JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, Plate/Skin, newest first.
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 = '5330' 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 = '5330' 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 SWAA2023032304775Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13.24 AT PASSENGER CABIN 2023-116968<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13.24 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A5400 SHEET 6 REV-. SEE SDR SWAA2023032304777Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN AT PASSENGER CABIN 2023-116967<[01] REPLACED FLOOR STRUCTURE ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWGSDR IPXA2023030591548Floorbeam · corrodedINSPECTION TYPE:SEG3, *MAJOR REPAIR* MAIN CARGO FLOOR BEAM AT STA 1681.8 RBL 12.5-26 HAS CORROSION OUT OF LIMITSACCOMPLISHED REPAIR ON FLOOR BEAM PER SRM 53-60-51-2R-3 DETAIL IISDR DALA2023030201577None · noneSHIP 5649 FOUND DENT BELOW CAPTAINS WINDSCREEN, FWD OF AOA VANE. CORRECTIVE ACTION: REF ERA 606283-14. (4148190)SDR SWIA20230218None · damagedLOWER FWD FUSELAGE HAS LIGHTNING STRIKE 1.75" OUTBOARD OF STGR 27L, BETWEEN FR17 AND FR18 AS MARKED (C-CHECK RO 2/25/2023) REPAIRED LOWER FWD FUSELAGE AT STGR 27L BETWEEN FR 17-18 REF ETD2023-170-004835-A. ADDITIONAL INSPECTION REQUIRED EXTERNAL LOW FRSDR N6WA2023022301Skin · unknownPERFORM PERMANENT REPAIR TO FUSELAGE SKIN BTWN FS250.00 AND FS265.00 AT STRINGER 16L (C/O 12204). REPAIRED IAW REO 670-53-11-183 & EO C55-53MR-005-O.SDR DALA2023022201350None · none(LOG 2633943) DURING INSPECTION FOUND AFT RT WHEEL WELL CONNECTOR PANEL MISSING. REPAIRED PER ER/A 606115-14 REV ORIGINAL.SDR SWAA2023032304399Angle · crackedCRACK ANGLE - CLIP LOCATED BS 480 FWD FACE STR 26L AT FWD CARGO COMPARTMENT 2023-116961<[01] REPLACED ANGLE - CLIP LOCATED BS 480 FWD FACE STR 26L AT FWD CARGO COMPARTMENT AND FASTENER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG143A1220 SHEET 30 SDR SWAA2023031604496Gusset · crackedCRACK GUSSET LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT 2023-127580<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -;[02] REPLACED GUSSET AND FASTENERS LOCASDR SWAA2023031604502Gusset · crackedCRACK GUSSET LOCATED BS 500D STRINGER 21L FWD CARGO COMPARTMENT 2023-127581<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -;[02] REPLACED GUSSET AND FASTENERS LOCASDR SWAA2023031604497Gusset · crackedCRACK GUSSET LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT 2023-127582<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D STRINGER 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 143A7902 REV -;[02] CORRECTED STEP 1.REPLACED GUSSET ASDR IPXA2023022191202Venturi · noneINSPECTION TYPE:CK1CFOR RCD PURPOSES ONLY TO DOCUMENT VENTURI MODIFICATION.COMPLIED WITH RCD 262517 AND UPS EO A300-5330-72601-B.SDR ASAA2023021742005Skin · dentedREF L/P 60246073, DENT LOCATED 9" FWD OF STA 787 & 4" ABOVE STR 22L. GROUNDED - YES. REPAIRED REF REF B737-800 SRM 53-00-01-2R-3 & EA 800-53EA-25281. THIS