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 HALA2022012500030None · noneA CHECK MAJOR REPAIR - THRU BLEND ON RT WING LOWER SKIN AT XRS 535, RS AND REAR SPAR CAP BLEND NEAR XRS 534 // REPAIRED PER E105-488206-PERMSDR SWIA202265402None · damagedLH LOWER WING PLANK ACCESS HOLE 540BB LANDING IS PITTED AT IB AND OB ENDS. (C-CHECK RO 4/20/2022) REPAIRED ACCESS HOLE IAW CRJ 200 REO 601R 57-21-030 REV L DATED: 2014-02-05. REFERENCE CONTINUE CARD FOR WORK PERFORMEDSDR IXXA20220217001Skin · crackedLH WING LOWER SKIN HAS EVIDENCE OF A CRACK AT WS 980SDR IXXA2022011903Rib · bentLOAD AIR RIB BENTSDR 2022F00080None · damagedDURING TRANSIT CHECK, IT WAS DETECTED SEVERAL LIGHTNING STRIKE ON RIGHT WINGLET TIP AND LEFT ENGINE THRUST REVERSER SLEEVE, MAITENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CODITIONAL INSPECTION PHASES I AND II, DETECTING SEVERAL LIGHTNING STRIKES DAMAGES ONSDR SWIA202265093None · gougedCENTER HINGE FITTINGS FOR THE RH AILERON HAS GOUGES (MARKED) (C-CHECK RO 3/14/2022) BLENDED RH AILERON CENTER HINGE FITTINGS TO A SMOOTH CONTOUR. REF: CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS REF REF CRJ 200 SRM 57-51-14 FIGURE 101.RECIEVED REO 601SDR IXXA20220125001Former · crackedRIGHT WING LES 563 RIB NOSE L/E CLIP IS CRACKEDSDR IXXA20220121001None · crackedLEFT WING L/E LOWER RIB SUPPORT AT FWD END AS A CRACK AT LES 504SDR CALA2022011700165Panel · missingPDA 3 FAIRING REMOVED FOR MISSING SCREW PANEL # LOG ITEM PAGE 7808433. FAIRING # 542EB CREATED PDA REF LOG # 7808433 ON CDL.SDR A6WA202202178105None · corrodedPITTING CORROSION ON LH WING UPPER SKIN LANDING FOR PANEL 540AT. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE ON LH WING UPPER SKIN LANDING P/N 601R10042-7 FOR PANEL 540AT. PERFORMED HFEC WITH NO INDICATIONS. PERFORMED ROTO PEEN TO REWORKED AREAS. RSDR 2022F00097Winglet · damagedDURING TRANSIT CHECK, THE AIRCAFT WAS HIT LH WINGLET VENTRAL, MAITENANCE PERSONAL PERFORMED WINGLET STRIKE CONDITION, WAS PERFORMED INSPECTION, DETECTING LH WINGLET WITH DAMAGES, SO THE LH WINGLET WAS DEFERRED, AT MEX, DURING OVERNIGHT CHECK, THE LH WINGLET WSDR DALA2022011800335None · noneSHIP 6822 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 583989-14 REV C. CORRECTIVE ACTION: REF ERA 583989-14 REV C. (2086489)SDR FDEA202201140066Skin · noneLEFT WING #6 SPOILER LOWER SKIN HAS A PUNCTURE REPAIRED LEFT WING #6 SPOILER LOWER SKIN IAW B767 SRM 57-70-01 FIG. 201 SHEET 4 AND 51-70-04-0GSDR SWIA202265430None · corrodedRH FLIGHT SPOILER PCU, LOWER MOUNT HARDWARE CORRODED. (C-CHECK RO 4/20/2022) REPLACED R/H FLIGHT SPOILER LOWER MOUNT HARDWARE IAW CRJ-200 AMM 27-62-01-400-801, SEE CONTINUATION CARD FOR ALL WORK PERFORMED.SDR SWIA202265429None · corrodedLH INBD GROUND SPOILER PCU HARDWARE IS CORRODED. (C-CHECK RO 4/20/2022) REPLACED UNSERVICABLE HARDWARE ON THE L/H INBD GROUND SPOILER IAW CRJ 