Boeing 737-330
Service difficulty reports · 430
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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 aircraft_model_key = '737330' 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 aircraft_model_key = '737330' 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 NACA20230720002Unknown · unknown#2 ENGINE.- DURING ACCOMPLISHMENT OF AD 200-16-51 WAS FOUND RH 5TH STAGE ENGINE BLEED VALVE CORRODED AND STUCKED P/N 3202222-1 AND S/N 2243. "REMOVED AND REPLACED RH 5TH STAGE ENG BLEED AIR CHECK VALVE IAW B737 AMM 36-11-35 PAG 401-408. PERFORMED LEAK CHECK IASDR TSAA20230606107Unknown · unknownCA 1464/361 WHILE PERFORM CUSTOMER PROVIDE TASK CARD ECO 3531-R10 WHICH INDICATED IN SB 737-53A1240, FOUND FASTENER HAD BEEN UPSIDE. PERFORM TASK CARD ECO 3531-R10 INSP FOUND FASTENER WRONG. PERFORM PER AIRASIA EL-737-230508.SDR TSAA20230606106Unknown · unknownCA 1464/100 CORROSION AT FUSELAGE SKIN BETWEEN STA579 AND STA616, S-14R AND S-15R ( L:4.5" W:1"). ALL CORROSION REMOVED AT FUSELAGE SKIN BETWEEN STA 579 AND STA 616, S-14R AND S-15R (L:4.5", W:1"). REMOVED 0.004" AND REMAINING 0.114" IS WITHIN ALLOWABLE LIMISDR 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 TSAA20230606103Unknown · unknownCA 1464/9 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 20 STATION 767 TO 787, 867 TO 897, 927 TO 929. ALL CORROSION REMOVED AT STA500 & STA500E, S-1R & S-2R (L:3.1", W:2.2") (L:14", W:1.4") (L:0.9", W:0.5") L:0.5", W:0.4") (L:1.9",SDR TSAA20230606102Unknown · unknownCA 1464/303 LIGHT CORROSION AT RH SIDE EXTERNAL SKIN AT STA 1088, S-16R. ALL CORROSION REMOVED AT RH SIDE EXTERNAL SKIN AT STA 1088, S-16R. REMOVED 0.004" MATERIAL & REMAINING 0.049" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.A.W. B737-300 SRM 51-SDR TSAA20230606101Unknown · unknownCA 1464/302 LIGHT CORROSION AT LH SIDE EXTERNAL SKIN AT STA 1073 S-20L. ALL CORROSION REMOVED AT LH SIDE EXTERNAL SKIN AT STA 1073 S-20L. REMOVED 0.004" MATERIAL & REMAINING 0.049" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.A.W. B737-300 SRM 51-10SDR 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 TSAA20230606088Unknown · unknownCA 1464/264 DRILL OFF HI-LOCK FASTENER ON FWD ENTRY DOOR LOWER HINGE EXTERNAL DOUBLER, STA 303.9 S-13L AND S-14L.
FASTENER REMOVED AT FWD ENTRY DOOR LOWER HINGE EXTERNAL DOUBLER STA 303.9, S-13L & S14L. REINSTALL FASTENER I.A.W. B737-300 SRM 51-40-2 PARA 7SDR 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 TSAA20230606081Unknown · unknownCA 1464/233 LIGHT CORROSION AT RUDDER LEADING EDGE RIB AT RUDDER STA 90 NEARBY RUDDER HINGE 4. ALL CORROSION REMOVED AT RUDDER LEADING EDGE RIB AT RUDDER STA 90 NEARBY RUDDER HINGE 4. REMOVED 0.002" MATERIAL & REMAINING 0.038" IS WITHIN ALLOWABLE LIMIT. ARESDR TSAA20230606080Unknown · unknownCA 1464/232 LIGHT CORROSION AT LH SIDE VERTICAL STABILIZER EXTERNAL SKIN AT REAR SPAR AREA AT FIN STA 247. ALL CORROSION REMOVED AT LH SIDE VERTICAL STABILIZER EXTERNAL SKIN AT REAR SPAR AREA AT FIN STA 247. REMOVED 0.002" MATERIAL & REMAINING 0.097" IS WITHSDR