JASC 5300
Service difficulty reports · 8,204
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 SWAA2023090585553Vapor Barrier · crackedCUSTOMER REQUEST EVALUATE CRACK ON VAPOR BARRIER LH SIDE BSTA 663 2023-491653<[01] TOOL USED CALIPER: PN: 500-197-30 SN: B20189416; DUE DATE: 19-DEC-23.;[02] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 24-SEP-23.;[03] TOOL USED SCALE P/N: CL50SDR SIMA20230803016Unknown · unknownSSI 53-10-027 FWD GALLEY RH FLOOR BEAM GUSSETT CORRODED AT FR 17 (LEVEL 2 CORROSION) (MAJOR REPAIR)-C/A-REPAIRED THE FWD GALLEY RH FLOOR BEAM GUSSET AT FR 17 IAW ERJ 170 SRM 53-10-10/ REPAIR 01P.SDR IPXA2023083064708Frame · dentedAFT CARGO COMPT, FRAME STA 1320, FOUND DENT AT S-26L. MAJOR REPAIR. REVIEWED.PERFORMED CUTOUT OF DAMAGED AREA.PERFORMED SURFACE HFEC INSP AT FRAME STA 1320, S-25L TO S-26L.CRACK AND SURFACE AREA DEFECT FREE AT THIS TIME IAW SRM 53-00-07-2R-5.SDR IPXA2023083064680Frame · dentedFAULT: AFT CARGO COMPT, FRAME STA 1260, FOUND DENT, BETWEEN S-25R TO S-26R. MAJOR REPAIR. REVIEWED.PERFORMED CUTOUT OF DAMAGED AREA.PERFORMED SURFACE HFEC INSP AT FRAME STA 1260, S-25R TO S-26R.CRACK AND SURFACE AREA DEFECT FREE AT THIS TIME IAW SRM 53-00-07-2SDR IPXA2023083064606Frame · dentedFAULT: AFT CARGO COMPT, FRAME STA 1320, FOUND DENT, BETWEEN S-25R TO S-26R REVIEWED. DEFERRAL REQUIRED.PERFORMED CUTOUT OF DAMAGED AREA.PERFORMED SURFACE HFEC INSP AT FRAME STA 1320, S-25R TO S-26R.CRACK AND SURFACE AREA DEFECT FREE AT THIS TIME IAW SRM 53-00-SDR IPXA2023083064568Frame · dentedFAULT: AFT CARGO COMPT, FRAME STA 1440, FOUND DENT AT S-25L. REVIEWED. DEFERRAL REQUIRED.PERFORMED CUTOUT OF DAMAGED AREA.PERFORMED SURFACE HFEC INSP AT FRAME STA 1440, S-25L. CRACK AND SURFACE AREA DEFECT FREE AT THIS TIME IAW SRM 53-00-07-2R-5.SDR IPXA2023083064558Frame · dentedFAULT: AFT CARGO COMPT, FRAME STA 1580 FOUND DENT AT S-26L. MAJOR REPAIR. REVIEWED.PERFORMED SURFACE HFEC INSP AT FRAME STA 1580 S-26L.CRACK AND SURFACE AREA DEFECT FREE AT THIS TIME IAW SRM 53-00-07-2R-5.SDR IPXA2023083064541Frame · dentedAFT CARGO COMPT, FRAME, STA 1480 L/H AT S-25L TO S-26L FOUND DENT. MAJOR REPAIR. REVIEWED.PERFORMED SURFACE HFEC INSP AT FRAME STA 1480, S-25L TO S-26L. CRACK AND SURFACE AREA DEFECT FREE AT THIS TIME IAW SRM 53-00-06-1A-1.SDR IPXA2023083063960Frame · dentedFAULT: AFT CARGO COMPT, FRAME, STA 1460, R/H, AT S-26R, FOUND DENT. MAJOR REPAIR. REVIEWED.PERFORMED CUTOUT OF DAMAGED AREA. PERFORMED SURFACE HFEC INSP AT FRAME 1460 STA S26-R. THE CUTOUT EDGES AND SURROUNDING SURFACE ARE CRACK ARE DEFECT FREE AT THIS TIME IASDR CALA2023080902468Screw · missingPDA 3 ONE SCREW MISSING ON PANEL 191DL FWD SIDE. REINSTALLED NEW SCREW. REMAINING SCREWES ARE OK ON SAME PANEL.SDR SWAA2023080485299Panel · delaminatedPANEL 193B DELAMINATED<[01] REMOVED AND REPLACED PANEL PER AMM 53-51-21 AND SRM 51-40-02SDR SWAA2023090584933Panel · crackedCRACK ACCESS PANEL 192F BODY STATION 616 MARKER BEACON ANTENNA KEEL BEAM 2023-477632<[01] REPLACED MARKER BEACON ANTENNA KEEL BEAM IAW AMM 34-32-11-000-802 AND 34-32-11-400-802.