JASC 5321
Service difficulty reports · 49,350
Reports filed under 5321 · Fuselage Floor Panel, 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 = '5321' 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 = '5321' 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 DALA2023020200831Not Entered · not enteredSHIP 689 CORROSION ON RH SIDE PANEL (UPPER SURFACE) FROM STA. 620 TO 645 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00208: RH SIDE PANEL FROM STA. 560 TO 645 AT FWD CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2610408)SDR SWAA2023030897321Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL #241XF; UPPER SURFACE DELAMINATED DOT 223-PCF241XF.<[01] RECEIVED NEW PANEL 241XF; PO#2005897. PANEL WILL BE INSTALLED ON TTG8Q00H2SLP.;[02] VERIFIED AND INSPECTED STEP #1.SDR SWAA2023030897333Floor Panel · crackedFLOOR PNL 242SF HAS CRACK ON UPPER SURFACE. 8-25<[01] RECEIVED NEW PANEL 242SF PO#2005895. PANEL WILL BE INSTALLED ON TTG8Q00H2URQ.;[02] VERIFIED AND INSPECTED STEP #1.SDR DALA2023020100807None · noneSHIP 3122 - CORROSION WEB AT LEVEL FR20 AND FLOOR BEAM -Y1584 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB AT LEVEL FR20 TO FR24 AND FLOOR BEAM -Y1584 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11. (2608719)SDR DALA2023020100803None · noneSHIP 3122 - CORROSION SHEAR TIE LOC. FR29 BTW STR 40 TO STR 41 R/H IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOC. FR29 BTW STR 40 TO STR 41 R/H IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11. (2608763)SDR DALA2023020100802None · noneSHIP 3122 - CORROSION FLOOR STRUCTURE WEB LOWER SURFACE LOC BTW FR 69 AND FR 70 STR 23 R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE WEB LOWER SURFACE LOC BTW FR 69 AND FR 70 STR 23 R AT AFT GALLEY AREA AS PER A319 SRM 51-72-11. (2608701)SDR DALA2023013100793None · noneSHIP 689 CORROSION ON FLOOR SUPPORT ANGLE BTW STA 720 AND 740 LBL 65 IN REF NRC 00478 WIP #7. CORRECTIVE ACTION: SUMMARY OF NRC 572: REPAIR PARTS WERE REPLACED PER DWG AND PER B757-200 SRM. (2606157)SDR SWI2023F00037Unknown · corrodedCORROSION ON FS 280.00 FLOOR SUPPORT BEAM BETWEEN LBL 12 - RBL 12 (C-CHECK RO 3/11/2023) REPAIRED FS 280.00 FLOOR SUPPORT BEAM BETWEEN LBL 12 - RBL 12 REF REO 601R-53-11-136, REV: A 2007-11-01 DWG 600-34017 REV AD C/W 51-900-1003-SKYSDR SWI2023F00036Unknown · corrodedCORROSION ON FLOOR BEAM LBL 9 TOP INBD FLANGE BETWEEN FS 409.00 - 409.00+128 (C-CHECK RO 3/11/2023) REPLACED FLOORBEAM BETWEEN FS409 AND FS409+128 PER REO 601R-53-31-1260 (REV --) DATED 2023-02-07 AND DRAWING 601R31117 (REV E). COMPLETED SKYWEST TASK CSDR SWI2023F00007Unknown · corrodedCORROSION ON FS 280.00 FLOOR SUPPORT BEAM BETWEEN LBL 12 - RBL 12 (C-CHECK RO 3/11/2023) REPAIRED FS 280.00 FLOOR SUPPORT BEAM BETWEEN LBL 12 - RBL 12 REF REO 601R-53-11-136, REV: A 2007-11-01 DWG 600-34017 REV AD C/W 51-900-1003-SKYSDR SWI2023F00006Unknown · corrodedCORROSION ON FLOOR BEAM LBL 9 TOP INBD FLANGE BETWEEN FS 409.00 - 409.00+128 (C-CHECK RO 3/11/2023) REPLACED FLOORBEAM BETWEEN FS409 AND FS409+128 PER REO 601R-53-31-1260 (REV --) DATED 2023-02-07 AND DRAWING 601R31117 (REV E). COMPLETED SKYWEST TASK CSDR SWAA2023022796656Floor Panel · delaminatedCABIN FLOOR PANEL #231XF DELAMINATED.<[01] RECEIVED NEW FLOOR PANEL. INSTALLATION WILL BE ACCOMPLISHED ON ITEM TTG8Q00GK97E.;[02] RECEIVED NEW FLOOR PANEL 231XF. INSTALLATION WILL BE ACCOMPLISHED ON ITEM TTG8Q00GK97E.;[03] VERIFIED STEP #2.SDR SWAA2023022796657Floor Panel · delaminatedCABIN FLOOR PANEL #241AF DELAMINATED.