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 = '5541' 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 = '5541' 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 HNAA2026081400712Rib · damagedF143997 RUDDER I TOP RIB DAMAGED DURING REMOVAL OF HORIZONTAL STABILIZER. PERFORMED RE-CONTOUR AND SPLICE REPAIR TO THE RUDDER I TOP RIB IAW EMB ETD2026-145-01327 REV. A, AND EO1-55-26-0370SDR 2025FA0000758Spar · crackedCRACK EMANATING FROM UPPER LEFT CORNER OF THE RUDDER SPAR AND DOWN BEHIND THE HINGE CONNECTION PLATE FOR APPROXIMATELY 3.5" AND THEN TURNS INBOARD FOR A DISTANCE OF 1/2 THE WIDTH OF THE SPAR. THE CRACK WAS FOUND DURING THE REMOVAL OF THE RUDDER TO CHANGE THE BSDR SWIA2025F01379Rib · corrodedRUDDER BOTTOM RIB HAS CORROSION ON UPPER SIDE, HN00255797 (C-CHECK RO 09/24/2025)REMOVED CORROSION AND RESTORED FINISH ON REWORKED AREAS AT RUDDER BOTTOM RIB ON UPPER SIDE, COMPLIED TO ALL STEPS REO 601R-55-41-310 REV -- DATE: 2025-08-04 ( SEE CONTINUATIONSDR AALA202504151358Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO RUDDER CONDUCTIVE FRAME FROM RUDDER STA 257.9 TO STA 276. ACCOMPLISHED SPLICE REPAIR PER SRM 55-40-01-2R AND EA 363604.SDR JJBA20250403019Rib · crackedRUDDER II, FWD ON FRONT SPAR, UPPER RIB CRACKED AT UPPER MID HINGE FITTING. RUDDER II, FWD OF FRONT SPAR UPPER MID HINGE FITTING UPPER RIB REPLACED.SDR TSAA2024112600019Frame · corrodedCORROSION (19.0" X 1.0") RH SIDE CONDUCTIVE FRAME TRAILING EDGE AT RUD STA 233~252. CORROSION REMOVED LEVEL 1 AT RH SIDE CONDUCTIVE FRAME TRAILING EDGE AT RUD STA 233~252 FROM PN 65C31496-4 AFTER REMOVED SKIN THROUGH REPLACED CONDUCTIVE FRAME I.A.W B737-300 SSDR NACA2024070500009Frame · corrodedCORROSION AT RH SIDE RUDDER CONDUCTIVE FRAME AT RUDDER STA 234. REMOVED CORROSION AND REPLACED CONDUCTIVE FRAME IAW SRM 55-40-01 AND CMM 55-40-12SDR NACA2024070500008Frame · corrodedCORROSION AT LH SIDE RUDDER CONDUCTIVE FRAME AT RUDDER STA 234. REMOVED CORROSION AND REPLACED CONDUCTIVE FRAME IAW SRM 55-40-01 AND CMM 55-40-12SDR AALA202311309908Frame · peelingAIRCRAFT WAS GROUNDED: SHEET METAL PEELING UP ON TOP AFT OF RUDDER. REPAIRED RUDDER CONDUCTIVE FRAME PER AARD 55-40-01, SEE NON ROUTINE WORK RECORD 1023003.SDR AALA202307187153Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RUDDER SKIN CONDUCTIVE FRAME LOCATED AT RUDDER STA 282. REPAIRED FRAME PER SRM 55-40-01-2R PROCEDURE 2 REPAIR 2.SDR WX0A2022091674247None · noneREF. W/O 463019-2 PERMANENT REPAIR OF RUDDER DAMAGE REQUIRES REPAIR/PERFORMED RUDDER SKIN REPAIR AROUND TRAILING EDGE SCREW LINE IN THE GFRP AREA UP TO STEP 2.A.2 H.13 SRM 55-41-13-300-025.COMPLETED RUDDER SKIN REPAIR AROUND TRIALING EDGE SCREW IN GFRP AREA FRSDR SWIA202266637None · wornRUDDER ASS'Y