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 HNAA2023010300003Skin · crackedEXTERNAL FUSELAGE SKIN IS CRACKED AT FRAME 77 STRINGERS 6L-7L. PERFORMED SKIN BUSHING (.4375" BUSHING) REPAIR AT RIVET LOCATION ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 6L-7L IAW SRM 53-32-01RE, ITEM 9, FIG 213 AND EO1-53-22-0267.SDR HNAA2023010300002Skin · crackedEXTERNAL FUSELAGE SKIN IS CRACKED AT FRAME 77 STRINGERS 6R-7R. PERFORMED SKIN BUSHING (.4375" BUSHING) REPAIR AT RIVET LOCATION ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 6R-7R IAW SRM 53-32-01RE ITEM 9 FIGURE 213 AND EO1-53-22-0266.SDR HNAA2023010300001Skin · dentedACCOMPLISH PERMANENT REPAIR OF FUSELAGE SKIN DENT BETWEEN FR9 - 10, SL20L - 21L. ACCOMPLISHED PERMANENT REPAIR OF FUSELAGE SKIN DENT BETWEEN FR9 - 10, STR 20L - 21L IAW EMB 145 SRM 53--10-01RE, ITEM 6, FIG. 206 AND EO1-53-22-0265SDR ASAA2022122041265Skin · dentedDENT ON CROWN SECTION APPROX. STA 500A+2 - STR 22 REQUIRES EVAL. GROUNDED - YES. REPAIRED DENT ON FUSLAGE CROWN SECTION STA 500A STR 2L IAW B737-900 SRM 53-00-01-2R-35, CATEGORY B REPAIR INSPECTION THRESHOLD 50,000 FLIGHT CYCLES.TRACKED BY ENGINEERING. THIS CLSDR SWIA2022122267021Skin · dentedFUSELAGE SKIN DENTED AT BS 1031.00, S22R JUST AFT OF LP AIR GROUND AIR CONNECTION DOOR. OPENSDR DALA2023092007750Unknown · unknownSHIP 0659 REPAIR TO CTR WING FWD UPPER PANEL SKIN, B/W U-14C & U-15C AT LBL 64 & STA 960. CORRECTIVE ACTION: REF ERA 603710-14. (2545624)SDR SWIA20221219None · damagedTHERE ARE SIGNS OF DAMAGE ON THE RH NOSE OF THE AIRCRAFT BETWEEN THE ADG DOOR AND THE NLG DOOR. PLEASE PLOT, MAP AND EVALUATE DAMAGE. IF DAMAGE IS FOUND IN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES AND PROCEDURES. (C-CHECKSDR SWAA2023020783289Bracket · brokenBROKEN SUPPORT BRACKET LOCATED BS344 AT LEVEL STR15R AT FWD GALLEY AREA 2022-697150<[01] REPLACED SUPPORT BRACKET LOCATED BS344 AT LEVEL STR15R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND 51-10-02 PARAGRAPH 9 AND DWG 141A1150 SHEET 1 REV: C;[02] REPLACED SDR SWAA2023020783293Bracket · crackedCRACK SUPPORT BRACKET LOCATED BS277 BETWEEN STR8R TO STR9R AT FWD GALLEY AREA 2022-697147<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 17-DEC--23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 220272SDR SWAA2023020783291Door · crackedCRACK SERVICE DOOR CUT OUT COVER LOCATED BS332 AT LEVEL STR9R AT FWD GALLEY AREA 2022-697149<[01] REPLACED SERVICE DOOR CUT OUT COVER LOCATED BS332 AT LEVEL STR9R AT FWD GALLEY AREA IAW BOEING 737-700 AMM-52-71-11-400-801 STEP 3F (5);[02] REPLACED SERVICE DOORSDR JJBA20221222017Skin · corrodedCORROSION ON REAR FUSE 2 LOWER SKIN. BTW FR 80-61 AND BTW STR 19L-21L. ON FR2 LOWER SKIN, BTW FR80-81 AND BTW STR 19L-21L, CORROSION BLENDE DOUT OF LIMITS. CUTOUT AND REPAIR DOUBLER PERFORMED. REAR FUSE 2 LOWER SKIN BTW FR 80-81 AND BTW STR 19L-21L CORROSION RSDR DALA2022122008263Doubler · corrodedAFT FUSELAGE, WASTE BOX CUT OUT DOUBLER HAS CORROSION. REPAIRED PER PRI 604453-14 REV 0, REV 1, REV 2, AND REV 3 AND VERIFIED WORK ACCOMPLISHED MATCHES ER/A 604453-14 REV ORIGINAL. CORROSION PRESENT ON DOUBLER WAS BEYOND LIMITS