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 UIEA2023060500571Bushing · unknownCORROSION ON BUSHINGS FROM LH MAIN LANDING GEAR SUPPORT BEAM(<P>BUSHINGS WERE REPLACED PER SOPM 20-50-03 AND MXA EO TRE6757193 (CMM 57-54-13 REPAIR 2-1) MAJOR REPAIR. PN: 113T1108-17 AND 113T1108-23</P>)SDR UIEA2023060900626Unknown · unknownCENTRAL FUEL TANK WITH FOAM DEFORMED.(<P>FOAM CENTRAL FUEL TANK CAVITIES 3, 4 AND 125 WERE REPLACED IAW INVICTA-FRS INSTALLATION, B767 SERIES REV 1 01 JUN 18. PN: FF-00405-3079, FF-00405-3078, FF-00405-4012.</P>)SDR UIEA2023060900629Unknown · unknownWING CTR FUEL TANK WITH FOAM DEFORMED.(<P>WING CTR FUEL TANK WITH FOAM DEFORMED WERE REPLACED IAW INVICTA-FRS INSTALLATION, B767 SERIES REV 1 01 JUN 18. PN: FF-00405-6133, FF-00405-6032, FF00405-5132.</P>)SDR DALA2023061204758Unknown · unknownSHIP 680 AD - AWR - DAMAGES WERE FOUND ON LH ENG DRAG FTG AND CLAMP-UP COUNTERSINKS 11-18 AS FOLLOW: COUNTERSINK #11 WORN AREAS BETWEEN 3 TO 4 CLOCK POSITION; COUNTERSINK #12 WORN AREAS BETWEEN 10 TO 11 CLOCK POSITION; COUNTERSINK #13 CORROSION BETWEEN 5 TO 11SDR DALA2023061204757Unknown · unknownSHIP 680 AD - AWR - DAMAGES WERE FOUND ON LH ENG DRAG FTG AND CLAMP-UP COUNTERSINKS 1-10 AS FOLLOW: COUNTERSINK #1 CORROSION BETWEEN 9 TO 12 CLOCK POSITON AND WORN AREAS AT 1 AND 5 CLOCK POSITIONS; COUNTERSINK #2 CORROSION BETWEEN 9 TO 11 CLOCK POSITION; COUNTSDR UIEA2023060900619Unknown · unknownL/H AFT OVERWING EXIT BLANKET WIRING HAS TWO BROKEN WIRES (LINER REMOVED)(<P>REPAIRED WIRES PER WDM 21-45-22-1 AND SWPM 20-10-13.</P>)SDR UIEA2023060900620Unknown · unknownL/W INBD AILERON INBD LWR SEAL IS WORN AT AFT AREA(<P>CLEANED AND REPAIRED WORN SEAL AT LEFT WING INBOARD AILERON I/B LWR SEAL PER B767-300 AMM 52-09-00-358-056. PN: D117</P>)SDR UIEA2023060900621Unknown · unknownR/W INBD AILERON INBD LWR SEAL IS WORN AT AFT AREA .(<P>PREPARED, CLEANED AND REPAIRED WORN SEAL AT RIGHT WING INBOARD AILERON I/B LOWER SEAL PER B767-300 AMM 52-09-00-358-056. NO FURTHER DEFECTS NOTED. PN: D117</P>)SDR CALA2023060901799Skin · corrodedRT WING FWD SPAR WS 527 LOWER HAS SPOT OF CORROSION. REF. BAN N/R 001406187. ACTUAL WS IS 512 (RIB 17). ALL WORK ACCOMPLISHED. PLACED ON DIP TO " PERFORM AN INSPECTION ECRA 5721-01476 ON OR BEFORE NOVEMBER 30, 2024". OF THE R/H LOWER WING SKIN REPAIR IN ACCORSDR 2023FA0000306Unknown · unknownLEFT WINGTIP MADE CONTACT WITH AN ALUMINUM GATE. DAMAGE TO LEFT WINGTIPSDR FDEA202306071016Panel · damagedLH WING-OUTBOARD TOP PANEL HAS SEVERAL MISSING RIVETS COMPLIED WITH EO H-5720-E0353920 A PART: 5 (P5) & PART 6 (P6): WINGS - FIXED TRAILING EDGE UPPER CHORD AT WING STATION 943,1054 AND 1098 - SB 767-57-0136; WHICH CALL FOR BOTH SIDES TO HAVE PARTS REPLACESDR YENA2023060900604Unknown · unknownDURING HEAVY MAINTENANCE: WEAR ON LEADING EDGE LOC. SKIN AT WING ROOT UPPER AREA ON LH WING; REF AEROMAN W/O 2023-11/1 NR 2023-255566. PERFORMED PERMANENT REPAIR LOC. LEADING EDGE SKIN AT WING ROOT UPPER AREA ON LH WING IAW EA# 57-0164-23 PART 1 AND PART 2 ANSDR YENA2023060900598Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / LH WING / FIXED LEADING EDGE / CLOSEOUT RIB ATWFX 365.514 / WEAR DAMAGE AND ELONGATED HOLES - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR TSAA20230606105Unknown · unknownCA 1464/166 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 100.0 AND WBL 102.5. