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 FDEA202204241050Former · crackedR/H WING AT STATION .441 L/E FORMER IS CRACKED P/N: 114T2170-6 REMOVED AND REPLACED RH WING LEADING EDGE NOSE FORMER(114T2170-6), ANGLE (114T2171-4), AND LOOSE FASTNERS AT OSS 441.596 IN REF. TO EA# T H-5720-T0368175 P1SDR FDEA202204231088Former · crackedCRACKED FORMER AND LOOSE FASTENERS AT RS OSS 441.596 0000355851 : MITROVICH, DAVID T - 24-APR-2022 05:33 REMOVED & REPLACED FORMER & FASTENERS REF: E.A TH5720-T0368164 P1.SDR DALA2022042502882None · noneSHIP 3234 CRACKS WERE FOUND AT VARIOUS HOLE POSITIONS IN THE JUNCTION BETWEEN THE FLOOR BEAMS AND VERTICAL STIFFENERS AT Y-765,HOLES 1,2; Y-254,HOLES 1,2; Y254, HOLES 1,2; Y765, HOLES 1,2. CORRECTIVE ACTION: COMPLIED WITH SECTION II OF ERA 597663-14AD. (220836SDR DALA2022042602941Drag Fitting · no indicationSHIP 6821 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 598268-14 REV ORG. CORRECTIVE ACTION: REF ERA 598268-14 REF ORG. (2206939)SDR R61A2022050900331Skin · crackedSUSPECTED CRACK ON RH WING LOWER SKIN OUTBD OF RIB 10. COMPLIED WITH ETD2022-170-014848 WITH REAMING, FABRICATION AND INSTALLATION OF TEMPORARY REPAIR BUSHING ON RH LOWER WING SKIN OUTBD OF RIB 10.SDR DALA2022050303113Drag Fitting · noneSHIP 6821 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 592742-14 REV A. CORRECTIVE ACTION: REF ERA 592742-14AD REV A. (2204473)SDR IPXA2022042981555Bracket · brokenINSPECTION TYPE:CLT WING 3 FLAP I/B EDGE ANGLE BRACKET BROKEN/MISSINGREMOVED AND REPLACED IAW SRM 51-40-21SDR IPXA2022042981554Bracket · brokenINSPECTION TYPE:CLT WING 2 FLAP O/B EDGE ANGLE BRACKET BROKEN / MISSINGREMOVED AND REPLACED IAW SRM 51-40-21SDR 2022F00199Fuel Tank · crackedAIRCRAFT IS CURRENTLY UNDERGOING A C CHECK IN THE HANGAR. WHEN CARRYING OUT NDT INSPECTION AS PER ADSI IB777570073 IN RELATION TO FAA AD 2021-13-10, A CRACK INDICATION OF APPROXIMATELY 0.6 INCHES WAS FOUND ON THE LEFT-HAND WING LOWER WING SKIN FUEL TANK #533ABSDR DALA2022042102797Drag Fitting · noneSHIP 5813 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 590003-14 REV A. CORRECTIVE ACTION: REF ERA 590003-14 REV A. (2202818)SDR ABXA2023050474Splice Plate · corrodedDURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION ON THE LEFT WING FIXED LEADING EDGE UPPER SPLICE PLATE(114T0223-19) FWD OF THE FRONT SPAR. CORROSION IS LOCATED AT APPROXIMATELY WS 450. CORROSION WAS REMOVED BY BLENDING AND MINSDR ASAA2022041838708Skin · noneLESSOR ITEM 727: LEFT HAND WING SPOILER PANEL #1 UPPER REQUIRES FURTHER INSPECTION (UPPER SKIN) GROUNDED - YES. EVALUATED & REPAIRED 1EA AREA ON L/W #1 SPOILER UPPER SKIN LOCATED @ 32" FROM I/B & 10" FROM T/E ZONE A IAW A320 SRM 57-40-00, 57-70-00-283-001 ZONESDR SWAA2022050295400Web · crackedLEFT WING TRAILING EDGE TRANSVERSE WEB JUST I/B OF DEFLECTION CONTROL RIB CRACKED / [01] REMOVED LEFT WING TRAILING EDGE TRANSVERSE WEB CRACKED JUST I/B OF DEFLECTION CONTROL RIB AND INSTALLED NEW TRANSVERSE WEB P/N 115A2156U7 IAW SRM 51-40-02-0G-0.;[02] VERIFSDR CALA2022042101026Fitting · crackedB737-57-4-1262, SHEAR FITTING AT STA 540 AND LBL 6.14 IS CRACKED . SUPPORT TASK NSA EMX N/R 00102. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND LBL 6.14 IAW B ENTERED BY UAL INSPECTION U354653 4/18/2022 737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORG. DSDR CALA2022042101025Fitting · crackedB737-57-4-1262, SHEAR FITTING AT STA 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00104. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND LBL 32.40 IAW ENTERED BY UAL INSPECTION U354653 4/18/2022 B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORG. DSDR CALA2022042101021Fitting · crackedB737-57-4-1262, SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00107. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND RBL 32.40 IAW ENTERED BY UAL INSPECTION U354653 4/18/2022 B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORG. DSDR CALA2022042101024Fitting · crackedB737-57-4-1262, SHEAR FITTING AT STA 540 AND RBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00106. