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 FDEA202406230853Floorboard · damagedMAIN DECK FLOORBOARD 222MBF DAMAGED FABRICATED ZONE 220 FLOORBOARD PANEL 222MBF ON VTMAE TRAVELER #T24/1762151 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIRSDR FDEA202406230852Floorboard · damagedMAIN DECK FLOORBOARD 221MAF DAMAGED FABRICATED ZONE 220 FLOORBOARD PNL 221MAF ON VTMAE TRAVELER #T24/1762038 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIRSDR FDEA202406230851Floorboard · damagedMAIN DECK FLOORBOARD 222MAF DAMAGED FABRICATED ZONE 220 FLOORBOARD PANEL 222MAF ON VTMAE TRAVELER #T24/1762140 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIRSDR FDEA202406230850Floorboard · damagedMAIN DECK FLOORBOARD 221MBF DAMAGED FABRICATED ZONE 220 FLOORBOARD PANEL 221MBF ON VTMAE TRAVELER #T24/1762137 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIRSDR FDEA202406230849Floorboard · puncturedMDC FLOOR PANEL 251MWF HAS CRACK AND PUNCTURED. DOT 136-48 FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER # T24/1762817 IAW DWG SRZ-25-005R, MAJOR REPAIRSDR SWAA2024072304682Floor Panel · delaminatedAFT FLOOR PANEL 241ACF HAS UPPER SURFACE DELAMINATION AND DAMAGED INSERTS<[01] AFT FLOOR PANEL 241ACF HAD UPPER SURFACE DELAMINATION AND DAMAGED INSERTS REPAIED IAW SRM 53-00-50-2R-6;[02] JOB COMPLETE.SDR SWAA2024071104719Floorboard · pulledA225-018 CABIN FLOOR BOPARD 241 DF HAS MINOR FIBER DAMAGE (PULLED UPPER LAYER)<[01] REPLACED FLOORBOARD PANEL 241DF BY FABRICATION IAW B737 SRM 53-00-50-2R-0; BOEING DWG 1445810-0128; AND PER SAMPLE.;[02] VERIFIED ITEM 1.<BR>AUDITED.SDR DALA2024062406391Strap · corroded(LOG 0409057) CORROSION AT L/H FLOOR STRAP STA1016+5 - 1016+10, LBL 18, WL208. REMOVED, REPLACED AND INSTALLED NEW L/H FLOOR STRAP STA 1016+22 TO 1006 LBL 28 WL 208 IAW B737-800 SRM 51-40-02-0G.SDR FDEA202406210831Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 231AFF, SKIN WITH DENTS. MDC, FLOOR PANEL 231AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR FDEA202406210830Floor Panel · dentedMAIN CARGO COMPARTMENT, FLOOR PANEL 221CFF, SKIN WITH SEVERAL DENTS. MDC, FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV 88 DEC 15/2023SDR SWAA2024080203659Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231XF IS DELAMINATED<[01] FABRICATION OF NEW 231XF CABIN FLOOR PANEL HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0007.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] JOB COMPLETE.SDR SWAA2024080203660Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 232RF IS DELAMINATED<[01] FABRICATION OF NEW 232RF FLOOR PANEL HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0004.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.SDR SWAA2024080203662Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242AF HAS DAMAGED INSERT AND DELAMINATION<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW PASSENGER CABIN FLOOR PANEL 242AF IAW SRM 53-00-50-2R-0 & BOEING DWG 144A5810-189.SDR SWAA2024080203663Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231UF DELAMINATED<[01] UPDATED STEP 1;[02] PASSENGER CABIN FLOOR PANEL 231UF DELAMINATED AND MAINTENANCE WAS ACCOMPLISHED ON STEPS 1-4.;[03] FABRICATED NEW FLOOR PANEL USING BMS 4-17 TYPE VI LOT#1557541-1; LOCATED AND DRILLED INSERTSDR SWAA2024080203661Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241AF HAS DAMAGED INSERT AND DELAMINATION<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241AF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.SDR SWAA2024072403541Floor Panel · pulledAFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW FLOOR PANEL 241UF HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 146A5810 ID: 0054.SDR SWAA2024072403542Floor Panel · pulledAFT FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 241VF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-22 ITEM 161.