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 96ZZZM391Spar Web · crackedDURING D-CHECK, FOUND VERTICAL WEB ATTACHED TO FRONT SPAR FSS 106.8 CRACKED AT 3 PLACES, SEEN THROUGH ACCESS PANEL 6402. RENIVED FASTENERS PER SRM 51-30-2. STOP DRILLED CRACKS PER SRM 51-10-1. INSTALLED WEB REPAIR PER SRM 51-10-1. INSTALLED WEB REPAIR PER SDR RAAAB295013Spar Cap · corrodedDURING SCHEDULED 6C CHECK PER CARD 22004, FOUND RT WING CORRODED ON FORWARD SPAR UPPER CAP AT WS 290. REPAIRED IAW BOECOM MSG 7272-95-0834, DATED FEBRUARY 13, 1995. (X)SDR UPS202622Spar Chord · corrodedWHILE IN "D" CHECK MAINTENANCE FOUND CORROSION ON RT WING LWR AFT SPAR CHORD BS 870, RT WING STA 102-114. INSTALLED REPAIR PER SRM 51-30-2.SDR UPS202618Spar Chord · crackedWHILE IN "D" CHECK MAINTENANCE FOUND CRACK ON UPPER SPAR CHORD RT WING BS 870, WS 71-73. INSTALLED REPAIR PER UPS EO B727-5710-6737A, B727-5710-6722A.SDR 95ZZZW530Spar Cap · corrodedLEVEL 2 CORROSION RT WING LEADING EDGE UPPER AT FRONT SPAR CAP ATTACH FLANGE HAS CORROSION AROUND SCREW HEADS OUTBOARD OF NR 4 PYLON FROM APPROXIMATELY XFS 503 TO XFS 710. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1.SDR DLL16951404Spar Cap · crackedDURING HMV COMPLYING WITH AD 93-17-10 AND 94-05-01, CRACKS WERE FOUND IN THE RIGHT WING REAR SPAR UPPER CAP FASTENER HOLES AT IWS 293.58 AND IWS 346.109. THE HOLES WERE OVERSIZED TO REMOVE THE CRACKS. REPAIR APPROVAL PER FAA AMC LETTER DATED 3/13/95.SDR 95ZZZW319Spar Cap · corrosionDURING D-CHECK, LT WING LOWER LE SPAR CAP HAS CORROSION UPPER SURFACE 10 INCHES AND 30 INCHES O/B OF NR 3 LE SLAT ACTUATOR IN TWO PLACES. REMOVED CORROSION IAW SRM 51-10-6, MATERIAL LOSS .040 AND .050. CORROSION GRIND OUT ON UPPER SURFACE IS WITHIN LIMITS PESDR 95ZZZW318Spar · corrodedDURING D-CHECK, LT WING LOWER LE SPAR HAS EXFOLIATED CORROSION LOWER SURFACE 15 INCHES O/B OF NR 1 LE SLAT ACTUATOR. REMOVED CORROSION PER SRM 51-10-6 MAX DEPTH REMOVED .070 OUT OF LIMITS. ALODINE AND PRIMED AREA PER SRM 51-10-2 AND INSTALLED REPAIR 7075-T6 SDR 95ZZZW317Spar · corrodedDURING D-CHECK, LT WING LE LOWER SPAR CAP HAS CORROSION UPPER AND LOWER SURFACE 53 INCHES TO 60 INCHES O/B OF I/B END (JUST O/B OF NR 3 LE FLAP ACUTATOR MOUNT AND PREVIOUS GRIND OUT). REMOVED FASTENERS PER SRM 51-30-2, REMOVED CORROSION PER SRM 51-10-6 AT 43 SDR 95ZZZW316Spar Cap · corrosionDURING D-CHECK, LT WING LE LOWER SPAR CAP LOWER SURFACE HAS EXFOLIATED CORROSION AFT OF NR 3 LE SLAT ACTUATOR AT 6 INCHES I/B OF ACTUATOR MOUNT BRACKET. REMOVED DAMAGED SECTION, FABRICATED NEW SPAR CAP, INSTALLED NEW SECTION PER SRM 51-40-4 AND 51-10-1, MATERSDR 95ZZZW315Spar Chord · corrodedDURING D-CHECK, R/W FRONT SPAR LOWER CHORD CORRODED AT WS 383.0. REMOVED CORROSION PER SRM 51-10-6. CORROSION OUT OF LIMITS .093 REMOVAL PER SRM 51-20-1 FIG E. CUT OUT SPAR CHORD FROM WS 386 PER SRM 51-10-1, SPLICED IN NEW SECTION 24 INCHES PER SRM 51-40-4.SDR DL72S951054Spar Stifner · crackedFOUND ON CV 2 CHECK 1 INCH CRACK IN LEADING EDGE SPAR STIFFENER AT NR 7 SLAT O/B TRACK O/B ANGLE. REPAIRED AND REPLACED STIFFNER PER M/M 57-20-21 PG 813.SDR USAA950296Spar · corrodedPIT - DURING SCHEDULED Q-1 INSPECTION, FOUND CORROSION LEFT WING AFT LOWER SPAR, LOWER FLANGE STATION XRS 546. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 57-09 FIG 11. (W)SDR 95ZZZW207Spar · corrodedCENTER TANK (WING) TOP AFT SPAR FLANGE (CAP) HAS LEVEL II CORROSION ON TOP OF HORIZONTAL FLANGE AROUND FASTENER HEADS AT BL 23L FS 857 REF N/R NR 5086.SDR UPS202249Spar Chord · crackedDURING 'C' CHECK, MAINTENANCE FOUND REAR SPAR BULKHEAD CHORD HAS A CRACKED ANGLE ON THE RT SIDE AT F/S 1342, RBL 16. REPLACED ANGLE PER BOEING DRAWING 65-19104 AND SRM 51-10-1, 51-30-2.SDR ABXA9500160Spar · crackedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND THE RIGHT WING REAR SPAR CRACKED AT INBOARD LOWER HOLE FOR INBOARD FLAP HINGE. REPAIRED ANGLE IAW ABX REA D957-10642-SB.SDR ABXA9500210Spar Cap · corrodedDURING C-CHECK INSPECTION, FOUND RIGHT WING REAR SPAR LOWER T-CAP HAD LEVEL II CORROSION AT WING TIP. REPAIRED IAW ABX REA D957-11076-MR.SDR 95ZZZW417Spar · corrosionDURING D-CHECK, THE LT WING SPAR LOWER CHORD CORRODED FROM FS 188 TO 203. REMOVED CORROSION PER SRM 51-10-6. INSTALLED DOUBLER REPAIR PER SRM 51-40-4 FIG 1. REPAIR SIZE 2 INCHES BY 14 INCHES. TOTAL CYCLES 29235.SDR 95ZZZW255Spar Flange · corrodedLEVEL 2 CORROSION, RTT WING NR 3 AUX TANK LOWER SURFACE FRONT SPAR ATTACH FLANGE HAS AREAS OF BULGING CORROSION. REMOVED CORROSION, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 57-2-1.SDR DL72S950454Stiffener · crackedFOUND ON F1 LETTER CHECK, 1. 3 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NBR 7 SLAT INBD TRACK INBD ANGLE LOWER END 2. 3 IN CRACK IN WING FWD SPAR VERTICAL STIFFENER AT NBR7 SLAT INBD TRACK OUTBD ANGLE LOWER END, REPAIRED PER MM 57-20-21 PG 813.SDR ABXA9500189Spar Cap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR TEE CAP AT STATION XRS 494.5. REPAIRED LEFT WING LOWER SPAR CAP IAW ABX REA D957-10793-MR.SDR ABXA9500185Spar Cap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING REAR SPAR LOWER TEE CAP FROM XRS 509 TO XRS 563. REPAIRED RIGHT WING REAR SPAR IAW ABX REA D957-10641-MR.SDR 95ZZZX1112Spar · corrodedRIGHT WING AFT SPAR AT ATTACH POINT CORRODED. