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 jasc_code = '5700' 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 jasc_code = '5700' 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 NACA2023073150003Unknown · unknownDAMAGE NOTED ON UPPER WING SURFACE AFT OF SLAT #3. REPAIRED DAMAGE TO THE #3 SLAT REF SRM 51-70-01 REPAIR 4SDR IPXA2023072551495Unknown · unknown*SDR FILED OPEN* RH WING #12 SLAT CLOSURE PANEL SPLIT AND NOT FAIRED TO LOWER WING SKIN. PANEL IS SPLIT APPROX. 2 INCHES OUTBOARD TO INBOARD.**10 CYCLE LIMIT***SM20/LMX4*** WILL REQUIRE S/M 20 HOURS TO REPAIR CLOSEOUT PANEL. LINE MX 4 HOURS TO DROP AND LOCK SLSDR AALA202307262411Shear Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING LOCATED AT BS 540 AND LBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1.SDR DALA2023072906135Unknown · unknownSHIP 667 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609767-14AD. CORRECTIVE ACTION: ACCOMPLISH SECTION V: REPETITIVE BHEC INSPECTIONS PRIOR TO 50,922 TOTAL FLIGHT CYCLES (6,000 CYCLES AFTER REPAIR) SDR DALA2023072906133Unknown · unknownSHIP 667 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609767-14AD. CORRECTIVE ACTION: ACCOMPLISH SECTION IV: REPETITIVE BHEC INSPECTIONS TO 47,922 TOTAL FLIGHT CYCLES AND THEN REPETITIVELY WITHIN EVERSDR DALA2023072906132Unknown · unknownSHIP 667 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609767-14AD. CORRECTIVE ACTION: ACCOMPLISH REPETITIVE DVI INSPECTIONS PRIOR TO 47,922 TOTAL FLIGHT CYCLES (3,000 CYCLES AFTER REPAIR) AND THEN REPSDR YENA2023072500857Unknown · unknownDURING HEAVY MAINTENANCE: RH WING LOWER SKIN TE AREA APPROX RIB 10 HAS A CRACK; REF TOMX WO 2222 NR # 00134 CRACK IN RH WING LOWER SKIN TE AREA APPROX RIB 10 WAS REPAIRED PER EMB-190 SRM 57-10-01/REPAIR 54P, SRM 51-41-02 SRM 51-43-04 AND ETI-190-23-584 REV. OSDR DALA2023072506011Unknown · unknownSHIP 3355 DURING HCK AT SAL AND DURING ACCOMPLISHMENT OF EM 5716-01017, HOLE 260LH WAS FOUND CRACKED. A REPAIR WAS ACCOMPLISHED PER SECT I OF ERA 609837-14. CORRECTIVE ACTION: REF SECT III OF ER/A 609837-14. (2877502)SDR DALA2023072506004Unknown · unknownSHIP 3355 CRACK INDICATION FOUND AT FRAME 40 VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AT HOLE 260 LH. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLE #H260 L/H LOCATED ON FR40 L/H SIDE VERTICAL WEB ABOVE THE CENTER WING BOX LOWER PANEL AS PER ESDR FDEA202307211270Former · crackedTHE NOSE FORMER ANGLE AT OSS 499 ON THE RIGHT WING FIXED LEADING EDGE IS CRACKED. REPLACED CRACKED FORMER ON RIGHT WING AT OSS 499 REF. FEDEX DWG SR67-57-002SDR FDEA202307211263Angle · crackedEXISTING REPAIR FOUND AT LEFT HAND WING #2 SLAT OUTER SKIN TRAILING EDGE OUTBOARD CORNER XDLES 327.289 EXISTING REPAIR AT LEFT HAND WING NUMBER 2 SLAT OUTER SKIN TRAILING EDGE OUTBOARD CORNER XDLES 327.289 EVALUATED AND FOUND REPAIRED AS PER EA # 1-5750-T0SDR SWAA2023081787422Doubler · elongatedRIGHT WING DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATED PLATE HOLES ELONGATED 00202145090000012<[01] REMOVED SERRATED PLATES AT R/W DEFLECTION CONTROL RIB UPPER TAB AND UPPER SUPPORT BEAM IN REF B737-700 SRM 51-40-02-0G-0. FABRICATED