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 = '5752' 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 = '5752' 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 SWIA202266167None · dentedLH OB FLAP LOWER SKIN IS DENTED AT FLS268 10IN FWD OF TE. (C-CHECK RO 7/26/2022) LH OB FLAP LOWER SKIN DENT AT FLS268 10IN FWD OF TE WAS FOUND OUT OF LIMITS IAW CRJ 200 SRM 57-53-00. COMPLIED WITH CRJ 200 SRM 57-53-00 REPAIR NO.3 REV.38 B DATED 25 NOV 2SDR SWIA202265962None · wornLH WING FLAP TRACK 2A OUTBD SIDE HAS WIDTH REDUCTION APPROX. 1.4MM NOMINAL OF 21.0MM, A TOTALOF 4" IN LENGTH 1.4MM IS BEYOND ALLOWABLE BLEND LIMITS. CALIPER QA50384 CAL DUE 02-21-23 (C-CHECK RO 6/23/2022) REMOVED AND REPLACED L/H WING FLAP TRACK 2A OB WSDR SWIA202265961None · wornRH WING FLAP TRACK 2A OUTBD SIDE HAS WIDTH REDUCTION OF 1.2MM NOMINAL IS 21.0MM WEAR IS BEYOND BLEND LIMITS CALIPER QA50384 CAL DUE 02-21-23 (C-CHECK RO 6/23/2022) REMOVED AND REPLACED RH WING FLAP TRACK 2A OUTBOARD. REF: EMB175 AMM 57-57-35, ASSET# SDR SWIA202265938None · damagedL/H FLAP TRACK #2 A OUTBOARD HAS WIDTH REDUCTION DAMAGE ON UPPER AND LOWER SURFACE MEASURED AT 1.18MM. (C-CHECK RO 6/15/2022) REMOVED AND REPLACED L/H FLAP TRACK #2 A OUTBOARD HAS WIDTH REDUCTION DAMAGE ON UPPER AND LOWER SURFACE REFERENCE APPLICABLE STSDR SWIA202266094None · chafed*LH AILERON UPPER SKIN SHROUD CHAFFED FORWARD OUTBOARD SIDE (MARKED) (C-CHECK RO 7/9/2022) REMOVED AND REPLACED LEFTHAND AILERON LEADING EDGE SKIN P/N: CC670-13052-3 IAW CRJ 200 SRM 51-42-21 / CRJ 200 SRM 51-42-06 / CRJ 200 SRM 51-42-13 AND DRAWING CC6SDR SWIA202266093None · gouged*LH OUTBOARD FLAP CENTER HINGE LUG UPPER FITTING GOUGED ON INBOARD SIDE (MARKED) (C-CHECK RO 7/9/2022) BLENDED OUT GOUGE ON LH OB FLAP CENTER HINGE LUG AND FOUND ACCEPTABLE TO ENGINEERING REF REO 601R-57-53-1240 REV -- DATED 2022-06-11, ALL STEPS COMPLISDR SWIA202265439None · leakingRIGHT WING 2ND CANOE O/B OF MLG HAS FUEL LEAK AT THE FORWARD BOLTS OF THE BOX FITTING FORWARD HINGE ( REF 57-21-36 ) (FILED CLOSED) REMOVED AND REPLACED FOWARD AND AFT HARDWARE OF FLAP HINGE-BOX FITTING ON RIGHT WING 2ND CANOE IN REFERENCE TO AMM 57-21-36.SDR SWIA202265843None · chafed*LH AILERON ASSY UPPER LEADING-EDGE SKIN CHAFFED MULTIPLE AREAS ALONG ENTIRE WIDTH (MARKED) (C-CHECK RO 6/1/2022) REMOVED AND REPLACED LH AILERON ASSY UPPER LEADING-EDGE SKIN REF DWG CC670-13000 REV-D, CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-22, AND CRJ20SDR SWIA202265811None · corroded*LH OUTBD FLAP OUTBD HINGE BOX FWD SUPPORT FITTING HAS CORRODED HARDWARE. (C CHECK RO 5/23/22) REMOVED AND REPLACED DAMAGED HARDWARE WITH NEW. REF. CRJ 900 AMM 57-54-02-400-808-A01. NO LEAKS/DEFECTS NOTED. / SEE CONTINUATION CARD