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 CALA2020112001292Fitting · crackedSHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED SPT 5866320. REMOVED CRACKED SHEAR FITTING AND INSTALLED NEW SHEAR FITTING, IAW B737-700 SRM 51-40-02 AND ECRA 5714-01168 REV ORIGINAL.SDR FDEA202011142849Fairing · crackedLEFT WING FLAP FAIRING 571DB FORWARD EDGE IS CRACKED. REPAIRED LEFT WING FLAP FAIRING 571DB FORWARD EDGE, IAW B767 SRM 57-53-70-2R FIGURE 201 AND 51-70-07-0G PARA 5 G.SDR FDEA2020082091936Skin · gougedRIGHT WING LE NR 8 SLAT LOWER SURFACE TE HAS GOUGED. REPAIRED THE NR 8 SLAT LOWER SURFACE IAW SRM: 57-42-02-2R, AND 51-70-10-2R, REPAIR 4. MAJOR REPAIR.
SDR JJBA202008143020Structure · crackedNR 3 LEADING EDGE RT SHOWS EVIDENCE OF CRACK AT NR 8 VORTILON. R & R RT LEADING EDGE NR 3. OPS CHECK SAT.SDR FDEA202007211612Rivet · wrong partDURING AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR ON LEFT WING OUTBOARD MAIN FLAP LEADING EDGE SKIN DOES NOT MEET CURRENT SRM STANDARDS DUE TO INCORRECT RIVET SPACING,CUTOUT ORIENTATION,AND REPAIR PARTS USEDSDR UIEA202002210287Skin · corroded#26E V/C FLAP BULLNOSE EXTERIOR FOUND PITTING.(<P>RHW #26E V/C FLAP BULLNOSE EXTERIOR SKIN DAMAGED AREA REPAIRED IAW SRM 57-43-02-2R-2 REPAIR 2 FIG 201 DETAIL II.</P>)SDR UIEA2020022100288Skin · chafed#7 V/C FLAP BULLNOSE EXTERIOR AREA FOUND CHAFING MARK.(<P>LHW #7 V/C FLAP BULLNOSE EXTERIOR SKIN DAMAGED AREA REPAIRED IAW RI-57-44-13920 REV A</P>)SDR CALA2020021600438Seal · missingPDA 2 FOUND SEAL MISSING FROM INBD EGDE OF OTBD LH FLAP. RPL''D SEAL REF IPC 57-53-10-51 ITEM 100SDR JGVR20200209001Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON ALL AILERON, ELEVATOR, AND RUDDER BALANCE WEIGHTS. REMOVED LEVEL 1 CORROSION ON ALL AILERON, ELEVATOR, AND RUDDER BALANCE WEIGHTS IN ACCORDANCE WITH EMBRAER SB 505-55-A004 REV 5 "MASS BALANCE AND ATTACHMENT PARTS -(INSPECTION)"PARTS SDR DALA2020012900742Paint · damagedBROKEN PAINT AROUND OF FASTENER # 3, 5 AT LH ENG DRAG FTG LH PYLON. CORRECTIVE ACTION: REPAIRED PER ER/A 584777-14AD REV. ORIG., ETI-57-20-003 REV. 6.SDR DALA2020013190740Paint · damaged(AIRCRAFT 5657, L/P 1465992) BROKEN PAINT AROUND THE FASTENERS HEAD # 11 TO 18 AT LH WING DRAG FITTING. CORRECTIVE ACTION: REPLACED PER ETI-57-19-213 REV 11, ER/A 584851-14AD REV. ORIGINAL AND CARD 5720-01100-0101A JOB #015-0001.SDR DALA2020013190739Paint · damaged(AIRCRAFT 5657, L/P 1465937) BROKEN PAINT AROUND THE FASTENERS HEAD # 1 TO 10 AT LH WING DRAG FITTING. CORRECTIVE ACTION: REPLACED PER ETI-57-19-213 REV 11, ER/A 584851-14AD REV. ORIGINAL AND CARD 5720-01100-0101A JOB #015-0001.SDR DALA2020012860644Brace · damaged(AIRCRAFT 5647, L/P 1461537) PREVIOUS TO FASTENERS INSTALLATION OUT OF ROUND CONDITION WAS FOUND ON HOLE # 1, 2, 3, 6, 8, 9 AND 10 AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE. REPAIRED PER ER/A 584777-14AD REV. ORIG. AND ETI-57-20-003 REV. 6.SDR DALA2019122427527Fitting · corrodedLT ENG DRAG FTG CLAMP-UP & DIAG BRACE, STEP 26 CORROSION IN HOLES # 2, 3, 5, 8, AND 9 WAS FOUND. REPAIRED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190 