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 EIA2000139Spar · corrodedRIGHT WLG W/W BS 1241 BULKHEAD CORROSION REVEALED AT NR 7, 8, 9, 19 AND 20 RIVETS AREA MATING TO BULKHEAD FITTING. CORROSION REMOVED AND REPAIRED PER EO 57-747-1544-99. (M)SDR EIAA2000123Spar · damagedHAECO-HKG - C6/D-CHECK/PYL MOD - LHW AT FSS 688 UPPER SPAR CHORD FOUND 1 EACH CRACKED FASTENER HOLE AT WEB. OVERSIZED HOLE TO REMOVE CRACK, NDT INSPECTED, FREEZE PLUG INSTALLED PER BOEING MESSAGE EVG-HKG-00-00029H AND HAECO REPAIR SCHEME R57-21-34328. TIME LSDR UPS00832450Spar Cap · corrodedINSPECTION TYPE:C2, LEFT WING AUX TANK UPPER SPAR CAP IS CORRODED BEYOND LIMITS AT XFS 20. REPAIRED IAW SRM 57-2-1 FIG 37.SDR AU000340Spar · cracked(AUS) RIGHT LOWER SPAR CAP CRACKED. FOUND DURING EDDY CURRENT INSPECTION IAW AD/ACSNOW/24 (1). DEFECT CONFIRMED BY MPI.SDR SCNA00317Spar · corrodedDURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS IN THE RIGHT WING LOWER SPAR CHORD AT FUELING ACCESS BAY APPROXIMATELY WS 464.5. REMOVED DAMAGED SECTION IAW SRM 513006. FABRICATED 1 LOWER CHORD PLATE FROM 2024 T4 PER SAMPLE, FABRICATED 1 DOSDR QXEA0001188Spar · scratchedYYC- SCRATCHES FOUND IN RADIUS OF LEFT HAND FWD WING SPAR LEADING EDGE AND BETWEEN STATION YW351 - YW490. REPAIRED IAW RD 8-57-1119.SDR SCNA00310Spar · corrodedDURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND OUT OF LIMITS AT RIGHT WING AFT SPAR OUTBOARD OF NUMBER 8 SPOILER ACTUATOR REAR SPAR WEB. REMOVED CORRODED AREA IAW SRM 571004. FABRICATED NEW FILLER IAW SRM 57-10-04 FROM .040 2024 T3. FABRICATED NEW WEB SDR RRXA001914Spar Cap · damagedDURING A MAINTENANCE VISIT FOUND GOUGED HOLES AND ELONGATED UPPER SPAR CAP ON RT WING FRONT SPAR AT STA XFS 454, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 EO NR 00-055 WSDR RRXA001778Spar Cap · damagedDURING A MAINTENANCE VISIT, FOUND GOUGED AND ELONGATED HOLES IN THE RT WING UPPER SPAR CAP AT STA XFS 454, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. OVERSIZED FASTENER HOLES & RE-COUNTER SUNK AND INSTALLSDR 0001731232Doubler · corrodedDURING ''M'' CHECK, FOUND CORROSION ON LEFT HAND WING LEADING EDGE FRONT SPAR LOWER SURFACE SACRIFICIAL DOUBLER. REPAIRED PER EA 12-175599.SDR MWEA00251Spar · misdrilledDOUBLE DRILLED HOLE AT STATION XRS 189 LEFT WING FORWARD UPPER SPAR. FABRICATED AND INSTALLED PLUG.SDR EIAA2000094Spar · damagedEAC-MZJ - C6/D-CHECK - EXISTING FRONT SPAR WEB REPAIR AT APPROX FSS 695 - FSS 713, RT WING L/E INTERFERRED WITH ACCOMPLISHMENT OF FRONT SPAR MOD. REPAIRED PER ECRA 479-57-137-2. REMOVED EXISTING TRIPLER, DOUBLER, FILLER AND SHIMS. TRIMMED WEB BETWEEN FSSI 6SDR TWAA0005506Spar · crackedDURING OP 16 MAINT CHECK ON THE RT WING REAR SPAR, A CRACK WAS FOUND IN THE LOWER SPAR CAP AT I/B FLAP SUPPORT FITTING LOWER I/B HOLE, 1.25 INCH LONG. STOP DRILLED CRACK PER DOUGLAS DRAWING JO 60271 NOTE 29. EDDY CURRENT INSP WAS ACCOM PER NDT 51-00-03 AND CSDR UPS00832315Spar Cap · corrodedINSPECTION TYPE:C1 LEFT WING AUX TANK UPPER SPAR CAP CORROSION REMOVAL IS BEYOND LIMITS BETWEEN XFS 116 - 126.25. REPAIRED IAW SRM 57-2-1 FIG 37.SDR AU000382Fitting · cracked(AUS) RT MAIN LANDING GEAR BEAM OUTBOARD SUPPORT FITTING CRACKED. FOUND DURING EDDY CURRENT INSPECTION IAW SB B737-57-1216.SDR 0001546730Spar Cap · crackedDURING L CHECK FOUND CRACK, 39 INCHS O/B OF FUSELAGE SPAR CAP ON RIGHT WING UPPER SURFACE. REPAIRED PER EA 67-175083.SDR CA000329005Spar · corroded(CAN) THE AIRCRAFT WINGS WERE REMOVED FOR A DETAILED INSPECTION AND HEAVY INTERGRANULAR CORROSION WAS FOUND ON THE INBOARD FACE OF THE FUSELAGE REAR SPAR CARRY THROUGH BLOCKS. THE RIGHT SIDE HAD LIGHT CORROSION WHICH WAS DRESSED OUT AND THE LEFT SIDE HAD TO BSDR QXEA0000982Spar · gougedPDX - GOUGES AND EVIDENCE OF FRETTING ON AFT SIDE OF REAR SPAR WHERE RIGHT-HAND NR 5 LIFT DUMPER SPIGOT MOUNTS. REPAIRED IAW HORIZON AIR EA 4-57-370.SDR 0001166730Spar · corrodedDURING L-CHECK, FOUND CORROSION ON RIGHT WING FORWARD SPAR LOWER WEB FS 1380 - 1405. REPAIRED PER EA67-173205.SDR 0001086730Spar · corrodedDURING L-CHECK, FOUND CORROSION ON RIGHT WING, FORWARD SPAR LOWER CAP AT FS 1376. REPAIRED PER EA67-173207.SDR USAA000478Spar · crackedPIT - FOUND 4 INCH CRACK IN LEFT UPPER FORWARD SPAR CAP ENGINE MOUNT, STATION 965 LONG 14 LT, LT ENGINE PYLON. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER EO 5490D056, DOUGLAS DWG SRO 954004 AND 54427. (M)SDR UIEA0015Spar · corrodedSURFACE CORROSION DETECTED CENTER SECTION REAR SPAR LEFT/RIGHT. CORROSION MAPPED, MEASURED, CLEANED AND TREATED BY BOEING FIELD TEAM. ALL WITHIN LIMITS. AREAS OF REWORK ARE; LEFT FASTENERS NR 7, 8, 9, RIGHT FASTERNERS NR 2, 3, 4, 5, 6, 7, 8, 9, 13, 14, 23 ASDR 20000505AP036Spar · corrodedFOUND CORROSION ON WING CTR SECTION REAR SPAR RBL 99, COMMON TO REAR BULKHEAD FITTING AND INBOARD WEB OF LEG TO TWO BOLT HOLES WHILE PERFORMING SB 747-57-2263. CLEANED, TREATED, MEASURED CORROSION. APPLIED FINISH. ALL WITHIN ACCEPTABLE LIMITS. (M)SDR 20000427SH027Spar · crackedA CRACK INDICATION WAS NOTED IN THE LT FORWARD UPPER WING SPAR. THE CRACK INDICATION IS ABOVE THE OUTBOARD HI-LOK AND RUNS SPANWISE. THE INDICATION IS .765 INCH PLUS/MINUS LONG AND IS .3401 PLUS/MINUS ABOVE THE HI-LOK. INSPECTION WAS PERFORMED PER AD 91-25SDR 0001066730Spar · corrodedDURING L-CHECK, FOUND