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 = '5711' 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 = '5711' 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 AWXA200500530Spar · corrodedSAL - MAJOR REPAIR - DURING C-08 CHECK CORROSION WAS FOUND ON LT ACTUATING CYLINDER HOLES 52, 53, 55, 57, 59, 61, & 66. MAINTENANCE REPAIRED DAMAGE BY REWORKING LT ACTUATING CYLINDER HOLES PER AIRBUS REPAIR INSTRUCTION R572-58325 ISSUE D AND ER 26-5700-05121-SDR DHL2005741536Spar · corrodedLEFT WING REAR SPAR WBL124 CORROSION AT ATTACH CLIP TO LOWER SPAR (FWD OF APU BOTTLE DISCHARGE LINE). REMOVED AND RERPLACED T FITTING P/N 65-16201-185 PO NR 3348293 IAW B727 SRM 51-30-2 AND 57-10-2 FIG 3.SDR SFO2005F00000Spar · crackedDURING ANNUAL INSP, CRACKS WERE NOTED IN FWD CARRY-THRU SPAR WEB. LOCATED AT LT UPPER OB MOST HUCK BOLTS (2 EA) ON FWD SIDE OF CARRY-THRU ASSY. HEAD SIDE OF UPPER HUCK BOLT IS INACCESSIBLE FOR VIEWING WITHOUT WING REMOVAL. LWR HUCK BOLT IS ACCESSIBLE, NO MOSDR QXEA200500703Spar · chafedPDX - LEFTHAND WING FORWARD SPAR LOWER FLANGE IS CHAFED AT WING STATION YW 48.000. REPAIRED IAW RD 8-57-811.SDR QXEA200500702Spar · chafedPDX - LEFTHAND WING FORWARD SPAR LOWER FLANGE IS CHAFED AT WING STATION YW130 - YW138. REPAIRED IAW DHC-8 200 SRM 51-40-11 AND RD 8-57-1150.SDR 05FDEA00970Spar · corrodedRT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE ACTUATOR HOLE EVIDENT OF CORROSION. CORROSION REMOVED & FOUND I/B AND O/B LUG HOLES EXCEED LIMITS AS PER CMM 57-44-09.SDR 05FDEA00969Spar · corrodedRT WING O/B FLAP O/B REAR SPAR MOUNTED HINGE LWR MOUNT EVIDENT OF CORROSION. CORROSION REMOVED & FOUND I/B AND O/B BOLT HOLES EXCEED LIMITS AS PER CMM 57-44-09.SDR 05FDEA00967Spar · corrodedRT WING O/B FLAP I/B REAR SPAR MOUNTED HINGE ACTUATOR HOLE HAS EVIDENCE OF CORROSION. CORROSION REMOVED & FOUND I/B & O/B LUG HOLES EXCEED LIMITS PER CMM 57-44-08.SDR UPS05844301Spar · crackedINSPECTION TYPE: C2, FOUND POSSIBLE CRACK JUST I/B OF XCW 46 ON LOWER FRONT SPAR CAP VERTICAL ANGLE INSIDE RT CTR FUEL TANK. NDT VERIFIED CRACK APPROX 3 INCH LONG PER NDTSPM 06=10-01.001. CRACK RUNS FROM FASTENER HOLE TO FASTENER HOLE. REPAIRED CRACK IAW DCSDR 0500489611Spar Cap · crackedDURING M-CHECK FOUND CRACK IN RT WING REAR SPAR CAP AT XRS 267. REPAIRED PER EA 96-201450.SDR 05FDEA00709Spar Cap · corrodedRIGHT HAND WING UPPER REAR SPAR CAP FOUND CORRODED AT XORS= 980 ARC7413-2. CARRIED OUT AS PER FEDEX EA 1-5710-82938.SDR DHL2005740531Spar · crackedRT WING TRAILING EDGE FALSE SPAR HAS A TWO INCH CRACK JUST INBD OF NR 6 FLAP TRACK WBL 202 WING STA 330.5. REMOVED AND DISPLACED R/WING LOWER T/EDGE PANELS AS REQUIRED FOR ACCESS IAW B727 SRM 51-30-2. CUT OUT AND REMOVED 52" SECTION OF CRACKED AUX SPAR LWR CSDR UPS05844291Spar · crackedINSPECTION TYPE:C2 POSSIBLE CRACK BETWEEN VERTICAL