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 SWAA2023122125351Floor Panel · pulledPANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241WF 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] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125352Floor Panel · pulledPANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242AF WAS REPLACED WITH NEW SERVICEABLE PANEL IAW SRM 51-10-01-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.SDR SWAA2023122125355Floor Panel · pulledPANEL 242QF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 242QF 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] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125357Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FWD FLOOR PANEL 221CF WAS REPLACED WITH A NEW SERVICEABLE PANEL IAW SRM 51-10-02-0G-0 PAR 9.A.(1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.SDR SWAA2023122125360Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221DF UPPER SKIN HAD AREAS OF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED FLOOR PANEL 221DF PER IS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.SDR SWAA2023122125346Floor Panel · pulledPANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231ZF 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] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125347Floor Panel · pulledPANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 232SF 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 ACTION #1<BR>VERIFIESDR SWAA2023122125348Floor Panel · pulledPANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0127.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.SDR SWAA2023122125349Floor Panel · pulledPANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241BF WAS REPLACED WITH NEW SERVICEABLE PANEL IAW SRM 51-10-01-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.SDR SWAA2023122125350Floor Panel · pulledPANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241UF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF DAMAGE IAW SRM 53-00-50-2R-0; DWG 146A5810 ID:0470.;[02] ATTACHED CURE SHEET.<BR>SDR SWAA2023122125354Floor Panel · pulledPANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241EF 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] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125340Floor Panel · crackedAFT FLOOR PANEL 242WF O/B AFT CORNER IS CRACKED.<[01] REPAIRED DAMAGED O/B AFT CORNER ON AFT FLOOR PANEL 242WF IAW SRM 53-00-50-2R-6.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENTS TABLE.SDR SWAA2023122125343Floor Panel · pulledAFT FLOOR PANEL 242SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242SF 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 DAMAGE.;[02] PANEL REPLACED. JOB COMPSDR SWAA2023122125344Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] VERIFIED COMPLETION OF REPAIR TO AFT FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1;[02] VERIFIED REPAIR OF AFT FLOOR PANEL 242UF IAW SRM 53-00-50-2R-1;[03] WORKSCOPE IS COMPLETE.SDR SWAA2023122125345Floor 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.<BR><BR>ATTACHED CURE SHEETS.;[02] AL STEPS COMPLETESDR SWAA2023122125353Floor Panel · pulledPANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231YF 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] PANEL REPLACED. JOB COMPLETE.SDR SWAA2023122125337Floor Panel · pulledAFT FLOOR PANEL 241ABF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXCESSIVE DAMAGE AFT FLOOR PANEL 241ABF WAS REPLACED WITH A NEW SERVICEABLE PART IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION 1 AND THE MEASUREMENT TABLE.SDR SWAA2023122125338Floor Panel · pulledAFT FLOOR PANEL 241ADFF UPPER SKIN HAS AREAS OF PULLED STRANDS. CORRECT PANEL IS 241ADF.