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 SWIA202163743Nut · rustedLH IB GROUND SPOILER IB AND OB MOUNT BOLT NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REPLACED RUSTED NUTS ON LH IB GROUND SPOILER IB AND OB BOLTS IAW CRJ 200 AMM 27-65-01-400-801SDR SWIA202163742Nut · rustedLH OB GROUND SPOILER IB AND OB MOUNT BOLT NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED IB AND OB MOUNT BOLT NUTS ON THE LH OUTBOARD GROUND SPOILER WITH NEW SERVICEABLE NUTS IAW CRJ 200 AMM 27-65-01-000/400-801. OPS CHECK GOOD AT THIS TISDR SWIA202163741Nut · rustedLH WING FLIGHT SPOILER # 1, # 2, #3, AND #4 HINGE MOUNT BOLT NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REPLACED LH FLIGHT SPOILER HINGE BOLT NUTS AT HINGE # 1,2,3 AND 4 IAW CRJ 200 AMM 27-64-05-400-801SDR SWIA202163740None · rustedLH WING SPOILERON #1, # 2, AND # 4 HINGE MOUNT BOLT NUTS ARE RUSTED AND # 1 AND # 4 HINGE BOLT KEEPER BOLTS ARE ALSO RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED ALL CORRODED HARDWARE ON LH SPOILERON HINGE POINTS IAW CRJ-200 AMM 27-64-01-000/400-SDR MASA20211018492None · noneSLAT TRACK 2-3 OF SLAT #2 ON THE LH WING WAS FOUND TO HAVE CORRIOSON DAMAGE ON THE UPPER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 105, EA 69-2021-183.SDR MASA20211018491None · noneSLAT TRACK 2-1 OF SLAT #2 ON THE LH WING WAS FOUND TO HAVE CORRIOSON DAMAGE ON THE UPPER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 5, ITEM 15, EA 69-2021-182.SDR MASA20211018490None · noneSLAT TRACK 1-3 OF SLAT #1 ON THE LH WING WAS FOUND TO HAVE CORRIOSON DAMAGE ON THE UPPER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 105, EA 69-2021-181.SDR MASA20211018489None · noneSLAT TRACK 1-1 OF SLAT #1 ON THE LH WING WAS FOUND TO HAVE CORRIOSON DAMAGE ON THE UPPER FACE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 IPC 27-81-41, FIGURE 1, ITEM 45, EA 69-2021-180.SDR CALA2021101801903Skin · crackedSUPPORT TASK - EA 5725-01008 OP.4 AD 2018-13-06 RHW STR L-9.5 BETWEEN RIB27 & 28 CODE ''A'' HOLE FOUND CRACK , TRANSFER REF NR 9131132 AND ORIGINATED BY EMP V897399 RII INSPECTED BY HX146606 ADD EMP:V896834 RHW LOWER SKIN AT STRINGER L-9.5 BETWEEN RIB27 AND 28SDR CALA2021101801902Skin · crackedSUPPORT TASK EA5725-01008 OP.4 AD2018-13-06 RHW STR L-9.5 BETWEEN RIB 28 AND 29 CODE ''ZVQ'' 1EA HOLE FOUND CRACK TRANSFER REF NR 9131133 AND ORIGINATED BY EMP V897399 RII INSPECTED BY HX169509 ADD EMP:V898550 RHW LOWER SKIN AT STRINGER L-9.5 BETWEEN RIB28 ANDSDR CALA2021101801901Skin · crackedSUPPORT TASK - EA5725-01003 OP006 AD2018-13-06 RHW STR L-6.5 BETWEEN RIB31 AND 32 1EA CODE ''A'' HOLE FOUND CRACK , DETAILS REFER ATTACHED FIG. TRANSFER REF NR LP9131134 AND ORIGINATED BY EMP V897399 RII INSPECTED BY HX146606 RHW LOWER SKIN AT STRINGER L-6.5 BSDR SWIA202163739None · rustedR/H AILERON BOLT RETAINING PLATES (ALL OF THEM ) ,HAVE THERE BOLTS RUSTED. (C-CHECK RO 1/5/2022) REMOVED CORRODED BOLTS WASHERS AND NUTS FROM AILERON BOLT RETAINING PLATES AND INSTALLED SERVICABLE BOLTS WASHERS AND NUTS ON AILERON BOLT RETAINING PLATESSDR SWIA202163738Nut · rustedR/H AILERON CENTER HINGE ATTACH BOLTS, BOTH NUTS RUSTED (C-CHECK RO 1/5/2022) INSTALLED NEW NUTS ON CENTER HINGE ATTACH BOLTS OF RH AILERON IAW CRJ 200 AMM 27-15-01-400-801 STEPS 3.L.