FASTENERS ON RT WING REAR SPAR LOWER T-CAP RIGHT W/W STA 857 RBL 28-32. NDT DETECTED A 4 INCH CRACK PER NDT SPM 06-10-01.001. STOP DRILLED CRACK PER DWG SRO8570009. REPAIRED REAR SPAR LOWER T-CAP PER DWG SRSDR A6WA200540121Spar · misdrilledDUE TO HOLES SPACING ON RT LOWER WING SPAR AT WS 148, JOINT STRAP 601R100465-4 S/B CANNOT BE INSTALLED IAW SB 601R-57-037. REPAIRED RT WING SPAR AT WS 148, SHIFTED CUTLINE ON T/E RT WING AT WS 148. FABRICATED A NEW DOUBLE JOINT STRAP OUT OF 2024-T3.050 PO NRSDR IXXA0500158SSpar Cap · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE HAS CRACK DAMAGE BETWEEN STA XFS -6 CAP. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS. REMOVED CORROSION FROM SLANT PANEL UPPER CAP AND FOUND OUT OF LIMITS. CLEANED, TREATED SDR IXXA0500137SSpar Cap · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE CRACKED BETWEEN STA XFS-6 CAP. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND CORROSION FROM SLANT PANEL UPPER CAP. FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED AREA. SDR IXXA0500123SSpar Cap · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE CRACK DAMAGE BETWEEN STA XFS-6 CAP. MAJOR REPAIR ACCOMPLISHED BY REMOVING FASTENERS. REMOVING CORROSION FROM SLANT PANEL UPPER CAP AND FOUND OUT OF LIMITS. CLEANED, TREATED ANSDR DHL2005805513Frame · crackedLT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500, XFS 597.500. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP DRILL ON CRACK END AND FABRICATED (2EA) ANGLE DOUBLERS (AL7075-T6 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA ANDSDR DHL2005805511Frame · crackedLT OUTER WING INBOARD L/E UPPER FORMER CRACKED 0.500, XF 665.000. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLERS (AL7075T6 0.032) (2EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANSDR EIA2005021Spar · corrodedRT WING FWD T-CHORD CORRODED AT WSS 1336 FSSO 1349.0 LOWER T-CHORD. REPAIRED RIGHT WING FWD SPAR T-CHORD AT WS 1336 (FSSO 1349.0) LOWER CHORD PER ECRA 471-57-242-2.SDR EIA2005019Spar · crackedLEFT WING, FWD SPAR, LWR CHORD HEAVY CORROSION AND CONFIRMED CRACK AT FSSO 1410. REPAIRED LEFT WING, FWD SPAR LOWER CHORD AND LOWER WING SKIN FROM FSSO 1370-1410 PER ECRA 471-57-247-2.SDR EIA2005011Spar · corrodedRIGHT WING FWD SPAR AT WS 1485 LOWER T-CHORD CORRODED. REPAIRED THE RIGHT WING FWD SPAR WS 1485 PER ECRA 471-57-238-2P.SDR 05FDEA00308Frame · corrodedLT WING CORROSION FIXED L/E FRAME WEB LWR T-CHORD AT FSS 236.SDR SWAA050475Spar · crackedDURING SCHEDULED D-CHECK, FOUND RT WING REAR SPAR UPPER CHORD AT STATION 223, CRACKED. REMOVED AND REPLACED REAR SPAR SECTION PER ER AND BAC DRAWING.SDR SWAA050474Spar · crackedDURING SCHEDULED D-CHECK, FOUND LT WING REAR SPAR AT STATION 285, 12 O'CLOCK POSITION, CRACKED. REMOVED AND REPLACED REAR SPAR SECTION PER ER AND BAC DRAWING.SDR 