TSAA20230606079Unknown · unknownCA 1464/231 LIGHT CORROSION AT RH SIDE VERTICAL STABILIZER EXTERNAL SKIN AT REAR SPAR AREA AT FIN STA 79~93. ALL CORROSION REMOVED AT RH SIDE VERTICAL STABILIZER EXTERNAL SKIN AT REAR SPAR AREA AT FIN STA 79 ~ 93. REMOVED 0.002" MATERIAL & REMAINING 0.097" ISDR TSAA20230606078Unknown · unknownCA 1464/230 CORROSION AT RH REAR FUSELAGE SKIN AT STA 1016, S-4R~S-9R. ALL CORROSION REMOVED AT RH REAR FUSELAGE SKIN AT STA 1016, S-4R ~ S-9R. REMOVED 0.003" MATERIAL & REMAINING 0.059" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.A.W. B737-300 SRMSDR TSAA20230606077Unknown · unknownCA 1464/229 CORROSION AT RH REAR FUSELAGE SKIN AT STA 1088, S-3R~S-5R. ALL CORROSION REMOVED AT RH REAR FUSELAGE SKIN AT STA 1088, S-3R ~ S-5R. REMOVED 0.003" MATERIAL & REMAINING 0.060" WITHIN ALLOWABLE LIMIT. AREA CLEAN & PROTECTIVE I.AW. B737-300 SRM 51-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 TSAA20230606072Unknown · unknownCA 1464/193 CORROSION AT R/H SIDE HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 143 (1.0" X 0.4" IN AREA). ALL CORROSION REMOVED AT RH HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 143 (1.0" X 0.4" IN AREA). REMOVED 0.020" AND REMAINISDR TSAA20230606071Unknown · unknownCA 1464/192 CORROSION AT R/H SIDE HORIZONTAL STABILIZER REAR SAPR UPPER SURFACE AT STAB STA 116 (0.5" X 0.2" IN AREA). ALL CORROSION REMOVED AT RH HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 116 (0.5" X 0.2" IN AREA). REMOVED 0.015" AND REMAINISDR TSAA20230606070Unknown · unknownCA 1464/191 CORROSION AT L/H SIDE HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 153 (1.2" X 0.3" IN AREA). ALL CORROSION REMOVED AT LH HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 153 (1.2" X 0.3" IN AREA). REMOVED 0.040" AND REMAINISDR TSAA20230606069Unknown · unknownCA 1464/190 CORROSION AT L/H SIDE HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 116. (1.0" X 0.3" IN AREA). ALL CORROSION REMOVED AT LH HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE AT STAB STA 116 (1.0" X 0.3" IN AREA). REMOVED 0.002" AND REMAINSDR TSAA20230606068Unknown · unknownCA 1464/186 CORROSION AT FUSELAGE CROWN DOUBLER BETWEEN STA 500 AND STA 540, S-1R AND S-2R, 14 AREA (L:3.1",W:2.2")(L:1.4",W:1.4")(L:0.9",W:0.5")(L:0.5",W:0.4") (L:1.9",W:0.7")(L:2.3",W:1.4")(L:1.7",W:1")(L:1.3",W:0.6")(L:1.1",W:0.6")(L:0.4",W:0.3)(L:0.8",W:0.SDR TSAA20230606067Unknown · unknownCA 1464/185 CORROSION AT FUSELAGE CROWN SKIN STA727, BETWEEN S-3L AND S-3R, 5 AREA (L:0.7",W:0.5")(L:1.5",W:0.6")(L:5.7"W:0.8)(L:1",W:0.5")(L:0.8",W:0.7"). ALL CORROSION REMOVED AT FUSELAGE CROWN SKIN AT STA 727, BETWEEN S-3L AND S-3R (L:0.7", W:0.5") (L:1.5"SDR TSAA20230606066Unknown · unknownCA 1464/184 CORROSION AT FUSELAGE SKIN STA 947.5, BETWEEN S-2R AND S-3R (L:5.6",W:1.4"). ALL CORROSION REMOVED AT FUSELAGE SKIN AT STA 947.5, BETWEEN S-2R AND S-3R (L:5.6", W:1.4"). REMOVED MATERIAL 0.003" AND REMAINING 0.037" IS WITHIN ALLOWABLE LIMIT. ARESDR 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 B737-30
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