OUTBOARD DOUBLER (1) ISDR ABXA20230815171Beam · crackedDURING C1 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED CRACK DAMAGE ON LH WING LE NOSE BEAM WEB (114T2300-187), APPROXIMATELY AT OSS 679.82. THE LOWER FLANGE OF THE DAMAGE AREA IS AT THE ACCESS OPENING OF FUELING STATION DOOR LOCATION AS SHOWN IN SDR DALA2023072906148Unknown · unknownAIRCRAFT 0690, AD - 23 DISBONDED AREAS WERE FOUND ON LE SLAT 6 TRAILING EDGE WEDGE UPPER SKIN: 1)1.0IN LENGTH, 0.50IN WIDTH AT ISS 108, 2) 0.75IN LENGTH, 0.625IN WIDTH AT ISS 122.3, 3) 0.75IN LENGTH, 0.70IN WIDTH AT ISS 122.8, 4) 1.0IN LENGTH, 0.75IN WIDTH AT SDR DALA2023072906147Unknown · unknownAIRCRAFT 690, AD - 16 DISBONDED AREAS WERE FOUND ON LE SLAT 5 TRAILING EDGE WEDGE UPPER SKIN: 1) 2.25IN LENGTH, 1.70IN WIDTH AT ISS 129.7, 2 ) 0.875IN LENGTH, 0.81IN WIDTH AT ISS 141.5, 3) 0.80IN LENGTH, 0.75IN WIDTH AT ISS 142, 4) 0.75IN LENGTH, 0.50IN WIDTH SDR SWAA2023080779202Panel · pulledR/W T/E PANEL 661AB HAS SEVERAL PULLED FASTENER HOLES ON AFT END (MARKED)<[01] DAMAGE FASTENER HOLES WERE REPAIRED IAW SRM 51-70-04-2R-9.<BR><BR>VERIFIED CURE SHEETS UPLOADED.<BR><BR>JOB COMPLETE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.<SDR DALA2023071905837Unknown · unknownSHIP 676 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 609602-14AD. CORRECTIVE ACTION: REF ERA 609602-14AD. (2869490)SDR UIEA2023062800665Frame · unknownREFER TO EO 1957A593 PART 2, SB 747-57-2369, #8 FLAP TRACK FAIRING ACTUATOR FRAME FOUND EXISTING REPAIR MOD.(<P>EO 1957A593 PART 2, SB 747-57-2369, #8 FLAP TRACK FAIRING ACTUATOR FRAME EXISTING REPAIR MOD AREA ACCOMPLISHED IAW RI-57-50-16339 REV A. NO FURTHER SDR SWAA2023081685098Access Panel · crackedR/H FWD O/B ACCESS PANEL # 193AR HAS BULGING/CRACKED FASTENER HOLES<[01] SUMMARY :ACCOMPLISHED PULSE-ECHO ULTRASONIC INSP. FOR DELAMINATION ON R/H FWD O/B ACCESS PANEL # 193AR IAW B737 NDT PART 1; 51-01-02 AND PART 4; 51-00-01. NO DAMAGE NOTED. EQUIP: EPOCH 60SDR YENA2023071800804Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE LOCATED BTW RIB 10 TO RIB 11 FRONT SPAR AREA ON RH WING; ACCOMPLISHED REPAIR OF 8 CORROSION SPOTS AT RH WING TRAILING EDGE OVERHANG, TOP SKIN PANEL 2 UPPER AND LOWER SURFACE IN ACCORDANCE WITH AEROMAN EA# 57-02SDR SWI2023F00361Unknown · crackedLH WING INTERNAL TANK SLAT TRACK CANISTER 1-3 HAS POSSIBLE A CRACK IN MOUNTING FLANGE AS MARKED (C-CHECK RO 9/13/2023) REPAIRED LH WING TANK SLAT CANISTER REF. REO N0. 670-57-42-577, REV-- DATED 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAKSDR SWAA2023081681887Access Panel · bulgedR/H OVERWING FAIRING ACCESS PANEL # 195CR HAS BULGING/CRACKED AROUND FASTENER HOLES<[01] C/W;[02] CORRECTION TO READ SUMMARY=PREPARED DAMAGED AREA FOR REPAIR (FASTENER HOLES) AT PANEL #195CR AS PER B737 SRM 51-70-04-2R-9.<BR>APPLIED REPAIR IN DAMAGED AREA AS MSDR SWAA2023081684064Access Panel · exposedL/H UPPER AFT FAIRING ACCESS PANEL # 194FL HAS EXPOSED COMPOSITE AT PANEL AND EDGE OF APU DRAIN MAST<[01] VERIFIED STEP 1;[02] REPAIRED PANEL AT DAMAGED ARE PER B737 SRM 51-70-04-2R-6 PARA 4.E. MATERIALS USED RESIN P/O#2008859; CLOTH P/O#1738579;[03] VERIFIED SDR CALA2023071402254Brace · cracked(737-54-3-0115) R/H WING INBD OF PYLON L/E SUPPORT BRACE HAS CRACK IN RADIUSSDR SROM20230713001Skin · corrodedCORROSION DAMAGE TO CENTER WING SKIN AT FUEL TANK ACCESS PANEL'S PART NUMBER 521BT(LH WING), 521AT (LH WING) AND 621BT (RH WING). CORROSION EXCEEDS THE LIMITS ALLOWED IN GENERIC RD 8/4-57-441.SDR 2023F00224Angle · corrodedCORROSION, LH WING, AFT SPAR, WS 28. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR FR-680-0115-12138 REV-, DATED JULY 11, 2023 AND FAA FORM 8100-9 DATED 7/11/2023; FIELD REPAIR - CORROSION, LH WING, AFT SPAR, WS 28.SDR SWAA2023072877029Angle · crackedCRACK ON SUPPORT ANGLE LOCATED ON ACCESS PANEL 651GB OF TRAILING EDGE AT RT WING 2023-405234<[01] REPLACED SUPPORT ANGLE LOCATED ON ACCESS PANEL 651GB OF TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02;[02] COMPLETEDSDR ASAA2023071143989Door · leakingON PREFLIGHT INSPECTION FIRST OFFICER DISCOVERED ACTIVE FUEL LEAK FROM DRIPSTICK #3 PANEL ON UNDERSIDE OF RIGHT WING. GROUNDED - YES. REMOVED & REPLACED MAIN TANK ACCESS DOOR PANEL NUMBER 632CB IAW AMM 28-11-11-000-801 & 28-11-11-400-801. & PERFORMED LEAK CHECSDR DALA2023071005565Unknown · unknownSHIP 3123 CORROSION OB FLAP TRACK 4 HOUSING BEARING O/B POSITION. CORRECTIVE ACTION: COMPLIED WITH ER/A # 609616-14. (2857579)SDR FDEA202307081186Former · failedNOSE FORMER ANGLE CRACKED AT RIGHT WING OSS 565. VISUALLY INSPECTED FORMER AT FLE OSS 565 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F & A WITH SRM TR 57-111 AS REFERENCE.SDR FDEA202307081185Former · failedNOSE FORMER ANGLE CRACKED AT THE RIGHT WING OSS 499.6. PER EA H-5720-T0367172 REV A VISUALLY INSPECTED FORMER AT FLE OSS 499.603 AND REPLACED FOMRER WITH ANGLE USING FEDEX DRW B67-57-002 / AND -003 REV F WITH SRM TR 57-111 AS REFERENCE.SDR CALA2023071202237Bolt · missingPDA 3 WING TE STRUCTRURE LEFT PANEL 552HB MISSING ONE BOLT. REF. AMM TASK 06-44-00-992-001 ZONE 550 AND 650 ACCESS DOORS AND PANELS. SEE PIC. INSTALLED BOLT IN WING TE STRUCTRURE LEFT PANEL 552HB PER SRM 51-40-02, GOOD FOR SVC,PARTS USED: 00-0593-3-0257,QTY :SDR DALA2023071005578Unknown · unknownSHIP 3123 CRACK ON BUTTSTRAP LOC. BETWEEN RIB 7 TO RIB 9 UPPER SURFACE TRAILIN G EDGE LH WIG. CORRECTIVE ACTION: COMPLIED WITH ER/A 609655-14. (2854388)SDR SWIA20230824706Unknown · damagedRH LOWER AUX SPAR (PN CC670-10742-4) WAS FOUND TO BE DAMAGED AFTER REMOVING THE LOWER SKIN PANEL. (FILED CLOSED)PERFORMED TEMPORARY REPAIR OF RH LOWER AUX SPAR FLANGE BETWEEN WS24.00 - WS34.00 IN REF TO REO 670-57-21-952, REV--, DATED 2023-07-15. COMPLIED WITHSDR JJBA20230712010Unknown · unknownQTY (1) HOLE BORE IS NICKED, C/TO RH WING SPAR 3/TORQUE BOX #1 ATTACHMENT LOWER POSITION #2. HOLE OVERSIZED.SDR SWAA2023070775805Winglet · damagedLEFT WING TIP STRUCK LIGHT POLE ON TAXI. C/W CONDITIONAL INSP REPLACED WINGLET .OKAY TO CONTINUE PER EA 23-157-02129 FOR 2 NON REV CYCLES. OKAY TO CONTINUE PER MX NOTE. OPEN DEFECTS TRANSFERRED TO OTS W/O TTG8Q00M30SP WO# 57225482.SDR UIEA2023071000743Unknown · unknownGOUGE DAMAGE ON RH WING LOWER SKIN PANEL NO.2 BETWEEN STRINGER L-8 AND L-9 AT WBL 743.828(<P>1. ACCOMPLISHED EI T2023A57M-1479. SEQUENCE B REV 1. 