200500289Spar · corrodedDURING C-CHECK, FOUND CORROSION ON LEFT HAND WING LOWER FRONT SPAR CHORD. THE MAJOR REPAIR REQUIRED REPLACING 186 INCHES OF THE SPAR CHORD.SDR UPS05443926Fitting · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 6 FOUND CRACKED AT SPLICE FITTING APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.SDR UPS05443925Fitting · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 8 FOUND CRACKED AT SPLICE FITTING APPROX 0.040 INCH. HOLE REWORKED PER BSB 747-57A2314.SDR UPS05443924Fitting · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 NR 4 HOLE FOUND CRACKED AT INTERNAL SPLICE FITTING APPROX 0.060 INCH. HOLE REWORK PER SB 747-57A2314.SDR UPS05443923Fitting · crackedINSPECTION TYPE: C, RT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 5 FOUND CRACKED .125 INCH. HOLE REWORKED PER BSB 747-57A2314.SDR C2XA05TY010Spar · crackedTYS DURING THE ACCOMPLISHMENT OF A NDI TASK(57-28-00) A CRACK INDICATION WAS DISCOVERED. MAINTENANCE FAB`D AND INSTALLED A REPAIR DOUBLER IAW EA5710-01041. AIRCRAFT RETURNED TO SERVICE.SDR 2005FA0000387Spar · crackedDURING A BORESCOPE INSPECTION OF THE REAR WING SPAR, A CRACK WAS FOUND AT THE IB FLAP TRACK ATTACH POINT. PROBABLE CAUSE IS FATIGUE. THIS IS A VERY HIGH TIME AC WITH OVER 13,000 HOURS TT. IT HAS ALSO BEEN USED AS A FLIGHT TRAINER FOR ITS ENTIRE LIFE. (K)SDR 2005FA0000366Spar · crackedDURING A BORESCOPE INSPECTION, A CRACK WAS FOUND IN THE RT REAR SPAR AT THE IB FLAP TRACK ATTACH POINT. PROBABLE CAUSE IS FATIGUE. THIS IS A VERY HIGH TIME, AC WITH OVER 13, 000 HOURS TT. IT HAS ALSO BEEN USED AS A FLIGHT TRAINER FOR ITS ENTIRE LIFE. (K)SDR 2005FA0000389Spar · crackedDURING A BORESCOPE INSPECTION, A CRACK WAS FOUND IN THE RT REAR SPAR AT THE IB FLAP TRACK ATTACH POINT. PROBABLE CAUSE IS FATIGUE. THIS IS A VERY HIGH TIME AIRCRAFT WITH OVER 12,000 HOURS TT. IT HAS ALSO BEEN USED AS A FLIGHT TRAINER FOR ITS ENTIRE LIFE. (KSDR 2005FA0000388Spar · crackedWHILE CHANGING THE FLAP TRACKS ON THE LT WING 2 SMALL CRACKS, .2500 INCH LONG, EACH WERE NOTICED ON THE IB AFT WING SPAR AT THE IB FLAP TRACK ATTACH POINT. PROBABLE CAUSE IS FATIGUE. THIS IS A VERY HIGH TIME AIRCRAFT WITH OVER 12,000 HOURS TT. IT HAS ALSO BSDR 2005FA0000014Spar · crackedDURING PRE-PURCHASE, COMPLIED WITH INSPECTION. BOTH SPARS IN BOTH WINGS WERE FOUND TO HAVE LOOSE AND MISSING NAILS THAT HOLD RIBS OT THE SPARS. SEVERAL LONGITUDINAL CRACKS WERE FOUND. RECOMMENDATION TO OWNER WAS TO REPLACE ALL WOOD SPARS, WITH STC METAL SPASDR IXXA0500205SSpar · crackedDURING ROUTINE C-CHECK COMPLY WITH AD 2001-06-02, INSPECT LOWER FRONT SPAR CAPS. REMOVED FASTENERS AND PHENOLIC FAIRINGS AS REQUIRED TO FACILITATE INSPECTION OF FRONT LOWER SPAR CAPS. PERFORMED HFEC ON LEFT WING NO CRACKS INDICATED. PERFORMED HFEC ON RIGHT WSDR CA050329006Spar · corroded(CAN) UPON