FOR DETAILS OF WORK PERSDR SWIA202264785None · corrodedL/H AND R/H WING FLAP TRACK SUPPORT #2, #3, AND #4 FWD ATTACHMENT TO WING FITTING SPRING WASHERS CORRODED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED L/H AND R/H WING FLAP TRACK SUPPORT #2, #3, AND #4 FWD ATTACHMENT TO WING FITTING SPRING WASHERS. REF ESDR SWIA202264784None · damagedL/H WING #2A O/B FLAP TRACK HAS WIDTH REDUCTION DAMAGE OF .031". (C CHECK RO 03/07/2022) LH WING #2A OB FLAP TRACK OUT OF LIMITS. NOMINAL 1.003" REMOVED.44" REMAINING .959" REF ERJ 175 SRM 57-52-03. TC2-8910 DATE11-23-22. REPLACED LH OB #2A FLAP TRACK. RSDR N6WA2022020902Bolt · corrodedL/H O/B FLAP, CENTER HINGE ARM, ALL ATTACH HDW IS DAMAGED AND CORRODED,R&R CENTER HINGE ARM, L/H O/B FLAP HARDWARE IAW CRJ 700 AMM 57-53-27SDR SWIA202264566None · seizedR/H WING T/E O/B FLAP CRUISE ROLLER FROZEN. (C CHECK RO 2/20/2022) REPLACED RH WING TE OB FLAP CRUISE ROLLER. REF ERJ 175 AMM 27-51-11. TC2-8911 DATE 11-9-22SDR SWIA202264093None · dentedTRANSFER FROM EAML 835555 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 835345 DENT FOUND ON RIGHT OUTBOARD FLAP TRAILING EDGE 18 INCHES FROM FLAP INBOARD EDGE. (FILED CLOSED) REMOVED AND REPLACED RH OUTBOARD FLAP IN REF TO TASK CARD 27-900-10SDR SWIA202264987None · damagedREPLACE L/H WING FLAP VANE OUTBOARD VANE CAP ( MARKED) (C-CHECK RO 3/14/2022) REMOVED AND REPLACED LH IB FLAP VANE, OB VANE CAP WITH NEW, REF CRJ 200 SRM 51-42-13 AND DWG 601R14302 REV E. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) SDR SWIA202264339None · damagedFOUND DAMAGED HARDWARE ON RH FLAP HINGE ARM AT WS 220.0. REPLACE MOUNTING HARDWARE. (C CHECK RO 02-12-2022) REPLACED DAMAGED HARDWARE ON RH FLAP HINGE ARM AT WS220 IN REF TO CRJ200 AMM 57-53-02-400-803 / CAL TOOL TUC4822 DUE 30 JUN 2022SDR SWIA202264976None · corrodedFOUND 2EA. BOLTS AND ALL NUTS TO BE UNSERVICEABLE AT W.S. 178.00, 220.00 AND 264.00 REQUIRE REPLACEMENT. (C CHECK RO 3/11/2022) REMOVED AND REPLACED ALL UNSERVICEABLE LH OB FLAP HINGE BOX HARDWARE AT W.S. 178, W.S. 220, AND W.S. 264.00 IAW CRJ-200 AMM 57-2SDR SWIA202264749None · corroded*ON MID-FLAP HINGE OF O/B FLAP, CORROSION ON MULTIPLE AREAS OF HARDWARE AND BUSHING ON SPRING ACTUATOR AT APPROXIMATELY / WS 216.90. (MARKED) (C CHECK RO 02/25/2022) REMOVED AND INSTALLED NEW HARDWARE ON MID-FLAP HINGE OF O/B FLAP AND BUSHING ON SPRING ASDR SWIA202264748None · corroded*I/B FLAP HINGE OF O/B FLAP, CORROSION ON HARDWARE PIN AT SPRING ACTUATOR AT APPROXIMATELY WS 170.83. (MARKED) (C CHECK RO 02/25/2022) REMOVED AND INSTALLED NEW HARDWARE ON I/B FLAP HINGE OF O/B FLAP, ON HARDWARE PIN AT SPRING ACTUATOR AT APPROXIMATELY WSDR SWIA202263821None · seizedRH OB FLAP CAM FOLLOWER BEARING APPEARS