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 SWAA2024061385513Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 242DF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-002<[01] RECEIVED NEW FLOOR PANEL 242DF; IT WILL BE INSTALLED ON TTG8Q00S5CR7.;[02] VERIFIED STEP 1.SDR SWAA2024061385514Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 232SF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-003<[01] RECEIVED CABIN CENTER SECTION FLOOR PANEL 232SF WILL BE INSTALLED ON ITEM TTG8Q00TBLTB;[02] RECEIVED CABIN CENTER SECTION FLOOR PANEL 232SF WILL BE INSTALLED ON ITEM TTGSDR SWAA2024061385517Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 241FF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-004<[01] RECEIVED NEW FLOOR PANEL 241FF; IT WILL BE INSTALLED ON TTG8Q00S5CRD.;[02] VERIFIED STEP 1.SDR SWAA2024061385518Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 241AF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-005<[01] RECEIVED NEW FLOOR PANEL 241AF; IT WILL BE INSTALLED ON TTG8Q00S5CRP.;[02] VERIFIED STEP 1SDR SWAA2024061385520Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 231YF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-006<[01] RECEIVED NEW FLOOR PANEL 231YF; IT WILL BE INSTALLED ON TTG8Q00S5CS3.;[02] VERIFIED STEP 1.SDR SWAA2024061385522Floor Panel · peelingCABIN CENTER SECTION FLOOR PANEL 231XF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-007<[01] RECEIVED NEW FLOOR PANEL 231XF; IT WILL BE INSTALLED ON TTG8Q00S5CS5.;[02] VERIFIED STEP 1.SDR SWAA2024061385682Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241ADF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-012<[01] RECEIVED AFT CABIN FLOOR PANEL 241ADF WILL BE INSTALL ON ITEM TTG8Q00SCGYU;[02] RECEIVED AFT CABIN FLOOR PANEL 241ADF WILL BE INSTALL ON ITEM TTG8Q00SCGYW;[03] VERIFIED SSDR SWAA2024061385684Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241ACF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-015<[01] RECEIVED REPAIRED FLOOR PANEL 241ACF. <BR>P/N: 147A5810-13.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGYY.;[02] VERIFIED STEP 1SDR SWAA2024061385685Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 242VF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-016<[01] RECEIVED NEW FLOOR PANEL #242VF P/N:147A5810-350; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZD.;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILLSDR SWAA2024061385687Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241ABF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-018<[01] RECEIVED REPAIRED FLOOR PANEL 241ABF. <BR>P/N: 147A5810-88.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGZ1.;[02] VERIFIED STEP 1SDR SWAA2024061385688Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241AAF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-020<[01] RECEIVED NEW FLOOR PANEL # 241AAF P/N:147A5810-8; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZ3.;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILSDR SWAA2024061385690Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 242UF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-022<[01] RECEIVED NEW FLOOR PANEL # 242UF P/N: 147A5810-95; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZF;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILLSDR SWAA2024061385692Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241XF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-025<[01] RECEIVED REPAIRED FLOOR PANEL 241ABF. <BR>P/N: 147A5810-100.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGYJ.;[02] VERIFIED STEP 1SDR SWAA2024061385697Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241YF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-026<[01] RECEIVED REPAIRED FLOOR PANEL 241YF. <BR>P/N: 147A5810-77.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGZ7.;[02] VERIFIED STEP 1SDR SWAA2024061385698Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 241ZF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-027<[01] RECEIVED NEW FLOOR PANEL # 241ZF; P/N:147A5810-98; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZ5.;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILSDR SWAA2024061385693Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 242RF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-028<[01] RECEIVED NEW FLOOR PANEL # 242RF P/N:147A5810-2; INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00SCGZM.;[02] VERIFIED RECEIVED NEW FLOOR PANEL AND INSTALLATION WILL SDR SWAA2024061385694Floor Panel · peelingAFT CABIN WET AREA FLOOR PANEL 242SF HAS PEELED UPPER SURFACE LAYER FIBERS. 124-029<[01] RECEIVED REPAIRED FLOOR PANEL 242SF. <BR>P/N: 147A5810-99.<BR>PO: 2059779.<BR>PANEL WILL BE INSTALLED ON TTG8Q00SCGZK.;[02] VERIFIED STEP 1SDR SWAA2024061385766Floor Panel · delaminatedCABIN FLOOR PANEL 231XF UPPER SKIN DELAMINATED AND TORN IN SEVERAL AREAS.<[01] RECEIVED AND REPLACED PANEL 231XF IAW SRM 53-00-50-2R-0.<BR>INSTALLATION WILL BE ACCOMPLISHED ON ITEM TTG8Q00SJKID;[02] VERIFIED STEP 1SDR SWAA2024061385768Floor Panel · delaminatedCABIN FLOOR PANEL 241UF UPPER SKIN DELAMINATED AND TORN IN SEVERAL AREAS<[01] RECEIVED AND REPLACED PANEL 241UF AS PER SRM 53-00-50-2R-0. PANEL CLOSING WILL ACCOMPLISHED IN TASK CARD TTG8Q00SJJZX.;[02] VERIFIED REPLACED.