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 = '5751' 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 = '5751' 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 SWIA202266162None · chafedR/H INBOARD FLAP, FLAP VANE IS CHAFED AT (3) LOCATIONS ALONG THE LEADING EDGE FROM CONTACT WITH FLAP VANE STOPS. (C-CHECK RO 7/26/2022) REMOVED AND REPLACED R/H INBOARD FLAP VANE MID. LEADING EDGE CAP I.A.W. BOMBARDIER CRJ200 SRM 51-42-13 REV.38B, DATESDR SWIA202265940Rail · damagedR/H FLAP TRACK 1A HAS THICKNESS REDUCTION DAMAGE ON UPPER FORWARD SURFACE MEASURED AT .12MM. (C-CHECK RO 6/15/2022) R/H FLAP TRACK 1A REMOVED AND REPLACED. REF AMM57-54-25 / TW:TC1-458 / DUE:7-22-22SDR SWIA202265939None · damagedL/H FLAP TRACK 1A HAS DEPTH REDUCTION DAMAGE AT UPPER FORWARD SURFACE MEASURED AT .26MM. (C-CHECK RO 6/15/2022) REMOVED AND REPLACED L/H FLAP TRACK 1A. REF EMB-175 AMM 57-54-25. TW TC2-7543 CAL DUE 5-10-23SDR SWAA2022052410119Bracket · crackedLEFT WING HYD. SUPPLY LINE BRACKET CRACKED JUST OTBD. OF L/H MLG FWD. TRUNNION FITTING. / [01] REMOVED AND REPLACED BRACKET PER EA 22-157-01535;[02] REMOVED AND REPLACED BRACKET PER EA 22-157-01535SDR SWIA202266081None · gouged* R/H INBOARD FLAP, OUTBOARD HINGE ARM LOWER LUG IS GOUGED, MARKED. (C-CHECK RO 7/8/2022) BLENDED OUT GOUGE ON R/H INBOARD FLAP OUTBOARD HINGE ARM LOWER LUG REF CRJ 700 SRM 51-12-00-001-001-A01. FOUND OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPSSDR AALA202205235723Aileron · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON TRAILING EDGE INBOARD BOTTOM CORNER DELAMININATED. REPAIRED AILERON PER SRM 57-61-21-300-012 AND EA 336241SDR LR7A2022051203114Skin · corrodedDURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5711, FOUND LH AILERON UPPER SKIN PANEL BULGING AT AS55.4L TO AS143.6L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0194.SDR LR7A2022051203113Shroud · crackedDURING SCHEDULED C-2 CHECK UNDER JOB CARD HC5711, FOUND LH AILERON LEADING EDGE SHROUD WITH MULTIPLE CRACKED AND DENTS AT AS0L TO AS562L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0193.SDR IPXA2022052382384Skin · chafedINSPECTION TYPE:3CR/H I/B AILERON LOWER L/E SKIN HAS CHAFE DAMAGE.REMOVED, FABRICATED AND REPLACED SKIN IAW DWG. ARC1250 AND SRM 51-35-01. (MINOR)SDR SWIA202265634None · damagedLH FLAP TRACK 1A HAS DEPTH LOSS TO THE UPPER RAIL WITH MAX MATERIAL LOSS OF .9MM CALIPER TC2-7153 DUE 11-18-22 (C CHECK RO 5/19/22) REMOVED AND REPLACED LH FLAP TRACK 1A RAIL SEE CONTINUATION CARD FOR WORK ACCOMPLISHEDSDR N6WA2022050202Skin · improper partLHIB FLAP REQUIRES I/B UPPER SKIN SPLICE REPAIR, FABRIKATED ALL DOUBLERS IAW CRJ700 SRM 57-52-01 INSTALL REPAIR IAW CRJ 700 SRM 57-52-01, REPAIR LHIB FLAP REQUIRES I/B UPPER SKIN SPLICE IAW CRJ 700 SRM 57-52-01.SDR AALA202205060390Access Panel · departedAIRCRAFT WAS GROUNDED: PASSENGER REPORTED AND MAINTENANCE VERIFIED RIGHT WING AILERON TOP SIDE INBOARD ACCESS PANEL CAME APART IN FLIGHT. **SUPPLEMENTAL REPORT FOR AALA202204290390: INSTALLED PANEL 675AT PER AMM 57-51-37-400-007-A** (CLOSED)SDR AALA202204290390Access Panel · departedAIRCRAFT WAS GROUNDED: PASSENGER REPORTED AND MAINTENANCE