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 DALA2023070505434Unknown · unknownSHIP 0685 OUT OF SCOPE MONITOR INSPECTION REQUIRES REWORK AND TERMINATNG ACTION OF FLAME SPRAY REPAIR. CORRECTIVE ACTION: REF ERA 591757 (2844315)SDR SWAA2023072873237Bracket · crackedCRACK INBOARD TRAILING EDGE BRACKET LOC IRSS 212 AT RT WING 2023-405175<[01] REPLACED BRACKET LOCATED ON INBOARD TRAILING EDGE IRSS 212 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. LENGTH OF CRACK IS 0.816 INCHES TOOL USED CALIPER P/N: 500-1SDR SWAA2023071772344Panel · crackedPANEL 621YB I/B CORNER IS CRACKED.<[01] PERFORMED PARTIAL WORK ON STEPS 3 AND 4.;[02] COMPLETED STEPS 1; 4; 5;[03] COMPLETED STEPS 6 AND 8; PARTIAL UPDATE STEPS 7 AND 9;[04] CORRECTION TO STEP 12 ITEM 1.;[05] CORRECTION TO STEP 12 ITEM 2.;[06] PANEL 621YB WITHSDR SWIA2023090800627Unknown · wornRH WING AILERON HAS WEAR ON LOWER LEADING EDGE SHROUDS. MARKED. (C-CHECK RO 9/6/2023) REPLACED SHROUD AT R/H WING AILERON LWR I/B L/E WITH NEW FASTENERS REF. CRJ200 SRM 51-42-21 & BOMBARDIER DWG. CC670-1300 REV. -D AND RESTORED FINISH ON FASTENERS REF.SDR CALA2023062802045Fastener · missingPDA 1 PASSENGER REPORTS MISSING FASTENERS RIGHT WING LEADING EDGE INBOARD OF THE NO.2 ENGINE. INSPECTED RIGHT WING INBOARD FIXED LEADING EDGE UPPER SKIN. FOUND LOOSE AND DAMAGED FASTENERS AND NO MISSING FASTENERS. REMOVED AND REPLACED LOOSE AND DAMAGED FASTENESDR EE4Y2023062717944Rib · corrodedDURING THE INSPECTION ACCOMPLISHMENT PER ALLEGIANT WORK CARD Nº: ZL-575-01-1-001 IT WAS FOUND THE RIBLET J CORRODED. DUE TO THIS FACT IT WILL BE REPLACED BY NEW ONE, DUE TO FLY BY WIRE CABLES PASS THROUGH THE MENTIONED RIBLET J, DETAILS WERE SENT TO AIRBUS ASKSDR 2024FA0000020Stiffener · crackedFOUND RIGHT WING LOWER, INBOARD, FORWARD SKIN, AFT STIFFENER CRACKED. REPLACED STIFFENERSDR SWI2023F00314Unknown · gougedLH WING AILERON CENTER HINGE (WING SIDE) HAS GOUGES. MARKED. (C-CHECK RO 9/6/2023) REPAIRED GOUGE ON LH WING AILERON (WING SIDE) CENTER HINGE TO A SMOOTH CONTOUR REF CRJ200 SRM 51-12-00. AND REO 601R-57-51-1018 REV--, DATED 2023-07-19 ALL STEPS COMPLIEDSDR SWAA2023072871770Panel · elongatedLEFT WING FWD UNDER WING PANEL #191FL; FASTENER HOLES ELONGATED.<[01] REPAIRED DAMAGE HOLES AT LEFT WING FWD UNDER WING PANEL #191FL AS PER SRM 51-70-04-2R-9. MATERIAL USED EY3804 PO#1800550 PLUS BMS9-3-120TYD CL7 PO#1690463. RESTORED ORIGINAL FINISHED AT PANESDR SWAA2023072871760Bracket · damagedELONGATED HOLE SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS250 AT LT WING 2023-405040<[01] REPLACED SUPPORT BRACKET LOCATED ON TRAILING EDGE ORSS250 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 115A5300;[02] CERTIFIED WORK PERFORMEDSDR