200 AMM 27-63-01-400-801. REFERENCE CONTINUE CARD FOR WORK PERFORMED .SDR CALA2022011400138Spar · crackedSUPPORT TASK-AD 2019-11-02 EA 5310-06900 REV D OP 12- BS 1035 RH UNDERWING LONGERON CENTER TANK FRONT SPAR LOWER CHORD 3EA FASTENER HOLE FOUND CRACK DETAIL REFER REPORT TRANSFER REF. NON ROUTINE LP 9131981 AND ORIGINATED BY EMP V914372 BS 1035 RH UNDERWING LONSDR IXXA2022011302Beam · chafedFLAP SUPPORT BEAM CHAFEDSDR MASA20220110073Rib · cracked"CRACK ON RIB LEADING EDGE SS58.41 AT LEFT WING LEADING EDGE
RIB LEADING EDGE SS58.41 AT LEFT WING LEADING EDGE WAS REPAIRED PER REO 690-57-41-240 REV. --"SDR CALA2022011000095Screw · missingPDA 3 SEVEN SCREWS MISSING FROM INDOARD FLAP, OUTBOARD TRACK TAILCONE FAIRING. % FROM LEFT WING, 2 FROM RIGHT WING SHOULD SAY 5 FROM LEFT WING FAIRING. SEE LP 7778796 AND 7778803 FOR DISPOSITIONSDR A6WA202201088167Winglet · dentedAIRCRAFT L/H WINGLET O/B SKIN HAS 1 EACH DENT AT WS 12.5 TO WS 19.00 & WINGLET F/S AND R/S. DENT DIMENSION IS: (P1) 2.6"L X .900"W X .015"D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 57-31-31 REV 38 FIG 1 SHT 1. ****************AIRSDR SWIA202264049None · corrodedL/H FLIGHT SPOILER I/B PCU FAILS BACKLASH CHECK. TROUBLESHOOT & REPAIR AS REQUIRED PER MM & COMPLETE BACKLASH CHECK OF FLIGHT SPOILER I/B PCU (C CHECK RO 1/20/22) REMOVED AND REPLACED LOWER MOUNTING HARDWARE AT LH FLIGHT SPOILER INBOARD PCU IAW CRJ 200 ASDR FDEA202201080080Skin · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR SURFACE L/E PANEL 613AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DSDR SWIA202264984None · corroded* L/H WING AILERON PCU BAY, INBOARD AND OUTBOARD PANNELL ATTACH FLANGES HAVE CORROSION AROUND 15 EA. FASTENER HOLES. (C-CHECK RO 3/14/2022) REMOVED CORROSION FROM LH WING PCU BAY INBD AND OTBD PANEL ATTACH FLANGES REF CRJ200 SRM 51-21-06. NDT IS DEFECSDR REXA2022021000223Fitting · elongatedL AILERON LUG "E" OVERSIZED TO BETWEEN 0.9755" AND 0.9765".
"REPAIRED L/H AILERON LUG ""E"" IAW MHIRJ REO 690-57-61-242 REV--
DATED 2021-12-16.SDR FDEA202201070079Skin · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON L/H WING LWR SURFACE L/E PANEL 513AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DSDR SWIA202265089None · gouged*RIGHT WING FUSELAGE ATTACHMENT FITTING AT BL45 AND FS 513 HAS A SMALL GOUGE ON THE INBD SIDE. (IN WHEEL WELL AREA) (C-CHECK RO 3/14/2022) BLENDED DAMAGED AREA OF THE R/H WING FUSELAGE ATTACHMENT FITTING AT BL45 COMMON TO FS 513 INBD. SIDE (WHEEL WELL ARSDR MASA20220107017None · noneSLAT TRACK 2-2 OF SLAT#2 ON THE LH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE LOWER FACE. PERFORM PERMANENT REPAIR IAW CRJ7/9 ILLUSTRATED PARTS CATALOG (IPC} 27-81-41, FIGURE 5, ITEM 80 (REV 70 DATED 10 AUG 2021)SDR MASA20220107016None · noneSLAT TRACK 1-2 OF SLAT#1 ON THE LH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE LOWER FACE. PERFORM