<[01] AFT FLOOR PANEL 241ADF 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 DAMAGSDR SWAA2023122125339Floor Panel · pulledAFT FLOOR PANEL 242RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242RF 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] PANEL REPLACED. JOB SDR SWAA2023122125342Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOORBOARD 241ACF UPPER SKIN HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED FLOOR PANEL 241ACF UPPER SKIN HAS BEEN REPAIRED PER SRM 53-00-50-SDR SWAA2023122125335Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ZF UPPER SKIN HAD AREAS OF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED FLOOR PANEL 241ZF IS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.SDR SWAA2023122125341Floor Panel · pulledAFT FLOOR PANEL 241XF UPPER SKIN PREVIOUS REPAIR HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241XF UPPER SKIN PREVIOUS REPAIR AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED CURE SHEETS.;[02] ALL STEPS COMPLETESDR SWAA2024011225192Floor Panel · damagedFWD CABIN WET AREA FLOOR PANEL 221CF TOP SURFACE PREVIOUS REPAIR SOFT SPOT<[01] RECEIVED FLOOR PANEL P/N: 141A5810-9<BR><BR>PANEL WILL BE INSTALLED ON TASK CARD: 'TTG8Q00PSW3V';[02] VERIFIED STEP 1SDR SWAA2024011225195Floor Panel · deterioratedFWD CABIN WET AREA FLOOR PANEL 222DF TOP SURFACE DETERIORATED<[01] RECEIVED AND REPLACED PANEL 222DF AS PER SRM 53-00-50-1A-1.;[02] VERIFIED NEW PANEL. NOTE INSTALLATION WILL BE ACCOMPLISHED ON ROUTINE WORK CARD.SDR SWAA2024011225196Floor Panel · delaminatedAFT CABIN WET AREA FLOOR PANEL 242UF TOP SURFACE DELAMINATED MKD DOT<[01] RECEIVED AND REPLACED PANEL 242UF AS PER SRM 53-00-50-1A-1.;[02] VERIFIED NEW PANNEL. NOTE: INSTALLATION WILL BE ACCOMPLISHED ON ROUTINE CLOSING CARD.SDR SWAA2024011225193Floor Panel · delaminatedAFT CABIN WET AREA FLOOR PANEL 241AAF TOP SURFACE DELAMINATED MKD DOT<[01] RECEIVED AND REPLACED PANEL 241AAF AS PER AMM 53-00-50-1A-1.;[02] RECEIVED AND REPLACED PANEL 241AAF AS PER SRM 53-00-50-1A-1.;[03] VERIFIED NEW PANNEL. NOTE: INSTALLATION WILL BE ACCOMSDR SWAA2024011225197Floor Panel · delaminatedAFT CABIN WET AREA FLOOR PANEL 241ABF TOP SURFACE DELAMINATED MKD DOT<[01] RECEIVED AND REPLACED PANEL 241ABF AS PER SRM 53-00-50-1A-1.;[02] VERIFIED NEW PANEL. NOTE INSTALLATION WILL BE ACCOMPLISHED ON ROUTINE WORK CARD.SDR SWAA2024011225198Floor Panel · deterioratedAFT CABIN WET AREA FLOOR PANEL 242D TOP SURFACE DETERIORATED MKD DOT<[01] RECEIVED AND REPLACED PANEL 242D AS PER AMM 53-00-50-1A-1.;[02] RECEIVED AND REPLACED PANEL 242D AS PER SRM 53-00-50-1A-1.;[03] VERIFIED NEW PANNEL. NOTE: INSTALLATION WILL BE ACCOMPLISHSDR SWAA2024011225194Floor Panel · deterioratedAFT CABIN WET AREA FLOOR PANEL 241XF TOP SURFACE DETERIORATED MKD DOT<[01] RECEIVED AND REPLACED PANEL 241XF AS PER SRM 53-00-50-1A-1.;[02] VERIFIED NEW PANEL. NOTE: PANEL INSTALLATION WILL BE DONE ON ROUTINE CARDSDR IPXA2024010663829Floor Panel · damaged*MAJOR REPAIR* DAMAGE TO THE LEFT SIDE MAIN DECK FLOOR PANEL, P/N 141U5876-153 (REFERENCE IPC 53-21-02-82A, ITEM 461), INSTALLED BETWEEN STA 480 - 520.***SM26/LMX8*** INSTALLED NEW FLOOR PANEL PER SREO 42648. ACCOMPLISHED STEPS 10,11,13 PER SREO-42648-REQ1.SDR SWAA2023122125220Floor Panel · crackedMAIN CABIN FLOOR PANEL #221GF FWD SECTION TIP CRACKED<[01] APPLIED PERMANEMT REPAIR ON DAMAGE AREA AS MARKED ON MAIN CABIN FLOOR PANEL 221GF AS PER B737 SRM 53-00-50-2R-6 PARAG 3-G-M; MATERIAL USED PO#1798939; PO#1690463.;[02] VERIFIED AND INSPECTED STEP #1. PSDR AALA202312133348Floor Panel · corrodedAIRCRAFT IN BASE MAINTENACE: CORROSION ON CABIN FLOOR PANEL 262BG SLEEVE. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.SDR SWAA2023120125205Floor Panel · crackedAFT CARGO FLOOR PANEL 140DF HAS A DENT WITH A CRACK<[01] VERIFIED MATERIAL FOR FLOOR PANEL FABRICATION; 2024-T3 .071'ATAG A209385 IAW AMM 50-10-04-400-801 SECTION 3.A. REMOVED FLOOR PANEL 140DF IAW AMM 50-10-04-000-801. VERIFIED STEP 1;[04] STARTED FABRICATISDR SWAA2023122124939Floor Panel · crackedMAIN CABIN STA 540 RBL 2' FLOOR PANEL BREAK CRACK<[01] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 RBL 2' AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 RBL 2' AS PER SRM 51-40-02-0G-0; BOEING DWG #SDR SWAA2023122124940Floor Panel · crackedMAIN CABIN STA 540 LBL 2' FLOOR PANEL BREAK CRACK<[01] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 LBL 2' AS PER SRM 51-40-02-0G-0.;[02] REMOVED AND REPLACED FLOOR PANEL BREAK AT MAIN CABIN STA 540 LBL 2' AS PER SRM 51-40-02-0G-0; BOEING DWG #SDR SWAA2023122124942Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ZF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 