORMED T/S ACC TO TSM 77-21-00 AND AMM 77-21-03-5-A. FOUND ESDR 05FDEA01967Bleed Valve · malfunctionedAFTER TAKEOFF FROM LISBON HAD NR 2 BLEED VALVE FAULT. DURING RETURN TO LISBON RESET NR 2 BLEED AND FOUND FOLLOWING CONDITIONS: AT 3000 FT NR 1 BLEED TEMP 175 / NR 2 BLEED TEMP 175. THE OVERHEAT WITHIN 2 MINS AT 210 - 220 WITH SUBSEQUENT BLEED VALVE NR SDR 05FDEA01966Wire · damagedNR 2 BATTERY OVERHEATED DURING CRUISE. NR 2 BATT SHOWED 21V AND SWITCHED OFF FOR DURATION OF FLIGHT. VERIFIED BATTERY WAS HOT, AND PERFORMED BATT CHARGE CONT BITE TEST. ALL NORMAL. FOUND RED AND BLUE WIRES 195 AND 196 AT BAT2 SHUNT 19PE DAMAGED AND CHAFINSDR 05FDEA01963Battery · overheatedNR 2 BATTERY OVERHEATED DURING CRUISE. NR 2 BATT SHOWED 21V AND WAS SWITCHED OFF FOR DURATION OF FLIGHT. VERIFIED BATTERY WAS HOT, AND PERFORMED BATT CHARGE CONT BITE TEST. ALL NORMAL. FOUND RED AND BLUE WIRES 195 AND 196 AT BAT2 SHUNT 19PE DAMAGED AND CSDR 05FDEA01962Hose · leakingAT APPROXIMATELY 1000 FT ON CLIMB-OUT RECEIVED ECAM WARNING FOR GREEN HYD SYSTEM RESERVOIR LOW. THIS CONFIRMED ON OVERHEAD PANEL ACCOMPLISHED ECAM ITEMS AND RED TABS. GEAR EXTENDED BY GRAVITY EXTENSION METHOD SYSTEM QTY DID NOT GO TO ZERO. FOUND RUPTURED LISDR 05FDEA01916Filter · cloggedREJECTED TAKE OFF AS 95 KNOTS DUE TO ECAM WARNING 'ENG FUEL FILTER CLOG' WARNING WAS RESOLVED AS SOON AS THROTTLES WERE RETARDED. TOGA POWER WAS USED (104.7 PERCENT N1) MESSAGE DISAPPEARED QUICKLY AND WE WERE UNC ERTAIN OF WHICH ENGINE WAS AFFECTED. PULLESDR 05FDEA01899Access Panel · damagedACCESS PANEL 650GB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863.SDR 05FDEA01898Access Panel · damagedACCESS PANEL 650 FB HAS 1 ELONGATED HOLE, COMPLIED WITH EA6-5710-90863.SDR 05FDEA01772Warning Light · false indicationFWD CARGO DOOR LIGHT CAME ON DURING TAKEOFF. RTO (LIGHT CAME ON & OFF.) AC RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 11JUL05 DOOR CLOSED & LOCKED INDICATION ON ECAM DOOR PAGE - INOPERATIVE. DOOR VISUALLY CHECKED CLOSED & LOCKED. DOOR VISUALLY VERIFIED CLOSDR 05FDEA01750Warning Light · illuminatedBLEED AIR NR 1 FAULT WITH ANTI-ICE SELECTED AFTER SELECTING WITH ANTI ICE THEN BOTH PACKS WOULD FAULT AND NOT RESET COULD NOT MAINTAIN CABIN PRESSURE WITH APU BLEED NR 2 BLEED WAS DEFERRED NR 1 ENGINE BLEED WOULD NOT RESET. UNSCHEDULED LANDING T/S PER A310 TSMSDR 05FDEA01744Engine · bird ingestionRTO AT 120 KIAS DUE TO LOUD BANG,VIBRATION,AND PULL TO THE RIGHT. F/O SAW AT LEAST TWO BIRDS MOMENTARILY BEFORE EVENT. MAX POWER DUE WET RUNWAY WINDS CALM. VIBRATION CEASED WHEN NR 2 ENGINE SHUTDOWN ON RUNWAY. REMOVED AND INSTALLED NR 2 ENG, NOSE COWL, RT SDR 05FDEA01714Indicator · malfunctionedREJECTED TAKE OFF, CAPT'S AIRSPEED READ 100 KTS, FO STILL BELOW 80. REJECT NORMAL. PUMPED UP BOTH FO AND CAPT AIRSPEED WITH TEST BOX. FO LAGGED BEHIND CAPT. REMOVED AND REPLACED ADC 2 PER AMM 34-11-34-4. TESTED FO AIRSPEED INDICATOR WITH TEST BOX PER AMSDR 05FDEA01546Frame · corrodedCORROSION ON FRAME 20A AFT SIDE AT STRINGER 44R FORWARD CARGO. FR20A LOWER SECTION AT STR 44R CORROSION WAS FOUND TO BE OUT OF LIMITS IAW A310/200N SRM 53-10-00 FIG 102. REPAIRED BY CUTTING AND REMOVING FRAME SECTION 20A FROM STR 38R TO STR 45R. INSTALLED SDR 05FDEA01544Strap · corrodedCORROSION AROUND NUT PLATE HOLES ON PANEL SPLICE FOR 326EL. REMOVAL OF CORROSION OUT OF LIMIT PER SRM 55-40-00. REMOVED AND REPLACED STRAP IAW A310/200 SRM 51-72-10.
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