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED MARKER BEACON ANTENNA KEEL BEAM IASDR SWAA2023083085192Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727G TO 727H.<[01] FINAL SIGN OFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFSDR SWAA2023083085194Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727H TO 727J.<[01] FINAL SIGN OFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFSDR SWAA2023083085197Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727J TO 747.<[01] FINAL SIGN OFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFSDR SWAA2023083085220Web · corrodedAFT CARGO DOOR ENTRY WEB BELOW THRESHOLD HAS SIGNS OF MINOR SURFACE CORROSION<[01] REMOVED CORROSION WITH .003? MATERIAL LOSS OUT OF .050? ORIGINAL WHICH IS WITHIN ALLOWABLE LIMITS PER SRM 53-6015-1A-1. ALODINED AND PRIMED PER SRM 51-20-01;[02] REMOVED CORROSISDR SWAA2023083085219Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 747 TO 767.<[01] FINAL SIGNOFF TO BE ACCOMPLISHED ON TTG8Q00ML0YFSDR SWAA2023083085198Angle · corrodedAFT CARGO RIGHT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 767 TO 787.<[01] REJECT: IN THE MEASUREMENTS SECTION; ITEM #20 STATES 'YES' FOR THERE BEING A PICTURE ATTACHED WHEN THERE ARE NO PICTURES CURRENTLY ATTACHED. SEE STEP #1 FOR REJECT.;SDR SWAA2023083085199Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727C TO 727D.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;SDR SWAA2023083085200Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727D TO 727E.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;SDR SWAA2023083085201Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727F TO 727G.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .003. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;SDR SWAA2023083085221Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727E TO 727F.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;SDR SWAA2023083085222Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727G TO H<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;[02]SDR SWAA2023083085223Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727H TO 727J.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;SDR SWAA2023083085202Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 727J TO 747.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;[SDR SWAA2023083085224Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS CORROSION IN/AROUND NUTPLATE HOLES AT BS 747 TO 767.<[01] REMOVED DAMAGE PER SRM 51-10-02. FOUND WITHIN ALLOWABLE LIMITS PER SRM 53-00-53-1A-2. MATERIAL LOSS OF .002. TREATED PER SRM 51-20-01 AND PRIMED PER SOPM 20-41-02.;[0SDR IPXA2023081352701Fitting · brokenFAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN AT STA ( 870 & 890 ) RBL47.5 & STA890 BL0 & STA ( 999 & 1087 & 1131 ) LBL47.5 TTL: 6EA(REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.139 RESTORED MAIN DECK CARGO HANDLING<BSDR SWAA2023080884686Hinge Pin · brokenA255 -025 PANEL 192G CENTER TANK SUMP PANEL HINGE PIN BROKEN.