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 99FDEA00312Spar · gougeRIGHT WING AFT SPAR AFT TANG HAS A GOUGE ACROSS THE FLANGE AT XROS 414. COMPLIED WITH EA 8-5710-42395 RT REAR SPAR DEVIATION FROM EO 8-5710-7-30041.SDR ABXA9900666Spar Cap · crackedDURING C-CHECK, FOUND RIGHT WING LOWER REAR SPAR CAP TANG, STATION XRS 267 CRACKED. REPAIRED IAW DC9 SRM 51-30-10 AND ABX REA 957-32858 MR.SDR UPS99230295Spar Chord · corrodedINSPECTION TYPE:C, CORROSION C57-562-02-1B, L/W FWD UPPER SPAR CHORD ON HORIZONTAL FLANGE AT NR 4 SLAT ACTUATOR O/B MOUNT ANGLE. CORROSION OUT OF LIMITS PER SRM 57-10-1. REMOVED SECTION FROM FSS 346-FSS 642 FRONT SPAR TO BE REPLACED ON NRC 934257.SDR CALA9900925Spar · wornINSPECTION FOUND RT WING REFUELING STA WING FRONT LOWER SPAR WORN IN TWO AREAS WHERE ACCESS DOOR LATCHES AT XRS 331. THE WORN AREAS WERE CUT OUT AND REPAIR PARTS WERE INSTALLED IAW SRM 57-06, FIGURE 10.SDR UPS99230294Spar Chord · corrodedINSPECTION TYPE:C C57-562-02-1B, EXFOLIATION CORROSION ON LW FWD UPPER SPAR CHORD AT WS 510.0 (MARKED), NR 3 SLAT AT TAI TELESCOPING DUCT. CORROSION OUT OF LIMITS PER SRM 57-10-1. REMOVED DAMAGE CHORD FROM FSS 346 TO FSS 642. REPLACEMENT CHORD WILL BE INSTASDR AT9900579Spar · crackedDURING SCHEDULED INSPECTION AT TIMCO, TERMINATED TEMPORARY REPAIR OF LT WING AFT SPAR AT XRS 164. REMOVED TEMPORARY REPAIR, INSTALLED PERMANENT REPAIR IAW DOUGLAS DRAWING JO60165.SDR AT9900578Spar · crackedDURING SCHEDULED INSPECTION AT TIMCO, TERMINATED TEMPORARY REPAIR OF RT WING AFT SPAR AT XRS 164. REMOVED TEMPORARY REPAIR. INSTALLED PERMANENT REPAIR IAW DOUGLAS DRAWING JO6016.SDR CALA9900881Spar · crackedINSPECTION FOUND A .5 INCH CRACK EMANATING FROM NR 3 TRANSFER PUMP COVER O/B ATTACHMENT HOLE IN REAR SPAR AT STA XORS 217, RT WING. THE SPAR WAS REPAIRED IAW SRM 57-10-00.SDR 99UAL900404Spar Web · misdrilledDURING ACCOMPLISHMENT OF THE CENTER WING BOX REAR SPAR WEB MODIFICATION AS MANDATED BY AD97-25-15, EIGHTY THREE HOLES WERE MISDRILLED COMMON TO THE REAR SPAR CENTER WEB ACCESS PLATE AND THE REAR SPAR WEB. OVERSIZED FASTENERS OF THE SAME TYPE WERE INSTALLED. SDR AALA991081Spar · corrodedTUL - FOUND LEFT WING, FORWARD LOWER SPAR CHORD HAS CORROSION AT WS 546 WITH PREVIOUS BLEND. INSTALLED DOUBLER PER AARD 53-30-00-02 AND ESO DATED 7/20/99. (M)SDR AU990767Fitting · corroded(AUS) RIGHT WING AFT SPAR FITTING CORRODED.SDR AU990718Cap · corroded(AUS) LEFT FORWARD UPPER SPAR CAP CORRODED. FOUND DURING VISUAL INSPECTION.SDR AU990717Fitting · cracked(AUS) RIGHT AFT SPAR FITTING CRACKED. FOUND DURING FLUORESCENT DYE PENETRANT INSPECTION.SDR