VERIFIED RIGHT WING AILERON TOP SIDE INBOARD ACCESS PANEL CAME APART IN FLIGHT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)SDR CALA2022042701086Fastener · missingPDA 3 1 MISSING FASTENER RH WING PANEL 674AB. FASTENER MISSING IS IN MIDDLE OF INBD EDGE BROWN, , MICHAEL ( (V926252))COMPLIED WITH INTERIM RPR REF ECRA 5751-01421. AT THE END OF EACH FLIGHT, ACCOMPLISH INSPECTIONS PER PART 2. A PART 3 PERMANENT REPAIR IS TO SDR SWIA202265553None · gougedRH WING #2 FLAP TRACK SUPPORT, FAIRING FITTING ASSY INBOARD AND OUTBOARD BEARING NON-METALLIC INTERNAL SLEEVES ARE TORN/GOUGED. (C-CHECK RO 5/3/2022) REMOVED AND REPLACED RH WING #2 FLAP TRACK SUPPORT, FAIRING FITTING ASSY INBOARD AND OUTBOARD BEARING RSDR FDEA202204241090Panel · crackedRH WING WIGGLE PLATES BROKEN AT JACK POINT 0000280794 : SHAEFFER, DAVID C - 25-APR-2022 00:15 REPLACED DAMAGED PANELS REF B767 SRM 57-51-02-2R FIG 201, SHT 1-3 REPAIR 5SDR SWIA202265550Rail · out of toleranceR/H FLAP TRACK 1A HAS THICKNESS REDUCTION OF .030". ASSET TC2-7153 DUE 11-18-22. (C-CHECK RO 4/29/2022) REMOVED AND REPLACED R/H FLAP TRACK 1A REF E-175 AMM 57-54-25 FLAP SYSTEM OPS CHECKED GOOD TC1-602 CAL DUE 2-2-23SDR SWIA202265549None · out of toleranceL/H FLAP TRACK 1A HAS THICKNESS REDUCTION OF .028". ASSET TC2-7153 DUE 11-18-22. (C-CHECK RO 4/29/2022) REMOVED AND REPLACED L/H FLAP TRACK 1A REF E-175 AMM 57-54-25 TC1-602 CAL DUE 2-2-23SDR SWIA202265893None · damagedDURING REMOVAL OF L/H INBD FLAP LOWER SKIN, 2 EA. RIBS WERE DAMAGED AT FLS84.20 AND FLS92.80. (C-CHECK RO 6/6/2022) REMOVED 3 EA. DAMAGED RIBS AND INSTALLED NEW 1 EA. RIB P/N CC670-14169-1 (FLS84.20), NEW 1 EA. RIB P/N CC670-14170-3 (FLS92.80) & 1 EA. NSDR SWIA202265548None · damagedRH WING IB FLAP TRACK #2 SUPPORT ASSY HAS 2 BUSHINGS AT FLAP TRACK FAIRING LINKAGE ATTACH POINT THAT WERE DAMAGED ON REMOVAL OF SEIZED-IN LINKAGE CLAMP BUSHING. (C-CHECK RO 4/29/2022) REMOVED AND REPLACED 2EA BUSHINGS AT RH WING IB FLAP TRACK #2 SUPPORTSDR SWIA202265547Bushing · damagedRH WING FLAP FAIRING #2 LINKAGE TO #2 FLAP TRACK SUPPORT CLAMP BUSHING DAMAGED ON REMOVAL DUE TO BEING SEIZED INTO LINKAGE AND FLAP TRACK SUPPORT ATTACHMENT POINT. (C-CHECK RO 4/29/2022) REMOVED AND REPLACED ON RACK CLAMP BUSHING ON RH WING FLAP FAIRINGSDR SWIA202265440None · leakingRIGHT WING 2ND CANOE O/B OF MLG HAS FUEL LEAK. (FILED - CLOSED) REMOVED AND REPLACED THE TWO FORWARD BOLTS, TWO WASHERS, AND TWO NUTS OF R/H WING FWD HINGE-BOX FITTING BY 2ND CANOE OF MLG IN REF TO AMM 57-21-36. SEE CP 24695858 FOR LEAK CHECK.SDR SWIA202265279None · delaminatedRIGHT HAND WING INBD FLAP IS REMOVED. (REF AMM 27-15-06) (FILED - CLOSED) INSTALLED NEW RIGHT HAND WING INBD FLAP IN REFERENCE TO AMM 27-15-06. RIG CHECKED GOOD FLAP OPERATES NORMAL FROM 0-45-0SDR IPXA2022042581462Fitting · corrodedINSPECTION TYPE:SEG1CORROSION UNDER BONDING STRAP TERMINAL END ON LH AILERON O/B HINGE SUPPORT FITTINGREPAIRED PER UPS EO B757-5750-83478-A AND VT MAE EA 757-5751-A2896 REV -SDR MASA20220329160None · noneTHE RH AILERON CENTER HINGE ASSEMBLY WAS DISCOVERED TO HAVE TOOL MARKS DURING THE REMOVAL OF THE PCU ATTACH LINK BOLT AT AS343.53. PERFORMED PERMANANT REPAIR