CAT B REPAIR WAS SUBMITTED TO ENGINEERING FOR TRACKING.SDR CALA2023022000473None · corrodedFWD CARGO PIT R/H FR29 BETWEEN STRINGERS 40R-41R HAS CORROSION O N CLEAT DOT M069 A3NB-53-3-6105 GENERATED AT HAECO LCQ BY V91915 0 PER NR 9292692(40692) REMOVED AND REPLACED DISCREPANT FWD CARGO CLEAT AT R/H FR29 STR 40R-41R IAW A320 SRM 51-72-11-911-002 BY MSDR DALA2023021901250None · noneAIRCRAFT 3122, CORROSION INTERNAL STRUCTURE SKIN LOC. FR 30 TO FR 34 BTW STR 40 L/H TO STR 40 R/H IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON INTERNAL STRUCTURE SKIN LOC. FR 30 TO FR 34 BTW STR 40 L/H TO STR 40 R/H INFWD CARGO COSDR SWAA2023032004084Angle · corrodedFWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500C-500D<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE SDR SWAA2023032004134Angle · corrodedFWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500D-500E<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE SDR SWAA2023032004135Angle · corrodedFWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500E-500F<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE SDR SWAA2023032004086Angle · corrodedFWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500F-500G<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE SDR SWAA2023032004136Angle · corrodedFWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500G-500H<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE SDR SWAA2023032004087Angle · corrodedFWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500H-500I<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I. NEW TRANSITION ANGLE TO BE REPLACED ON NON ROUTINE SDR SWAA2023031704083Angle · corrodedFWD CARGO COMPARTMENT RT TRANSITION ANGLE HAS AREAS OF CORROSION FROM STA 500A-500B<[01] R/H TRANSITION ANGLE OUT OF ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. REMOVED R/H TRANSITION ANGLE FROM STA 500A TO 500I PER SRM 51-40-02.;[02] C/W INSPECTION.;[03] FABRICATSDR FDEA202302160339Skin · failedE.A.#:H-5330-T0372987 REPAIR FOR DAMAGE TO FORWARD WING-TO-BODY FAIRING AND SKIN, R/H SIDE, STA 698-720, STR 31-32R. COMPLY WITH E..A. H-5330-T0372987 REV NO: A PS P2 EA H-5330-T0372987 REV NO, P2 WAS SUPERSEDED BY EA H-5330-T0372987 REV A, P2. COMPLIED WSDR DALA2023021701237None · noneSHIP 3354 EM 5330-01152 REVISION C INCORPORATES THE INSPECTIONS AND MODIFICATIONS AS REQUIRED PER FAA AD 2014-16-04 WITH THE PROVISIONS AUTHORIZED BY GLOBAL AMOC 22-297. THE AD MANDATES THE INCORPORATION OF AIRBUS SB A330-53-3152 REV 3, GLOBAL AMOC 22-297 AUTHSDR SWAA2023021703545Support · crackedFLOOR BOARD SUPPORT L/H PANEL BRAKE ASSY CRACKED - LOCATED AT STA. 540<[01] R & R L/H FLOOR BOARD SUPPORT BRAKE ASSY AT STA 540 IAW <BR>SRM 51-40-02SDR SWAA2023021703547Support · crackedFLOOR BOARD SUPPORT R/H PANEL BRAKE ASSY CRACKED - LOCATED AT STA. 540<[01] R&R R/H FLOOR BOAR SUPPORT BRAKE ASSY AT STA 540 IAW SRM <BR>51?40-02SDR DALA2023021701238None · noneSHIP 5636 COMPLY WITH FINAL ERA 606050-14AD REV. ORIGINAL. CORRECTIVE ACTION: COMPLIED WITH FINAL ERA 