<[01] RECEIVED NEW FLOOR PANEL 241AF. INSTALLATION WILL BE ACCOMPLISHED ON ITEM TTG8Q00GK972.;[02] VERIFIED STEP #1.SDR DALA2023013100792None · noneSHIP 6815 SECONDARY NRC, IN REF NRC: 00233: CORROSION ON LH SIDE PANEL (UPPER AND LOWER SIDES) BTW STA 1310-1410 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00580: (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED, AREA BTW STA 1310 / STA 1410 IT IS SDR AALA202301310372Floor Panel · delaminatedAIRCRAFT WAS GROUNDED: AFT CARGO COMPARTMENT FLOOR PANEL 151DF DELAMINATED. MAINTENANCE REPLACED FLOOR PANEL PER AMM 53-42-14.SDR SWAA2023030694809Floor Panel · tornFLOOR PANEL 221BF HAS AREAS OF TORN SKIN AND CORE<[01] IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2 <BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 E(2)<BR><BR>DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-6<BR><BR>REMOVED DAMSDR SWAA2023021595373Floor Panel · pulledCABIN FLOOR BOARD 242BF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX4.;[02] C/W INSPECTION.SDR SWAA2023021595372Floor Panel · pulledCABIN FLOOR BOARD 241FF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX6.;[03] C/W INSPECTION.SDR SWAA2023021595365Floor Panel · pulledCABIN FLOOR BOARD 241EF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX8.;[03] C/W INSPECTION.SDR SWAA2023021595364Floor Panel · pulledCABIN FLOOR BOARD 241DF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXA.;[03] C/W INSPECTION.SDR SWAA2023021595371Floor Panel · pulledCABIN FLOOR BOARD 241CF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXC.;[03] PART ADDED.;[04] C/W INSPECTION.SDR SWAA2023021595363Floor Panel · pulledCABIN FLOOR BOARD 241BF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXE.;[03] C/W INSPECTION.SDR SWAA2023021595370Floor Panel · pulledCABIN FLOOR BOARD 241AF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXG.;[03] C/W INSPECTION.SDR SWAA2023021595362Floor Panel · pulledCABIN FLOOR BOARD 232SF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXL.;[03] C/W INSPECTION.SDR SWAA2023021595369Floor Panel · pulledCABIN FLOOR BOARD 232RF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXN.;[03] C/W INSPECTION.SDR SWAA2023021595368Floor Panel · pulledCABIN FLOOR BOARD 231ZF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXQ.;[03] C/W INSPECTION.SDR SWAA2023021595361Floor Panel · pulledCABIN FLOOR BOARD 231YF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXS.;[03] C/W INSPECTION.SDR SWAA2023021595360Floor Panel · pulledCABIN FLOOR BOARD 231XF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRXU.;[03] C/W INSPECTION.SDR SWAA2023021595367Floor Panel · pulledCABIN FLOOR BOARD 242AF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWS0B.;[03] C/W INSPECTION.SDR SWAA2023021595359Floor Panel · pulledCABIN FLOOR BOARD 242CF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX2.;[03] C/W INSPECTION.SDR SWAA2023021595366Floor Panel · pulledCABIN FLOOR PANEL 242DF HAS NUMEROUS DENTS AND PULLED FIBERS<[01] REMOVED PASSENGER CABIN FLOOR PANEL PER AMM 53-21-00.;[02] RECEIVED SERVICEABLE PANEL FROM STOCK; TO BE INSTALLED ON TASK CARD TTG8Q00GWRX0.;[03] C/W INSPECTION.SDR SWAA2023021595376Panel · deformedFLIGHT COMPARTMENT FLOOR PANEL 211AF DEFORMED<[01] LOCATED AND DRILLED NEW ACCESS PANEL PER SRM 51-40-05.;[02] C/W INSPECTIONSDR DALA2023013100799None · noneCRACK SHEAR PLATE RH SIDE BTW FR 69 AND FR 70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE RH SIDE BTW FR 69 AND FR 70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11; A321 SRM 51-72-11 AND DWGD53474180; ISSUE: Z; RELEASE DATE: 14 JUL 22. MEASURE OF CRACK: 0.200 INCH.SDR DALA2023013100798None · noneCRACK SHEAR PLATE LH SIDE BTW FR 68 AND FR 70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE LH SIDE BTW FR 68 AND FR 70 AT AFT GALLEY AREA AS PER A321 SRM 51-42-11; A321 SRM 51-72-11 AND DRAWINGD53474180; ISSUE: Z; RELEASE DATE: 14 JUL 22. MEASURE CRACK: 0.250 INCHSDR DALA2023012500622Frame · corrodedSHIP 3309 CORROSION RBL 48 TO RBL 62 FRAME 73.10. CORRECTIVE ACTION: REMOVED AND