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA THROUGH WHEELWELLS AT EACH 100-HOUR OR ANNUAL. REMEMBER, THESE ACFT ARE GETTING OLD. THE TIME ON THE SPAR IS BETWEEN 4-6,000 HOURS.SDR 95ZZZX1144Spar · damagedWHILE PERFORMING 5-YEAR WING BOLT INSPECTION, NOTED FORWARD LOWER RT WING BOLT/NUT WAS INSTALLED BACKWARDS. LOGBOOKS REVEALED BOLT INSTALLED 5 YEARS PREVIOUSLY BY A BEECH SERVICE CENTER AND TORQUE CHECKED AT ANOTHER BEECH SERVICE CENTER AND NUMEROUS 150-HOUR SDR ABXA9500177Spar · corrodedDURING C-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LOWER FLANGE OF THE RIGHT WING LOWER REAR SPAR FROM XRS 488 TO XRS 560. REPAIRED RIGHT WING LOWER REAR SPAR IAW ABX REA D957-10795-MR.SDR ABXA9500196Spar Cap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE RIGHT WING LOWER SPAR CAP BETWEEN XRS 387 AND XRS 395. REPAIRED RIGHT WING REAR LOWER SPAR CAP IAW ABX REA D957-10715-MR.SDR SWAA950075Spar · corrodedDURING SCHEDULED TRANSITION CHECK, FOUND RIGHT WING SPAR UPPER SURFACE AT WS 500 JUST AFT OF FRONT SPAR CORRODED. REPAIRED PER TRAMCO EWO 95-0051.SDR EIAA9503Spar Cap · corrodedDURING C-CHECK INSPECTION, FOUND CORROSION ON RIGHT UPPER REAR SPAR CAP AFT FLANGE XRS -133 TO -137. CORROSION BLENDOUT EXCEEDED DC9 SRM LIMITS. THE BLENDED AREA WAS TEMPORARILY REPAIRED USING 7075-T6 DOUBLERS, ANGLES AND FILLERS INSTALLED WET WITH SEALANT. SDR 95ZZZX1248Spar · corrosionSEVERE CORROSION ON REAR SPAR RT WING AT AFT END OF NACELLE. THIS REPAIR REQUIRED A DER AND 337 FOR MAJOR REPAIR AT WS 119.29 - WS 133.29 AND 8110-3.SDR ABXA9500199Spar · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR FROM STATION XRS 488 TO XRS 520. REPAIRED LEFT WING LOWER REAR SPAR IAW ABX REA D957-10692-MR.SDR DL72W950280Frame · damagedDURING HMV, FOUND THE RT UPLOCK FRAMES AT STA 910 AND 913 HAVE TEMPORARY REPAIRS. REPAIRED PER MM 53-11-0.SDR ABXA9500176Spar · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION ON THE LEFT WING LOWER REAR SPAR CAP BETWEEN XRS 385 AND XRS 390. REPAIRED LEFT WING LOWER REAR SPAR CAP IAW ABX REA D957-10773-MR.SDR 95ZZZX593Spar · bentUPON 100-HOUR INSPECTION, FOUND WING SURFACE DISTORTED, SKINS CREASED ON LOWER SURFACE WS 93.00 AT MAIN SPAR. REMOVAL OF SKIN REVEALED LOWER SPAR CAP BENT, SPAR WEB CREASED AND RIBS DAMAGED. CAUSE UNKNOWN. SPAR CAP TOO WEAK AT JACK POINTS.SDR 95ZZZW76Spar · corrodedLEVEL 2 CORROSION - ON RT WING NR 3 AUX TANK LOWER SURFACE FRONT SPAR ATTACH FLANGE HAS AREAS OF BULGING.SDR TSAA9557022Spar Web · corrodedDURING HEAVY MAINTENANCE VISIT, CORROSION FOUND UNDER NR 5 SLAT ACTUATOR ATTACH FITTING FRONT SPAR WEB AT FSS 433. REPAIRED PER ECO 2132R2. AIRCRAFT RETURNED TO SERVICE. (Z)SDR ABXA9500188Spar Cap · corrodedDURING D-CHECK ACCEPTANCE INSPECTION, FOUND CORROSION BLEND OUT THAT EXCEEDED THE SRM LIMITS. LEFT WING REAR SPAR AT APPROXIMATELY WING STATION XRS 515. REPAIRED LEFT WING REAR SPAR TEE CAP IAW ABX REA D957-10701-MR.SDR 94UAL747083Spar Chord · corrodedAT APPROXIMATELY, BS 1000, LBL 80 - 84, AN AREA OF CORROSION WAS DISCOVERED ON THE WING CENTER SECTION FRONT SPAR INSTALLATION. THE CORROSION (LEVEL 2) EXISTED ON LOWER CHORD (P/N 65B 08234-2) AND REQUIRED MATERIAL REMOVAL THAT EXCEEDED MAX ALLOWABLE LIMITATI
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