2. ACCOMPLISHED EI T2023A57M-1479, REV 2. 3. JOB COMPLETED AND COND CHK NORMAL.</P>)SDR SWAA2023071774867Panel · brokenR/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END IS BROKEN<[01] REMOVED R/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END PER SRM 51-40-02-0G-0. STEP 4.;[02] INSTALLED R/W T/E PANEL 651FB FWD SIDE 3RD BRACKET FROM O/B END IAW SRM 51-40-02-0G-0 STEP 4.SDR CALA2023070502165Fastener · missingRIGHT WING LANDING LIGHT PANEL 611AB HAS 1 EA FASTENER MISSING. QC COMPLETING MATERIALS NEEDED FOR EPLACE.RECORDS UPDATE -- DC SPEED TAPE APPLIED, COMPLIED WITH EC/RA:#:3340-01562. ON WALK AROUND FOUND R WING LANDING LIGHT ACCESS PANEL 611AB MISSING 1 EA FASTESDR SWI2023F00287Unknown · damagedRH WING TRAILING EDGE AILERON HINGE#1 FITTING I/B LUG BORE HAS OVERSIZE BORE ( NOMINAL DIAMETER SHOULD BE .6247"-.6253" AND CURRENT DIMENSION IS .6260". (C-CHECK RO 8/31/2023) COMPLIED WITH REO 670-57-51-501 REV-- DATED 2023-07-03 REPAIR STEPS 1-11. FABSDR AALA202308222869Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR JACK FITTING BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2 AND 3. REPAIRED JACK FITTING PER SRM 57-26-13-300-025.SDR DALA2023070405380Unknown · unknownSHIP 3118 CORROSION I/B LUG BUSHING IB AND OB ACTUATOR ON LH AILERON. CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) OF I/B LUG I/B ACTUATOR AND I/B LUG O/B ACTUATOR ON AILERON LH WING AS PER AIRBUS CMM 57-61-21. (2847364)SDR DALA2023070305350Unknown · unknownSHIP 3118 CORROSION IB AND OB BUSHING HINGE 1 ON LH AILERON (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) OF HINGE #1 ON AILERON LH WING AS PER AIRBUS CMM 57-61-21. (2845754)SDR DALA2023070305349Unknown · unknownSHIP 3118 CORROSION I/B AND O/B BUSHING HINGE 3 ON LH AILERON (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) OF HINGE #3 ON AILERON LH WING AS PER AIRBUS CMM 57-61-21. (2845749)SDR DALA2023070305348Unknown · unknownSHIP 3118 CORROSION I/B AND O/B BUSHING HINGE 4 ON LH AILERON (2EA). CORRECTIVE ACTION: REPLACED BUSHINGS (2 E/A) OF HINGE #4 ON AILERON LH WING AS PER AIRBUS CMM 57-61-21. (2845744)SDR VNAA202307020001Skin · gougedLH LEADING EDGE PANEL (FIXED UPPER SKIN) 521AT WAS FOUND TO HAVE GOUGESDR NACA202307070025Unknown · unknownRHW I/B FLAP O/B AFT FAIRING LOWER SURFACE FOUND CRACK. RHW 2/B FLAP O/B AFT FAIRING LOWER REAIRED AS PER B767-300 SRM 57-53-70-2R-1 TABLE 2 & SRM 51-70-03. REV 122 - APR 15/2023SDR NACA202307070024Unknown · unknownRHW O/B FLAP I/B AFT SUPPORT FAIRING FOUND CRACK. RHW O/B FLAP I/B AFT SUPPORT FAIRING REPAIRED AS PER B767-300 SRM 57-53-70-2R-1 TABLE 1 & SRM 51-70-17. REV 122 - APR 15/2023SDR NACA202307070020Unknown · unknown- RHW NO.9 SLAT L/E SKIN AT 41.25 INCH FROM I/B SIDE FOUND CRACK. REPAIRED THE RHW NO.9 SLAT L/E CRACKED SKIN AT 41.25 INCH FROM I/B SIDE AS PER B767-300 SRM 57-43-01-2R-2 FIG 201 REVISION NO.122 - 15 APR/2023SDR NACA2023070100019Unknown · unknownRHW NO.10 SLAT L/E SKIN AT 41.5 INCH FROM O/B SIDE FOUND CRACK. REPAIRED THE RHW NO.10 SLAT L/E CRACKED SKIN AT 41.5 INCH FROM O/B SIDE AS PER B767-300 SRM 57-43-01-2R-2 FIG 201 REVISION NO.122 - 15 APR 2023
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