AALA991082Spar · corrodedTUL - LEFT FRONT SPAR HAS CORROSION ON LOWER CHORD ANGLE VERTICAL LEG. INSTALLED SPAR CHORD REPAIR DOUBLERS PER SRM 57-10-6. (M)SDR UIEA99053Spar Web · corrodedLEFT WING GEAR WHEEL, SPOT CORROSION FOUND ON CENTER TANK REAR SPAR WEB BEHIND THE BS 1241 LT BULKHEAD FITTING. REF: AD 98-26-23 AND SB 747-57-2263R2. CORROSION REMOVED IAW SB 747-57 2263 REV R2 AND FAX KLM TLS 99-0008H. FORM 8110-3 ISSUED.SDR QXEA9901593Spar · scratchedPDX - THERE IS A 3.5 INCH SCRATCH IN REAR SPAR AT YW RIGHT. REPAIRED IAW DHC8 SRM 51-20-11.SDR DL72S991587Spar · crackedWING CENTER SECTION, REAR SPAR, WEB RBL 10.75 AND LBL 14 CRACK REPAIR. THE CENTER WING REAR SPAR WAS FOUND WITH TWO SMALL TYPICAL CRACKS NEAR THE UPPER SPAR CAP AT RBL 10.75 AND LBL 14.5. THE CRACKS WERE REMOVED WITH A .25 HOLE AND .625 SLOT RESPECTIVELY. TSDR AU990714Spar · corroded(AUS) LEFT AND RIGHT WING UPPER SPARS CONTAINED SEVERE INTERGRANNULAR CORROSION. ON THE LT WING A SECTION OF THE REAR HINGE HAD BEEN REMOVED WITH NO MATERIAL REPLACED. ON THE RT WING A SUSPECT REPAIR HAD BEEN CARRIED OUT WITH A DOUBLER ADDED. SUBMITTER SUSPESDR EIAA990244Spar · crackedHKG - DURIGN C/D CHECK, BS 1241 BULKHEAD FITTING AT RIGHT SIDE, CRACK FOUND OF SPAR WEB AT INBOARD FITTING LEG LOWEST BOLT HOLE. REPAIRED SPAR WEB AND FITTING PER RS-R-53-43-34090 REV B, 8110-3. (M)SDR EIA990247Spar · crackedHKG - DURING C/D CHECK, LEFT WING FOWARD SPAR, WS 670 LOWER CHORD FITTING VERTICAL LEG 2 FASTENER HOLES CRACKED. FASTENER HOLES REPAIRED PER RS-R-57-24-34095, 8110-3. (M)SDR CALA9900808Spar · corrodedINSPECTION FOUND LEFT WING I/B FALSE SPAR UPPER CAP CORRODED O/B OF SPAR INNER MOST END AT XW 158. THE CORROSION WAS REMOVED AND FALSE SPAR WAS REPAIRED IAW ECRA 5722-01004.SDR CALA9900807Spar Cap · corrodedINSPECTION FOUND LOWER SPAR CAP CORRODED AT RT WING O/B T/E AILERON CAVITY AT STA XW 802.5 TO XW 895.5. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5710-01962.SDR 99T64R350ARSpar · crackedRIGHT WING LOWER FORWARD TANG OF FRONT SPAR OUTBOARD OF STATION XFS 515, 3 HOLES CRACKED. REMOVED NUT CHANNEL IAW DC-8 SRM 51-1-21. REAMED HOLES, EDDY CURRENT HOLES, NO DEFECTS. INSTALLED BUSHING IAW BOEING MESSAGE XXX-MEM-99-0007RR. (M)SDR UPS99830209Spar Chord · crackedINSPECTION TYPE:C123, RT WING FWD LWR SPAR CAP, LWR TAG IS CRACKED AT THE FASTENER HOLE AT XFS 17. CUT OUT DAMAGED AREA AND REPAIRED IAW SB 57-30 AND DWG SRO8570012.SDR AU990861Spar · corroded(AUS) LEFT WING SPAR CAP CONTAINED SEVERE INTERGRANULAR CORROSION ON THE VERTICAL FLANGE.SDR 9903436632Spar Web · crackedDURING M-CHECK, RIGHT WING MIDSPAR WEB