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024072403543Floor Panel · pulledAFT FLOOR PANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED AFT FLOOR PANEL 241WF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-22 ITEM 185.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024072403544Floor Panel · pulledPANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARAR 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024072403546Floor Panel · pulledFLOOR PANEL 232FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW FLOOR PANEL 232FF HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 143A5810 ID: 0116.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024072403547Floor Panel · pulledFLOOR PANEL 232QF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW FLOOR PANEL HAS BEEN COMPLETED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 143A5810 ID: 0107.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024072403548Floor Panel · delaminatedFWD FLOOR PANEL 222AF HAS UPPER SURFACE DELAMINATION<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 222AF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024072403549Floor Panel · delaminatedFWD FLOOR PANEL 221AF HAS UPPER SURFACE DELAMINATION<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FWD FLOOR PANEL 221AF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 35.;[02] VERIFIEDSDR SWAA2024072403550Floor Panel · delaminatedFWD FLOOR PANEL 222BF HAS UPPER SURFACE DELAMINATION<[01] FWD FLOOR PANEL 222BF WITH UPPER SURFACE DELAMINATIONS 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 SWAA2024072403551Floor Panel · delaminatedFWD FLOOR PANEL 221BF HAS UPPER SURFACE DELAMINATION<[01] FWD FLOOR PANEL 221BF WITH UPPER SURFACE DELAMINATION 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 SWAA2024072403552Floor Panel · delaminatedFWD FLOOR PANEL 221DF HAS UPPER SURFACE DELAMINATION<[01] FWD FLOOR PANEL 221DF WITH UPPER SURFACE DELAMINATION 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 SWAA2024072403555Floor Panel · delaminatedFWD FLOOR PANEL 221EF HAS UPPER SURFACE DELAMINATION<[01] FWD FLOOR PANEL 221EF WITH UPPER SURFACE DELAMINATION 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 SWAA2024072403556Floor Panel · delaminatedFWD FLOOR PANEL 231AF HAS UPPER SURFACE DELAMINATION<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED FWD FLOOR PANEL 231AF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 365.;[02] VERIFIED JOB COMPLETESDR SWAA2024072403558Floor Panel · delaminatedAFT FLOOR PANEL 242CF HAS UPPER SURFACE DELAMINATION<[01] CORRECTION: FLOOR PANEL SHOULD BE 242VF.<BR>PANEL TO BE REPAIRED ON FAULT #TTG8Q00U3266;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024072403566Floor Panel · delaminatedAFT FLOOR PANEL 241AAF HAS UPPER SURFACE DELAMINATION<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241AAF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024072407730Floor Panel · crackedCOCKPIT PANEL 211B IS CRACKED<[01] RECEIVED REPLACEMENT COCKPIT PANEL 211B <BR>(BRANT NEW); WILL BE INSTALLED ON CUST SYSTEM ID: TTG8Q00T9E95.<BR>MAINT REF SRM 51-10-02-0G-0 STEP 9.;[02] RECEIVED REPLACEMENT COCKPIT PANEL 211B<BR>(BRANT NEW); WILL BE INSTALLEDSDR SWAA2024072303545Floor Panel · pulledFLOOR PANEL 231MF UPPER SKIN HAS AREAS OF PULED STRANDS.<[01] FLOOR PANEL 231MF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024072303553Floor Panel · delaminatedFWD FLOOR PANEL 222DF HAS UPPER SURFACE DELAMINATION<[01] UPPER SURFACE DELAMINATION ON FWD FLOOR PANEL 222DF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024072303554Floor Panel · delaminatedFWD FLOOR PANEL 222CF HAS UPPER SURFACE DELAMINATION<[01] REPAIRED DAMAGED UPPER SURFACE ON FWD FLOOR PANEL 222CF IAW SRM 53-00-50-2R-1.;[02] VERIFIED COMPLETESDR SWAA2024072303559Floor Panel · delaminatedAFT FLOOR PANEL 242VF HAS UPPER SURFACE DELAMINATION<[01] AFT FLOOR PANEL 242VF UPPER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 147A5810 ID:0350.