SEIZED. WS163. ( AGING AIRCRAFT INSP RO 1/16/2022) REMOVED AND REPLACED RH OB FLAP CAM FOLLOWER BEARING IN REFERENCE TO AMM 20-21-00. / NEW BEARING SPINS FREELY.SDR SWIA202264076None · crackedR/H WING LOWER SURFACE HAS CRACK AT FORWARD EDGE OF MLG CUTOUT I/B OF GEAR. (C CHECK RO 01/28/2022) REPAIRED R/H LOWER SURFACE WING CRACK AT FWD EDGE OF MLG CUTOUT I/B OOF GEAR PER ETD2022-170-000846 REV.: ASDR SWIA202164299None · gouged*LH WING OTBD FLAP VANE HAS GOUGE ON LOWER LEADING EDGE INBD OF FLS 296.07 (C CHECK RO 02-12-2022) REMOVED AND REPLACED LH WING OTBD FLAP VANE AT FLS 296.07. REF CRJ 200 CRJ 200 SRM 51-42-13 AND INSTALLATION DWG 601R14502 REV -D. COMPLIED WITH 51-900-1003SDR SWIA202163102None · installedROBBED LH WING OUTBOARD MAIN FLAP ROLLER RAIL TO BE USED FOR 292SY. PN: 170-24554-003 (FILED - CLOSED) INSTALLED LH WING, OUTBOARD MAIN FLAP ROLLER RAIL FOR INBOARD/OUTBOARD ROLLER PER AMM 57-55-00. OPS CHECK GOOD.SDR SWIA202164342None · worn*RH INBOARD FLAP THE OUTBOARD FLAP VANE ACTUATOR CARRIAGE LOWER ROLLER HAS A FLAT SPOT. (C CHECK RO 02-12-2022) REMOVED AND REPLACE LOWER ROLLER ON THE RH INBOARD FLAP OUTBOARD FLAP VANE ACTUATOR REF CRJ200 CMM 57-52-03SDR SWIA202163088None · damagedLH WING OUTBOARD MAIN FLAP ROLLER RAIL DAMAGED. ( FILED - CLOSED) REMOVED AND REPLACED LH WING OUTBOARD MAIN FLAP ROLLER RAIL IN REFERENCE TO AMM 20-10-01 AND AIPC 57-55-00, OPS CHECK GOODSDR SWIA202164238None · damagedWS 178 R/H FLAP HINGE BOX AFT O/B MOUNT FITTING I/B LUG I/B FACE AFT CORNER HAS TOOLING DAMAGE (C CHECK RO 2-11-2022) REPAIRED WS 178 R/H FLAP HINGE BOX AFT O/B MOUNT FITTING I/B LUG I/B FACE AFT CORNER TOOLING DAMAGE IAW MHIRJ REO 601R-57-21-3557 REV -- DSDR SWIA202164237None · corrodedWS 264 O/B HINGE BOX ATF O/B FITTING I/B LUG I/B FACE AFT EDGE HAS TOOLING DAMAGE (C CHECK RO 2-11-2022) REPAIRED WS 264 O/B HINGE BOX ATF O/B FITTING I/B LUG I/B FACE AFT EDGE TOOLING DAMAGE IAW MHIRJ REO 601R-57-21-3557 REV -- DATED 2021-12-15 AND SKY CSDR SWIA202164653None · chafed* R/H INB FLAP OBD HINGE ARM INB ALIGNMENT PLATE CHAFED. (C CHECK RO 02/22/2022) REMOVED CHAFING DAMAGE FROM R/H INB FLAP- OBD INB HINGE ARM ALIGNMENT PLATE REF CRJ-700 SRM 51-12-00-0001-001-A01 / PART IS OUT OF LIMITS, REPLACEMENT REQUIRED, RECEIVED NEW PSDR SWIA202164545None · corrodedLEFT WING O/B FLAP O/B HINGE BOX SUPPORT FITTING HAS CORRODED HARDWARE (C CHECK RO 2/17/2022) REMOVED AND REPLACED THE HARDWARE ON THE LH WING O/B FLAP O/B HINGE BOX REF CRJ700 AMM 57-54-02-400-808-A01, LEAK CHECKS AND OP CHECKS GOOD.SDR SWIA202164544None · corrodedLEFT HAND OUTBOARD FLAP INBOARD HINGE LUG FITTINGS HAVE CORRODED HARDWARE (C CHECK RO 2/17/2022) REMOVED AND REPLACED L/H O/B FLAP I/B HINGE LUG FITTING BOLT