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 = '7372M8' 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 = '7372M8' 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 AWXA200601286Wire Harness · damagedSAL - EEL - MAINTENANCE EMERGENCY EXIT LIGHT INOP SEAT ROW 9. EMERGENCY EXIT LIGHT INOP SEAT ROW 9 WAS CORRECTED. REMOVED AND REPLACED SEAT HARNESS, OPS GOOD.SDR CA021108022Apu · failed(CAN) ON APPROACH, APU WAS STARTED AS NORMAL. SHORTLY AFTER START UP A VIBRATION WAS FELT THROUGHOUT THE AIRFRAME. AUTO SHUTDOWN OF THE APU OCCURRED,AS WELL AS A FIRE WARNING IN THE COCKPIT. APU FIRE QRC WAS ACCOMPLISHED WITH ASSOCIATED FIRE HANDLE PULLED AND SDR CA010313021Gearbox · worn(CAN) AIRCRAFT WAS ENROUTE FROM CALGARY TO WINNIPEG WHEN THE RIGHT HAND ENGINE EXPERIENCED A LOSS OF ENGINE OIL. THE CREW SHUT DOWN THE ENGINE WHEN THE OIL PRESSURE STARTED TO DROP AND THE ENGINE OIL TEMPERATURE BEGAN TO CLIMB. THE OIL APPEARED TO HAVE LEAKED SDR CA001122016Engine · failed(CAN) DURING CLIMB FROM VANCOUVER THE CREW NOTICED NR 2 ENGINE OIL QUANTITY DROP TO ZERO. THEY INITIATED A PRECAUTIONARY SHUT DOWN OF THE ENGINE AND RETURNED TO VANCOUVER. MAINTENANCE PERSONNEL IN VANCOUVER FOUND NORMAL OIL QUANTITY IN THE ENGINE. THEY CARRIEDSDR CA001016011Bolt · missing(CAN) CREW REPORTED ON TAXI OUT WHEN THEY CHECKED THE FLIGHT CONTROLS THE ELEVATOR FELT VERY RESTRICTED IN DOWN TRAVEL MOTION. OPERATION FELT NORMAL WITH A SYSTEM HYDRAULIC DEPRESSURIZED. UPON INVESTIGATION FOUND A SYSTEM ELEVATOR PCU INPUT ROD TO ELEVATOR INPSDR AWXA9900477Battery Pack · dischargedROW 6-14 EMERGENCY EXIT LIGHTS DID NOT WORK DURING TEST. BATTERY CHARGED BY CONTRACT MAINTENANCE PREVIOUS FLIGHT. REPLACED AFT EMERGENCY LIGHT BATTERY PACK IN DROP CEILING. OPS CK GOOD RECOMMENDATION. NO RELATED HISTORY.SDR AWXA9900400Wire · brokenEMERGENCY LIGHT INOP, ROW 4. REPAIRED BROKEN WIRE, OPS CK NML.SDR AWXA9900337Rib · crackedC-CHECK, 2 INCH CRACK ON I/B UPPER ANGLE ON LEADING EDGE INT OF I/B FRAME AT WS 185.5 RT WING OF PYLON. REMOVED, FABRICATED, HEAT TREATED TO T3 COND, ALODINED AND REPLACED RIB IAW SRM 57-20-2 AND 57-30-2.SDR AWXA9900340Tie Clip · crackedC-CHECK, STRINGER TIE CLIP CRACKED, 16L FS 727A. REMOVED STRINGER TIE CLIP IAW SRM 51-30-2, FAB'D NEW STRINGER TIE CLIP IAW 51-10-1. TREATED AND PRIMED NEW CLIP IAW SRM 51-10-2.SDR AWXA9900341Angle · crackedC-CHECK, .75 INCH CRACK ON UPPER ANGLE OF LT WING L/E RIB I/B SIDE OF NR 1 ENG PYLON. FABRICATED AND INSTALLED REPAIR PART AT WING STA 185.5 IAW 51-30-00, MATERIAL 2024-0 .063 HEAT TREATED TO 2024-T4.SDR AWXA9900339Skin · crackedC-CHECK, APPROX 2.5 INCH CRACK ON FUSLAGE SKIN 3.5 FT BELOW L-2 DOOR. REMOVED EXISTING DOUBLER PER SRM 51-40-2, CUTOUT DAMAGE PER PT6 51-00-00 FIG 23. FABRICATED DOUBLER AND INSTALLED PER SRM 53-30-1 FIG 1 AND 51-30-2 MATL 2024TB .090.SDR AWXA9900338Skin · crackedC-CHECK, LT FUSLAGE CRACK AT SR17L. ALSO, LT WTB BETWEEN 2ND AND 3RD REPAIR, 4 TO 