606050-14AD REV. ORIGINAL. (2629478)SDR CALA2023021600446None · corrodedFWD CARGO PIT R/H FR26 BETWEEN STRINGERS 41R-42R CLEAT HAS CORROSION DOT M067. PER HAECO LCQ NONROUTINE 9298576/20576. GENERATED BY V919150. SPEC: A3NB-53-3-6105. FOUND CLEAT CORRODED AT FR26 BETWEEN STRINGERS 41R-42R TO BE OUT IAW A319 SRM 51-44-11/001A AND ISDR SWAA2023031003240Skin · debondedTAIL CONE SKIN HAS A DISBOND AT BS 1156+13.5' AND 7' LOWER FROM TAIL CONE ACCESS DOOR CUT OUT SKIN LOWER EDGE<[01] IDENTIFIED TAIL CONE IAW SRM 53-80-70-0I-1 FIGURE 2 TABLE 2 ITEM 1<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-80-70-1A-1 PAR.4 B(4)SDR DALA2023022201325None · none"FAA APPROVAL PENDING" FOR ERA 605849-14 REV ORIG. FUSELAGE SKIN / STA 1002-1022 / L-24-L-26 / GROUND DAMAGE SECTION I PERMANENT REPAIR INSTRUCTIONS. SUMMARY SEE NRC 003-0001:0514-2001/005 00005: COMPLIED WITH ER/A PRI 605849-14 REV A PRI REV 0 REPAIR INSTRUCTSDR CALA2023021400438Skin · gougedRH FUSE SKIN IS DEEPLY GOUGED JUST AFT OF RH HORIZONAL STAB UPR MOVEABLE SEAL TRACK. GRID MAPPED DAMAGED AREA. LENGTH AND WIDTH ARE 1.00" X 0.50" BLENDED DAMAGED AREA. REF SRM 53-80-01. ACP''D HFECPER NDT PT6, 51-00-00-23, NO CRACKS NOTED. AND MAX DEPTH IS 0SDR SWAA2023031502583Track · crackedCRACK TRACK RBL 13.84 AT BS 460 WL 155 AT FWD CARGO COMPARTMENT 2023-119519<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[02] TOOL USED CALIPER P/N: 500-193-30; S/N: 0017054; DUE DATE: 05-OCT-23;[03] REPLACED TRASDR DALA2023021501182None · noneAIRCRAFT FUSELAGE DAMAGED BY BELT LOADER STA 1002 STR 25R. C/W FUSELAGE TEMPORARY SKIN REPAIR STA 1002 STR 25R PER ERA 605962-14 REV A SECTION 1. RII C/W. ASSOCIATED ER/A 14-605962 ADDED FOR AC 9570. (LP #9046786)SDR DALA2023021501178None · noneCOMPLY WITH FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L-26 PER ER/A 605849-14 REV ORIG. C/W ER/A 605849-14 REV ORIG. PERMANENT REPAIR AND ER/A 605849-14 REV A. RII C/W. ASSOCIATED ER/A 14-605849 ADDED FOR AC 9521. (LP #4025639)SDR DALA2023021401137Unknown · unknownC/W ERA 605849-14 REV ORIG, FUSELAGE SKIN PERMANENT REPAIR STA 1002 TO STA 1022 L-24 TO L26. SUMMARY NRC 003-0001:0514-2001/001 00001: COMPLIED WITH ER/A PRI 605849-14 REV "0","1","2","3". ALL REPAIR INSTRUCTION STEPS, ENSURE FINALE ER/A 605849-14 REV. ORIG. SSDR DALA2023021301090Unknown · unknown(LOG 2626127) DURING INSPECTION FOUND BENT FRAME STA. 500J BTW STR 23R TO STR 24R AT FWD CARGO COMPARTMENT. PERFORMED PERMANENT REPAIR ON FRAME STA 500J STR 23R TO STR 24R AT FWD CARGO COMPARTMENT AS PER B737-900ER SRM 53-30-07-2R-2 REPAIR 2.SDR SWAA2023031502024Gusset · crackedCRACK GUSSET LOCATED AT BS 500D S-19R WL 190 FWD CARGO COMPARTMENT 2023-119350<[01] REPLACED GUSSET AND FASTENERS LOCATED ON AT BS 500D S-19R WL 190 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV-<BR>SEE INDIVIDUAL SIGN-OFF BELOSDR SWAA2023031502025Gusset · crackedCRACK GUSSET LOCATED AT BS 500D S-19L WL 190 FWD CARGO COMPARTMENT 2023-119349<[01] REPLACED GUSSET LOCATED AT BS 500D S-19L WL 190 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG NO. 143A7902; SHEET 209; REV.