FAILED BACKLASH CHECK, V-STAB REAR SPAR RUDDER HINGE FITTING #2 (UPR MIDDLE) SPHERICAL BEARING HAS EXCESSIVE PLAY (C-CHECK RO 10/24/2022) REMOVED AND REPLACED WORN SPHERICAL BEARING AT V-STAB REAR SPAR RUDDER HINGE FITTING #2 (UPR MIDDLE) WSDR SWAA2022082539485Rib · crackedCRACK DORSAL FIN PANEL 321A RIB AT BS 867 AT VERTICAL STABILIZER 2022-423338 / [01] TOOL USED:CALIPER P/N 4996A52 S/N 201219744 CAL DUE DATE 22 FEB 23.;[02] REPLACED RIB AND FASTENERS LOCATED ON DORSAL FIN PANEL 321A RIB AT BS 867 AT VERTICAL STABILIZER IAW B7SDR REXA2022032400492Spar · deformedRUDDER LEADING EDGE HAS DAMAGE TO LIGHTING HOLE AT FRONT SPAR LOWER SECTION JC:55-320-519 EMP#:2006BRT REPAIRED RUDDER L/E LIGHTING HOLE @ FRONT SPAR IAW ENDEAVOR E.A. CRJ255-13042SDR SWIA202265153None · groovedRUDDER #1 HINGE BOLT AND FLOATING BUSHING ARE GROOVED. (C CHECK RO 3-21-22) REPLACED RUDDER #1 HINGE BOLT AND FLOATING BUSHING. REFERENCE CP 24320822 FOR FINAL INSTALL. REF EMB 175 AMM 27-21-05SDR SWIA202265152None · groovedRUDDER #2 HINGE BOLT IS GROOVED. (C CHECK RO 3-21-22) REPLACED RUDDER #2 HINGE BOLT ON RACK. REFERENCE CP 24320822 FOR FINAL INSTALL. REF EMB 175 AMM 27-21-05SDR SWIA202265151None · groovedRUDDER #3 HINGE BOLT AND FLOATING BUSHINGS ARE GROOVED. (C CHECK RO 3-21-22) REPLACED RUDDER #3 HINGE BOLT AND FLOATING BUSHINGS ON RACK. REFERENCE CP 24320822 FOR FINAL INSTALL. REF EMB 175 AMM 27-21-05SDR SWIA202265155None · wornLATE FIND-LH ELEVATOR #1 HINGE BOLT AND BUSHING WORN (C CHECK RO 3-21-22) REPLACED LH ELEVATOR #1 HINGE BOLT AND BUSHING ON RACK. REFERENCE CP 24320802 FOR FINAL INSTALL. REF EMB 175 AMM 27-31-05SDR SWIA202265154None · wornLATE FIND-LH ELEVATOR #3 HINGE BOLT AND NUT WORN (C CHECK RO 3-21-22) REPLACED LH ELEVATOR #3 HINGE BOLT AND NUT ON RACK. REFERENCE CP 24320802 FOR FINAL INSTALL. REF EMB 175 AMM 27-31-05SDR SWIA202163253None · damagedR/H AILERON AFT SPAR #2 I/B HINGE FITTING BUSHING BORE IS PITTED (C-CHECK RO 12/26/2021) REMOVED AND REPLACED R/H AILERON AFT SPAR #2 I/B HINGE FITTING BUSHING. COMPLIED WITH REO 670-57-51-464 REV-- DATED 2021-11-24. / COMPLIED WITH SKYWEST TASKCARD 51-SDR SWIA202162727None · misalignedVERTICAL STABILIZER TRAILING EDGE RUDDER MIDDLE LOWER HINGE DOES NOT LINE UP CORRECTLY. (C-CHECK RO 11-20-2021) REMOVED MIDDLE LOWER HINGE ON VERTICAL STABILIZER TRAILING EDGE REF. CRJ700 SRM 51-42-21-001-001-A01 AND INSTALLED MIDDLE LOWER HINGE ON VERTICSDR LR7A2021070802870Stiffener · crackedSUPPLEMENTAL INFORMATION DURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LOWER INTERIOR STRUCTURE WITH CRACKED MAIN BEAM STIFFENER AT FS1150, RBL6, VSS33. / REPAIRED IAW LOCKHEED SMP583 SRM, FIGURE 51-140-19. NR# 1000461150.SDR LR7A2021070902870Stiffener · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LOWER INTERIOR STRUCTURE WITH CRACKED MAIN BEAM STIFFENER AT FS1150, RBL6, VSS33. / REPAIRED IAW LAC MEA 382-55-21-031. NR# 1000461150.SDR SIMA20210113004Skin · crackedRUDDER II FWD SPAR SKIN APPEARS TO HAVE A CRACK PROTRUDING FROM A HIGH LOCK FOR THE MIDDLE LOWER ATTACH POINT. VIEWED THREW ACCESS PANEL 327 BL. C/A: R & R RUDDER, IAW AMM 27-20-02, REF NON-ROUTINES E839469, E839910 AND E839976 FOR GAP CHECKS, FCF AND BACKLASDR AALA202012219002Frame · damagedAIRCRAFT IN BASE MAINTENANCE. RUDDER LEFT UPPER CONDUCTIVE FRAME UNDERNEATH LOWER STATIC WICK BASE HAS HOLE AT RSTA 282.12. REMOVED FRAME AND DAMAGED SKIN. REPAIRED IAW B737NG SRM 55-40-01-2R-2, B737NG SRM 51-70-10, AND B737NG SRM 51-70-04-2R-1.SDR KCSA202006261098Rib · crackedUPPER RUDDER HAS A 17 INCH CRACK ON INTERSPAR RIB AT RUDDER STA 146.7 UNDER PANEL 326ALSDR SIMA2020040702007Rib · dentedRUDDER 1 LEADING EDGE RIB BELOW CENTER HINGE FITTINGS (ZV=1897.0) IS DENTED.-C/A-REMOVED AND REPLACED RIB AT ZV=1897.0 FOR RUDDER LEADING EDGE BELOW CENTER HINGE FITTING IAW SRM 51-40-02.SDR SIMA2020040602004Rib · bentRUDDER 1 SKIN SUPPORT FLANGE (RIB) AT THE LOWER CENTER HINGE IS BENT.-C/A-REMOVED AND REPLACED RIB IAW EMB SRM 51-40-02.SDR SIMA2020040602003Rib · bentRUDDER 1 SUPPORT FLANGE SKIN AT THE UPPER CENTER HINGE IS BENT.-C/A-REMOVED AND REPLACED RIB IAW EMB SRM 51-40-02.SDR SIMA2020040602005Rib · damagedRUDDER 1 LEADING EDGE RIB ABOVE CENTER HINGE FITTINGS (ZV=2312.0) HAS DAMAGED FLANGE ON INTERIOR SIDE.-C/A- REMOVED AND REPLACED RIB AT ZV=2312.0 IAW EMB SRM 51-40-02.SDR SWAA2021081732667Frame · deformedTRANSFERRED FROM DIS# 1105520 DURING WALK AROUND CHECK; FOUND RUDDER LEFT SIDE CON DUCTIVE FRAME WAS DEFORMED. DAMAGE IS 6 IN LONG X 3 IN WIDE / REMOVED & REINSTALLED RUDDER (P/N 173A0103-10 ; S/N CASA-1318) PER M/M 27-21-11. REFERENCE RO # 0550042-70R FOR REPSDR ASAA2019122431666Spar · puncturedRUDDER FWD SPAR FRONT FACE LOWER R/H CORNER PUNCTURED JUST ABOVE #1 ATTACH FITTING GROUNDED - YES. REPAIR RUDDER FWD SPAR FRONT FACE LOWER R/H CORNER PUNCTURE IAW A319-111 SRM: 51-42-00, 51-77-11-911-008, 51-75-12, 54-42-21, 55-31-11-300-017, NTM: 51-90-00, 51SDR 7C7A2019110800518Spar · gougedGOUGE DAMAGE TOO FORE RUDDER, FRONT SPAR ON R/H SIDE AT RIB# 25. THE PERMANENT REPAIR FOR GOUGE DAMAGE TO FORE RUDDER, FRONT SPAR ON THE R/H SIDE AT RIB#25 WILL BE ACCOMPLISHED IAW DEHAVILLAND AIRCRAFT OF CANADA LIMITED RD 8-55-3406 ISSUE 1 DATED 08 NOVEMBER SDR JGVR20190919006Rib · crackedREPAIRED RUDDER BY REPLACING CRACKED LOWER AFT RIB AND CLIP WITH NEW RIB P/N 6933160-3 AND CLIP P/N 6933160-2 PER SRM 51-40-03, 51-40-06, 51-40-09, AND CSPM 20-40-20.SDR LR7A2019062401961Frame · corrodedDURING SCHEDULED C-1 CHECK UNDER JOB CARD HC5511, FOUND THE RUDDER LOWER FRAME WEB CORRODED BEYOND LIMITS AT SEVERAL PLACES. FS1128-1200, LBL12-RBL12, WL286. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 6270.SDR AALA201905239022Frame · peelingAIRCRAFT WAS GROUNDED: RUDDER TOP RIGHT HAND SURFACE CONDUCTIVE FRAME LOWER CORNER PEELING. REPAIRED CONDUCTIVE FRAME PER AARD 55-40-00-1.SDR CA190308014Rib · corroded(CAN) UPPER RUDDER MACHINED RIB CORRODED.SDR RAIA2019020400002Rib · damagedRUDDER #2 2ND NOSE RIB FROM BOTTOM DAMAGED AT L/H NUTPLATE- REMOVED DAMAGED RIB ON #2 RUDDER NOSE BOTTOM AT L/H AND STARTED LOCATING FASTNER HOLES. DRILLED UP AND INSTALLED NEW RIB ON RUDDER, PAINT REQUIRED. REMOVED & REPLACED #2 RUDDER 2ND LWR NOSE RSDR CA190321002Rib · cracked(CAN) LOWER RIB PART NUMBER 043301015 WAS FOUND CRACKED DURING INSPECTION.SDR V6NA201902192019Rib · crackedAT SCHEDULED INSPECTION, DISCOVERED RUDDER RIB AT WL 126.0 TO BE CRACKED. RIB REPAIRED WITH DOUBLER PER LEARJET 60 STRUCTURAL REPAIR MANUAL SECTION 55-40-01.SDR ASOA2018102485275Rib · corrodedREF: CO 7315618 JOB 7731568 OP 36: RUDDER BOTTOM RIB P/N 600-22032 HAS EVIDENCE OF CORROSION. C/A:REPAIRED DAMAGE IAW SRM 51-21-06, 55-40-00, 51-25-01, STS EA 32-2018-208 AND EC/TC EA 32-2018-208 WO#559076.SDR DXTA2018FA0000361Spar Web · damagedREPAIR OF RUDDER FWD SPAR LIGHTENING HOLE DAMAGED FLANGE. ENGINEERING REPAIR LETTER DQ1562M1 DATED SEPTEMBER 6, 2018.SDR EBVR20170406001Rib · corrodedCORROSION FOUND ON LOWER RIB OF THE RUDDER AT THE BONDING POINT. REPAIRED EXISTING LOWER RUDDER TORQUE TUBE RIB PER AQRD ERO-891028 REV IR. ATTACHED NEW REPAIR DOUBLER TO LOWER RIB OF RUDDER WET WITH PS870B1/2 LOT# 70540 AND CR3213-4-2 RIVETS.SDR QXEA2017030100093Rib · corrodedFORE RUDDER, NOSE RIB 9 CORRODED. NOSE RIB 9 AND STRAP REMOVED IAW SRM 51-42-05. NEW NOSE RIB 9 AND STRAP INSTALLED IAW SRM 51-42-05.SDR 7C7A2017013100283Rib · crackedTRAILING RUDDER, CENTER HINGE, TOP LEADING EDGE RIB CRACKEDSDR 4AER20161102007Frame · corrodedRIGHT HAND RUDDER UPPER AFT CORNER CONDUCTIVE FRAME AT RUDDER STATION 234.89 HAS CORROSION.SDR IPXA2016101109236Rib · corrodedINSPECTION TYPE: 3C, RIB CORRODED INSIDE UPPER FWD RUDDER. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT RIB IAW DWG AMC7292 AND SRM 51-35-01.SDR IGXR20160921004Trim Tab · crackedTHE LOWER AFT CORNER OF THE RUDDER TRIM HAS A CRACK MEASURING 0.76 INCHES LONG. PERFORMED PERMANENT REPAIR USING APPROVED ENGINEERING ORDER ERO-859505.SDR JJBA20160514008Rib · damagedDAMAGE FOUND ON TOP OF TRAILING RUDDER. REMOVED DAMAGE ON TOP OF TRAILING RUDDER.SDR DALA2016051203953Tab · unknownFLAME SPRAY COAT ON RUDDER CONTROL TAB. REPAIRED IAW SRM 55-41-01.
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