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 FDEA202401030016Floor Panel · dentedNUMEROUS DENTS ON FLOOR PANEL 252 MAF. PERMANET REPAIR HAS BEEN PERFORMED ON FLOOR 252 MAF IAW B757 SRM 53-00-50-2R REPAIR #1 PARA 3.A.3 FIG 201 SHEET 1-2 NOTE D-G. MAJOR REPAIR.SDR FDEA202401030015Floor Panel · dentedNUMEROUS DENTS ON FLOOR PANEL 232 MRF. PERMANET REPAIR HAS BEEN PERFORMED ON FLOOR PNL 232 MRF IAW B757 SRM 53-00-50-2R, REPAIR #1 PARA 3.A.3 FIG 201 SHEET 1-2 NOTE D-GSDR FDEA202401030014Floor Panel · dentedNUMEROUS DENTS ON FLOOR PANEL 242MDF. PERMANET REPAIR HAS BEEN PERFORMED ON FLOOR PNL 242MDF IAW B757 SRM 53-00-50-2R REPAIR #1 PARA 3.A.3 FIG 201 SHEET 1-2 NOT D-G. MAJOR REPAIRSDR SWAA2024012537068Floor Panel · deformedFLIGHT COMPARTMENT FLOOR PANEL 211AF DEFORMED<[01] REMOVED DAMAGED PANEL 211AF PER SRM 51-40-02. DRILLED UP REPLACEMENT PANEL PER SRM 51-40-05. APPLIED EXTERIOR FINISH PER AMM 51-21-00.;[02] C/W INSPECTION.;[03] INSTALLED REPLACEMENT PANEL PER SRM 51-40-02.;[0SDR ASAA2024010149620Floor Panel · crackedFLOOR PANEL 131BF UPPER SKIN CRACKED GROUNDED - YES. REPAIRED FLOOR PANEL 131BF IAW A320-214 SRM 53-02-000-283-001 AND SRM 53-02-00-300-004 AND SRM 51-77-11-911-031. REPAIR IS LOCATED 12.75" FROM AFT END AND 6.25" FROM LOWER END. FLOOR PANEL IN ZONE B. REPAIR SDR IPXA2024012933121Floor Panel · crackedFAULT- FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-20 (REPAIR) CUT OUT THE DAMAGE AND CLEAN. MEASURE THE CUTOUT (LENGTH: 1.4", WIDTH: 0.3", AT AFTER EDGE AND 10" FROM LEFT HAND ON PANEL NO.453T1996-20). APPLY THE COMPOUND TO THE CUTOUT CURED AT 125°F FOR SDR IPXA2024012433143Floor Panel · crackedFAULT - FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-12 (REPAIR) REVIEW COMPLETESDR IPXA2024010333121Unknown · unknown*SDR FILED OPEN* FAULT- FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-20 (REPAIR) OK TO WORKSDR IPXA2024010333143Unknown · unknown*SDR FILED OPEN* FAULT - FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-12 (REPAIR) OK TO WORKSDR SWAA2024011636649Floor Panel · crackedREJECT: CRACK FOUND ON PASSENGER CABIN FLOOR SUPPORT PANEL STA-540 BL-0 TO BL-25R FLOOR PANEL 231UF.<[01] PARTIAL STEP 1;[02] COMPLETED STEP 1; REINSTALLED PASSENGER CABIN FLOOR PANEL 231UF PER AMM 53-21-00-400-801. USED SCREWGUN ID PER1811; S/N A5792887; DUE SDR AALA202401054980Floorboard · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOORBOARD PN 869Z3620-34 IS DELAMINATED AT BS 509 FROM SEATS 6J TO 9L. REMOVED AND REPLACED MAIN CABIN FLOORBOARD. PER AMM DMC-B787-A-53-01-01-02A-720A-A/520A-A.SDR SWAA2024010236775Floor Panel · crackedAFT CARGO BAY FLOOR HAS 2 FT CRACK<[01] R&R CARGO FLOOR PANEL 140BF IAW AMM TASK 25-52-10SDR ASAA2023123047372Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-443 DELAMINATED. GROUNDED - YES. ACCOMPLISHED PERMANENT CLASS A REPAIR OF DELAMINATION ON MAIN CABIN FLOOR PANEL 147A5810-443 IAW ASA B737-900ER SRM 53-00-50-2R-0 REPAIR 7, AND FIG 210.SDR AALA202401047284Floorboard · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOORBOARD PN 869Z5520-11 IS DELAMINATED AT 11J TO 15J. REMOVED AND REPLACED CABIN FLOOR BOARD. PER B787-A-53-01-01-02A-520A-A AND B787-A-53-01-01-02A-720A-A.SDR SWAA2024013136056Floor Panel · delaminatedCABIN FLOOR PANEL 232QF UPPER SKIN AFT EDGE DENTED/DELAMINATED 1' SQUARE APPROX.