-<BR>SEE INDIVIDUSDR SWIA2023020011Skin · dentedTRANSFER FROM EAML 1081722 : PLEASE REF EAML 1081576. BIRD STRIKE BELOW CAPTAINS WINDSHIELD. DURING BIRD STRIKE INSPECTION, FOUND DENT BELOW CA WINDSHIELD BETWEEN FR04-FR05 STGR06L-STGR10L. L=2.5 INCH W=2.25 INCH. DEPTH=0.08390 INCH. THE EDGE OF THE DENT TO CLSDR SWIA202302011Skin · dentedTRANSFER FROM EAML 1081722 : PLEASE REF EAML 1081576. BIRD STRIKE BELOW CAPTAINS WINDSHIELD. DURING BIRD STRIKE INSPECTION, FOUND DENT BELOW CA WINDSHIELD BETWEEN FR04-FR05 STGR06L-STGR10L. L=2.5 INCH W=2.25 INCH. DEPTH=0.08390 INCH. THE EDGE OF THE DENT TO CLSDR IPXA2023021691057Skin · dentedINSPECTION TYPE:C*MAJOR REPAIR* DENT ON RH FUSELAGE SKIN AT FR 3REPAIRED IAW SRM 53-11-12-201-C1 FIG 202 AND UPS EO A300-5330-86030-ASDR DALA2023021401161None · noneSHIP 3409 LT SIDE OF FUSELAGE- 5EA UNIDENTIFIED BLENDOUTS ON FUSELAGE SKIN BETWEEN FR10A AND FR13A AFT OF CAPTAINS FIXED SIDE WINDOW. CORRECTIVE ACTION: EVALUATED PER A330 SRM 53-21-11. (2625062)SDR AALA202302132468Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FUSELAGE SKIN AT EXTERNAL POWER ACCESS DOOR AFT AREA OF CUTOUT LOCATED AT BS 232 AND S22R. REPAIRED SKIN PER EA 342011 AND SRM B737NG 53-10-15-2R PROCEDURE 4.SDR SWIA20230210None · misalignedHOLE MISS-DRILLED BETWEEN FR77/78 AT STR29R (C-CHECK RO 2/18/2023) REMOVED THE ORIGINAL FASTENER AND REPLACE IT BY BRFZ-XX-E FASTENER. INSTALLED A MS20470E-4-5 FASTENER IN NEW HOLE.RESTORED SURFACE PROTECTION ETD2023-170-003930 REV.A AND SRM 51-40-08SDR YENA2023021400168None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE HORIZONTAL FLANGE RADIUS AT STGR 22 AFT WEB FACE, CRACK LENGTH IS 1.500 INCH APPROX, AT AFT GALLEY AREA (1EA); ACCOMPLISHED PERMANENT REPAIR IAW AEROMAN WO 2022-453/1, NR 2022-676465 AND JETBLUE ECSDR YENA2023021400160None · noneDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / MLG ACTUATOR FITTING – STRUCTURAL REINFORCEMENT. (CONSIDERED AS A MAJOR REPAIR)SDR DALA2023021401131Unknown · unknownC/W ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. SUMMARY NRC 001-0002:2040-0015/001 00026: COMPLIED WITH ERA 597013-14 REV A FUSELAGE SKIN REPAIR AT LAV WASTE VENT. (LP #2621093)SDR DALA2023021301085Unknown · unknown(LOG 2622082) DURING INSPECTION FOUND LIGHTNING STRIKE BTW FS 500H TO 500I STR-25L. EPAIR CATEGORY B ON LIGHTNING STRIKE BTW FS 500H TO 500I STR-25L WAS PERFORMED PER B737-900ER SRM 53-00-01-2R PROCEDURE 1 REPAIR 1.SDR IPXA2023020990831Skin · noneINSPECTION TYPE:SEG4*MAJOR REPAIR* MAJOR REPAIR LOCATED AT LWR CENTER FUSELAGE IS NOT LISTED ON THE MAJOR REPAIR MAP. REPAIR EXTENDS FROM STA 1490-1520 STR 29R-STR 30ACCOMPLISHED REPAIR PER EO B757-5330-85888-A, UPS RCD 266520 AND VT MAE EA 757-5360-27-A3134 RSDR DALA2023022201337None · noneSHIP 5635 ***DTE REQUIRED*** B757-200 / FUSELAGE / SKIN / FR 620 640 / STR 2R 2L / SHORT CENTER TO CENTER SPACING. CORRECTIVE ACTION: REF ERA 605920-14. (2620715)
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