IAW CRJ700/900 ILLUSTRATED PARTS CATALOG {IPC) 57-60-00, FIGURE 1, ITEM 146 (REV.37 DATED AUG. 15, 201SDR SWIA202265594None · chafed*CHAFFING NOTED AT L/H AILERON LOWER L/E SKIN (MARKED) (C-CHECK RO 5/16/2022) BLENDED CHAFE TO A SMOOTH CONTOUR. BLEND IS OUT OF LIMITS OF REO670-57-61-194 REV -C DATED 2019-01-07, REPLACED LH AILERON LE SKIN REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-2SDR 7C7A2022031700011Skin · damagedDAMAGE TO LH AILERON SPRING TAB LOWER SKIN. REF. 008.27-22.02SDR 7C7A2022031700010Skin · crackedCRACK DAMAGE ON RH AILERON LOWER SKIN PANEL PN 85740055 AT TAB HINGE STATIONS YW 442.50 AND YW471.50 ALONG THE REAR SPAR. REF 008.27-22.01SDR 7C7A2022031700005Skin · crackedCRACK DAMAGE TO UPPER SKIN PANEL PN 85740016 OF RH AILERON ASSY. PN 85740002-003 AT YW 491 ALONG THE FRONT SPAR. REF. 008.27-22.03SDR AALA202203176463Aileron · debondedAIRCRAFT WAS GROUNDED: RIGHT HAND AILERON TRAILING EDGE BROKEN AND DISBONDED AT INBOARD UPPER SIDE. REPLACED AILERON PER AMM 27-14-41.SDR 2022F00132None · noneDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01, ONE AILERON MASS BALANCE WEIGHT WAS FOUND TO BE BELOW MINIMUM WEIGHT. REPLACED WEIGHT WITH NEW, PART NUMBER PE915109-L31 PER SERVICE BULLETIN INSTRUCTIONS. THIS REPORT SUBMITTED TO COMPLY WISDR DALA2022031601737None · noneSHIP 172 LH O/B AILERON I/B SIDE NOSE UPPER AND LOWER SKIN PANEL FOUND BROKEN. CORRECTIVE ACTION: PANEL REPAIRED AS PER PRI 597398-14 (2153638)SDR FDEA202203120486Skin · delaminatedRH WING AILERON (113T7100-414G) HAS AS SPLIT IN THE TRAILING EDGE (WS 1114) WHICH WAS STARTING TO DELAM ONN UPPER SKIN (113T7112-6 SKIN) REPAIRED AILERON SKIN (UPPER 113T7112-6 SKIN, SIZE 5Ï¿½ X 6Ï¿½) USING 767 SRM 57-60-02-2R REPAIR 1, & 767 SRM 51-70-05 SDR SWIA202265419None · damagedR/H WING AFT MOUNT FLAP HINGE BOX ATTACHMENT I/B AND O/B LUG FITTINGS DAMAGED AT WS220 (C-CHECK RO 4/20/2022) COMPLIED WITH REO 601R-57-21-3579 REV - - DATED 2022-03-14 BLENDING GOUGE DAMAGE TO RHS FLAP HINGE BOXES AND FITTINGS. COMPLETED SKYWEST TASDR SWIA202265418None · damagedR/H WING FLAP HINGE BOX LUG FITTINGS I/B AND O/B DAMAGED AT WS264 FLAP HINGE BOX REQUIRES REMOVAL FOR REPAIR. (C-CHECK RO 4/20/2022) REPAIRED R/H WING FLAP HINGE BOX LUG FITTINGS ON I/B AND O/B POSITIONS AT WS. 264 IAW CRJ 200 REO 601R57-21-3529 REV-- SDR SWIA202265417None · damagedR/H WING FLAP HINGE BOX LUG FITTINGS I/B AND O/B DAMAGED AT WS178 FLAP HINGE BOX REQUIRES REMOVAL FOR REPAIR. (C-CHECK RO 4/20/2022) COMPLIED WITH REO 601R-57-21-3579 REV - - DATED 2022-03-14 , BLENDING OF GOUGES ON ON FLAP HINGE BOXES AND LUGS. COMPLESDR REXA2022040800616Lug · gougedRH AILERON LUG MARKED F HAS GOUGE INSIDE BORE. - REPAIRED RH AILERON LUG IAW BOMBARDIER GREO 670-57-61-237 REV. -- DATED 2017-07-25.SDR SWIA202265812None · corrodedL/H OUTBD GROUND SPOILER. INBD HINGE HARDWARE CORRODED. (C CHECK RO 5/23/22) REPLACED NEW HARDWARE . ON L/H OUTBD GROUND SPOILER. INBD HINGE .REF CRJ 900 SRM 51-41-02-001-001-A01, REF CRJ 900 AMM 51-80-00-910-816-A01 AND ELECTRICAL BONDING TEST GOOD. RESDR AALA202203013689Aileron · delaminatedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND AILERON