<[01] INSTALLED FLOOR PANEL 232QF AS PER B737 AMM 53-21-00-400-801.;[02] CORRECTION: RECEIVED AND INSTALLED NEW PANEL 232QF.<BR>P/N: 143A5810-110. PO#2051706 AS PER B737 AMM 53-21-SDR ASAA2024011747354Floor Panel · delaminatedFLOOR PANEL P/N 141A5810-155 DELAMINATED. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-155 IAW B737-900 SRM 53-00-50-1A-1 AND SRM 53-00-50-2R-0.SDR ASAA2024011747353Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-444. GROUNDED - YES. REPAIRED PANEL 147A5810-444 WITH CATEGORY A PERMANENT REPAIR IAW B737-900 SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SRM 53-00-50-2R-7.SDR ASAA2023122847227Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-421 DELAMINATED. GROUNDED - YES. COMPLETED WET LAY UP REPAIR ON FLOOR PANEL P/N 147A5810-421 IAW B737-900ER SRM 53-00-50-2R.SDR AALA202401238394Floor Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR PANEL 262LG SCREW HOLES. REPLACED FLOOR PANEL PER TASK CARD 26C26053014.SDR ASAA2023122747373Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-398 DELAMINATED. GROUNDED - YES. REPAIRED DELAMINATIONS ON PANEL PN: 147A5810-398 IAW B737-900ER SRM 53-00-50-2R-7.SDR ASAA2024011747352Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-109 DELAMINATED. GROUNDED - YES. ACCOMPLISHED PERMANENT CLASS A REPAIR OF DELAMINATED FACE SHEET ON MAIN CABIN FLOOR PANEL 147A5810-109 IAW ASA B737-900ER SRM 53-00-50-2R-0, REPAIR 7, AND FIG 210.SDR ASAA2024011747351Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-439 DELAMINATED. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 147A5810-439 IAW B737-900 SRM 53-00-51-1A-1 AND SRM 53-00-50-2R-0.SDR ASAA202011747350Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-398 DELAMINATED. GROUNDED - YES. REPAIRED DELAMINATIONS ON PANEL PN: 147A5810-398 IAW B737-900ER SRM 53-00-50-2R-7.SDR ASAA2023122747040Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-446 DELAMINATED. GROUNDED - YES. EVALUATED AND REPAIRED FLOOR PANEL 147A5810-446 DELAM AND 1 INSERT IAW B737-900ER SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SRM 53-00-50-2R-7.SDR ASAA2023122747039Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-445 DELAMINATED. GROUNDED - YES. REPAIRED DELAMINATION ON FLOOR PANEL PN 147A5810-445 IAW B737-900ER SRM 53-00-50-2R-7.SDR ASAA2023122747038Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-440 DELAMINATED. GROUNDED - YES. EVALUATED FLOOR PANEL P/N 147A5810-440 AND FOUND MULTIPLE