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED COMPLETESDR SWAA2024072303565Floor Panel · delaminatedAFT FLOOR PANEL 242UF HAS UPPER SURFACE DELAMINATION<[01] AFT FLOOR PANEL 242UF; WITH UPPER SURFACE DELAMINATION; WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.SDR SWAA2024072303570Floor Panel · delaminatedAFT FLOOR PANEL 241XF HAS UPPER SURFACE DELAMINATION<[01] AFT FLOOR PANEL 241XF UPPER SURFACE DELAMINATION WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPOLETE.SDR FDEA202406200978Floor Panel · delaminatedTHE #162HF FLOOR PANEL OF BULK CARGO COMPARTMENT WAS FOUND SOFTEN FABRICATED NEW FLOOR PANEL 162HF FR67~FR69, -Y46.7~-Y805 I.A.W FEDEX STANDARD REPAIR DRAWING SRZ-25-005 & SRZ-25-011. THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202406200977Floor Panel · delaminatedTHE #161GF FLOOR PANEL OF BULK CARGO COMPARTMENT WAS FOUND SOFTEN FABRICATED NEW FLOOR PANEL 161GF FR69~FR70, -Y307~Y1304 I.A.W FEDEX STANDARD REPAIR DRAWING SRZ-25-005 & SRZ-25-011. THE REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100SDR UIEA2024061800537Floor Panel · crackedZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 123FXF, CRACK ON UNDERFLOOR SKIN PLATE.(<P>ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 123FXF, CRACK ON UNDERFLOOR SKIN PLATE.WAS PERFORMED REPAIRED IAW SRM 53-00-53-SDR UIEA2024061800542Floor Panel · damagedZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE.(<P>ZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124BXF CORROSION EVIDENCE ON UNDERFLOOR PLATE WAS REPAIRED IAW SRM 53-00SDR UIEA2024061800543Floor Panel · damagedZONE 100, LOWER HALF FUSELAGE, FORWARD CARGO COMPARTMENT FLOOR PANEL 124AXF, MISSING MATERIAL AFT RIGHT CORNER, CRACK ON RIGHT LATERAL EDGE (NEAR LOCK) AND MISSING MATERIAL FWD RIGHT CORNER(<P><SPAN>ZONE 100, LOWER HALF FUSELAGE, </SPAN><SPAN>FORWARD CARGO COMSDR SWAA2024072503170Floor Panel · delaminatedCABIN FLOOR PANEL 242DF WITH UPPER SKIN AREA DELAMINATED / TORN.<[01] RECEIVED FLOOR PANEL 242DF WILL BE INSTALLED ON TTG8Q00TMJLS.;[02] VERIFIED STEP 1 <BR><BR>AUDIT C/W MPM 52.02.02SDR SWAA2024072503175Floor Panel · delaminatedCABIN FLOOR PANEL 242CF UPPER SKIN WITH DELAMINATED / TORN AREAS.<[01] RECEIVED FLOOR PANEL 242CF WILL BE INSTALLED ON TTG8Q00TMK0C;[02] VERIFIED STEP 1<BR><BR>AUDIT C/W MPM 52.02.02SDR SWAA2024072402671Floor Panel · pulledPANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED REPLACEMENT PANEL 241CF IAW SRM 53-00-50-2R-0 ALONG WITH BOEING DRAWING 144A5810 SHEET 0130.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024072402679Floor Panel · pulledPANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED REPLACEMENT PANEL 241DF IAW SRM 53-00-50-2R-0 ALONG WITH BOEING DRAWING 144A5810 SHEET 0009.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024072402672Floor Panel · pulledPANEL 241FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED A NEW FLOOR PANEL USING BMS4-23TYII LOT 1553922-1 AND BMS5-107A ADHESIVE; CURED THE ADHESIVE; UNDER A HEAT LAMP USING THERMOMETER CAL ID: ATS2402 CAL DUE: 08/2024 TO VERIFY TEMPERATURES DURINGSDR SWAA2024072402673Floor Panel · pulledPANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED A NEW FLOOR PANEL USING BMS4-23TYII LOT 1553922-1 AND BMS5-107A ADHESIVE; CURED THE ADHESIVE; UNDER A HEAT LAMP USING THERMOMETER CAL ID: ATS2402 CAL DUE: 08/2024 TO VERIFY TEMPERATURES DURINGSDR SWAA2024072402675Floor Panel · pulledPANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED A NEW FLOOR PANEL USING BMS4-17TYVI LOT 155754-1 AND BMS5-107 ADHESIVE LOT AK3BA2380A-A; CURED ADHESIVE; UNDER A HEAT LAMP USING THERMOMETER; CAL ID: ATS2402 CAL DUE: 08/2024 TO MONITOR THE TESDR FDEA202406171040Crossbeam · corrodedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSS BEAM SURFACE WAS FOUND CORROSION AT FR54.2,-Y70~-Y140 I.A.W A300-600 AMM:20-21-12-00 REPLACED MAIN DECK CARGO COMPATEMENT FLOOR STRUCTURE CROSS BEAM AT FR54.2-Y70-Y140, REPAIR IS CLASSIFIED AS MAJOR PER GMM
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