CORROSION ON LEFT WING LEADING EDGE FRONT SPAR WEB AND LOWER CHORD AT FS 1476. REPAIRED PER EA67-175079.SDR TWAA0004813Spar · crackedDURING OP 16 MAINT CHECK, ON THE RT WING, HAD CRACK INDICATION ON WING SPAR CAP AT I/B FLAP HINGE FITTING, STA XRS164, LOWER I/B BOLT HOLE EXTENDED INTO LOWER RADIUS. REPLACED LOWER REAR SPAR CAP PER DOUGLAS DRAWING JO60165 AND MCD-AD-35.SDR DL72L000543Spar · damagedDURING ACCOMPLISHMENT OF S/B 727-57A0182 MODIFICATION SEVERAL FASTENERS HOLES WERE OVERSIZED THROUGH ALL LAYERS OF THE REPAIR. MODIFICATION IS TO THE WING CENTER SECTION REAR SPAR WEB. ER/A 334197-14AD REV A.SDR 0001076730Spar · corrodedDURING L-CHECK, FOUND CORROSION ON FRONT SPAR WEB AT LOWER CHORD, FS 1408-1419. REPAIRED PER EA67-174916.SDR UPS00432191Spar · corrodedINSPECTION TYPE: C, RT WING FRONT SPAR. CORROSION ON FRONT SPAR AT ILES 427. REPAIRED ACCOMPLISHED I.A.W QUERY NOTE N522UP/15/2000,AND APPROVED 8 110-3.SDR UPS00431930Spar · corrodedINSPECTION TYPE: C, RT WING LEADING EDGE. CORROSION ON FRONT SPAR OF LT WING AT ILES 621. REPAIRED IAW QUERY NOTE N522UP/08/2000, AND APPROVED 8110-3SDR UPS00432186Spar · corrodedINSPECTION TYPE: C, LT WING LEADING EDGE. CORROSION ON FRONT SPAR OF LT WING WEB BETWEEN OLES 1543 AND OLES 1562.SDR USAA000359Spar · crackedPIT - FOUND CRACK 1.125 INCH LONG AT STATION 164 LEFT WING AFT SPAR LOWER OUTBOARD FLAP HINGE. REPAIR DOUBLER INSTALLED PER EO 5788D348. (M)SDR 0001156730Spar · corrodedDURING L-CHECK, FOUND CORROSION ON RIGHT WING FRONT SPAR WEB AT FS 1536-1540. REPAIRED PER EA67-173204.SDR 0001096730Spar · corrodedDURING L-CHECK, FOUND CORROSION ON RIGHT WING, FRONT SPAR WEB, ABOVE LOWER CHORD FROM FS 960 - FS 1025. REPAIRED PER EA67-174913.SDR UPS00832114Spar · corrodedINSPECTION TYPE: C 1 RT WING LE. AUX TANK UPPER SPAR HAS HEAVY CORROSION BETWEEN XFS 88.75 AND XFS 167.5 REMOVED AND REPLACED SPAR CAP I.A.W. DWG.5766433 AND SRM. 51-1-20D, 51-1-21SDR UPS00432194Spar · corrodedINSPECTION TYPE: C, RT WING LEADING EDGE. CORROSION ON RT FRONT SPAR WEB AT OLES 1418-1446. REPAIRED I.A.W QUERY NOTE N522UP/10/2000,AND APPROVED 8110-3.SDR UPS00432192Spar · corrodedINSPECTION TYPE: C, RT WING FRONT SPAR. CORROSION ON RT UPPER SPAR SKIN EXTENSION, AT OLES 1395. CORROSION REMOVED I.A.W SRM 51-10-01 AND REPROTECTED I.A.W SRM51-10- 02.REF NRC 44255054 FOR NDT INSPECTION.SDR TSAA0057093Spar · corrodedRIGHT WING FORWARD SPAR LOWER CHORD AND WEB AT FSS 108 AND WBL 355 CORRODED. REPAIRED IAW ECO 3090. AIRCRAFT RETURNED TO SERVICE. (M)SDR ABXA000139Spar · corrodedDURING C CHECK, FOUND CORROSION ON THE LEFT REAR SPAR XA 461. CORROSION REMOVED IAW DC9 SRM 57-09. REPAIRED