5 INCHES LONG. BOTH PLACES FABRICATED NEW REPAIR FROM 2024T3 .090 R646704 IAW SRM 53-30-3 FIG 1. TREATED AND PRIMED NEW REPAIR AND AREA, INSTALLED REPAIR DOUBLER PER 53-30-3 FSDR AWXA9900047Skin · crackedDURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK LEFT SIDE AT STRINGER 17, BS 727, BELOW TEMP REPAIR FWD OF BS 747. INSTALLED REPAIR USING BLIND FASTENERS IAW FIG 1 SHEET 2 OF SRM 53-30-3, REPLACE BLIND FASTENERS AFTER 10,000 FLIGHT CYCLES WITH SSDR AWXA9900046Skin · crackedDURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK BELOW STRINGER 16 RT SIDE, AFT OF WING TO BODY FAIRING FROM STATION 747 TO 767. REPAIRED PER ER 2-53-34-09 STEP 7, REPLACE SKIN OR REPAIR WITH SRM APPROVED REPAIR WITHIN 24 MONTHS NOT TO EXCEED 600SDR AWXA9900045Skin · crackedDURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK AT STRINGER 19 RT SIDE AT BS 727 TO 747. REPAIRED PER ER 2-53-34-08 STEP 8, NEED TO REPLACE SKIN OR REPAIR WITH SRM APPROVED REPAIR WITHIN 24 MONTHS NOT TO EXCEED 6000 FLIGHT HOURS.SDR AWXA9900012Battery Pack · dischargedRT EMERGENCY EXIT LIGHT OVER R-2 DOOR INOP. REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT LIGHT BATTERY PACK, OPS CK GOOD.SDR AWXA9800078Power Supply · inoperativeEMERG EXIT LIGHT CENTER AISLE OVERWING WON'T LIGHT WITH OTHER EXIT LIGHTS. REMOVED AND REPLACED BATTERY PWR SUPPLY UNIT, OPS CKD NORMAL. STC NR SA3432NM.SDR AWXA9700391Light · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLASHLIGHT INOP AT L-2 DOOR. REMOVED ANDANDREPLACED L-2 DOOR EMERGENCY FLASHLIGHT & HOLDER.SDR AWXA9700338Battery Pack · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT OVER R-2 DOOR INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. STC - SA3432NM.SDR AWXA9700329Connector · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND SEAT ROW 1 TO 5 EMERGENCY LIGHTS WILL NOT EXTINGUISH WITH EMERGENCY LIGHT SWITCH OFF AND SHIP'S POWER OFF. INSTALLED NEW SOCKET IN POWER SUPPLY CONNECTOR AT ROW 3. STC - SA3432NM.SDR AWXA9700302Battery Pack · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND FIRST CLASS EMERGENCY LIGHTS COME ON WHEN BATTERY TURNED OFF. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD. STC - SA3432NMSDR 97ZZZX2843Housing · crackedSPOILER ACTUATOR HAS A HOLE IN HOUSING. FOUND DURING PROOF PRESSURE TESTING FOR REPAIR.SDR AWXA9700233Position Ind · inoperativeUNSCHEDULED LANDING IN LAS. TRAILING EDGE FLAPS SPLIT, 1 AND 5 POSITIONS. REMOVED AND REPLACED FLAP T/E POSITION INDICATOR. CYCLED FLAPS SEVERAL TIMES, OPS CHECKS GOOD.SDR AWXA9700244Floorbeam · corrodedDURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 312, WL 208, LBL 11 TO RBL 11. REMOVED UPPER CHORD OF FLOORBEAM AT BS 312 FROM LBL 18 TO RBL 18 AND REPLACED CHORD PER SRM 53-10-9.SDR AWXA9700243Floorbeam · corrodedDURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM BS 328, RBL 11 TO 20, WL 208. REMOVED UPPER CHORD, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 