(10)-(15)SDR JJBA20211015027None · noneRIGHT WING CENTER LEADING EDGE #612, HAS LARGE DENT 37 INCHES FROM I/B END. REPAIRED DENT IN RIGHT WING CENTER LEADING EDGE 612 37 INCHES FROM INBD END.SDR DALA2021101806427None · noneSHIP 675 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588617-14 REV A. CORRECTIVE ACTION: REF 588617-14 REV A. (1984206)SDR CALA2021101801897Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRA CKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL54.60 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL DATA TRANSCRIBED FROM NSA EMX NR 00112 HANGAR NR 5867194 ACCOMPLISSDR CALA2021101801896Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRAC KED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL DATA TRANSCRIBED FROM NSA EMX NR 00108 HANGAR NR 5867190 ACCOMPLISHSDR CALA2021101801895Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRA CKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL DATA TRANSCRIBED FROM NSA EMX NR 00105 HANGAR NR 5867187 ACCOMPLISDR CALA2021101801894Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRA CKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 LBL 54.60 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL DATA TRANSCRIBED FROM NSA EMX NR 00107 HAN GAR NR 5867189 ACCOMPLISHESDR CALA2021101801893Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 40187 IS CRA CKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 40.87 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL DATA TRANSCRIBED FROM NSA EMX NR 00106 HANGAR NR 5867188 ACCOMPLISDR CALA2021101801892Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRA CKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL DATA TRANSCRIBED FROM NSA EMX NR 00109 HANGAR NR 5867191 ACCOMPLISDR CALA2021101801891Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 ABD LBL 15.04 IS CRA CKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL DATA TRANSCRIBED FROM NSA EMX NR 00104 AND HANGAR NR 5867186 ACCOSDR CALA2021101801890Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRA CKED. REMOVED AND REPLCED SHEAR FITTING AT STA 540 AND RBL 40.87 IAW B 737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL DATA TRAN SCRIBED FROM NSA EMX NR 00111 AND HANGAR NR 5867193 ACCOMPLSDR CALA2021101801889Fitting · corrodedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRAC KED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND LBL 6.14 IAW B 737-800 SRM 51-40-02 AND BAC DWG 111A20000 REV ORIGINAL CIR C/W DATA WAS TRANSCRIBED FROM NSA EMX NR 00103 AND HANGAR NE 5867SDR CALA2021101801888Fitting · crackedB737-57-04-1262 SHEAR FITTING AT STATON 540 AND RBL 32.40 IS CRA CKED. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND RBL 32.40 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL CIR C/W DATA WAS TRANSCRIBED FROM HANGAR NR 5867192 NSA EMX NR 00110 SDR FDEA202110142537None · noneL/H WING #2 SLAT HAS 2 HOLES IN THE UNDERSIDE OF THE SLAT PANEL JUST O/B OF THE #1 ENG PYLON. IN WORKSDR CALA2021101401873None · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 40.87 HANGER N/R 6228721, WORK ACCOMPLISHED BY V905004, AND INSPECTED IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SESDR CALA2021101401872None · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 N/R 6228729, WORK ACCOMPLISHED BY V905004, AND INSPECTED BY IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE V020SDR CALA2021101401871None · noneB737-57-4-1262-SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 6.14 AND HANGER N/R 6228718, WORK ACCOMPLISHED BY V905004, AND IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE INSPECSDR CALA2021101401870None · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 54.60 6228730, WORK ACCOMPLISHED BY V905004, AND INSPECTED BY V020312. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SSDR CALA2021101401869None · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 RBL 15.04 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 HANGER N/R 6228719, WORK ACCOMPLISHED BY V905004, AND INSPECTED IAW B737-800 SRM 51-40-02 AND BAC DWG 11A2000 REVORIGINAL SEE BY VSDR CALA2021101401868None · noneB737-57-4-1262-SHEAR FITTING AT STATION 540 LBL 54.60 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 54.60 6228715, WORK ACCOMPLISHED BY V905004, AND INSPECTED BY V020312. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSDR CALA2021101401867None · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 AND 32.40 IS CRACKED. REMOVED AND REPLACE SHEAR FITTING AT STATION 540 AND LBL 32.40 ACCOMPLISHED BY V905004, AND INSPECTED BY V020312. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NSA EMX N/R 0011SDR CALA2021101401866None · crackedB737-57-4-1262-SHEAR FITTING AT STATION 540 RBL 32.40 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STATION540AND RBL 32.40 6228720, WORK ACCOMPLISHED BY V905004, AND INSPECTED BY V020312. IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE NASSDR SWIA202161796None · failedR&R RH WING TRAILING EDGE AILERON BUSHINGS DUE TO FAILED BACKLASH ( FILED - CLOSED) R&R RH WING TRAILING EDGE AILERON BUSHINGS IN REFERENCE TO AMM 20-26-00. REF 23628362 FOR COMPLETION OF TASK CARD 27-900-1003-SKY.SDR DALA2021101506372None · noneSHIP 5642 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 594590-14. CORRECTIVE ACTION: REF ERA 594590-14. (1981957)SDR DALA2021101306317None · noneSHIP 5642 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 594591-14. CORRECTIVE ACTION: REF ERA 594591-14. (1981493)SDR DALA2021101306318None · noneSHIP 678 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 594672-14. CORRECTIVE ACTION: REF ERA 594672-14. (1981260)SDR IXXA2022010603Retainer · corrodedCORROSION ON UPPER TE SEAL RETAINER AT STA790 OB OF #12 SPOILER PCASDR SWIA202163219None · corrodedALL ATTACHING HARDWARE ON THE LH AILERON HINGE BOLT STOP BRACKETS ARE CORRODED & REQUIRE REPLACEMENT. (C CHECK RO 12-19-21) REPLACED 14EA BOLTS AND WASHERS ON L/H AILERON HINGE BOLT BRACKETS REF CRJ 700 AMM 20-21-00-910-801-A01, AND 20-51-00-400-807-A01. MSDR SWIA202163218None · corrodedALL ATTACHING HARDWARE ON THE RH AILERON HINGE BOLT STOP BRACKETS ARE CORRODED & REQUIRE REPLACEMENT. (C CHECK RO 12-19-21) REPLACED 14EA BOLTS AND WASHERS ON R/H AILERON HINGE BOLT BRACKETS REF CRJ 700 AMM 20-21-00-910-801-A01, AND 20-51-00-400-807-A01. SDR SWIA202163010None · corrodedLH SPOILERON PCUS HAS RUSTED HARDWARE AT MOUNTING POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTED HARDWARE WITH NEW HARDWARE LEFT SPOILERON PCU MOUNT POINTS REF CRJ 200 AMM 27-62-01-400-801 STEPS 2. B. (6) THRU (7) TORQUE WRENCH TUC5659 CAL DUE 28 FEB 20SDR SWIA202163009None · corrodedLH FLIGHT SPOILER PCUS HAS RUSTED HARDWARE AT MOUNTING POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTY HARDWARE WITH NEW HARDWARE LEFT FLIGHT SPOILER PCU MOUNT POINTS REF CRJ 200 AMM 27-62-01-400-801 STEP 2. B. (6) THRU (7). TORQUE WRENCH TUC5689 CAL DUE 28SDR SWIA202163008None · corrodedLH OUTBOARD GROUND SPOILER PCU HAVE RUSTED HARDWARE FOR MOUNTING AND HINGE POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTED HARDWARE WITH NEW HARDWARE LEFT OUTBOARD GROUNG SPOILER PCU FORK END AND HINGE LINK REF CRJ 200 AMM 27-63-01-400-801 STEP 2. B. (3)SDR SWIA202163007None · corrodedLH INBOARD GROUND SPOILER PCU HAVE RUSTED HARDWARE FOR MOUNTING AND HINGE POINTS (C-CHECK RO 12-4-2021) REPLACED RUSTY HARDWARE WITH NEW HARDWARE LEFT INBOARD GROUND SPOILER PCU FORK END AND HINGE LINK REF CRJ 200 AMM 27-63-01-400-801 STEP 2. B. (3) THSDR P5CA2021100300373Bracket · noneLHW NO.7 V/C FLAP TRANSLATING WIRE LINK BRACKET FOUND DAMAGED(<P>LHW NO.7 V/C FLAP WIRE LINK BRACKET REPLACED AS PER RI-57-00-15033 REV. A.</P>)SDR P5CA2021101300384None · noneNO. 19 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)SDR P5CA2021101300385None · noneNO. 6 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1.</P>)SDR P5CA2021101300386None · noneNO. 21 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)SDR P5CA2021101300387None · noneNO. 7 V/C FLAP LSA FOUND TORN.(<P>PERFORMED REPAIR AS PER CMM 57-55-42 REPAIR 17-1</P>)
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