<[01] REPLACED HINGE PIN OF PANEL 192G CENTER TANK SUMP IAW AMM 53-51-21-000-802 STEP 4.E.5.A.7. AND 53-51-21-400-802 STEP 5.I.2.D.G . <BR><BR>ISSUE TAG A197417;[02] REPLACED HINGE BRAKET P/N MS20001SDR TAMF20230803036Unknown · unknownDURING THE AIRCRAFT LOADING PROCEDURE FOR FLIGHT NO. 4052 VCP BRAZIL – BOG COLOMBIA, THE AMOUNT OF WEIGHT (1452 KG) WAS EXCEEDED IN THE CARGO POSITION (CER) AND 6 FLIGHTS WERE PERFORMED AFTER THIS EVENT. THE AIRCRAFT MANUFACTURER IS PERFORMING THE ANALYSIS OFSDR CALA2023080202400Unknown · corrodedFWD ACCY COMPARTMENT STA 227 BL 2R CHORD HAS CORROSION. ON OR BEFORE THE ACCIMULATION OF 50000 TOTAL FLT CYCLES, PERFORM STA 227.8 & RBL 24 AND TO THE REPAIR ON THE SKIN AND BEAR STRAP LATEST REVISION OF ECRA 5311-03042. REF AERSAL EO 5330-23020 AS AN INSPECTISDR SROM0073120231Panel · chafedCHAFE DAMAGE TO THE UPPER PANEL PN: 85217068 OF THE AIRSTAIR DOOR ASSEMBLY PN: 85217005-001. DAMAGE REQUIRES BLENDING AS PER DE HAVILLAND REPAIR DRAWING 8/4-52-227.SDR SWAA2023090584072Panel · crackedCRACK ACCESS PANEL 194BR BODY FAIRING AT LOWER FUSELAGE 2023-477520<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED SCALE P/N:CR5200 S/N:8342514510 DUE DATE: 13-FEB-24;[03] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 151023SDR SWIA202309080729Unknown · cracked*FS333.00 STRG 0 - STRG 1LH, FRAME POSSIBLY CRACKED AT LOWER MACHINE HOLE (MARKED) 26957001 (C-CHECK RO 9/6/2023) REPAIRED FS333.00 STRG 0 - STRG 1LH, FRAME REO 601R-53-21-3642 REV -- DATE 2023-08-11. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CSDR DALA2023073106173Unknown · unknownWASTE BOX CORRODED AT LOWER FWD CUT OUT AREA. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0085:5360-2017/001 00102 COMPLIED WITH ER/A 610625-14 PRI REV 0, ER/A 610625-14 PRI REV 1, AND FINAL ER/A 610625-14 REV ORIGINAL. SUMMARY SEE NR FOR ADDITIONAL INFORMATSDR CALA2023073102376Plate · corrodedMAIN CABIN FR70 CORROSION AROUND FASTENER HOLE ON LH LATERAL SHEAR PLATE PER HAECO LCQ N/R 9296749/36749 GEN BY V061708SDR DALA2023072906152Unknown · unknownAIRCRAFT 676, A.D. A.A. AWR "EXISTING REPAIR WAS FOUND IN THE INSPECTION AREA AT STA 1640 I-14F (S-14R). CONTACT LIAISON ENGINEERING TO DETERMINE ADDITIONAL INSPECTION FOR THE REPAIRED AREA". CORRECTIVE ACTION: AREA WAS REPAIRED PER PRI 591624-14 REV 4 AND ER/SDR DALA2023080306287Unknown · unknown(LOG 2889726) THE NOSE WHEEL WELL ACCESS DOOR PANEL 114AC WAS FOUND CORRODED AND REPAIRED. COMPLETED SECTION II OF ER/A 593147-14, REV A OR LATER.SDR DALA2023072906151Unknown · unknownAIRCRAFT 690, CORROSION ON INTERCOSTAL LOWER FLOOR STRNGER RBL 2.90 BETWEEN LBL STA. 1500-1520 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: INTERCOSTAL LOWER FLOOR STRNGER RBL 2.90 BETWEEN LBL STA. 1500-1520 AT AFT CARGO COMPARTMENT WAS FABRICATED PER BOEING DSDR DALA2023072906150Unknown · unknownAIRCRAFT 667, CORROSION ON INTERCOSTAL BTW STA 1420 - 1440 , RBL11 ALSO BTW STA 1500-1520, S-30 TO