53-10-9, FIG 5.SDR AWXA9700225Battery Pack · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND OVERWING CEILING PANEL EMERGENCY LIGHT INOP. REMOVED AND REPLACED OVERWING CEILING EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD, STC - SA3432NM.SDR AWXA9700191Rudder Pcu · malfunctionRUDDER AND AIRCRAFT SHUDDERED EXCESSIVELY DURING DEFLECTION OF RIGHT RUDDER. LEFT RUDDER DEFLECTION NORMAL. REMOVED AND REPLACED RUDDER PCU AND C/W ADJUSTMENT TEST. NO DEFECTS NOTED, OPS NORMAL.SDR AWXA9700190Bolts · looseVIBRATION NOTED BY INBOUND CREW AT FLAPS 2, RT INBOARD FLAP AREA. FOUND LT AND RT INBOARD FOREFLAP TOGGLE BOLTS LOOSE. TIGHTENED AND RE-SAFETIED BOLTS. ALSO, TIGHTENED AND RE-SAFETIED LT INBOARD FOREFLAP TRACK ATTACH BOLTS. INSPECTED ENTIRE FLAP AREA.SDR AWXA9700175Line · blownAIR TURNBACK, LOSS OF SYSTEM-A HYDRAULICS. SHORTLY AFTER TAKEOFF, NR 2 A-HYDRAULIC LOW PRESSURE LIGHT FOLLOWED BY A-SYSTEM QUANTITY TO ZERO. REMOVED AND REPLACED NR 3 BRAKE FLEX LINE AND A-SYSTEM HYDRAULIC CASE DRAIN FILTER, NO DEBRIS. REPLENISHED A-SYSTEM SDR AWXA960605Power Supply · inoperativePHX - FLT 2887 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 AND R-1 EMERGENCY EXIT LIGHTS INOP. REPLACED BOTH FORWARD EMERGENCY EXIT POWER SUPPLY. OPS CHECK GOOD. (M)SDR 96ZZZM1484Power Supply · inoperativePHX - FLT 2887 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 AND R-1 EMERGENCY EXIT LIGHTS INOP. REPLACED BOTH FORWARD EMERGENCY EXIT POWER SUPPLY. OPS CHECK GOOD. REFERENCE AWXA960605.SDR AWXA960592Power Supply · inoperativePHX - FLT 2592 - DURING ROUTINE MAINTENANCE CEHCK, FOUND RIGHT OVERWING EXIT INTERIOR EXIT SIGN ON DOOR FRAME INOP. REPLACED BATTERY POWER CHARGER WITH SERVICEABLE, OPS CHECK NORMAL. (M)SDR AWXA960591Battery · dischargedPHX - FLT 2550 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT L1 AND R1 DOORS. REMOVED AND REPLACED BATTERY PACK, OPS NORMAL AT THIS TIME. (M)SDR AWXA960533Battery Pack · dischargedPHX - FLT 2622 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR LIGHT SIGNS AT R1, L1 AND RIGHT OVERWING INOP. REMOVED AND REPLACED BATTERY PACK M1050. OPS CHECKED GOOD. (M)SDR AWXA960521Connector · shortedPHX - FLT 2267 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT EMERGENCY EXIT AFT VERTICAL EXIT LIGHT INOP. FOUND POWER CONNECTOR SHORTING ON A/C FRAME. REPLACED HEATSHRINK WRAP AND SECURED. (M)SDR AWXA960513Power Supply · inopPHX - FLT 2622 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED MID RIGHT EMERGENCY LIGHT POWER SUPPLY. OPERATES NORMALLY. (M)SDR AWXA960375Turbine Blade · failedLAS - FLT 2976 - AIR TURN BACK, AT CLIMB POWER FL 200 NR 1 ENGINE COMMENCED SEVERE VIBRATIONS. ALL ENGINE INDICATIONS NORMAL. RETARDED THRUST LEVER. VIBRATIONS CONTINUED. SHUTDOWN ENGINE IAW QRH. RETURNED LAS. FOUND TURBINE WHEEL BLADES MISSING MATERIAL.SDR AWXA960350Seat · not securedPHX - FLT 2890 - AIR TURNBACK, SEAT ROW 6 A, B, C, NOT SECURED. SECURED