<BR>QUALITY CONTROL PERFORMED A REVIEW OSDR IPXA2024051438686Floor Panel · crackedFOUND MAIN DECK CGO FLOOR PNL NO.262CF, P/N: 146U5880-10. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42648-REQ1 REV.3. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04.01.02.SDR IPXA2024051438700Floor Panel · crackedFOUND MAIN DECK CGO FLOOR PNL CRACK, PNL NO.231HF, P/N: 142U5854-7. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42648-REQ1 REV.3. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04.01.02.SDR IPXA2024051438723Floor Panel · crackedFOUND MAIN DECK CGO FLOOR PNL NO.262KF, P/N: 146U5817-16. (REPAIR). FABRICATE A NEW FLOOR PANEL I.A.W. SREO-42648-REQ1 REV.3. THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04.01.02 CLASSIFICATION OF REPAIRS.SDR AALA202405148073Floorboard · damagedAIRCRAFT WAS NOT GROUNDED: FLOOR BOARD IS SOFT BETWEEN ROW 18 AND ROW 19. ACCOMPLISHED REPAIRED. PER AARD 53-00-00-6 REPAIRED 6.SDR SWAA2024061384588Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN HAS AN AREA OF PULLED STARNDS. (MARKED)<[01] 04 - REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS.;[02] VERIFIED CORRECTIVSDR SWAA2024061384593Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AN AREA OF PULLED STARNDS. (MARKED)<[01] FLOOR PANEL 241ZF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024061384589Floor Panel · pulledAFT FLOOR PANEL 241YF UPPER SKIN HAS AN AREA OF PULLED STARNDS. (MARKED)<[01] AFT FLOOR PANEL 241YF WITH UPPER SKIN HAS AN AREA OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB CO;MPLETE.SDR SWAA2024061384594Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW FLOOR PANEL 241AAF HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024061384590Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] ARES OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 241ABF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024061384595Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF AFT FLOOR PANEL 241ACF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024061384597Floor Panel · pulledAFT FLOOR PANEL 241AEF UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] UPPER SKIN ON AFT FLOOR PANEL 241AEF HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1SDR SWAA2024061384596Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF AREAS OF PULLED STRANDS ON UPPER SURFACE WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024061384598Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024061384591Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024061384601Floor Panel · pulledFWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE SDR SWAA2024061384602Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024061384603Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 221CF WERE REPAIRED IAW SRM 53-00-50-2R-6.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024061384604Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024061384605Floor Panel · pulledFWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FLOOR PANEL 221GF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024061384606Floor Panel · pulledFWD FLOOR PANEL 221AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FAULT TTG8Q00T9SAV WILL BE RESOLVED ON FAULT TTG8Q00T9RB9.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024061384607Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024061384608Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024061384611Floor Panel · pulledFWD FLOOR PANEL 231BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024061384291Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] ATTACHED CURE SHEET.;[02] FLOOR PANEL 241AF WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 126.;[03] VERIFIED CORRECTIVE ACTION #2SDR SWAA2024061384284Floor Panel · pulledFLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024061384285Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] ATTHACED CURE SHEET;[02] FLOOR PANEL 241AF WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND BOEING DRAWING 144A5810 SHEET 126.;[03] VERIFIED CORRECTIVE ACTION #2SDR SWAA2024061384286Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2024061384292Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 241CF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-42A ITEM 55.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024061384293Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241ADF WAS REPLACED BY FABRICATION USING BMS4-23 TYPE II LOT 1553922-1 AND ADHESIVE: BMS5-107 CLASS 1 TYPE 1 LOT AK3BA2380A/A; CURED ADHESIVE UNDER A HEAT LAMP; USING THERMOMETER CAL IDSDR SWAA2024061384260Floor Panel · delaminated(DISCREPANCY RACK) AFT CABIN WET AREA FLOOR PANEL 241ABF DELAM (DOT N199)<[01] 02 - INSPECTED PER [SRM 53-00-50-2R-1-B00276 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)];[02] 04 - REPAIRED PER [SRM 53-00-50-2R-1-B00276 (SDR SWAA2024060684570Floor Panel · crackedCRACK FLOOR PANEL 120CF AT FWD CARGO COMPARTMENT 2024-318104<[01] REPLACED FLOOR PANEL 120CF FWD CARGO COMPARTMENT IAW B737-800 AMM 25-52-01-201-801 AND DWG 453A1610 SHEET 65 REV-<BR>MATERIAL USED ALUMINUM SHEET : P/N: 2024-T3 0.071. SEE INDIVIDUAL SIGN OFF BE
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