Boeing 737-330
Service difficulty reports · 430
Newest first. General aviation reporting is voluntary.
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 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 TSAA20230606056Unknown · unknownCA 1464/140 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 887 AND STA 907, (L:0.7",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 887 AND STA 907 (L: 0.7", W:0.3"). REMOVED 0.003" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVESDR TSAA20230606055Unknown · unknownCA 1464/139 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 867 AND STA 887, (L:0.7",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 867 AND STA 887. REMOVED 0.006" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM SDR TSAA20230606054Unknown · unknownCA 1464/135 T-BRACKET LOWER SKIN CORROSION AT BS 508 /S26R. DAMAGE T-BRACKET REMOVED AT BS 508, S-26R. INSTALL NEW PARTS I.A.W. B737-300 SRM 51-40-2 PARA 4. P2 (R130).SDR TSAA20230606053Unknown · unknownCA 1464/129 SURFACE CORROSION ON FUSELAGE EXTERIOR SKIN BS500B/S24R+2". ALL CORROSION REMOVED AT FUSELAGE EXTERIOR SKIN BS5008, S-24R+2". REMOVED 0.001" AND REMAINING 0.070" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-2SDR TSAA20230606052Unknown · unknownCA 1464/123 CORROSION AT APU INLET DOOR AT STA 1064, S-15R. CORROSION AT APU INLET DOOR AT STA 1064, S-15R, REPAIRED IAW AIR ASIA EL-737-230506. (ASAP INC. EO 5323-075)SDR TSAA20230606051Unknown · unknownCA 1464/122 CORROSION AT RH SIDE FUSELAGE AT STA 1071, S-20R. ALL CORROSION REMOVED AT RH FUSELAGE AT STA 1071, S-20R.. REMOVED 0.002" MATERIAL AND REMAINING 0.073" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-20-01 AND SDR TSAA20230606050Unknown · unknownCA 1464/121 CORROSION AT REPAIRED DOUBLER SKIN AT STA 1076, S-17AR. ALL CORROSION REMOVED AT REPAIRED DOUBLER SKIN AT STA 1076.5, S-17AR. REMOVED 0.003" MATERIAL AND REMAINING 0.053" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW 8737-300 SRM 51-1SDR TSAA20230606049Unknown · unknownCA 1464/119 CORROSION AT RH SIDE FUSELAGE AT STA 1115-1128, S-20R. ALL CORROSION REMOVED AT RH FUSELAGE AT STA 1115-1128, S-20R.
REMOVED 0.004" MATERIAL AND REMAINING 0.067" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51SDR TSAA20230606048Unknown · unknownCA 1464/118 CORROSION AT RH SIDE FUSELAGE AT STA 1156, S-20R. CORROSION ON FUSELAGE SECTION 48 STRAP 65-45688-172 AT STA 1156, REPAIR IAW AIR ASIA EL-737-230507. (V1 AEROSPACE, LLC REPAIR INSTRUCTION R23-01859-001 R01)SDR TSAA20230606047Unknown · unknownCA 1464/117 LIGHT CORROSION AT RIVET AREA OF STRINGER AT STA 1040~1060, S-24L. ALL CORROSION REMOVED AT RIVET AREA OF STRINGER AT STA 1040~1060 S-24L. REMOVED 0.005" AND REMAINING 0.040" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM SDR TSAA20230606046Unknown · unknownCA 1464/116 LIGHT CORROSION AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1058, S-20L. ALL CORROSION REMOVED AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1058, S-20L. REMOVED 0.002" MATERIAL AND REMAINING 0.054" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PRSDR TSAA20230606045Unknown · unknownCA 1464/115 LIGHT CORROSION AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1064, S-23L. ALL CORROSION REMOVED AT ACCESS AND BLOWOUT DOOR CUTOUT AREA AT STA 1064,S-23L. REMOVED 0.002" MATERIAL AND REMAINING 0.054" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROSDR TSAA20230606044Unknown · unknownCA 1464/114 DENT (1.0" X 0.5" IN AREA, MAX DEPTH=0.015") AT LH SIDE FUSELAGE EXTERNAL SKIN AT STA 1072, IN ABOVE S-22L 0.5" DENT (1.0" X 0.5" IN AREA, MAX DEPTH=0.015") AT LH FUSELAGE EXTERNAL SKIN AT STA 1072. ABOVE TO S-22L 0.5". CHECK WITHIN ALLOWABLE LIMSDR TSAA20230606043Unknown · unknownCA 1464/99 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 685 AND STA 706, 2 AREA (L:3.2",W:0.2")(L:0.5",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 685 AND STA 706 (L:3.2", W:0.2") (L:0.5", W:0.3"). REMOVED 0.003", 0.004" IS WITHISDR TSAA20230606042Unknown · unknownCA 1464/98 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 663.75 AND STA 685 (L:4",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 663.75 AND STA 685 (L:4", W:0.3"). REMOVED 0.003" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE SDR TSAA20230606041Unknown · unknownCA 1464/97 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 597 AND STA 616 (L:0.4",W:0.4"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 597 AND STA 616 (L:0.4", W:0.4"). REMOVED 0.009" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IASDR TSAA20230606040Unknown · unknownCA 1464/96 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 559 AND STA 578 (L:0.4",W:0.4"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 559 AND STA 578 (L:0.4", W:0.4"). REMOVED 0.009" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IASDR TSAA20230606039Unknown · unknownCA 1464/95 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 540 AND STA 559, 2 AREA (L:0.7",W:0.5")(L:0.6",W:0.2"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 540 AND STA 559 (L:0.7", W:0.5") (L:0.6", W:0.2"). REMOVED 0.006", 0.005" IS WITHISDR TSAA20230606038Unknown · unknownCA 1464/94 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 520 AND STA 540, 3 AREA (L:2",W:0.5")(L:0.5",W:0.5)(L:0.5",W:0.5").
ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 520 AND STA E540 (L:2",W:0.5") (L:0.5",W:0.5") (L:0.5",W:0.5"). REMOSDR TSAA20230606037Unknown · unknownCA 1464/93 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 500B AND STA 500C (L:0.6",W:0.5"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 500B AND STA 500C. REMOVED 0.006" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRSDR TSAA20230606036Unknown · unknownCA 1464/92 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 500A AND STA 500B (L:0.5",W:0.4"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 500A AND STA 500B (L:0.5",W:0.4"). REMOVED 0.004" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVESDR TSAA20230606035Unknown · unknownCA 1464/91 CORROSION AT RH WINDOWS CUTOUT EDGE, BETWEEN STA 400 AND STA 420 (L:0.5",W:0.3"). ALL CORROSION REMOVED AT RH WINDOWS CUTOUT EDGE BETWEEN STA 400 AND STA 420 (L:0.5",W:0.3"). REMOVED 0.005" IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAWSDR TSAA20230606033Unknown · unknownCA 1464/101 CORROSION AT FUSELAGE SKIN BETWEEN STA 685 AND STA 706, S-11R AND S-12R (L:3.5", W:1"). ALL CORROSION REMOVED AT FUSELAGE SKIN BETWEEN STA 685 AND STA 706, S-11R AND S-12R (L:3.5", W:1"). REMOVED 0.004" AND REMAINING 0.114" IS WITHIN ALLOWABLE LISDR 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. SDR TSAA20230606028Unknown · unknownCA 1464/61 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 907 AND STA 927, 6 AREA (L:1.3",W:0.5")(L:0.7",W:0.5")(L:0.8",W:0.5")(L:1",W:0.5")(L:0.3",W:0.3")(L:0.6",W:0.2"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 907 AND STA 927 (L:1.3",WSDR TSAA20230606027Unknown · unknownCA 1464/60 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 887 AND STA 907, 3 AREA (L:0.8", W:0.4")(L:0.3", W:0.3")(L:7.5", W:0.6"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 887 AND STA 907 (L:0.8, W:0.4")(L:0.3", W:0.3")(L:7.5", W:0.6"). SDR TSAA20230606026Unknown · unknownCA 1464/59 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 867 AND STA 887, 8 AREA (L:1.9", W:0.4")(L:1.6", W:0.5")(L:1.7", W:0.5")(L:1.9", W:0.5")(L:2.9", W:0.5")(L:0.4", W:0.3")(L:0.5, W:0.3")(L:0.5", W:0.4"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGSDR TSAA20230606025Unknown · unknownCA 1464/58 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 847 AND STA 867, 8 AREA (L:5.5", W:0.5")(L:1.7", W:0.5")(L:0.6", W:0.3")(L:0.5", W:0.3")(L:1.1", W:0.6")(L:0.5", W:0.4")(L:0.9", W:0.5")(L:1.6", W:0.5"). ALL CORROSION REMOVED LH WINDOWS CUTOUT EDGE,SDR TSAA20230606024Unknown · unknownCA 1464/57 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 827 AND STA 847, 3 AREA (L:1", W:0,3")(L:2,7", W:0.5")(L:1.4", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 827 AND STA 847 (L:1", W:0.3")(L:2.7", W:0.5")(L:1.4", W:0.5"). RSDR TSAA20230606023Unknown · unknownCA 1464/56 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 807 AND STA 827, 5 AREA (L:1", W:0.5")(L:0.4", W:0.3")(L:0.5", W:0.5")(L:0.6", W:0.4")(L:0.5", W:0.4"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 807 AND STA 827 (L:1", W:0.5")(L:0.SDR TSAA20230606022Unknown · unknownCA 1464/55 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 787 AND STA 807, 2 AREA (L:0.4", W:0.2")(L:1.1", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 787 AND STA 807 (L:0.4", W:0.2")(L:1.1", W:0.5"). REMOVED 0.002", 0.004" MATERISDR TSAA20230606021Unknown · unknownCA 1464/54 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 767 AND STA 787, 2 AREA (L:0.9",W:0.3")(L:1.2", W:0.3"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 767 & STA 787, 2 AREA (L:0.9",W:0.3")(L:1.2", W:0.3"). REMOVED 0.003" MATERIAL ISDR TSAA20230606020Unknown · unknownCA 1464/53 