MISSING/PEELING UPPER SURFACE AND 4EA DAMAGED INSERTS REQUIRING REPAIR IAW ASA B737-900ER SRM 53-00-50-1A-1. REPAIRED IAW ASA B737-900ER SRM 53-SDR ASAA2023122747037Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-477 DELAMINATED. GROUNDED - YES. COMPLETED WET BY UP AND REMOVED AND REPLACED INSERTS 6EA ON FLOOR PANEL P/N 147A5810-477 IAW B737-900ER SRM 53-00-50-2R-0.SDR DALA2023122810674Unknown · unknownSHIP 1603 MID LAV FLOOR BEAM UPPER CHORD SURFACE FOUND CORROSION AT STA 933 RBL 11. CORRECTIVE ACTION: DAMAGED AREA REPAIRED AS PER B767-300 SRM 53-00-51 (0127705)SDR DALA2023122810672Unknown · unknownSHIP 1603 BULK CARGO FRAME LOWER CHORD FOUND CORROSION AT STA 1562 BETWEEN S38L AND S38R. CORRECTIVE ACTION: DAMAGED AREA REPAIRED AS PER B767-300 SRM 51-40-02 (0127488)SDR AALA202312296070Floorboard · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOORBOARD IS DELAMINATED AT 27H TO 29H. (P/N# 869Z7450-1). REMOVED AND REPLACED NEW FLOOR PANEL. PER AMM BOEING 787-A-53-01-01-02A-520A-A/720A.SDR DALA2023122610602Unknown · unknownSHIP 6817 CRACK ON STABILIZATION STRAP ON PASSENGER FLOOR STRUCTURE AT STA. 365 LBL 25. CPAX W1. CORRECTIVE ACTION: SUMMARY OF NRC 00696: STABILIZATION STRAP ON PASSENGER FLOOR STRUCTURE AT STA. 365 LBL 25 WAS REPAIRED PER B757-200 SRM 53-00. (0123537)SDR SWAA2024020534834Floor Panel · peelingMAIN CABIN FLOOR PANEL 241UF UPPER SURFACE HAS PEELED FIBERS (017)<[01] FLOOR PANEL 241UF WILL BE ACCOMPLISHED ON TTG8Q00QKN94.;[02] STEP 1: ENTER IN ERROR.<BR>FLOOR PANEL 241UF WILL BE ACCOMPLISHED ON TTG8Q00QGLV7.;[03] VERIFIED CORRECTIVE ACTION; STEP 2.SDR SWAA2024020534825Floor Panel · peelingMAIN CABIN FLOOR PANEL 241ACF UPPER SURFACE HAS PEELED FIBERS (014)<[01] RECEIVED NEW FLOOR PANEL 241ACF; P/N D104MM0003-311.<BR>PO# 2052116.<BR>PANEL 241ACF WILL BE INSTALLED ON TTG8Q00PGLTL.;[02] VERIFIED STEP 1SDR SWAA2024020534838Floor Panel · peelingMAIN CABIN FLOOR PANEL 242UF UPPER SURFACE HAS PEELED FIBERS (015)<[01] RECEIVED AFT WET AREA FLOOR PANEL 242UF; PANEL WILL BE INSTALLED ON TTG8Q00PGM33.;[02] VERIFIED STEP 1SDR SWAA2024020534832Floor Panel · peelingMAIN CABIN FLOOR PANEL 241AAF UPPER SURFACE HAS PEELED FIBERS (016)<[01] RECEIVED AFT WET AREA FLOOR PANEL 241AAF; PANEL WILL BE INSTALLED ON TTG8Q00PGLTQ.;[02] VERIFIED STEP 1SDR SWAA2024020534835Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241C HAS CORRODED INSERTS (011)<[01] REMOVED AND REPLACED BROKEN INSERTS AT MAIN CABIN FLOOR PANEL 241C REF. SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534823Floor Panel · corrodedMAIN CABIN FLOOR PANEL 242VF HAS CORRODED INSERTS (004)<[01] REMOVED AND REPLACED. INSERTS BROKEN AT MAIN CABIN FLOOR PANEL 242VF. REF. SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534824Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241ACF HAS CORRODED INSERTS (005)<[01] THIS ITEM WILL BE ACCOMPLISHED ON TTG8Q00QGLT3; RECEIVED NEW