PERMANENT REPAIR IAW ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 1, ITEM 80 (REV 70 DATED 10 AUG 2021)SDR IXXA2022010601Support Beam · chafedFLAP LEFT WING INBOARD SUPPORT 1-2-3 BEAM CHAFEDSDR SWIA202264983None · crackedCRACK NOTED AND MARKED DURING SPECIAL DETAILED INSPECTION OF THE LEFT WING AFT LOWER WING PLANK AT WS148.019 (C-CHECK RO 3/14/2022) REPAIRED CRACK PER GREO 601R-57-21-130 REV-L DATED 2017/03/06 REPAIR OPTION II. COMPLIED WITH TASK CARD 28-900-1000-SKY SDR SWIA202264868None · gougedRH AILERON #2 HINGE FITTING AT WS319 AFT WING SPAR IS GOUGED. (C CHECK RO 3/11/2022) REPAIRED RH AILERON #2 HINGE FITTING AT WS319 AFT WING SPAR IAW MHIRJ REO 601R-57-51-984, REV --, DATE: 2022-01-28, SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED. M-33SDR SWIA202264866None · gougedLH AILERON #3 HINGE FITTING AT WS323 AFT WING SPAR IS GOUGED. (C CHECK RO 3/11/2022) REPAIRED LH AILERON HINGE #3 FITTING AT W.S.323.00 AFT SPAR IAW MHIRJ REO 601R-57-51-985 REV - - DATED 2022-01-31. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CSDR MASA20220105009None · noneSLAT TRACK 3-2 OF SLAT #3 ON THE LH WING WAS FOUND TO HAVE CORROSION DAMAGE ON THE LOWER FACE. PERFORM PERMANENT REPAIR IAW CRJ7/9 ILLUSTRATED PARTS CATALOG (IPC) 27-81-41, FIGURE 10,90 (REV. 70 DATED 10 AUG 2021) - DEFECT LOCATION: SLAT TRACK 3-2 OF SLAT#3SDR SWIA202265098None · seizedRH AILERON CENTER HINGE FITTING LOWER INBD BOLT IS SEIZED (C-CHECK RO 3/14/2022) REMOVED RH AILERON CENTER BOLT STOP FITTING TO F.O.M REF CRJ200 SRM 51-42-21. SEE INSTALL OF NEW HARDWARE ON CAMP#23855597 JOB#2738280 OP#519SDR SWIA202265097None · failedL/H INBOARD GROUND SPOILER HAS EXCESSIVE PLAY, FAILED BACKLASH CHECK. (C-CHECK RO 3/14/2022) REMOVED AND REPLACED THE LH INBOARD GROUND SPOILER LINK AND ATTACHMENT HARDWARE REF CRJ-200 AMM 27-65-01-400-801. BACKLASH AND OP TEST CHECKED GOOD.SDR IPXA2022011177771Stiffener · noneINSPECTION TYPE:C14CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-11) ON STA 785.9, LBL 33.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.82.01, UPS EO B767-5740-58151 -C AND UPS EO B767-5720-76672-ASDR IPXA2022011177769None · noneINSPECTION TYPE:C14CRACK ON CENTER WING TANK STIFFENER ( P/N:111T2011-6) ON STA 785.9, RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV 82.01, UPS EO B767-5740-58151-C AND UPS EO B767-5720-76672-ASDR DALA2022010600104None · noneSHIP 185 ERA 596167-14AD ISSUED FOR REPAIR TO WING CENTER FUEL TANK UPPER SKIN AND STRINGERS AT FUSELAGE STATION 899, RBL 88. AMOC REQUIR ED. CORRECTIVE ACTION: ASSOCIATED ER/A CHANGED FROM 00-596167 TO 14-596167 (2074040)SDR CALA2022010500019Pressure Web · crackedFOUND 2EA CRACKS IN VERTICAL PRESSURE WEB AT STA 663.75 AND APPROX LBL 33. REF FLEET CYCLE N/R 9793198.CARD COMPLETE SEE WIPS AND TASKS FOR WORK PERFORMED.PER AMM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE DIP 57-DIP NO TASK AND LIMITATIONS ENTERED INTO CORRECTIVE ACTSDR MK1Y202201023None · noneDENT DAMAGE AND AN EXISTING BLEND-OUT WAS FOUND ON THE LOWER WING SKIN PANEL (P/N 112T4702-1) COMMON TO THE OUTBOARD STRINGER L-9.5 (P/N 767-3421-7) BETWEEN WS 990.2 AND WS 1006. AN EXISTING FREEZEPLUG AND THE OUTBOARD STRINGER L-9.5 HAD BEEN INSTALLED PER SERSDR MK1Y202201019None · nonePROBLEM DESCRIPTION: SLAT NO. 4, OSS 579.05:
SHOP FOUND A DENT ADJACENT TO A BULGE IN UPPER LE SKIN OF SLAT NO. 4. THE DAMAGED AREA LOCATED ON A RIB AND STIFFENER. SLAT: P/N 114T4104-203G; S/N 000010.SDR MK1Y202201017None · nonePROBLEM DESCRIPTION: SLAT NO 5 AT OSS 389.71:
SHOP FOUND DENT AMONG FASTENERS AT THE EDGE OF SLAT LE SKIN ATTACHMENT COMMON TO A RIB. THE REPORTED DAMAGE WAS FOUND SMOOTH WITHOUT SHARP EDGES OR LOOSE FASTENERS.SDR MK1Y202201010None · nonePROBLEM DESCRIPTION: R/H WING LOWER SKIN SURFACE BETWEEN WS.994.7 AND WS.1001.7: SHOP FOUND TOOL MARK AMONG FASTENERS, PAINT STRIPPED AND PERFORMED NDT THICKNESS INSPECTION WAS PERFORMED .SDR SWIA202165075None · corrodedLEFT WING O/B GROUND SPOILER HAS CORRODED HARDWARE AT CENTER HINGE FITTING (C-CHECK RO 3/14/2022) REPLACED CORRODED HARDWARE WITH NEW HARDWARE ON LH WING OUTBOARD GROUND SPOILER AT CENTER HINGE FITTING. REF. CRJ200 AMM 27-63-01-400-801. OP TEST GOOD. SEESDR AALA202201031851Fastener · elongatedAIRCRAFT IN BASE MAINTENANCE: FOUND SUPPORT FRAME WITH EXCESSIVE PLAY BECAUSE OF LOOSE BOLT AND HI-LOCKS NEAR STA IRSS620 ON RIGHT-WING DOT 70-108. REMOVED ELONGATED FASTENERS AND REPLACED FASTENERS ON SUPPORT FRAME (ANGLE) NEAR STA IRSS 620 RIGHT WING PER B77SDR REXA2022021000231Lug · damaged"L AILERON BUSHING LUG ""G"" HAS MECHANICAL DAMAGE TO EXTERNAL EDGES
OF INBD & OTBD LUG FACES. "
"REPAIRED AILERON LH LUG ""G"" IAW BOMBARDIER REO 670-57-61-237 REV--
2017-07-25 SDR REXA2022021000228Lug · damaged"L AILERON BUSHING LUG ""B"" HAS MECHANICAL DAMAGE TO EXTERNAL EDGES
OF INBD LUG FACE. "
"REPLACED L AILERON BUSHING LUG ""B"" IAW REO 670-57-61-237 REV--SDR CALA2021122902469Fitting · crackedAD 2012-15-12, EA 5710-02220 REV.D OP 003 LH UNDERWING LONGERON FITTING TENSION BOLT HOLE INSP FOUND 3EA CRACKS AT 1ST LAYER COUNT FROM AFT TRANSFER REF. NON-ROUTINE ZGY511880 & ORIGINATED BY EMP V924733 RII APPROVED LH UNDERWING LONGERON FITTING (BATHTUB FITTSDR CALA2021122902467Stringer · crackedAD 2012-15-12, SUPPORT TASK - EA 5710-02220 OP 01 - LH LONGERON FITTING FOUND 1EA CRACK RUNNING AFT APPROX 7/8" IN LENGTH TRANSFER REF. HX NON-ROUTINE LP 9130257 & ORIGINATED BY EMP V924 735 LH LONGERON FTG REPLACED PER EA 5710-02220 REV D OP3 AND OP7 ACCOMPLISDR IPXA2022011177765None · noneINSPECTION TYPE:C3GOUGE ON EXISTING REPAIR DOUBLER OF TOP PANEL ON R/H OUTBD AFT FLAPREPAIR I.A.W BOEING SRID : 3-5236994806 AND UPS EO 747-5750-64795-C
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