AND DOUBLER WAS SPLICED PER ER/ASDR DALA2022122008261Repair · mechanic errorDURING GET OK TO INSTAL REPAIRS PARTS FOUND MISSED DRILLED NEW HOLE CLOSER TO STR 19. ACCOMPLISHED AND RECORDED REPAIR TO FUSELAGE SKIN DENT AT FR 78- 79 BELOW STR 19L PER PRI 587671-14 REV B, REV 1 AND VERIFY WORK ACCOMPLISHED ON PRI COMPLIES WITH FINAL ERA 5SDR DALA2022121908177Skin · crackedCRACK ON EXTERNAL SKIN ABOVE LONGERON 15 RH AND STA 1087 AT FUSELAGE. SUMMARY OF NRC 00026: CRACK ON EXTERNAL SKIN ABOVE LONGERON 15 RH AND STA 1087 AT FUSELAGE WAS REPAIRED PER PRI 604254-14 REV 4 AND PER ER/A 604254-14 REV ORIGINAL, SECTION I: PERMANET REPAISDR CALA2022121903433Skin · damagedFUSELAGE SKIN DAMAGE AT STA 2108 AT STR 24L . REF LOG PAGE 6945293 FOR INSPECTION OF DAMGE AND WORK ACCOMPLISHED. REPAIR ON OR BEFOR 500 CALANDER DAYS OF PART 3 OF EC/RA 5330-06860 REFE ECRA 5330-06860, REPEAT INSPECTION EVERY 100 FLIGHT CYCLES TOMC-APPROVAL FSDR SWAA2023020182729Angle · crackedCRACK ANGLE - CLIP LOCATED FWD FACE BS500C AND STR26R FWD CARGO COMPARTMENT 2022-695449<[01] REPLACED ANGLE - CLIP LOCATED FWD FACE BS500C AND STR26R FWD CARGO COMPARTMENT IAW B737-700 51-10-02 AND DWG 143A7505 REV: - SHEET 75. TOOL USED DIGITAL CALIPER P/N: 5SDR SWAA2023020182723Angle · crackedCRACK ANGLE - CLIP LOCATED AFT FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT 2022-695457<[01] REPLACED ANGLE - CLIP LOCATED AFT FACE BS500C AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 75 REV: -. PART NUMBERSDR SWAA2023020182731Angle · crackedCRACK ANGLE - CLIP LOCATED FWD FACE BS500B AT LEVEL STR26L FWD CARGO COMPARTMENT 2022-695460<[01] REPLACED ANGLE - CLIP LOCATED BS500B AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG NO. 143A7505; SHEET 75; REVSDR SWAA2023020182730Gusset · crackedCRACK GUSSET LOCATED BS500D AT LEVEL STR19L FWD CARGO COMPARTMENT 2022-695455<[01] REPLACED NEW GUSSET AND FASTENERS LOCATED BS500D AT LEVEL STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 STEP 9 AND SRM 51-40-02 AND DWG 143A7902 SHEET 69 REV: C. SEE INSDR DALA2022121908170Skin · gouged(LOG 2542937) DURING INSPECTION FOUND DENT + GOUGE ON FUSELAGE SKIN STA 264.25 BTW STRG 5LH & 6LH. DAMAGE REPAIRED PER ERA 604475-14.SDR DALA2022121908208Repair · misrepairedREPAIR DUE DISCREPANT PLUGS ON EXTERNAL DOUBLER BETWEEN BS 660 - 760 AND STRINGERS 4R & 4L. EXTERNAL DOUBLER WAS REPAIRED PER ER/A 604249-14 REV: A, SECTION I.SDR 2022F00520Skin · debondedSHIN DISBONDED BETWEEN BS 360 AND BS 500C, S-14L TO S-19-LSDR SWIA2023011967128Skin · dentedRIGHT FUSELAGE SKIN AT AEB DOOR CUTOUT NEAR BS 682 HAD A PROTRUDING DENT. REPAIRED THE SKIN IAW SRM 53-00-31, REPAIR 3, STEPS 4.A. (1)-(12) , ADDITIONAL 7EA DENTS IDENTIFIED NEAR BS 688 REWORKED AND FOUND TO BE WITHIN LIMITS IAW REO 601R-53-61-7935 REV -.SDR FDEA202212150099Skin · gougedUPPER FUSELAGE - UPPER CARGO DOOR AREA - LOWER FORWARD EXTERNAL SKIN IS DAMAGED, ADJACENT TO THE DOOR SEAL RETAINER (MARKED). REPAIRED DAMAGED SKIN AT LOWER FORWARD AREA OF UPPER CARGO DOOR, REF SRM 53-00- 15-2R, REPAIR 8 FIGURE 203, SHEET 3.SDR SWAA2022121681998Skin · buckledEXTERNAL LOWER SKIN BUCKLED AT BS 818 COMMON TO