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND RBL 15.04 IAW ENTERED BY UAL INSPECTION U354653 4/18/2022 B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORG. DSDR CALA2022042101023Fitting · crackedB737-57-4-1262, SHEAR FITTING AT STA 540 AND RBL 6.14 IS CRACKED . SUPPORT TASK NSA EMX N/R 00105. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND RBL 6.14 IAW B ENTERED BY UAL INSPECTION U354653 4/18/2022 737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORG.DASDR CALA2022042101022Fitting · crackedB737-57-4-1262, SHEAR FITTING AT STA 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00103. REMOVED AND REPLACED SHEAR FITTING AT STA 540 AND LBL 15.04 IAW ENTERED BY UAL INSPECTION U354653 4/18/2022 B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORG. DSDR FDEA202204170981None · noneLH WING LE AT STA OSS441 FORMER CRACKED P/N 114T2170-5 C/W WITH EA H-5720-T0368062P1SDR EE4Y2022041715404Skin Panel · corrodedDURING THE STRUCTURAL INSPECTION PER TASK CARD Nº: 572066-01-1-002 MPD, IT WAS FOUND AT RH WING, T/E FALSE REAR SPAR OVERHANG AREA BETWEEN STA 3592 AND STA 4012 OVERHANG TOP SKIN LOWER SURFACE WITH CORROSION AND LIGHTNING STRIKE ON UPPER SURFACE. THE RESULTINGSDR UIEA2022041400306None · noneRH WING UPPER SIDE BODY SPLICE CENTER WING WBL.95 BTWN. 1, 2 STRINGERS U 10, U7 SKIN FOUND CORRODED AREA DOT 11/ 0013(<P>REMOVED CORROSION FROM RH WING UPPER SIDE BODY SPLICE CENTER WING WBL.95 BTWN. 1, 2 STRINGERS U 10, U7 SKIN. ORIGINAL MATERIAL .200" REMAINSDR DALA2022041902688None · noneSHIP 698 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 598549-14AD REV ORG . CORRECTIVE ACTION: REF ERA 598549-14 REV ORG. (2198007)SDR DALA2022041902687None · noneSHIP 698 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 598620-14AD REV ORG. CORRECTIVE ACTION:REF ERA 598620-14AD REV ORG. (2197981)SDR UIEA2022041200292Skin · brokenBROKEN - SKIN AND CAP, RH WING INBD AILERON TE WEDGE OUTBD END(<P>1. PERFORM REPAIR OF RH WING INBD AILERON, PLEASE REFER THE JOB CARD ATTACHING SHEET FOR THE DETAILED REWORKING INFORMATION. 2. CONDITION CHECK IS SATISFACTORY</P>)SDR REXA2022050300796Lug · damagedRH AILERON LUG MARKED "C" HAS DAMAGE TO BORE. CA: REPAIRED BORE AND REPLACED BUSHING IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25.SDR REXA2022050300793Lug · damagedLH AILERON LUG MARKED "F" HAS DAMAGE TO BORE. CA: REPAIRED BORE AND REPLACED BUSHING IAW BOMBARDIER REO 670-57-61-237 REV -- DATED 2017-07-25.SDR DALA2022041802648None · noneSHIP 5815 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589466-14 REV A. CORRECTIVE ACTION: REF EAR 589466-14 RAV A. (2193734)SDR DALA2022041802642Skin · damagedSHIP 5815 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589334-14 REV A. CORRECTIVE ACTION: REF ERA 589334-14 REV A. (2193766)SDR UIEA2022041000286Static Line · damagedLEFT O/B AILERON WITH STATIC DISCHARGE DAMAGED(<P>REMOVED AND REPLACED DAMAGED DAMAGED STATIC DISCHARGER AT L/H O/B&; AILERON PER B767-300; 23-61-01-022-008 AMM 23-61-01-402-013. PERFORMED STATIC DISCHARGER RESISTANCE TEST AS PER 767-300 AMM 23-61-01-732-SDR SWIA202265368None · dentedDENT #4 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS12.50- ROOT OF WINGLET REQUIRES DAMAGE EVALUATION AND ALLOWABLE DAMAGE MAPPING. (FILEED - CLOSED) EVALUATED DENT #4 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS12.50- ROOT OF WINGLET AND FOUND DENSDR SWIA202265367None · dentedDENT #3 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS21.75-WGLTS12.50 REQUIRES DAMAGE EVALUATION AND ALLOWABLE DAMAGE MAPPING. (FILED - CLOSED) EVALUATED DENT #3 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS21.75-WGLTS12.50 AND FOUND DENT TO BE OUT OSDR SWIA202265366None · dentedDENT #2 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS31.25 - WGLTS21.75 REQUIRES DAMGE EVALUATION AND ALLOWABLE DAMAGE MAPPING. (FILED - CLOSED) EVALUATED DENT #2 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS31.25 - WGLTS21.75 AND FOUND DENT TO BE OUSDR SWIA202265365None · dentedDENT #1 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS40.50-WGLTS31.25 REQUIRES DAMGE EVALUATION AND ALLOWABLE DAMAGE MAPPING. (FILED - CLOSED) EVALUATED DENT #1 ON L/H WINGLET INBOARD SKIN PANEL BETWEEN WGLTS40.50-WGLTS31.25 AND FOUND DENT TO BE OUT OF SDR CALA2022041400967Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX 00104. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 54.60 U354653, 04/11/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00104 IAW B737-800 SRM 51-40-02 AND BACSDR CALA2022041400966Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX N/R 00103. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 40.87 U354653, 04/11/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00103 IAW B737-800 SRM 51-40-02 ANDSDR CALA2022041400965Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00102. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 U354653, 04/11/2022. DATA WAS TRANSCRIBED FROM NSA EMS N/R 00102 IAW B737-800 SRM 51-40-02 ANDSDR CALA2022041400964Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX 00101. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 15.04 U354653, 04/11/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWG 1SDR CALA2022041400963Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX 00100. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 U354653, 04/11/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00100 IAW B737-800 SRM 51-40-02 AND BAC DSDR CALA2022041400962Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX N/R 00099. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 54.60 U354653 04/11/2022.DATA WAS TRANSCRIBED FROM NSA EMX N/R 00099, IAW B737-800 SRM 51-40-02 AND SDR CALA2022041400961Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 40.87 IS CRACKED. SUPPORT TASK NAS EMX 00098. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 40.87 U354653, 04/11/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00098 IAW B737-800 SRM 51-40-02 AND BACSDR CALA2022041400960Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00097. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 U354653, 04/11/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00097 IAW B737-800 SRM 51-40-02 ANDSDR CALA2022041400959Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00096. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL15.04 U354653, 04/11/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00096 IAW B737-800 SRM 51-40-02 AND SDR CALA2022041400958Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND LBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00095. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 6.14 U354653, 04/11/2022. DATA WAS TRANSCRIBED NSA EMX N/R 00095, AND IAW B737-800 SRM 51-40-02 AND BSDR REXA2022051300887Hinge Fitting · damagedL/H AILERON HINGE FITTING, FOUND LUG MARKED "C" TO HAVE DAMAGE TO LUG REPAIRED LUG MARKED "C" IAW BOMBARDIER REO 670-57-61-107 REV B DATED 2019-01-14SDR REXA2022051300886Hinge Fitting · damagedL/H AILERON HINGE FITTING, FOUND LUG MARKED "C" TO HAVE DAMAGE TO LUG REPAIRED LUG MARKED "C" IAW BOMBARDIER REOCENTER HINGE ASSY 670-57-61-107 REV B DATED 2019-01-14SDR YENA2022041200362None · noneDURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE OVERHANG LOC. AT LEVEL RIB 15 ON LH WING (CPCP RELATED 572179-01); "EVALUATED REWORK AREA TRAILING EDGE OVERHANG LOC. AT LEVEL RIB 15 +7 INCH ON LH WING AND FOUND OUT OF LIMITS IAW SRM 57-21-11-283-007 TABLE 00SDR YENA2022041200361None · noneDURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE OVERHANG LOC. AT LEVEL RIB 15 ON LH WING (CPCP RELATED 572179-01); EVALUATED REWORK AREA TRAILING EDGE OVERHANG LOC. AT LEVEL RIB 15 +7 INCH ON LH WING EN FOUND OUT OF LIMITS IAW SRM 57-21-11-283-007 TABLE 002 SDR CALA2022040800936Access Panel · missingINSPECTION ACCESS PANEL MISSING RT WING LEADING EDGE SLAT MECHANISM LUBRICATION ACCESS DOOR 621XB ITEM PLACED ON CDL MISSING PLACED ON CW CDL OK TO CONTINUE DISPATCH DESK:LEADING EDGE SLAT MECHANISM LUBRICATION ACCESS DOOR 621XB - CDL 57F UPDATE REPLACED MISSISDR COEA2022060206911Flange · noneWO 235607 NR 500022 HEAVY CHECK COE/MAJOR REPAIR: L/H WING REAR SPAR LOWER SURFACE FLANGE AT RIB 8, UPPER FITTING INBOARD HOLE HAS A FLAW INDICATION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0158358_01...18954 ISSUE A, DATED 5/13/2022.
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