SWAA2023072871755Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING 2023-405039<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG #115A2001 REV: -;[02] CORRECTED STEP 1<BR>REPLACED CORRUGATED PLSDR SWIA2023072700626Unknown · gougedEVALUATE GOUGE/SCRATCH INSIDE LH WING FUEL BAY UNDER PANEL 540CB, FWD SIDE, ON LOWER WING PLANK STRINGER BETWEEN WS85.50 - WS65.75, STGR 15 (C-CHECK RO 7/23/2023) BLENDED GOUGE/SCRATCH INSIDE LH WING FUEL BAY UNDER PANEL 540CB FWD SIDE ON LOWER WING PLASDR DXTA2023062689640Seal · damagedFUSELAGE STRUCTURE: LOUD HUMMING NOISE/VIBRATION COMING FROM CABIN NEAR SEAT #4. ABOVE FL380 AND AT CRUISE SPEED. REMOVED AND REPLACED FLAP SEAL ON PANEL 532AB IN REFERENCE TO EMB PHENOM 300 SRM 51-40-00. SSDR SWI2023F00225Unknown · chafedR/H INBD. FLAP, VANE CAP CHAFED. (C-CHECK RO 8/16/2023) BLENDED OUT CHAFE ON RH INBD, CENTER VANE CAP. FOUND OUT OF LIMITS PER CRJ700SRM 57-52-01-101-001-A01. REPLACED WITH NEW R/H INBD. FLAP VANE CAP (P/N CC670-14022-1) PER CRJ700 SRM 51-42-13-001-001SDR SWIA20230625Unknown · chafedL/H INBD. FLAP, VANE CAP CHAFED. (C-CHECK RO 8/16/2023) BLENDED OUT CHAFE ON LH INBD, CENTER VANE CAP. FOUND OUT OF LIMITS PER CRJ700SRM 57-52-01-101-001-A01. REPLACED WITH NEW L/H INBD. FLAP VANE CAP (P/N CC670-14022-1) PER CRJ700 SRM 51-42-13-001-001-SDR SWAA2023072871184Structure · delaminatedR/H ENGINE STRUT TO WING. UNDER WING SKIN AREA OF STRUT; SHOWING COMPOSITE DELAMINATION. SEE DOT HT-5 AND DOT HT-12<[01] REMOVED AND INSTALLED DAMAGE PHENOLIC STRIPS 2 EACH ON TOP SURFACE OF PANEL AS MARKED AS PER B737 AMM. 51-51-00-340-803 AND AMM 51-31-00-39SDR SWAA2023072871087Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS323 AT RT WING 2023-404922<[01] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS323 AT RT WING I.A.W B737-700 SRM 51-10-02 AND DWG#115A3700 SHEET:41; REV: -.;[02] REPLACED CORRUGATED PLATE TRAILING EDGE ORSS323 AT RT WING ISDR SWAA2023072871088Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE IRSS233 AT RT WING 2023-404923<[01] REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS233 AT RT WING IAW B737-700 DWG 115A2001 SHEET 34 REV - AND SRM 51-40-02-0G-0 .SRM 51-10-02-0G-0 PARAGRAPH 9 .SEE INDIVIDUAL SIGN OFF BSDR SWAA2023072871089Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS140 RT WING 2023-404930<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 RT WING; IAW BOEING SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2000 SHEET 22 REV. A.;[02] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 RT WINGSDR SWAA2023072871081Access Panel · elongatedELONGATED HOLE ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2023-404900<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189527; DUE DATE: 26/DEC/23.;[02] TOOL USED HOT BONDER PN: HCS9200B-AV; SN: 18196127; DUE DATE: 22/JAN/24;[03] TOOL USED: SCALE; PN: SPX621; SNSDR SWAA2023072871080Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ORSS307 LT WING 2023-404897<[01] REPLACED ANGLE AND FASTENERS LOCATED TRAILING EDGE LOCATED ORSS307 LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A3700 SHEET 32 REV -. AND DWG 115A3712 SHEET 5 REV.