KEEL BEAM, STRINGER 27L. C/W EA 22-153-03634-WIP5. INSPECTED WORK. REPAIRED PER EA 22-153-03634SDR CALA2022121603406Skin · unknownSKIN RPR BETWEEN FR33-35 STR1R DUE TO STR1R RPR REF ELB LP 3323039. @ INTERVALS OF 2400FC/4800FH REF SRI 53-21-11-205-071 TABLE 001 ZONE D. AIRCRAFT PTT 34577FC/88004FH. INITIATE DIP TO ACP EDDY CURRENT INSP FROM TIME OF ADL/RPR EMBOD 40500FC/81000 @ SUBSEQUENSDR CALA2022121603405Skin · noneAFT OF FR34 STR1R, 1EA ADDITIONAL FASTENER FOUND BETWEEN 2EA PRODUCTION FASTENERS WITH DAMAGE TO INTERNAL STR. REF SRI 53-21-13-300-018 TABLE 001. CURRENT PTT 34577FC/88004FH. INITIATE DIP TO ACCOMPLISH HFEC INSP THRESHOLD FROM TIME OF ADL/ RPR EMBODIMENT 4800SDR 2022F00499Skin · debondedSKIN DISBONDED BETWEEN BS 727 AND BS 727G AT UPPER ROR OF FASTENERS AT S-25R LAP SEAMSDR SWAA2023012681823Doubler · crackedELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER EDGE SIDE HAS A CRACK AT APROX BS 235.8 BELOW MIDDLE OF LATCHING DOOR AREA. TRIMMED OUT THE DAMAGED AREA OF THE ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER IAW SRM 53-10-15-2R-4 REPAIR 4. PERFORMEDSDR SWAA2022122981735Clamp · crackedCRACK ON CLIP LOCATED AT FWD CARGO COMPARTMENT AT BS400 AFT FACE AT LEVEL OF STRG26L 2022-688568<[01] REPLACED CLIP LOCATED AT FWD CARGO COMPARTMENT AT BS400 AFT FACE AT LEVEL OF STRG26L IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 REV B<BR>SEE INDIVISDR SWAA2022122981736Clamp · crackedCRACK ON CLIP LOCATED AT FWD CARGO COMPARTMENT ON BS440 AFT FACE AT LEVEL OF STRG26L 2022-688569<[01] REPLACED CLIP LOCATED AT FWD CARGO COMPARTMENT ON BS440 AFT FACE AT LEVEL OF STRG26L IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 REV B<BR>SEE INDIVISDR SWAA2022122981737Fastener · crackedCRACK ON CLIP LOCATED AT FWD CARGO COMPARTMENT ON BS500C AFT FACE AT LEVEL OF STRG26R 2022-688570<[01] REPLACED CLIP AND FASTENERS LOCATED AT FWD CARGO COMPARTMENT ON BS500C AFT FACE AT LEVEL OF STRG26R IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505 REVSDR AALA202301030278Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AND A CRACK ON FUSELAGE SKIN AT LAVATORY VENT PORT AT BS 917 BETWEEN S21L AND S22L. MAINTENANCE REPAIRED SKINPER SRM 53-70-01-R2-3SDR SWIA202266973Skin · damagedAFTER COMPLETION OF SECTION 2 INTERMEDIATE ACTION OF ETD 2022-170-036415 BY USE OF HIGH FREQUENCY EDDY CURRENT INSPECTION; FOUND SUSPECTED DAMAGE NOT DOCUMENTED ON ORIGINALLY SUBMITTED ETD. DAMAGE REQUIRES FURTHER INVESTIGATION AND EVALUATION. EVALUATED THSDR A6WA202212138410Skin · noneTEMPORARY REPAIR TO FUSELAGE SKIN AT BS 257.75, S15L. DENT MEASURES 0.55" X 0.4" X 0.004" DEPTH - HAS BEEN COMPLIED WITH IAW EA AWAC-CRJ253-01543. PERFORMED PERMANENT REPAIR AS REQUIRED ****AIRCRAFT REMOVED FROM SERVICE**** COMPLIED WITH REO 601R-53-11-3811 SDR A6WA202212118421Skin · corrodedEXTERIOR SKIN UNDER FORWARD DRAIN MAST CORRODED. AIRCRAFT REMOVED FROM SERVICE. BLENDED & CUT OUT CORROSION AND INSTALLED EXTERNAL DOUBLER IAW EA AWAC-CRJ253-01922.SDR MK1Y20221211008Skin · noneEXTERNAL FUSELAGE SKIN B/T STA 1809.5 AND 1824 ABOVE STR 22L EXISTING UNDOCUMENTED DOUBLER REPAIR.SDR MK1Y20221211007Skin · damagedDURING