TRAILING EDGE HAS DELAMINATION. REPLACED AILERON PER AMM 27-14-41.SDR SWIA202265806None · corroded*ON R/H WING, AT AFT SPAR, AT APPROXIMATELY WS282R, MOUNT HARDWARE OF FLAP BPSU HAS CORROSION. (MARKED). (C CHECK RO 5/23/22) REMOVED AND INSTALLED NEW R/H WING FLAP BPSU MOUNT HARDWARE REF CRJ-900 SRM 51-41-02-001-001-A01 BPSU NOT ELECTRICALLY DISCONNESDR SWIA202264757None · corrodedL/H INBD FLAP. UPPER FLAP VANE ACTUATOR MOUNT HARDWARE CORRODED, UNDER 584AB ACCESS PANEL. (C CHECK RO 02/25/2022) INSTALLED NEW SERVICEABLE HARDWARE PER CRJ700 AMM 27-52-23-400-801-A01 OPS CHECK GOOD AT THIS TIMESDR SWIA202265047None · bentAFT RIB ON THE LH INBOARD FLAP IS BENT AT PREVIOUS SKIN REPAIR (MARKED) (C-CHECK RO 3/14/2022) REMOVED PREVIOUS SKIN REPAIR AND REPLACED WITH NEW DOUBLER, FILLER AND ANGLE REF CRJ200 SRM 57-52-00 REPAIR NO. 3 / COMPLIED WITH TASK CARD 51-900-1003-SKYSDR SWIA202264756None · corrodedL/H INBD FLAP. UPPER FLAP VANE ACTUATOR MOUNT HARDWARE CORRODED, UNDER 584AB ACCESS PANEL. (C CHECK RO 02/25/2022) REMOVED AND REPLACED LH INB FLAP VANE ACTUATOR HARDWARE UNDER PANEL 584AB REF CRJ 700 AMM 27-52-23-400-801-A01 OPS TEST GOODSDR SWIA202265650None · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA46433-670-57-53-004 RT 813SK-RI - RT IB FLAPS HAVE MULTIPLE DENTS ON UPPER SURFACES (20) SEE MAPPING FOR LOCATIONS. COMPLIED WITH TEMPORARY DISPOSITION REO 670-57-52-004. REINSPECTS OF FILLER INTEGRITY DUE AT EVERY 50SDR SWIA202265214None · corroded* THE LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE IS CORRODED AROUND NUTPLATE HOLES. (MARKED) (C-CHECK RO 3-25-22) REMOVED DAMAGE AT LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE REF. CRJ-200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. RECSDR SWIA202265210None · chafed* THE LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE IS CHAFFED. (MARKED) (C-CHECK RO 3-25-22) BLENDED CHAFFING ON LH INBD FLAP OUTBD HINGE ARM SIDE PLATE ON OUTBD SIDE REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITHSDR SWIA202264737None · wornLH FLAP STUB FAIRING 171DL, RETAINING PLATE WORN/CHAFFED AND HINGED ATTACH POINT WORN. (C CHECK RO 02/25/2022) REMOVED AND REPLACED 1EA HINGE ASSY P/N CC670-39239-1 ON LH FLAP STUB FAIRING 171DL. CRJ-700 SRM 51-42-21-001-001-A01.SDR SWIA202265330Skin · chafedL/H INBD. FLAP VANE HAS MULTIPLE LONG LEADING EDGE CHAFFES (AS MARKED) (C-CHECK RO 4/9/2022) L/H INBD FLAP VANES WERE REPAIRED AND REPLACED AS REQUIRED IAW CRJ 700 SRM 51-42-13-001-001-A01 & REO 670-57-52-521 REV-- DATED: 2022-03-07 COMPLETED SKYCARD SDR SWIA202265329None · chafedR/H INBD. FLAP VANE HAS MULTIPLE LONG LEADING EDGE CHAFFES ( AS MARKED) (C-CHECK RO 4/9/2022) REMOVED AND REPLACED R/H FLAP VANE CAP, INBD MID L/E SKIN AND O/B MID L/E SKIN IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-13-001-001-A01SDR SWIA202264990None · damagedREPLACE R/H WING FLAP VANE OUTBOARD VANE CAP ( MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED R/H WING FLAP VANE OUTBOARD VANE CAP. REF CRJ200 SRM 51-42-13 REV 38 JUL 10/2019 AND DWG # 601R14302 REV E. SEE CONTINUE CARD FOR DETAILS. COMPLIED WIT
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