-. SEESDR SWAA2023072870641Bracket · crackedCRACK BODY STATION 540 BRACKET LBL 6 AT AIR CONDITIONING BAY 2023-404838<[01] REPLACED BRACKET LOCATED ON BODY STATION 540 LBL 6 AT AIR CONDITIONING BAY IAW B73-700 SRM 51-40-02-0G-0 AND DWG 212A1101 SHEET 3 REV- AND SRM 51-10-02-0G-0 PARAGRAPH 9. SEE INDIVIDUSDR SWAA2023072870639Angle · crackedCRACK ANGLE TRAILING EDGE ON SUPPORT BEAM LOCATED ORSS279 LT WING 2023-404821<[01] REPLACED ANGLE TRAILING EDGE ON SUPPORT BEAM LOCATED ORSS279 LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A6200 SHEET: 10 REV: -;[02] CERTIFIED WORK PERFORMSDR CALA2023062301990Skin · corrodedB767-28-3-0067, RHW FUEL TANK OVERWING FILL PORT ATTACH UPPER SKIN FOUND CORROSION REF HX NR WO.1865480, ORIG BY V897897 RHW FUEL TANK OVERWING FILL PORT UPPER SKIN PANEL CORROSION REPAIRED AS PER ECRA 5725-01126 REV.- ATTACHED MAINTENANCE WORK SHEET FORM 44.SDR FDEA202306211074Drag Fitting · unknownLT PYLON HAS 2 CRACK INDICATIONS AT #6 HOLE, 2 O'CLOCK & 7 O'CLOCK POSITIONS IN THE FITTING. 0.850 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WING UPPER SKIN AT IB PYLON DRAG FITTING CRACK INDICATION AT HOLE #6SDR FDEA202306211073Drag Fitting · unknownLT PYLON HAS 1 CRACK INDICATION AT #3 HOLE, 6 O'CLOCK POSITION IN THE SKIN, 0.250 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WNG UPPER SKIN AT IB PYLON DRAG FITTING CRACK INDICATION AT HOLE #3.SDR FDEA202306211072Drag Fitting · unknownLT PYLON HAS 1 CRACK INDICATION AT #8 HOLE 3 O'CLOCK POSITION IN THE FITTING 0.850 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WING UPPER SKIN AT IB PYLON DRAG FITTING CRACK INDICATION AT HOLE #8.SDR FDEA202306211071Drag Fitting · unknownLT PYLON HAS 2 CRACK INDICATIONS AT #7 HOLE, 12 O'CLOCK POSITION IN THE FITTING 0.850 DEPTH. COMPLIED WITH EA# F-5730-T0374640 PART 1 (P1) LH WING UPPER SKIN AT IB PYLON DRAG FITTING CRACK INDICATION AT HOLE #7.SDR SWAA2023071760668Plate · crackedLEFT WING LOWER T/E WIGGLE PLATE IS CRACKED AND LOOSE JUST I/B OF #1 PYLON<[01] REMOVED AND REPLACED LEFT WING LOWER T/E WIGGLE PLATE I/B OF #1 PYLON<BR>IAW SRM 51-40-02-0G-0;[02] UPDATED PARTS;[03] VERIFIED CORRECTION ACTION ITEM 1;2; CARD COMPLETE.SDR CALA2023062101952Panel · corrodedTWO AREAS OF CORROSION FOUND ON THE RH WING LOWER WINGTIP PANEL BETWEEN WBL 616.75 TO 658.17 WHILE AT GYR C-CHECK. BOTH LOCATION S WERE BLENDED