SEAT ROW 6 A, B, C IN SEAT TRACK AS NEEDED. (M)SDR AWXA960331Engine · bird strikeLAS - FLT 0981 - ABORTED TAKEOFF. BIRD STRIKE ON TAKEOFF ROLL. LEFT HAND FORWARD PART OF A/C. C/W AWA FORM 382 FOD INSPECTION PARAGRAPH A, SECTIONS 1 AND 2. FOD DID NOT ENTER ENGINE AND NO DAMAGE NOTED. (X)SDR AWXA960320Engine · overtempPHX/ONT - FLT 2622 - AIR TURNBACK. NR 1 ENGINE OIL TEMPERATURE CLIMBED TO 118 DEGREES AT CRUISE, 123 CELSIUS ON DESCENT, 140 CELSIUS FOR 10 MINUTES AT 110 FEET. POWER UP TEMPERATURE NORMAL. REMOVED AND REPLACED NR 1 ENGINE PER R5M71003, RIGGED PER CARD F5M7SDR AWXA960255Skin · dentedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND SMALL DENT AFT OF L-2 DOOR (CENTER OF DOOR, 2 INCH AFT). REFERENCE FORM 106 NR 23581. REPLACED SKIN PER ER 2-53-35-06. ENGINEERING REFERENCE TCO-PAN-95-0605RR-621RR. (M)SDR SWXA960252Seat Track · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK BS 947-967, LBL 25, WL 208. REMOVED AND INSTALLED FABRICATED SEAT TRACK AT BS 947-967, LBL 25, WL 208 PER SRM 51-30-2, 51-10-1 AND 51-30-8. ALODINED AND PRIMED. (SDR AWXA960256Skin · dentedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND SKIN DENTED STATION 1047-1063, STRINGER 18 RT, WL 206. REMOVED DAMAGED SKIN, FABRICATED REPAIR DOUBLER, INSTALLED REPAIR PARTS PER SRM 53-30-3. (M)SDR AWXA960254Floor Beam · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 947, LBL 0-4, WL 208. REMOVED STRAP AND REPAIRED PER ER 2-53-15-44 (TCO-PAN 96-0624RR). (M)SDR AWXA960253Floor Beam · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 967, LBL 21-19, WL 208. REMOVED DAMAGED AREA AT BS 967, LBL 21-29, WL 208. FABRICATED PART AND INSTALLED PER SRM 53-10-9. (M)SDR AWXA960251Splice · corrodedFLT 7812 - PAE - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON STRINGER 27, RIGHT SPLICE BS 905. REMOVED STRINGER SPLICE AT BS 905 AND STRINGER 27R. FABRICATED REPAIR PARTS IAW SRM 53-10-3, FIG 1. ALODINED, PRIMED AND INSTALLED. (M)SDR AWXA960250Floor Beam · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 1006, LBL 11, WL 208. REMOVED CORROSION BS 1006, LBL 11, WL 208. OUT OF LIMIT PER SRM 53-10-1. REPAIRED IAW ER 2-53-15-43 (TCO-PAN-96-0612RR) (M)SDR AWXA960249Floor Beam · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 986.5, RBL 41, RBL 50, WL 208. REMOVED CORROSION BS 986.5, RBL 37, RBL 39 AND FOUND OUT OF LIMIT PER SRM 53-10-1 AND REPAIR. INSTALLED IAW ER 2-53-15-42 (TCO-PASDR AWXA960158Actuator · brokenTUS-PHX - FLT NR 604 - GATE RETURN, A SYSTEM HYDRAULIC FAILURE DURING TAXI. NR 8 SPOILER ACTUATOR BROKEN AT CASTING. REPLACED NR 8 SPOILER ACTUATOR PER CARD R3M27016. LEAK AND OPERATION CHECK GOOD. (M)SDR AWXA960155Static Inverter · failedLAS - FLT NR 1931 - AIR TURN BACK, AFTER TAKEOFF LOST NAVIGATION AND COMMUNICATION ON CAPTAINS SIDE. REMOVED AND REPLACED STATIC INVERTER AND R-36 RELAY IN P-6. CHANGED R-37 AS A PRECAUTION. (M)
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