S-29R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: INTERCOSTAL BTW STA 1420 - 1440, RBL11 ALSO BTW STA 1500-1520, S-30 TO S-29R AT AFT CARGO COMPARTMENT WERE REPSDR DALA2023072906149Unknown · unknownAIRCRAFT 667, CORROSION ON FLOOR SUPPORT STA 595 LBL16 BILGE AREA AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SECTION FLOOR STRINGER WAS REPLACED PER B757-200 SRM 51-40-02-0G PAR. 7. (LP 2889264)SDR DALA2023072906143Unknown · unknownAIRCRAFT 690, CORROSION ON FLOOR SUPPORT BETWEEN S 26R - S 26L AND STA 1640 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: FLOOR SUPPORT BTW S- 26R TO S-26L AND STA 1640 AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM 51-40-02-0G PAR. 7. (LP2888629)SDR DALA2023072906142Unknown · unknownAIRCRAFT 676, DURING HCK AT QRO, WHILE PERFORMING A BASE ZONAL INSPECTION PER WC 2020-2397, CORROSION WAS FOUND AT FUSELAGE SKIN, BETWEEN STA 810 TO 850 AND S-16R TO S-17R. CORRECTIVE ACTION: SUBSEQUENTLY THE CORROSION WAS BLENDED OUT PER B757-200 SRM 51-10-02SDR SWAA2023090583272Stiffener · crackedCRACK STIFFENER ASSY LOCATED BS540 BETWEEN BL0 TO LBL24.75 AT PASSENGER CABIN 2023-469920<[01] REPLACED STIFFENER ASSY LOCATED BS540 BETWEEN BL0 TO LBL24.75 AT PASSENGER CABIN IAW B737-700 #DWG: 143A0060 SHEET: 36 REV:ASEE INDIVIDUAL SIGNOFF BELOW.;[02] COMPLESDR DALA2023072906141Unknown · unknownAIRCRAFT 652, CORROSION ON ANGLE STA 296 BTW S23R OF ACCESS PANEL (116 AR) AT INNER SKIN NLG. CORRECTIVE ACTION: ANGLE STA 296 BTW S23R WAS REPLACED PER B757-200 SRM 51-40-02-0G AND DWG 141N3271 REV. D. (LP 2886605)SDR DALA2023072706099Unknown · unknownCORROSION AT ANGLES (2 EA) WAS FOUND DURING DOOR JAMB DISASSEMBLY. SUMMARY OF NRC 00196: CORROSION LEVEL 2. ANGLES (2 EA) WERE FABRICATED AND INSTALLED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7 AND 51-41-05-0G. (LP #2886801)SDR AALA202309015114Support · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT BULKHEAD SUPPORT ASSEMBLY AT BS 500I AND LBL 24. REPLACED SUPPORT ASSEMBLY PER AARD 51-00-05-1.SDR SIMA2023081426002Unknown · corrodedSSI 53-23-003 AFT CARGO COMPARTMENT SHEAR CLIP AT FR 83 BETWEEN STGR 27R-28R CORRODED (LEVEL 2 CORROSION)-C/A-RAR SHEAR CLIP AT FR 83 BTW STGR 27R-28R IAW EMB 170 SRM 51-40-08SDR DALA2023072906140Unknown · unknownAIRCRAFT 667, AWR. AD, AA, IN REFERENCE TO AMDS 5311-01218-01B STEP 4: EXISTING REPAIR WAS FOUND ON FRAME STA 1640 BTW STR9R-STR10, STR15R-STR16R AND ANGLE AT STR14R WITH IDENTIFICATION ER/A 571298-14 REV A. CORRECTIVE ACTION: ADDITIONAL MTC IS NOT REQUIRED PESDR SWAA2023072882172Bracket · crackedLEFT FWD WING TO BODY FAIRING SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED LH FWD WING TO BODY FAIRING SUPPORT BRACKET IAW SRM 51-40-02.SDR SWAA2023072882173Bracket · crackedRIGHT FWD WING TO BODY FAIRING SUPPORT BRACKET CRACKED<[01] REMOVED AND REPLACED RIGHT FWD WING TO BODY FAIRING SUPPORT BRACKET PER SRM 51-40-02. REMOVED AND REINSTALLED WING TO BODY FAIRING PANELS 191FR AND 191AR TO FOM PER AMM 53-1-21.
Back to JASC 5300