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 100.0 & WBL 102.5. REMOVED 0.001" MATERIAL AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMITS. AREA CSDR TSAA20230606104Unknown · unknownCA 1464/82 RH WING O/B AFT FLAP LOWER SKIN DELAMINATION BETWEEN WBL 245-WBL 249.5. TRIMMED AND REMOVED THE DAMAGE AREA ON RH WING O/B AFT FLAP LOWER SKIN BETWEEN WBL 245 ~ WBL 247.5. MADE THE REPAIR SKIN AND DOUBLER AND CORE. INSTALLED THE REPAIR PARTS AND SDR TSAA20230606100Unknown · unknownCA 1464/298 THE CORROSION WAS FOUND AT LH WING I/B FLAP LOWER PNL 8407, AROUND FASTENER (6EA). ALL CORROSION REMOVED AT LH WING I/B FLAP LOWER PANEL 8407 AROUND FASTENER. REMOVED 0.004" MATERIAL & REMAINING 0.121" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PSDR TSAA20230606099Unknown · unknownCA 1464/297 THE CORROSION WAS FOUND AT LH WING I/B FLAP LOWER PNL 8406, AROUND FASTENER (10EA). ALL CORROSION REMOVED AT LH WING I/B FLAP LOWER PANEL 8406 AROUND FASTENER. REMOVED 0.004" MATERIAL & REMAINING 0.121" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND SDR TSAA20230606098Unknown · unknownCA 1464/296 THE CORROSION WAS FOUND AT LH WING I/B FLAP LOWER PNL 8404, AROUND FASTENER (9EA). ALL CORROSION REMOVED AT LH WING I/B FLAP LOWER PANEL 8404 AROUND FASTENER. REMOVED 0.005" MATERIAL & REMAINING 0.120" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PSDR TSAA20230606097Unknown · unknownCA 1464/293 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN WBL 266.25 AND WBL 266.75. ALL CORROSION REMOVED AT LH WING LOWER SURFACE BETWEEN WBL 266.25 AND WBL 266.75. REMOVED 0.028" MATERIAL AND REMAINING 0.283" IS WITHIN ALLOWABLE LIMIT. AREA CSDR TSAA20230606096Unknown · unknownCA 1464/292 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 468.2 AND W STA 469.0. ALL CORROSION REMOVED AT LH WING LOWER SURFACE BETWEEN WSTA 468.2 AND WSTA 469.0. REMOVED 0.023" MATERIAL & REMAIN 0.149" IS WITHIN ALLOWABLE LIMIT. AREA CLEASDR TSAA20230606095Unknown · unknownCA 1464/291 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 475.0 AND W STA 477.0. CORROSION AT LH WING LOWER SURFACE, BETWEEN W STA 475.0 AND W STA 477.0, REPAIR IAW AIR ASIA EL-737-230503. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01849-001 SDR TSAA20230606094Unknown · unknownCA 1464/290 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 581.3 AND W STA 582.1. CORROSION AT LH WING LOWER SURFACE, BETWEEN W STA 581.3 AND W STA 582.1, REPAIR IAW AIR ASIA EL-737-230503. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01849-001SDR TSAA20230606093Unknown · unknownCA 1464/289 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 477.75 AND W STA 478.25. ALL CORROSION REMOVED AT LH WING LOWER SURFACE BETWEEN WSTA 477.75 AND WSTA 478.25. REMOVED 0.011" MATERIAL & REMAIN 0.139" IS WITHIN ALLOWABLE LIMIT. AREA SDR TSAA20230606092Unknown · unknownCA 1464/288 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 627.5 AND W STA 629.7. CORROSION AT LH WING LOWER SURFACE, BETWEEN W STA 627.5 AND W STA 629.7, REPAIR IAW AIR ASIA EL-737-230503. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01849-001RSDR TSAA20230606091Unknown · unknownCA 1464/287 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN W STA 614.0 AND W STA 617.7. CORROSION AT LH WING LOWER SURFACE, BETWEEN W STA 614.0 AND W STA 617.7, REPAIR IAW AIR ASIA EL-737-230503. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01849-001RSDR TSAA20230606090Unknown · unknownCA 1464/284 THE CORROSION WAS FOUND AT LH WING LOWER SURFACE, BETWEEN WBL 559 AND WBL 560.9. ALL CORROSION REMOVED AT LH WING LOWER SURFACE BETWEEN WBL 559 AND WBL 560.9. REMOVED 0.002" MATERIAL & REMAIN 0.048" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTSDR TSAA20230606089Unknown · unknownCA 1464/269 THE CORROSION WAS FOUND AT #1 SPOILER LOWER SURFACE, RSS 412. ALL CORROSION REMOVED AT #1 SPOILER LOWER SURFACE, RSS412. REMOVED 0.001" MATERIAL & REMAIN 0.019" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE I.A.W. B737-300 SRM 51-10-2 / 5SDR TSAA20230606087Unknown · unknownCA 1464/256 CORROSION AT RH WING I/B MID FLAP UPPER SKIN BETWEEN WBL 83, WBL 111 AND WBL 138. ALL CORROSION REMOVED AT RH WING I/B FLAP UPPER SKIN BETWEEN WBL83, WBL111 AND WBL138. REMOVED 0.001" MATERIAL & REMAIN 0.019" IS WITHIN ALLOWABLE LIMIT. AREA CLEASDR TSAA20230606086Unknown · unknownCA 1464/255 SKIN GOUGE AT RH WING I/B FORE FLAP LOWER SURFACE WBL 99. REMOVED SURFACE FINISH OF GOUGE AREA AT RH WING I/B FORE FLAP LOWER SURFACE WBL 99. FILLED THE DAMAGE WITH FILM ADHESIVE. MADE REPAIR DOUBLER. INSTALLED REPAIR PARTS AND CURED THE BOND. SDR TSAA20230606085Unknown · unknownCA 1464/244 THE DENTS WERE FOUND AT LH WING O/B AFT FLAP LOWER SKIN, BETWEEN WBL 342.64 AND WBL 344.9 (WBL 342.9, L:0.8", W:0.6", D:0.008"),(WBL 343.9, L:0.8", W:0.4", D:0.002"). REMOVED SURFACE FINISH OF DENTS AND DID SURFACE PREPARATION AT LH WING O/B AFT FSDR TSAA20230606084Unknown · unknownCA 1464/243 THE DENT WAS FOUND AT LH WING O/B AFT FLAP LOWER SKIN, WBL 335.4, L:1.2 INCH, W:0.9 INCH, D:0.007 INCH. DENT AT LH WING O/B AFT FLAP LOWER SKIN WBL 335.4, L:1.2", W:0.9", D:0.007" CHECK WITHIN ALLOWABLE LIMIT. I.A.W. B737-300 SRM 57-53-01 ALLOWABSDR TSAA20230606083Unknown · unknownCA 1464/242 THE DENT WAS FOUND AT LH WING O/B AFT FLAP LOWER SKIN, WBL 287.05, L:2.8 INCH, W:2.7 INCH, D:0.070 INCH. REMOVED THE DAMAGE AREA AT LH WING O/B AFT FLAP LOWER SKIN WBL 287.05. MADE THE REPAIR SKIN AND DOUBLER. INSTALLED THE REPAIR PARTS AND PERFSDR TSAA20230606082Unknown · unknownCA 1464/241 THE DENTS WERE FOUND AT LH WING O/B AFT FLAP LOWER SKIN, BETWEEN WBL 276.55 AND WBL 281.05. (WBL 277.55, L:0.9", W:0.8", D:0.018"),(WBL 279.05, L:0.7", W:0.6", D:0.005"),(WBL 280.5, L:1.1", W:0.9", D:0.014"),(WBL 280.8, L:0.7", W:0.4" , D:0.003"). SDR TSAA20230606076Unknown · unknownCA1464/199 SURFACE CORROSION ON CENTER WING EXTERIOR LOWER SKIN BS570 FORM RBL 44 TO RBL 50. CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS570 FORM RBL 44 TO RBL 50, REPAIRED IAW AIR ASIA EL-737-230501. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01840-001)SDR TSAA20230606075Unknown · unknownCA 1464/198 SURFACE CORROSION ON CENTER WING EXTERIOR LOWER SKIN BS645 LBL 47. CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS600, BS640 AND BS645, REPAIRED IAW AIR ASIA EL-737-230502. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01839-003)SDR TSAA20230606074Unknown · unknownCA 1464/197 SURFACE CORROSION ON CENTER WING EXTERIOR LOWER SKIN BS640 LBL44. CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS600, BS640 AND BS645, REPAIRED IAW AIR ASIA EL-737-230502. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01839-002)SDR TSAA20230606073Unknown · unknownCA 1464/196 SURFACE CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS600 LBL 50. CORROSION ON CENTER WING LOWER EXTERIOR SKIN BS600, BS640 AND BS645. REPAIRED IAW AIR ASIA EL-737-230502. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01839-001)SDR TSAA20230606065Unknown · unknownCA 1464/173 CORROSION AT LH WING I/B AFT FLAP UPPER SKIN BETWEEN WBL 88.5 AND WBL 90.5. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP UPPER SKIN BETWEEN WBL 88.5 AND WBL 90.5. REMOVED MATERIAL 0.001" AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMIT. AREA CLEASDR TSAA20230606064Unknown · unknownCA1464/172 CORROSION AT LH WING I/B AFT FLAP UPPER SKIN BETWEEN WBL 84.0 AND WBL 85.5. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP UPPER SKIN BETWEEN WBL 84.0 AND 85.5. REMOVED MATERIAL 0.001" AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN ANDSDR TSAA20230606063Unknown · unknownCA 1464/167 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 116.0 AND WBL 118.0. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 116.0 AND WBL 118.0. REMOVED MATERIAL 0.003" AND REMAINING 0.013" IS WITHIN ALLOWABLE LIMIT. AREA SDR TSAA20230606062Unknown · unknownCA 1464/165 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 92.75 AND WBL 94.05. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 92.75 AND 94.05. REMOVED MATERIAL 0.003" AND REMAINING 0.013" IS WITHIN ALLOWABLE LIMIT. AREA CLEASDR TSAA20230606061Unknown · unknownCA 1464/164 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 87.25 AND WBL 91.25. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 87.25 AND 91.25. REMOVED MATERIAL 0.001" AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMIT. AREA CLEASDR TSAA20230606060Unknown · unknownCA 1464/163 CORROSION AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 86.25 AND WBL 87.25. ALL CORROSION REMOVED AT LH WING I/B AFT FLAP LOWER SKIN BETWEEN WBL 86.25 AND 87.25. REMOVED MATERIAL 0.001" AND REMAINING 0.015" IS WITHIN ALLOWABLE LIMIT. AREA CLEASDR TSAA20230606059Unknown · unknownCA 1464/162 CORROSION AT LH WING I/B EXHAUST GATE LOWER SKIN WBL 183. ALL CORROSION REMOVED AT LH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 183. REMOVED MATERIAL 0.002" AND REMAINING 0.078" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-30SDR TSAA20230606058Unknown · unknownCA 1464/161 CORROSION AT LH WING I/B EXHAUST GATE LOWER SKIN WBL 169. ALL CORROSION REMOVED AT LH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 169. REMOVED MATERIAL 0.002" AND REMAINING 0.078" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-30SDR TSAA20230606057Unknown · unknownCA 1464/160 LH WING I/B FORE FLAP LOWER SKIN DELAMINATION BETWEEN WBL REPAIR IAW AIR ASIA EL-737-230504. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01844-001)SDR TSAA20230606032Unknown · unknownCA 1464/83 CORROSION AT RH WING O/B T/E EXHAUST GATE TRAILING EDGE WEDGE BETWEEN WBL 202.5 AND WBL 224. ALL CORROSION REMOVED AT RH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 202.5 AND WBL 224. REMOVED MATERIAL 0.002" AND REMAINING 0.018" IS WITHIN ALLOWABSDR TSAA20230606031Unknown · unknownCA 1464/77 CORROSION AT RH WING I/B MIDDLE FLAP LOWER SKIN BETWEEN WBL 74 AND WBL 114.5. ALL CORROSION REMOVED AT RH WING I/B MIDDLE FLAP LOWER SKIN BETWEEN WBL 74 AND WBL 114.5. REMOVED MATERIAL 0.009" AND REMAINING 0.116" IS WITHIN ALLOWABLE LIMIT. AREA CSDR TSAA20230606030Unknown · unknownCA 1464/76 CORROSION AT RH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 169 AND WBL 183. ALL CORROSION REMOVED AT RH WING I/B EXHAUST GATE LOWER SKIN BETWEEN WBL 169 AND WBL 183. REMOVED MATERIAL 0.002" AND REMAINING 0.018" IS WITHIN ALLOWABLE LIMIT. AREA CSDR TSAA20230606029Unknown · unknownCA 1464/75 CORROSION AT RH WING I/B AFT FLAP LOWER NOSE SKIN BETWEEN WBL 120 AND WBL 146. ALL CORROSION REMOVED AT RH WING I/B AFT FLAP LOWER NOSE SKIN BETWEEN WBL 120 & WBL 146. REMOVED 0.007" MATERIAL AND REMAINING 0.009" OVER LIMIT. PERFORM REPAIR I.A.W.
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