241ZF AND WILL BE INSTALLED ON T/C TTG8Q00PDXP8.;[02] VERIFIED STEP 1SDR IPXA2023112854981Floor Panel · damagedFLOOR PANEL POSITION 4 CENTER HAS A HOLE IN IT (REMOVED FOR SHEET METAL) HOLE IS MARKED VERIFIED COMPLETION OF FLOORBOARD REPAIR PER SRM 53-00-50-2R. OK TO INSTALL REPAIRED FLOORBOARDSDR SWAA2023122124238Floor Panel · frayedMAIN CABIN FLOOR PANEL 222DF UPPER SURFACE FRAYING<[01] RECEIVED FLOOR PANEL 222DF. INSTALLATION WILL BE ACCOMPLISHED ON TASKS CARD TTG8Q00PDYQU.;[02] VERIFIED STEP 1SDR SWAA2023122124239Floor Panel · frayedMAIN CABIN FLOOR PANEL 221CF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 221CF AND WILL BE INSTALLED ON T/C TTG8Q00PDYRA;[02] VERIFIED STEP 1SDR FDEA202311211876Floor Panel · dentedFOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11862182-13 BTW RBL 46-50 AND STA 720- 780. REMOVED FLOOR PANEL P\N 11864182-13 FROM STA 720-780 IAW B-757 AMM 53-01-01-4, EVALVATED AND REPAIRED 2 EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 DETSDR FDEA202311211875Floor Panel · dentedFOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11862182-21 BTW RBL 46-50 AND STA 780- 880. REMOVED FLOOR PANEL #11862182-21 FROM STA 780 - 880 IAW (B 757) AMM 53-01-01-4, EVALUATED AND REPAIRED 3EZ DENTS ON FLOOR PANEL IAW B757 SRM 53-00-50-R2 REP 1 DETAIL SDR FDEA202311211874Floor Panel · dentedFOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11864182-10 BTW RBL 46-50 AND STA 1320- 1420. REMOVED FLOOR PANEL P\N 11862182-10 FROM STA 1320-1420 BTW RBL 46-50 IAW B-757 AMM 53- 01-01-4, EVALUATED AND REPAIRED 2EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-5SDR FDEA202311211873Floor Panel · dentedFOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-2 BTW RBL 46-50 AND STA 900- 1020. REMOVED FLOOR PANEL P\N 11862182-2 FROM STA 900-1020 BTW IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 3EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 SDR FDEA202311211872Floor Panel · dentedFOUND DENT AT MAIN CARGO FLOOR PANE; P\N: 11862182-28 BTW RBL 46-50 AND STA 880-900 REMOVED FLOOR PANEL P\N 11862182-28 FROM STA 880-900 BTW RBL 46- RBL 50 IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 1EA DENT ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R RSDR FDEA202311211871Floor Panel · dentedFOUND 6EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11864182-2 BTW RBL 46-50 AND STA 1200- 1320. REMOVED FLOOR PANEL P\N 11864182-2 FROM STA 1200-1320 IAW B-757 AMM 53-01-01-4, EVALVATED AND REPAIRED 6 EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 DESDR FDEA202311211870Floor Panel · dentedFOUND 4EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-26 BTW RBL 46-50 AND STA 1100- 1200. REMOVED FLOOR PANEL P\N 11863182-26 FROM STA 1100-1200 IAW B-757 AMM 53-01-01-4, EVALVATED AND REPAIRED 4EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-R2 REP 1 DETSDR FDEA202311211869Floor Panel · dentedFOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-38 BTW RBL 46-50 AND STA 1055- 1100. REMOVED FLOOR PANEL P\N 11862182-38 FROM STA 1055-1100 IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 3EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 DSDR FDEA202311211868Floor Panel · dentedFOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-34 BTW RBL 46-50 AND STA 1020- 1055. REMOVED FLOOR PANEL P\N 11862182-34 FROM STA 1020-1055 IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 2EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 SDR DALA2023112109618Unknown · unknownSHIP 3506 DURING SERVICE CHECK FOUND AFT CARGO FLOOR PANEL DAMAGED WITH SMALL PUNCTURE. PANEL FIN 151MAF. CORRECTIVE ACTION: DAMAGE FOUND TO BE WITHIN LIMITS FOR REPAIR. REPAIRED DAMAGED UPPER SKIN AND CORE PER A350 ASR 53-02-XX-05001-664A. (8945581)SDR SWAA2023113023141Floor Panel · delaminatedPASSENGER CABIN FLOOR BOARD PANEL 231RF DELAMINATED.<[01] REMOVED PASSENGER CABIN FLOOR PANEL 231RF IAW AMM 53-21-00-000-801;[02] DUE TO EXTENT OF DAMAGE FABRICATED NEW 231RF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1545419-1; INSERTS INSTALLED USING BMS5-107 LOT#1
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