IAW REA D957-35569MR.SDR AWXA0000102Frame · crackedLEFT WING L/E STA 222 ACCESS AREA 6301 INBD RIB UPPER AFT SIDE HAS CRACK. REMOVED AND REPLACED FORMER IAW 737 SRM 51-30-2.SDR CA000224030Spar · cracked(CAN) DURING FUEL LEAK TROUBLESHOOTING, DAMAGE OBSERVED IN RIGHT WING CAVITY. INVESTIGATION REVEALED CRACKING AT REAR SPAR ATTACH POINT OF NR 3 AND NR 4 FLAP TRACKS. INVESTIGATION IS ONGOING. ATTACH BRACKETS 20-518-003 AND 20-518-02 REPLACED. (X)SDR USAA000477Spar · crackedPIT - FOUND SPAR CAP 1.25 INCH CRACK, LEFT WING AFT SPAR STATION 164 LOWER INBOARD FLAP STUD. INSTALLED DOUBLER PER J9-15-93807 (EO 5788D220). (M)SDR P2EA00061Spar · corrodedSJO - DURING Q-CHECK, FOUND CORROSION ON RIGHT WING FRONT SPAR UPPER CHORD AT FS 562. REPAIRED RIGHT WING SPAR UPPER CHORD BETWEEN FS 544.5 AND FS 588 IAW COOPESA EO COO-3-57-088-00 DATED 2/18/2000. (M)SDR RRXA001685Spar · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LT WING REAR SPAR UPPER SURFACE AT STA XRS 162 TO 163, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED -L- ANGLES FROM 7075-T6 5SDR CA000301007Spar · deformed(CAN) DURING INSPECTION A SMALL DEFORMATION WAS FOUND ON TOP OF THE WING. FOUND AT DISASSEMBLY OF THE MAIN SPAR AT THE STATION 150.5 TO 164. THE WING PANEL AT THE SPAR WAS REMOVED AND SPAR SECTION REPLACED.SDR 20000515SH024Spar · crackedPILOT REPORTED VIBRATION FELT IN THE ACFT AND RT WING TIP TANK TRAILING END COULD BE SEEN ''FLUTTERING'' APPROX 1 INCH IN-FLIGHT. INSP FOUND A CRACK EXTENDING THROUGH THE LOWER SPAR CAP AND UP APPROX 1 INCH INTO FACE OF THE AFT WING SPAR AT STA 132. SEVERAL SDR TWAA0003014Spar · crackedDURING OP 16 MAINT CHECK, RT WING HAD APPROX .375 IN CRACK AT LOWER INBD HOLE ON SURFACE OF REAR SPAR AT INBD FLAP HINGE, STA XRS 164. STOP DRILLED CRACKS PER DAC DRAWING JO 60271. HIGH FREQ EDDY CURRENT ACCOMP PER 51-00-13, PART 6. REPAIRED CRACKED WING SPSDR RRXA000873Spar Cap · gougedDURING A MAINTENANCE VISIT FOUND A GOUGE AT THE SCREW HOLE ON THE LT WING I/B L/E LWR FRONT SPAR CAP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DRILL START SMOOTH AND RETURNED TO SERVICE PSDR 2000UALA00062Spar · crackedDURING INSPECTION PER S/B 727-57A0182 AS MANDATED BY AD97-25-15 ON THE REAR SPAR WEB, RBL 34.00, ONE FASTENER HOLE WAS FOUND CRACKED. FATIGUE THE FASTENER HOLE WAS OVERSIZED UNTIL THE CRACK WAS REMOVED (0.327 IN DIA) AND VERIFIED WITH NDT. THEN OVERSIZED TO SDR 2000ZZZX284Spar · corrodedRIGHT WING REAR SPAR VERTICAL LEG AT STA 267.0 HAS HEAVY CORROSION. REPAIRED BY TRIMMING UPPER CAP BETWEEN XRS 180.1 AND XRS 319.5. NEW SECTION SPLICED IN PER SB 57-179 AND ECRA 941-57-015-2.
Back to JASC 5711