REPLACED PER A330 SRM 51-72-11. (2598145)SDR DALA2023012500621Frame · corrodedSHIP 3309 CORROSION RBL 62 FRAME 71 TO 73. CORRECTIVE ACTION: REMOVED AND REPLACED PER A330 SRM 51-72. (2598139)SDR DALA2023012500620Frame · corrodedSHIP 3309 CORROSION RBL 62 FRAME 73 TO 74. CORRECTIVE ACTION: REMOVED AND REPLACED PER A330 SRM 51-72-11. (2598123)SDR SWIA20230123Not Reported · crackedCRACKED ANGLE - COCKPIT FLOOR STRUCTURE FR 12, BL 0.0 LOWER RADIUS. (C-CHECK RO 2/6/2023) REMOVED, REPLACED AND RESTORED SURFACE PROTECTION TO ANGLE BRACKET ON COKPIT FLOOR STRUCTURE AT FR 12. REF EMB SRM 51-40-08, SRM 51-23-06, AND CPM 51-25-00 PO# 291SDR DALA2023012400593Floor Panel · puncturedBULK CARGO COMPARTMENT, LEFT AFT CARGO FLOOR PANEL HAS NUMEROUS PUNCTURES. REPAIRED PUNCTURED PANEL @ BULK CARGO L/H AFT FLOOR PANEL REF A330-300 SRM 53-02-00.SDR SWAA2023020894116Floor Panel · crackedMAIN CABON CENTER WING BOX FLOOR SUPPORT BREAK CRACKED @ LBL-1 STA 540 WATER LINE 182<[01] REMOVED CABIN FLOOR PANEL 231UF FOR ACCESS AS PER 53-21-00-000-801.;[02] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT BREAK AT LBL-1 STA-540 IN REFERENCE B-737-700 SRM 5SDR AALA202301235298Floor Panel · peelingAIRCRAFT WAS NOT GROUNDED: AFT CARGO COMPARTMENT FLOOR PANEL AT DOOR PEELING UP. MAINTENANCE REPLACED FLOOR PANEL PER AMM 53-42-14.SDR SWAA2023022193821Floor Panel · perforatedPERFORATION FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2023-83427<[01] REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT AIW B737-700 AMM 25-52-01-201-801;[02] CERTIFIED WORK PERFORMED.SDR SWAA2023021693554Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 242DF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4; TABLE 4; AND DWG DOC: 144A5800 ID: 0004. <BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR. 4.C. & FSDR SWAA2023021693555Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 241CF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4 AND DWG: 144A5810 ID: 0019.<BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.C AND 4.F.<BR><BSDR SWAA2023021693552Floor Panel · pulledFLOOR PANEL 241FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIG 4 TABLE 4 LOW TRAFFIC<BR>NUMEROUS PULLED STRANDS DENTS & HEAL STRIKES EXCEEDS ALLOWABLE DAMAGE LIMITS & IS BEYOND ECONOMICAL REPAIR . AS SDR SWAA2023021693546Floor Panel · pulledFLOOR PANEL 231XF UPPER SURFACE HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] IDENTIFIED PANEL 231XF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4 AND DWG: 144A5810 ID: 0007.<BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.C AND 4.F.<BRSDR DALA2023012300478Support Fitting · corrodedSHIP 689 SECONDARY NRC IN REF NRC. 00472: CORROSION ON FITTING SUPPORT STA.1672 OF LOWER SILL R4. CORRECTIVE ACTION: SUMMARY OF NRC 00545: FITTING SUPPORT STA .1672 OF LOWER SILL R4 WAS REPLACED PER B757-200 SRM. (2592049)SDR DALA2023012300476Web · corrodedSHIP 6815 CORROSION ON WEB FROM STA 740 TO STA 780 BETWEEN S-27L AND S-26L.FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00244: WEB FROM STA 740 TO STA 780 BETWEEN S-27L AND S-26L.FWD CARGO COMPARTMENT WAS REPAIRED SRM. (2590680)SDR FDEA202301200142Fastener · missingCENTER ACCESSORY COMPARTMENT - BELOW CABIN FLOOR AND RIGHT OF FUSELAGE CENTER LINE AT STATION 6-80 TO 6-100, X= -8.5 HAS SEVERAL FLOOR PANEL FASTENERS MAKING CONTACT WITH THE SEAT TRACK FLANGE CAUSING DAMAGE. CABIN FLOOR AND RIGHT OF FUSELAGE CENTER LINE SDR FDEA202301200141Fastener · missingCENTER ACCESSORY COMPARTMENT - BELOW CABIN FLOOR AND LEFT OF FUSELAGE CENTER LINE AT STATION 6-80 TO 6-100, X=8.5 HAS SEVERAL FLOOR PANEL FASTENERS MAKING CONTACT WITH THE SEAT TRACK FLANGE CAUSING DAMAGE. CABIN FLOOR AND LEFT OF FUSELAGE CENTER LINE AT S
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