AND ONE LOCATION REQUIRED A CUTOUT AND DOUBLER RE INFORCEMENT. THE REPAIR IS CONSIDERED AN INTERIM REPAIR AND REQU ISDR 29GA2023061800002Rib · crackedAROUND 1:35PM WE WERE TAXIING VIA N3 APPROACHING APRON 2, WE SAW THE RAMP AGENTS SIGNALING THE GO AHEAD, APPROACHED THE PARKING ACCORDING TO THE RAMP AGENT INSTRUCTIONS. HE WAS SIGNALING THE GO FORWARD SO I WENT FORWARD AS SOON HE SIGNALED TO MAKE A RIGHT TURNSDR 29GA2023061800001Flange · bentAT APPROXIMATELY 1340 EASTERN TIME, N406SV WAS BEING TAXIED FROM THE MAINTENANCE HANGAR AFTER RTS BY A MAINTENANCE TECHNICIAN WITH A SECOND TECHNICIAN IN THE FO SEAT. WHILE TAXING VIA N3 APPROACHING APRON 2, THE WINGTIP OF 406 STRUCK 408. 408 WAS PARKED ON THESDR 2024FA0000019Stiffener · crackedFOUND LEFT WING LOWER, INBOARD, FORWARD SKIN, AFT STIFFENER CRACKED. REPLACED
STIFFENERSDR CALA2023061901939Winglet · wornLH UPPER SCIMITAR WINGLET CONTACTED DELTA APU TAILCONE.PER CREW TAXI SPEED WAS VERY SLOW APPROX 1 KNOT. FLAGGING SDR REF GMM 04-20-16 UPDATED PICTURES FROM LIFT TRUCK., VERY MINIMAL DAMAGE .NO DLAMINATION , LOOKS LIKE EROSION TAPE IS JUST WORN THROUGH IN A FSDR REXA2022062700418Bushing · corrodedFOUND 4EA L/H AILERON SIDE BUSHING LUGS LABELED Ï¿½BÏ¿½, Ï¿½CÏ¿½, Ï¿½FÏ¿½, AND Ï¿½GÏ¿½ TO HAVE PITTING AND CORROSION REPAIRED IAW BOMBARDIER REO 670-57-61-237 REV - DATED 2017-07-25SDR REXA2022062700417Bushing · corroded"FOUND 2EA R/H AILERON BUSHING LUGS LABELED Ï¿½CÏ¿½ AND Ï¿½FÏ¿½ TO HAVE PITTING AND CORROSION REAMED 2EA BUSHING LUGS LABELED ""C"" AND ""F"" PER REPAIR F. STEPS 1-4 OF BOMBARDIER REO 670-57-61-237 REV - DATED 2017-07-25. COMPLIED WITH STEP# F (7) OF BOMBARDIESDR JR2R20230615540Angle · crackedLOH WING TRAILING EDGE WING SPAR 2 LWR STUB ANGLE JUST FWD OF THE LH MLG WHEEL WELL FWD BULKHEAD CRACKEDSDR YENA2023061600645Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION IB FLAP END RIB UPPER SURFACE ON RH WING(CPCP RELATED MPD TASK 575211-01); PERFORMED REPAIR IB FLAP END RIB UPPER SURFACE ON RH WING I.A.W. EC. NO. A23-457-01 AND EA NO. 57-0186-23 COVER REVISION# 0, PART# 1 AND PART# 2, THSDR YENA2023061600644Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION OB FLAP LOC INBOARD RIB UPPER AND LOWER CUT OUT STRUCTURE EXTERNAL SKIN RH WING P2; PERFORMED REPAIR OB FLAP LOC. INBOARD RIB UPPER AND LOWER CUT-OUT STRUCTURE EXTERNAL SKIN ON RH WING I.A.W. EC. NO. A23-458-01 AND EA NO. 57SDR YENA2023061600633Unknown · unknownDURING HEAVY MAINTENANCE: WING / CENTER WING / BOX TOP SKIN FR41-42 & BTW Y1292 TO Y1732 (APU FEEDER AREA) - CORROSION – PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR DALA2023061404866Unknown · unknownAIRCRAFT 682, AD RELATED DURING ROTO TEST OF ENGINE 2 UPPER SKIN, DRAG FITTINGS HOLE #3 WAS FOUND TO