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 747 AND STA 767 (L:4.6", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 747 & STA 767 (L:4.6", W:0.5"). REMOVED 0.006" MATERIAL IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTESDR TSAA20230606019Unknown · unknownCA 1464/52 CORROSION AT LH WINDOWS CUTOUT EDGE, BETWEEN STA 727E AND STA 747 (L:0.7", W:0.5"). ALL CORROSION REMOVED AT LH WINDOWS CUTOUT EDGE BETWEEN STA 727E AND STA 747 (L:0.7", W:0.5"). REMOVED 0.0078" MATERIAL IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND SDR TSAA20230606018Unknown · unknownCA 1464/50 CORROSION AT FUSELAGE SKIN STA 907, BETWEEN S-15L AND S-16L (L:10", W:0.5"). ALL CORROSION REMOVED AT FUSELAGE SKIN STA 907, BETWEEN S-15L & S-16L (L:10", W:0.5"). REMOVED 0.004" MATERIAL AND REMAINING 0.061" IS WITHIN ALLOWABLE LIMIT. AREA CLEANSDR TSAA20230606017Unknown · unknownCA 1464/49 CORROSION AT FUSELAGE SKIN STA 947.5, BETWEEN S-13L AND S-16L, 2 AREA (L:11", W:0.7")(L:5", W:1"). REMOVED MATERIAL AND REMAINING IS WITHIN ALLOWABLE LIMIT. AREA CLEAN AND PROTECTIVE IAW B737-300 SRM 51-10-2, 51-20-01 AND 53-00-01 ALLOWABLE DAMAGESDR TSAA20230606016Unknown · unknownCA 1464/37 MAIN DECK CARGO DOOR SEAL RETAINER CRACK ON FWD LOW CORNER. DAMAGE SEAL RETAINER REMOVED AT FWD LOWER CORNER MAIN DECK CARGO DOOR. INSTALL NEW PARTS IAW B737-300 SRM 51-40-2 PARA 4 P2 (R130).SDR TSAA20230606015Unknown · unknownCA 1464/31 FILIFORM CORROSION WERE FOUND ON THE AFT CARGO DOOR EXTERNAL SKIN EDGE AND HANDLE CUTOUT COVER AS MARK. ALL CORROSION REMOVED AT AFT CARGO DOOR EXTERNAL SKIN EDGE AND HANDLE CUTOUT COVER. REMOVED 0.001" MATERIAL AND REMAINING 0.035" IS WITHIN ALLOSDR TSAA20230606014Unknown · unknownCA 1464/22 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN AFT CARGO CUTOUT FWD EDGE AS MARK. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AFT CARGO CUTOUT FWD EDGE. REMOVED 0.001" MATERIAL AND REMAINING 0.035" IS WITHIN ALLOWABLE LIMIT. AREA CLESDR TSAA20230606013Unknown · unknownCA 1464/21 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 27 STATION 987, 900 TO 903. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN S-27L STA 987, STA 900 TO STA 903. REMOVED MATERIAL AND REMAINING IS WITHIN ALLOWABLE LIMIT. AREASDR TSAA20230606012Unknown · unknownCA 1464/20 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 26 STATION 900 TO 905. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN S-26L, STA 900 TO 905. REMOVED 0.002" MATERIAL AND REMAINING 0.061" IS WITHIN ALLOWABLE LIMIT. AREA CLSDR TSAA20230606011Unknown · unknownCA 1464/19 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 27 STATION 938 TO 951, 903 TO 907.
ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-27R STA 938 TO STA 951, STA 903 TO STA 907. REMOVED MATERIAL AND REMAINING IS WITHINSDR TSAA20230606010Unknown · unknownCA 1464/18 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN RH SIDE STRINGER 26 STATION 922, 926 TO 928, 938 TO 942, 954 TO 957, 982 TO 990. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-26R STA 922, STA 926 TO STA 928, STA 938 TO STA 942, STA 9SDR TSAA20230606009Unknown · unknownCA 1464/17 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STA 986 BETWEEN STRINGER 18 AND 19. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT STA 986 BETWEEN S-18L AND S-19L. REMOVED MATERIAL 0.002" AND REMAINING 0.069" IS WITHIN ALLOWABLSDR TSAA20230606008Unknown · unknownCA 1464/16 FILIFORM CORROSION WERE FOUND ON FUSELAGE EXTERNAL SKIN LH SIDE STRINGER 25 STATION 827 TO 847, 881 TO 901. ALL CORROSION REMOVED AT FUSELAGE EXTERNAL SKIN AT S-25L STA 827 TO STA 847, STA 881 TO STA 901. REMOVED MATERIAL AND REMAINING IS WITHIN A
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