MAINTENANCE INSPECTION AT IAI, SHOP FOUND A SUNKEN FASTENER HEAD ON THE EXTERNAL FUSELAGE SKIN AT STA 1728.5, STR 22R. IN ADDITION, 2.2” FROM THE NOTED AREA, SHOP PERFORMED CORROSION CLEANUP AND NDT THICKNESS INSPECTION ON THE EXTERNAL SKIN AND EOUND THSDR MK1Y20221211006Skin · corrodedSEC 43, BETWEEN STA 434 TO STA 456, STR 39L: SHOP FOUND CORROSION ON STR-39L, AFTER THE CORRODED STRINGER REMOVED (NEW STRINGER WERE ORDERED), SHOP FOUND CORROSION ON THE INNER SKIN. NDT PERFORMED H.F.C. INSPECTION AND CORROSION WAS FOUND, PERFORMED CLEANUP COSDR MK1Y20221211001Skin · dentedBS 1419, S36L, FOUND A DENT APPROX. 2” INCHES FROM AN EXISTING LARGE REPAIR.SDR VNAA2022121100001Skin · damagedPERFORMED 60 EACH BLENDS ON LOWER RT FUSELAGE SKIN EXTERIOR PANEL AT FS 1028.3 - 1044, S21-26R IAW EA 22-C7-53-1500 REV IR. ACCOMPLISHED HFEC INSPECTION AT EACH BLEND AREAS AND DENTS IAW NDT MANUAL PART 1 51-20-06, REV 36 AND EA 22-C7-53-1500, REV IR. NO INDSDR DALA2022121308083Skin · not reportedSHIP 3305 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR.30 TO FR.31 BTW STR1L TO STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER 2325-01059-03. INSTALLATION IS APPROVED BY STC . STC IS APPROVED FOR DAMAGE SDR SIMA2023010629001Skin · crackedACCOMPLISH EO-EJ-53MA-066, REWORK TO REAR FUSELAGE UPPER SKIN BY ADDING STRUCTURAL REINFORCEMENT. MAJOR REPAIR. ACCOMPLISHED REWORK AND REPAIR TO REAR FUSELAGE UPPER LT AND RT SKIN PANELS IAW EO-EJ-53MA-066 AND ERS-EJ-53MR-4686.SDR DALA2022121308085Skin · corrodedCENTER WING BOX UPPER SKIN PANEL U- 10, RBL 52.00 TO RBL 70.50 CORRODED. REPAIRED IAW ERA 603536-14.SDR DALA2022121208000Skin · nickedSHIP 3157 - NICK EXTERNAL SKIN LOCATED BTW FR 2 TO FR 3 AND 8 INCH BELOW OF LH S IDE STRINGER AT LOWER FUSELAGE. REWORKED AREA AS PER A319 SRM 51-73-00 AND EVALUATED AREA FOUND OUT OF LIMITS AS PER A319 SRM 53-11-11-283-011FIG.001;FIG.002. (2531296)SDR SCNA20230110034Skin · damagedDEFECT JC 802558 NR 00265: REPAIR AT STA 1016+6 BETWEEN STR 13L & STR14L. RESOLUTION: ACCOMPLISHED REPAIR AT STA 1016+6 BETWEEN STR 13L AND 14C IAW SCA ENG-53SCA-11093 REV 00.SDR R61A2022120900773Skin · gougedWHILE IN HEAVY CHECK - REAR FUSELAGE EXTERNAL LOWER SKIN HAS 2 EACH GOUGES AT FRAME 93-95 STRINGER 29R- 29L. PERFORMED PERMANENT REPAIR ON REAR FUSELAGE EXTERNAL LOWER SKIN BETWEEN FR 92-95 STGR 29L-29R. REF EMB SRM 53-30-01/REPAIR 13P.SDR DALA2022120907938Skin · crackedHFEC INSPECTION FOUND ONE CRACK APPROX. 0.60 INCH IN LENGTH ON THE FUSELAGE SKIN BELOW THE 7TH STRINGER-ATTACH RIVET ALONG S13R, AFT OF FRAME BS 1654.5 IAW W/C 5330- 01229-01B STEP 4. THE CRACKED AREA OF SKIN TRIMMED OUT AND REPAIRED IAW SRM 53- 80-01-2R-7, RSDR DALA2022120907937Skin · crackedHFEC INSPECTION FOUND 01EA CRACK APPROX. 0.90 INCH IN LENGTH ON THE FUSELAGE SKIN BELOW THE 13TH STRINGER-ATTACH RIVET ALONG S-14R, FORWARD OF FRAME STA1654.5. THE CRACKED AREA OF SKIN TRIMMED OUT AND REPAIRED AS PER SRM 53- 80-01-2R-7 REPAIR 7 FIG201 RELEASSDR NACA202212080500Skin · debondedFUSELAGE SKIN DISBOND BS360 AND BS500C AT UPPER ROR OF FASTENERS AT THE S-26L LAP SEAM.
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