HAVE A CRACK IN THE FITTING LAYER. CRACK IN THE FITTING LAYER NOTED AT THE 9:00 POSITION. CORRECTIVE ACTION: REPAIRED WING/ OUTER WING/ RHS UPPER SKIN AND DRAGSDR DALA2023061404865Unknown · unknownAIRCRAFT 682, AD RELATED DURING ROTO TEST OF ENGINE 2 UPPER SKIN, DRAG FITTINGS HOLE #4 WAS FOUND TO HAVE MULTIPLE CRACKS IN THE SKIN AND FITTING LAYERS. CRACK IN THE SKIN LAYER NOTED AT 3:00 POSITION. CRACKS IN THE FITTING LAYER NOTED AT THE 1:00 AND 8:00 POSSDR DALA2023061404864Unknown · unknownAIRCRAFT 682, AD RELATED DURING ROTO TEST OF ENGINE 2 UPPER SKIN, DRAG FITTINGS HOLE #6 WAS FOUND TO HAVE CRACK IN THE FITTING LAYER. CRACK IN THE FITTING LAYER AT THE 11:00 POSITION. CORRECTIVE ACTION: REPAIRED WING/ OUTER WING/ RHS UPPER SKIN AND DRAG FTGS/CSDR DALA2023061404863Unknown · unknownAIRCRAFT 682, AD RELATED DURING ROTO TEST OF ENGINE UPPER SKIN, DRAG FITTINGS HOLE#9 WAS FOUND TO HAVE IN THE FITTING LAYER. CRACK IN THE FITTING LAYER NOTED AT THE 4:00 POSITION. CORRECTIVE ACTION: REPAIRED WING/ OUTER WING/ RHS UPPER SKIN AND DRAG FTGS/CORROSDR DALA2023061404862Unknown · unknownAIRCRAFT 682, AD RELATED DURING ROTO TEST OF ENGINE 1 UPPER SKIN, DRAG FITTINGS HOLE#6 WAS FOUND TO HAVE A CRACK IN THE SKIN LAYER. CRACK IN THE SKIN LAYER NOTED AT 8:00 POSITION. CORRECTIVE ACTION: ACCOMPLISHED EA#609176-14 AD ON L/H WING DRAG-FITTING HOLE#6 SDR DALA2023061404861Unknown · unknownAIRCRAFT 682, AD RELATED DURING ROTO TEST OF THE ENGINE 1 UPPER SKIN. DRAG FITTING CRACKS NOTED IN HOLE 1 SKIN AND FITTING LAYERS, HOLE 4 FITTING LAYER, HOLE 5 SKIN LAYER, HOLE 6 SKIN LAYER, HOLE 7 SKIN LAYER AND HOLE 8 FITTING LAYER. REJECTABLE INDICATION DURSDR R61A2023070800384Skin · crackedCRACK RH WING BOTTOM SIDE AREA OF RIB 4A. PERFORMED TEMPORARY REPAIR ON RH WING LOWER SKIN AREA OF RIB 4A BY CUTTING OUT DAMAGE AND INSTALLING REPAIR FILLER AND DOUBLER. REF EMB ETD2023-170-014723.SDR FDEA202306111023Slat · dented#8 SLAT LOCATED JUST OB OF OB TRACK, SLAT TE HAS A DENT . CLEANED SANDED AND REMOVED DAMAGE ON RIGHT WING #8 SLAT AND REPAIRED IAW B767 SRM 57-43-02-2R AND 51-70-10-2R REPAIR 4, REPAIR WAS A PERMANENT REPAIR ON #8 SLAT JUST O/B OF O/B TRACK / SLAT T/E.SDR FDEA202306111022Spoiler · delaminatedLH WING #4 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 40MM*15MM, DEPTH: 1.15MM COMPLIED WITH EA: 6-5750-T0374744 P1. TITLE: WING - FLIGHT SURFACES - LH 4# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WISDR UIEA2023060500572Bushing · unknownCORROSION ON BUSHINGS FROM RH MAIN LANDING GEAR SUPPORT BEAM(<P>BUSHINGS WERE REPLACED PER SOPM 20-50-03 AND MXA EO TRE6757194 (CMM 57-54-13 REPAIR 2-1)</P> / <P>MAJOR REPAIR PN: 113T1108-17 AND 113T1108-23</P>)
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