WAS FOUND WITH CRACKS BETWEEN WS 574 AND 582 AT FASTENER LOCATIONS COMMON TO THE UPPER CHORD. REPAIRED PER EA 66-168586 (P/N 65B17246-4).SDR EIA990268Spar · bentDURING C-CHECK, THE LOWER HORIZONTAL FLANGE OF THE LEFT LOWER REAR SPAR CHORD AT XRS 169 WAS FOUND BENT. REPAIRED BY INSTALLING FILLER PER ECRA 942-57-073-2. (M)SDR QXEA9901462Spar · chafedPDX - INBOARD LOWER SPAR FLANGE HAS CHAFE DAMAGE FROM LOOSE LEADING EDGE. REPAIRED IAW HORIZON AIR EA 8-57-811.SDR AU990699Cap · corroded(AUS) LEFT WING UPPER SPAR CAP CONTAINED EXFOLIATION CORROSION.SDR 99ZZZX3159Spar · crackedINSPECTED SPARS ON LEFT WING AFTER GROUND LOOP. FOUND A COMPRESSION FAILURE ON THE REAR SPAR. COULD NOT TELL CONCLUSIVELY IF FRONT SPAR WAS CRACKED OR NOT. AFTER DISASSEMBLY OF WING, 5 COMPRESSION FAILURES WERE FOUND IN THE AFT SPAR.SDR EIA990214Spar · crackedHKG - DURING C/D CHECK, LEFT WING FRONT SPAR, 2 FASTENER HOLES FOUND CRACKED AT FSSI 688, UPPER AND LOWER CHORD AREA. WEB REPAIRED PER RS-R-21-34097, SB 747-57A2303 FIG 5, 8110-3. (M)SDR 99ZZZX2780Spar · crackedREMOVED UPPER WINGS TO FACILITATE HOPPER REMOVAL. FOUND BOTH LEFT AND RIGHT UPPER WING REAR SPARS CRACKED AT ATTACH POINT IN UPPER RADIUS BETWEEN BOLT HOLE AND UPPER FLANGE OF SPAR. CRACKS ARE APPROXIMATELY .25 INCH LONG AND RAN UNDER MILLED FITTINGS, P/N'S SDR 99ZZZX2779Spar · crackedREMOVED UPPER WINGS TO FACILITATE HOPPER REMOVAL. FOUND BOTH LEFT AND RIGHT UPPER WING REAR SPARS CRACKED AT ATTACH POINT IN UPPER RADIUS BETWEEN BOLT HOLE AND UPPER FLANGE OF SPAR. CRACKS ARE APPROXIMATELY .25 INCH LONG AND RAN UNDER MILLED FITTINGS, P/N'S SDR 99ZZZX2571Rivet · shearedALL RIVETS WERE FOUND SHEARED THAT ATTACH THE REAR WING SPAR ATTACHMENT BRACKETS TO THE REAR CENTER SECTION SPAR. (BOTH LEFT AND RIGHT SIDES). DISCOVERED DURING ANNUAL INSPECTION.SDR DL72W991428Stiffener · crackedTPA LTR CHK B-1, O/B SPAR STIFFENER CRACKED AT NR 3 SLAT I/B TRACK. REPLACED STIFFENER PER M/M 57-20-21 .SDR DLL19991434Stiffener · crackedTHE LBL 30 VERTICAL STIFFENER ON THE CENTER WING FRONT SPAR WAS FOUND CRACKED AT A LIGHTENING HOLE 12 FROM THE UPPER END OF THE STIFFENER. THE UPPER END OF THE STIFFENER WAS TRIMMED OFF AND A NEW SECTION SPLICED IN PER ER/A 367639-14, REV A.SDR EIA990194Spar · crackedHKG - DURING C/D CHECK, LEFT WING REAR SPAR WEB CRACKED AT NR 2 TANK O/B JETTISON PUMP CUTOUT, FASTENER HOLE. WEB FASTENER HOLE REPAIRED PER EO 747-1022-90 REV A PART 2, OVERSIZED TO .341 INCH. (M)SDR 99ZZZX2921Spar · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LEFT WING FRONT SPAR LOWER CHORD PLATE AT WS 400 AND WS 422.SDR TSAA9957315Spar Web · corrodedRT WING FRONT SPAR WEB CORROSION FROM FSS 425 - 433. REPAIRED PER ECO 2970. (M)SDR 99ZZZX2447Spar · corrodedFOUND AFT UPPER SPAR CAP ON RIGHT WING TO BE EXFOLIATED AND CORRODED AT WS 70.340. AFFECTED AREA IS APPROXIMATELY 6-8 INCHES IN LENGTH. OUTBOARD END OF CORRODED AREA SEVERELY BLISTERED AND DISINTEGRATED THROUGH ENTIRE THICKNESS OF SPAR CAP EXTRUSION.SDR UPS99229989Spar Web · corrodedINSPECTION TYPE:C&SI, ON REMOVAL OF CENTER SECTION UPPER CHORD REAR SPAR BS 870, WEB FOUND CORRODED RBL 70.5 TO LBL 70.5. WEB REPLACED IAW SNN MRO EO 99-14-015 UPS ENGINEERING FILE NR 727-51-2060.SDR UPS99229987Spar Chord · corrodedINSPECTION TYPE:C&SI, ON REMOVAL OF CENTER SECTION WEB BS 870 RBL 70.5 TO LBL 70.5 LWR CHORD, REAR SPAR FOUND CORRODED. REPLACEMENT CHORD INSTALLED IAW SNN MRO EO NR 99-14-015 UPS ENGINEERING FILE NR 727-51-2060.SDR DLL10991352Spar · crackedFS 1163 CENTER WING INTERMEDIATE UPPER SPAR CAP WAS FOUND CRACKED IN THE RT OUTBOARD END NEAR RBL 116. REPAIRED PER ERA 367554-14, REV.ASDR AT9900442Spar · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT WING OUTBOARD TRAILING EDGE AFT UPPER SPAR CAP (TOP AND BOTTOM) AT XRS 531.7-560 CORRODED. REMOVED CORRODED SPAR CAP, SPLICED IN A NEW SECTION IAW DC9 SRM 57-09 FIG 24, 51-10-4, 51-10-3, 51-30-2 ANDSDR UPS99229990Spar · corrodedINSPECTION TYPE:C&SI, ON REMOVAL OF FASTENERS CORROSION FOUND ON VERT FLANGE UPPER CHORD REAR SPAR BS 870 CENTER SECTION AT RBL 35 APPROX. UPPER CHORD REPLACED IAW SNN MRO EO 99-14-015 UPS ENGINEERING FILE NR 727-51-2060.SDR 99ZZZX2423Spar · corrodedWIDESPREAD LEVEL 3 CORROSION ON THE RT WING REAR SPAR UPPER CHORD AND WEB AT WBL-78.0.SDR 99T64R265ARSpar · corrodedNR 2841 - LT WING REAR SPAR HAS 4 EACH AREAS OF CORROSION BETWEEN XRS 139-172. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED SPECIAL WASHERS AND DOUBLER, INSTALLED PER EO 99-061 WITH APPROVEDF FAA FORM 8110-3 DATED 6-14-99. REF: ARROW AIR, ARWA. (X)SDR 99T64R345ARSpar · corrodedLT WING AFT SPAR HAS 7 EACH AREAS OF CORROSION AT XRS 190. REMOVED CORROSION, FABRICATED SPECIAL WASHERS AND DOUBLERS AND INSTALLED PER EO 99-061. (M)SDR AU990520Spar · cracked(AUS) WING MAIN SPAR CRACKED IN TWO PLACES ON THE LT SIDE AND IN THREE PLACES ON THE RT SIDE IN THE AREA COVERED BY AD/BN2/62 AND SB BN2/SB237. THE AIRCRAFT STILL HAD 111 CYCLES TO RUN BEFORE THE NEXT AD INSPECTION WAS DUE.SDR CALA9900647Spar · crackedINSPECTION FOUND A 1.5 INCH CRACK IN RT WING DROOPED LEADING EDGE ON INTERNAL SPAR AT STA XORS 317. A REPAIR WAS PERFORMED IAW ECRA 5720-01738.
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