P/N 601R14633-3 AND NUT P/N MS17825-4 REF. CRJ-700 CMM 57-53-04 PG. 3005 STEPS 5A(6)-(8) AND PG. 7SDR SWIA202164543None · corrodedLEFT HAND OUTBOARD FLAP OUTBOARD HINGE LUG FITTINGS HAVE CORRODED HARDWARE (C CHECK RO 2/17/2022) REMOVED AND REPLACED L/H O/B FLAP O/B HINGE LUG FITTING BOLT P/N 601R14633-3 AND NUT P/N MS17825-4 REF. CRJ-700 CMM 57-53-04 PG. 3006 STEPS 7A(5)-(8) AND PG. SDR SWIA202164185None · crackedBRACKET BETWEEN #2 & #3 HINGE ON RH AILERON CRACKED (C CHECK RO 02-03-22) REMOVED AND REPLACED RH AILERON BRACKET @ WS340.236 REF. CRJ700 SRM 51-42-21-001-001-A01.SDR KCSA2021112912None · noneDAMAGE TO RIGHT SIDE HORIZONTAL STAB AND RIGHT SIDE OF FUSELAGE FOUND ON LANDING INSPECTION. ADDENDUM WILL BE PROVIDED UPON MAJOR REPAIRS BEING PERFORMED AND RECTIFICATION COMPLETED.SDR SWIA202163194None · gougedR/H OTBD FLAP VANE GOUGED IN MULTIPLE LOCATIONS FROM INADVERTENT CLECO ENTRAPMENT WHILE CYCLING FLAP CONTROL SYSTEM. (C CHECK RO 12-19-21) REMOVED GOUGES FROM RH OTBD FLAP VANE AND COMPLIED WITH ALL STEPS OF REO 670-57-53-305 REV-- DATED 2021-11-27. COMPLSDR SWIA202164197None · corroded* LEFT WING OUTBOARD FLAP, OUTBOARD FORWARD HINGE BOX FITTING HAS CORRODED HARDWARE. (C CHECK RO 02-03-22) REMOVED 4 EA CORRODED AND INSTALLED 4 EA NEW, L/H WING OUTBOARD FLAP, OUTBOARD HINGE BOX, ANTI-MIGRATION PLATE HARDWARE REF CRJ 700 AMM'S 57-54-02-00SDR SWIA202164106None · dented*RIGHT INBOARD FLAP - LOWER SKIN IS DENTED AT THE TRAILING EDGE, APPROXIMATE WS38.00. (MARKED) (C CHECK RO 02-03-22) PERFORMED DOUBLER REPAIR ON RH INBD FLAP LOWER TRAILING EDGE SKIN. REF CRJ700 SRM 57-52-01-201-001-A01 FIGURE 57-52-01-991-812 (SHEET 4 OFSDR SWIA202163872None · damagedCANN RH O/B FLAP CENTER HING BOX P/N CC670-10801-4 FOR AC N716SK SN 10180 (C CHECK RO 1/16/2022) REMOVED AND INSTALLED SERVICEABLE R/H O/B FLAP HINGE BOX AND 3 EA BONDING WIRES AT WS 220 REF CRJ 700 AMM 57-54-02-000-804-A01, AND 57-54-02-400-804-A01.SDR SWIA202164279None · failedDURING BACKLASH CHECK OF THE R/H I/B FLIGHT SPOILER, FOUND THE MAXIMUM BACKLASH TO BE 0.130 (MAX ALLOWABLE LIMIT IS 0.114) (C CHECK RO 2-11-2022) REMOVED AND REPLACED RH IB FLIGHT SPOILER MOUNTING HARDWARE IAW CRJ 200 AMM 27-62-01-000/400-801 BACKLASH CHECSDR SWIA202163870None · corrodedCANN R/H OUTBD FLAP PART# CC670-14500-968 FOR USE ON N606SK (C CHECK RO 1/16/2022) REMOVED AND REPLACED R/H O/B FLAP REF CRJ 700 AMM 27-52-29-000-801-A02, AND 27-52-29-400-801-A02. ALL CHECKS GOODSDR MASA20211117560None · noneSEVEN DENTS WERE FOUND AFFECTING THE LOWER SKIN OF LEFT INBOARD FLAP LOCATED AT APPROXIMATELY FSL 20. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-52-01, FIGURE 57-52-01-991-801, ITEM 27A.SDR SWIA202163956None · corrodedLEFT WING O/B FLAP O/B HINGE BOX SUPPORT FITTINGS HAS CORRODED HARDWARE MARKED (C CHECK RO 1/18/2022) CLEANED LEFT WING O/B FLAP O/B HINGE BOX SUPPORT FITTING HARDWARE AND UPON FURTHER INSPECTION FOUND NO CORROSION.SDR SWIA202163942None · corrodedLEFT WING O/B FLAP O/B HINGE LUG FITTINGS HAS CORRODED HARDWARE MARKED (C CHECK RO 1/18/2022) REMOVED AND REPLACED LEFT WING OTBD FLAP OTBD HINGE LUG CORRODED HARDWARE: 1EA. BOLT, 1EA. NUT AND 2EA.WASHERS REF. CRJ-700 SRM 51-41-02-001-001-A01. CALIBRATEDSDR SWIA202163941None · corrodedLEFT WING O/B FLAP MID HINGE LUG FITTINGS HAS CORRODED HARDWARE MARKED (C CHECK RO 1/18/2022) REMOVED AND REPLACED LEFT WING OTBD FLAP MID HINGE LUG CORRODED HARDWARE: 1EA. BOLT, 1EA. NUT AND 2EA.WASHERS REF. CRJ-700 SRM 51-41-02-001-001-A01. CALIBRATED SDR SWIA202163940None · corrodedLEFT WING O/B FLAP I/B HINGE LUG FITTINGS HAS CORRODED HARDWARE MARKED (C CHECK RO 1/18/2022) REMOVED AND REPLACED LEFT WING OTBD FLAP INBD HINGE LUG CORRODED HARDWARE: 1EA. BOLT, 1EA. NUT AND 2EA.WASHERS REF. CRJ-700 SRM 51-41-02-001-001-A01. CALIBRATEDSDR SWIA202163939None · corrodedLEFT WING O/B FLAP O/B FLAP HINGE ACTUATOR TIE ROD HAS CORROSION ON BOTH CLEVIS ENDS (C CHECK RO 1/18/2022) REMOVED AND REPLACED 1EA. L/H CORRODED, OUTBOARD FLAP HINGE ACTUATOR TIE ROD. INSTALLED 1EA. NEW L/H OUTBOARD FLAP HINGE ACTUATOR TIE ROD. TO INCLUSDR SWIA202163938None · corrodedLEFT WING O/B FLAP MIDDLE FLAP HINGE ACTUATOR TIE ROD HAS CORROSION ON BOTH CLEVIS ENDS (C CHECK RO 1/18/2022) REMOVED AND REPLACED LEFT WING OTBD FLAP MIDDLE FLAP HINGE ACTUATOR TIE ROD (WITH NEW HARDWARE: 2EA. WASHERS, 2EA. PINS, 1EA. ROD ASSY) REF. CRJSDR SWIA202163246None · dented*DENT ON LH OTBD FLAP LOWER EXTERNAL SKIN, LOCATED ON LOWER OTBD CORNER (C-CHECK RO 12/26/2021) REPAIRED DENT DAMAGE ON LH OTBD FLAP LOWER EXTERNAL SKIN, LOCATED ON LOWER OTBD CORNER PER CRJ 700 SRM 57-53-01-201-001-A01 REV 38 DATED JUL 25 2020 TYPE IISDR MASA20211115558None · dentedNBOARD FLAP LOWER SKIN OF THE RH WING WAS FOUND TO HAVE (2) DENTS AT FLS 24.00. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM57-52-01, ITEM 28A, B, EA 80-2021-153SDR MASA20211111556None · noneWEAR DAMAGE WAS FOUND ON THE L/H INBOARD FLAP UPPER ACCESS PANEL 584EB, THE DAMAGE IS LOCATED IN THE FORWARD EDGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-52-01-001-001-A01, DATED AUG-20-2010, EA 20-2021-199.SDR SWIA202164101None · dentedADM# 710SK-2782 SEVERAL DENTS LOCATED ON TOP SKIN ON LH AILERON.1ST DENT MEASURES .6195" X .7390" X .005"; 2ND DENT .3575" X .3750" X .0012"; 3RD DENT .3265" X .4030" X .004" . IF DAMAGE IS WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE OF DAMAGE USI
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