FLOOR PANEL 241ACF.;[02] VERIFIED STEP 1SDR SWAA2024020534837Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241ADF HAS CORRODED INSERTS (006)<[01] REMOVED AND REPLACED BROKEN INSERTS AT MAIN CABIN FLOOR PANEL 241ADF REF.SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534827Floor Panel · corrodedMAIN CABIN FLOOR PANEL 242UF HAS CORRODED INSERTS (003)<[01] PANEL 242UF WILL BE REPLACED ON TTG8Q00QGN40;[02] VERIFIED STEP 1SDR SWAA2024020534829Floor Panel · corrodedMAIN CABIN FLOOR PANEL 242B HAS CORRODED INSERTS (001)<[01] REMOVED AND REPLACED INSERTS BROKEN AT MAIN CABIN FLOOR PANEL 242B. REF. SRM. 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024020534830Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241ABF HAS CORRODED INSERTS (009)<[01] PANNEL ASSY 241ABF WILL BE RE PLACED ON ITEM TTG8Q00QSA0K;[02] VERIFIED STEP 1SDR SWAA2024020534839Floor Panel · corrodedMAIN CABIN FLOOR PANEL 241AAF HAS CORRODED INSERTS (008)<[01] THIS ITEM WILL BE ACCOMPLISHED ON TTG8Q00QGLV0.;[02] VERIFIED STEP 1SDR SWAA2024013034684Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FABRICATED FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE: AND DRAWING 144A5810 ID 0126;[02] VERIFIED JOB COMPLETE AND MEASUREMENT TABLESDR DALA2023122610599Unknown · unknownSHIP 6817 CORROSION ON DECK PLATE STA 1716 BTW RBL 21 AND RBL 15 ALSO STA 1716 BTW LBL 16 TO 25 AT CPAX. CORRECTIVE ACTION: SUMMARY OF NRC 00686: CORROSION ON DECK PLATE STA 1716 BTW RBL 21 AND RBL 15 ALSO STA 1716 BTW LBL 16 TO 25 AT CPAX WAS REPAIRED PER B75SDR SWAA2024020534397Floor Panel · peelingCABIN FLOOR PANEL 231BF HAS PEELED UPPER SURFACE FIBERS. 124-028<[01] RECEIVED FLOOR PANEL #231BF WITH P/N: 141A5810-168. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00PGM3P;[02] VERIFIED STEP 1.SDR SWAA2024020534626Floor Panel · peelingCABIN FLOOR PANEL 231AF HAS PEELED UPPER SURFACE FIBERS. 124-030<[01] RECEIVED CABIN FLOOR PANEL 231AF WILL BE INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q00PGM3R;[02] RECEIVED CABIN FLOOR PANEL 231AF WILL BE INSTALLED ON TTG8Q00PGM3R;[03] VERIFIED STEP 2 (CORRESDR SWAA2024020534627Floor Panel · peelingCABIN FLOOR PANEL 222BF HAS PEELED UPPER SURFACE FIBERS. 124-024<[01] RECEIVED FLOOR PANEL #222BF; WITH P/N:141A5810-507. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00PGLLD.;[02] VERIFIED STEP 1.SDR SWAA2024020534618Floor Panel · peelingCABIN FLOOR PANEL 221EF HAS PEELED UPPER SURFACE FIBERS. 124-027<[01] RECEIVED PANEL: 221EF P/N: 141A5810-526 INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD: 'TTG8Q00PGM44';[02] VERIFIED STEP 1.SDR SWAA2024020534628Floor Panel · peelingCABIN FLOOR PANEL 221BF HAS PEELED UPPER SURFACE FIBERS. 124-032<[01] RECEIVED FLOOR PANEL #221BF WITH P/N: 141A5810-56. INSTALLATION WILL BE ACCOMPLISHED ON TASK CARD TTG8Q00PGM4B;[02] VERIFIED STEP 1.
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