REV 13.SDR ABXR2019112700315Bushing · wornRT WING SUMP DRAIN LEAKING AT BUSHINGSDR 2020F00044Tab · delaminatedNON-ROUTINE CHECK UNSCHEDSDR COEA2019121062804Panel · corrodedWO 197234 NR 57126 HEAVY CHECK HATS/MINOR REPAIR: PANEL 522CT HOUSING HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0107912_01...15404 ISSUE A, DATED 11/1/2019.SDR ASAA2019101131202Beam · crackedPANEL 571CB HAS A CRACK AT THE O/B FLANGE. GROUNDED - YES. REMOVED PANEL 571CB CRACKED T/E BEAM AND REPLACED WITH NEW BEAM IAW 737 900 ER SRM 51 40 02 0G 0 4.SDR CALA2019101101717Fitting · crackedSHEAR FITTING ON CENTER TANK UPPER SKIN AT RBL 40.87 IS CRACKED LP 5865532 SPT REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND DWG NO. 111A 200 REV ORIGINAL DATA WAS TRANSCRIBED FROM NR 5865 532 WORK ACCOMPLISHED BY MECHANIC V899172 INSPECTED SDR SWIA2019092746352Panel · chafedPANEL 599AB CHAFFED IN SEVERAL AREAS (MARKED) (C-CHECK) RO: 09/26/19 ORDERED AND RECEIVED NEW PART. DRILLED AND LOCATED NEW PANEL 599AB IAW SRM.SDR AALA201910039030Anchor Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION JACK ANCHORAGE FITTING BETWEEN RIB 2 AND RIB 3. REPAIRED ANCHORAGE FITTING PER EA 297739.SDR UIEA2019080204921Fairing · damagedRIGHT WING NR 7 CANOE FAIRING 665EB SCREW HOLE FOUND ELONGATED. FABRICATED A NEW CANOE FAIRING 665EB PANEL IAW EO 4457A693 PART 1.SDR DXTA2019060502465Bolt · wornDURING FLIGHT AT FL400 GOT A SEVERE UNKNOWN AIRFRAME VIBRATION. THE VIBRATION WAS FELT THROUGHOUT THE ENTIRE AIRCRAFT. THERE WERE NO ASSOCIATED CAS MESSAGES, NO UNSAVED GEAR INDICATIONS, NO SPOILER DEPLOYED INDICATIONS. THE AIRCRAFT DID NOT LAND OVER WEIGHT. PSDR ABXR2019020400159Strut · corrodedAIR LOAD STRUT CORRODED.SDR SWAA2022030162213Stiffener · crackedCUSTOMER REQUEST. CRACKED STIFFENER L/H663 ;LBL9; WL 152 / REPLACED CRACKED STIFFENER WITH NEW STIFFENER; PART# 7530146 IAW SRM 51-40-05 AND DWG 111A1000. REFERENCE NRC# N182531 FOR INSTALLATION.SDR SWAA2022022830529Support Beam · crackedRT WING LOWER TRAILING EDGE SUPPORT BEAM FOR PANEL 661AB IS CRACKED / REMOVED AND REPLACED RT WING LOWER TRAILING EDGE SUPPORT BEAM FOR PANEL 661AB P/N . 115A3758-10 IAW SRM 51-40-02 AND AIPC 57-50-00-18. 88920U 26DEC18SDR DALA2018112706847Structure · crackedHOLE #45 HAS CRACK INDICATION OUT OF AFT SIDE OF HOLE, APPEARS TO BE AT LEAST .060 IN LENGTH REPAIRED PER ERA 573213-14. (LP 0841629)SDR SWAA2022022844128Angle · crackedP3-LEFT WING MIDSPAN FIXED TRAILING EDGE PANEL LATERAL WEB ANGLE ATTACHED TO DEFLECTION CONTROL RIB IS CRACKED / REMOVED AND REPLACED L/WING MIDSPAN FIXED T/E LATERAL WEB CRACKED ATTACHED ANGLE WITH A NEW P/N 115A6260-1; A-TAG #55194 ANGLE INSTALLED AND CIC APSDR SWAA2018112727117Plate · crackedLT WING LOWER TRAILING EDGE WAFFLE PLATE CRACKED AT FASTENER HOLE. R&R WAFFLE PLATE IAW SRM.SDR SWIA2018120445324Panel · chafedPANEL 599CB IS CHAFED. (C-CHECK) RO: 12/1/18. BLENDED CHAFE DAMAGE FROM PANEL 599CB REF SRM. COMPLIED WITH ALL STEPS OF REO.SDR SWIA2018120445323Panel · chafedPANEL 599BB IS CHAFED. (C-CHECK) RO: 12/1/18. BLENDED CHAFE DAMAGE FROM PANEL 599BB IAW SRM. COMPLIED WITH ALL STEPS OF REO.SDR SWIA2018120445322Panel · chafedPANEL 599AB IS CHAFED. (C-CHECK) RO: 12/1/18. BLENDED CHAFE DAMAGE ON PANEL 599AB IAW SRM.SDR IPXA2018110235577Skin · dentedDENT FOUND ON THE RT WING OTBD AFT FLAP LOWER SKIN NEAR WBL 592. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1, SRM 51-70-10-2R-4, REPAIR 4, AND SRM 51-70-10, REPAIR GENERAL, REV 83.01.SDR COEA2018082103805Bellcrank · corrodedLT WING REAR SPAR BELLCRANK HAD CORROSION AT RIB 21. BELLCRANK REPLACED.SDR SWAA2022021634076Panel · elongatedSUPPLEMENTAL INFORMATION: **DELAY ONLY** L/WING FIXED T/E PANEL HAS 2 EA. ELONGATED HOLES. / REPARIED LEFT WING DEFLECTOR RIBRTS - 1633CSDR DALA2018040602625Door · crackedCRACK ON BUTTE DOOR INBOARD TRAILING EDGE LOWER CORNER LT WING. THE BUTTE DOOR WAS REPAIRED IAW SRM 57-00-00-2R, REPAIR 1.SDR SWAA2022021114795Web · crackedLT WING UPPER T/E PANEL JUST AFT OF #1 PYLON TRANSVERSE WEB IS CRACKED. / REMOVED AND REPLACED LT WING UPPER T/E PANEL AFT OF #1 PYLON TRANSVERSE WEB PER SRM 51-40-02-0G-0; AND DR# 115A2512SDR 2018FA0000029Skin · corrodedLEFT WING LOWER CENTER SKIN CORRODED. REPAIRED IAW ENGINEERING LETTER DQ10596M1.SDR SIMA20180105004Structure · erodedTHE RT NR 2 LEADING EDGE ERODED, AND IS OUT OF LIMITS IN ONE AREA AT ZONE NR 2. REPAIRED DAMAGE IAW ERS EM-55MR-574SDR SWIA201744218Access Panel · corrodedWING ACCESS PANEL IS CORRODED. REPAIRED THE DAMAGE IAW REO.SDR DALA2020111803770Not Reported · corrodedCORROSION IN FASTENER HOLES. CORRECTIVE ACTION: COMPLIED WITH ER/A 563869-14AD AND ER/A 588636-14AD.SDR MTNA2017110103Control Rod · corrodedTRIM TAB CONTROL ROD EXFOLIATED.SDR SWAA2017110617587Fairing · crackedRIGHT WING FAIRING INNER SKIN CRACKED JUST FORWARD OF THE AFT OUTBOARD DRAIN HOLE. REPAIRED THE FAIRING IAW EA AND ER.SDR AALA201710019011Hinge Arm · wornEXCESSIVE PLAY ON FITTING ASSEMBLY FORKED END LOOSE BEARING HINGE ARM 7. REPLACED HINGE ARM PER AMM 55-36-41-0401 AND SRM A319 51-72-11.SDR SWIA2017091943771Unknown · crackedFOUR HOLES WITH DEFECTS. ALL HOLES COLD WORKED AND REPAIRED IAW REO.SDR SWIA2017091943770Unknown · crackedFOUR HOLES WITH DEFECTS. ALL HOLES COLD WORKED AND REPAIRED IAW REO.SDR SWIA2017091943773Structure · dentedLEFT WING LEADING EDGE LWS 185. HAD A SMALL DENT THAT MEASURES .019 INCH IN DEPTH, X .75 INCH IN LENGTH, AND .5 INCH IN WIDTH. COMPLIED WITH DRESS BACK REPAIR TO DENT ON THE LH WING LEADING EDGE IAW REO. LEAK CHECKED GOOD.SDR SWIA201743772Structure · dentedWING STATION 139. HAS A DENT 3/4 INCH WIDE AND .010 INCH DEEP. HAND FORMED THE DENT BACK TO ORIGINAL CONTOUR IAW REO. CHECKED GOOD..SDR UIEA2017091401658Unknown · corrodedBETWEEN BS 852 ABD 871.5 BELOW WL 200, CORRODED. REMOVED DAMAGE AND REPAIRED IAW EA 170287.SDR GTIA2017071202070Seal · tornACFT VIBRATION & LOUD CLICKING FOUND BETWEEN ROW 12 & 13. HEARD & FELT DURING CLIMB & ENROUTE PORTIONS OF FLIGHT. AN ODOR OF BURNING HAIR WAS ASSOCIATED WITH THE VIBRATION. VIBRATION FELT IN THE FLOOR UP TO ROW 3, BUT PRONOUNCED AT 12 & 13 . COMPLIED WITH CO
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