ANNUAL INSPECTION, A SKIN DEFORMITY WAS FOUND ON UPPER SPAR OB OF FUEL CELL. RIVETS ATTACHING SKIN TO SPAR WERE DRILLED OUT EXPOSING SEVERE CORROSION OF SPAR CAP. IT WAS DETERMINED FROM THE EXTENT OF CORROSION THE SPAR WAS UNSERVICEABLE. SUSPECTESDR 05FDEA00080Spar Cap · corrodedRT WING, REAR SPAR UPPER CAP AT STA 1044 FOUND WITH CORROSION. REMOVED PER SRM 51-21-01 VOLUME II. COMPLIED WITH FEDEX EA 1-5710-81590SDR AU510001820Spar · corrodedDURING MOD REPAIR, NUMEROUS DEFECTS FOUND RELATING MAINLY TO CORROSION IN WING & ATTACH STRUCTURE. FOLLOWING DEFECTS FOUND, EXFOLIATION OF EXTRUSIONS ON REAR SPAR CAPS IN BOTH W/W. CNTR SECTION OF 1 PIECE WING OPENED UP FOR INSPECT & REVEALED OLD FIBERGLASSSDR UPS05443678Spar · crackedINSPECTION TYPE:C, RIGHT WING UPPER REAR SPAR SIDE-OF-BODY SPLICE PLATE FITTING CRACK FOUND AT HOLE NR 5 RUNNING FWD APPROX 0.060 INCH AND AFT APPROX .125 INCH. PLS REFER ATTACH FIG. HOLE REPAIRED AS PER S/B 747-57A2314.SDR UPS05443674Spar · crackedINSPECTION TYPE:C, RT WING UPPER REAR SPAR SIDE OF BODY SPLICE NR 11 FASTENER HOLE CRACKED AT UPPER SKIN LAYER APPROX 0.060 INCH RUNNING AFT. HOLE REPAIRED AS PER SB 747-57A2314.SDR EIA2005001Spar · crackedLEFT WING AUX SPAR UPPER T-CHORD CRACKED ON INBOARD END. FABBED T-CHORD AND INSTALLED PER ECRA 482-57-116-2.SDR UPS05443677Spar · crackedINSPECTION TYPE:C, LEFT WING UPPER REAR SPAR OF BODY SPLICE FOUND CRACK AT NR 8 HOLE UPPER SPLICE FITTING RUNNING AFT. BOLT HOLE REWORK AS PER S/B 747-57A2314.SDR UPS05443675Spar · crackedINSPECTION TYPE:C, LT WING UPPER REAR SPAR SIDE OF BODY SPLICE FOUND CRACK AT NR 1 HOLE AT SPAR CHORD (REFER FIGURE FOR DETAILS ). HOLE REPAIRED AS PER S/B 747-57A2314.SDR UPS05443673Spar · crackedINSPECTION TYPE:C, LT WING UPPER REAR SPAR SIDE OF BODY SPLICE FOUND CORROSION CRACK AT HOLE NR 4 AT INTERNAL SPLICE FITTING (REFER FIGURE FOR DETAILS ). HOLE REPAIRED AS PER SB 747-57A2317.SDR LJJ2005F00001Spar · corrodedCORROSION FOUND AT HOLE B, LWS 90.35, DURING INSPECTION OF LT S AND K SPAR STRAP. DER WAS CONSULTED FOR REPAIR. RECOMMEND CLOSE INSPECTION OF HOLES DURING REPETITIVE INSPECTIONS. ALSO RECOMMEND THE USE OF ANTI-CORROSION LUBRICANT DURING BOLT INSTALLATION. (SDR 2005FA0000365Spar · crackedWHILE REPLACING THE FLAP TRACK ASSY, A CRACK APPROXIMATELY 2 INCHES IN LENGTH AND RUNNING THROUGH THE LOWER RIVET HOLES WAS FOUND UNDER THE LT IB FLAP TRACK. PROBABLE CAUSE WAS A FLAP OVERSPEED DURING FLIGHT. (SO09200502861)SDR 04FDEA03393Spar · corrodedLT WING OUTBOARD AILERON OUTBOARD SIDE AT APPROX XORS 1048 FOUND CORROSION AT LOWER CHORD REAR SPAR CAVITY. REPAIR CARRIED OUT IAW FEDEX EA 1571081640.SDR 04FDEA03391Spar Cap · corrodedLEFT WING, REAR SPAR AT APPROX XORS 1042 UPP CAP FOUND CORROSION. REPAIRED AS PER FEDEX EA 1-5710-81640.
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