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 SWAA2024020534625Floor Panel · peelingCABIN FLOOR PANEL 222A HAS PEELED UPPER SURFACE FIBERS. 124-031 CABIN FLOOR PANEL 222AF HAS PEELED UPPER SURFACE FIBERS. 124-031<[01] RECEIVED CABIN FLOOR PANEL 222A WILL BE INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q00PGLLF;[02] RECEIVED CABIN FLOOR PANEL 222ASDR SWAA2024020534633Floor Panel · peelingCABIN FLOOR PANEL 222CF HAS PEELED UPPER SURFACE FIBERS. 124-025<[01] RECEIVED CABIN FLOOR PANEL 222DF WILL BE INSTALLED ON TTG8Q00PGM3W;[02] RECEIVED CABIN FLOOR PANEL 222CF WILL BE INSTALLED ON TTG8Q00PGM3W;[03] VERIFIED STEP 2 (CORRECTION FOR STEP 1)SDR SWAA2024020534617Floor Panel · corrodedCABIN FLOOR PANEL 221DF HAS CORRODED INSERTS. 124-023<[01] RECEIVED NEW FLOOR PANEL 221DF; PANEL WILL BE INSTALLED ON <BR>TTG8Q00PGM47.;[02] VERIFIED STEP 1SDR SWAA2024020534619Floor Panel · corrodedCABIN FLOOR PANEL 221CF HAS CORRODED INSERTS. 124-022<[01] RECEIVED NEW FLOOR PANEL 221CF; PANEL WILL BE INSTALLED ON TTG8Q00PGM49.;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2024012234166Floor Panel · deterioratedDETERIORATED FLOOR PANEL SKYFLEX STA 270 THRU STA 380 AT FWD GALLEY AREA 2023-761747<[01] REPLACED FLOOR PANEL SKYFLEX STA 270 THRU STA 380 AT FWD GALLEY AREA IAW B737-700 AMM 53-21-00-400-801 PARAGRAPH 3F ITEM 8 (5) (E).;[02] REPLACED FLOOR PANEL SKYFLEX STA SDR SWAA2024012234169Floor Panel · deterioratedDETERIORATED FLOOR PANEL SKYFLEX STA 887 THRU STA 1016 AT AFT GALLEY AREA 2023-761751<[01] REPLACED FLOOR PANEL SKYFLEX STA 887 THRU STA 1016 AT AFT GALLEY AREA IAW B737-700 AMM 53-21-00-400-801 SUBTASK 53-21-00-839-801 STEP 8.(A) AND 8.(E) PAGE 5;[02] REPLACESDR SWAA2024012634029Floor Panel · corrodedFORWARD CARGO FLOOR PANEL 120AF HAS SURFACE CORROSION.<[01] REMOVED AND REPLACED FLOOR PANEL I.A.W AMM 25-52-10.SDR REXA2024012200098Floor Panel · crackedRH FWD EQUIPMENT COMPARTMENT FLOOR AT FS 193 IS CRACKED JUST O/B OF THE ADG RETRACTION PUMP. REPAIRED RH FWD EQUIPMENT COMPARTMENT FLOOR AT FS 193 IAW CRJ 900 SRM 53-11-43-201-001-A01.SDR SWAA2024011633670Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SURFACE HAS PULLED STRAND OF FIBERGLASS.<[01] REPAIRED FWD FLOOR PANEL 221CF UPPER SURFACE PULLED STRAND OF FIBERGLASS IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSSDR SWAA2024011633671Floor Panel · delaminatedFWD FLOOR PANEL 221CF LOWER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 221CF LOWER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1<BR>VERIFIED MEASUREMENTSSDR SWAA2024011633672Floor Panel · delaminatedFWD FLOOR PANEL 222AF UPPER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 222AF UPPER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. JOB COMPLETE.SDR SWAA2024011633673Floor Panel · delaminatedFWD FLOOR PANEL 222AF LOWER SURFACE HAS AREAS OF DELAMINATION.<[01] REPAIRED FWD FLOOR PANEL 222AF LOWER SURFACE DELAMINATION IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1. JOB COMPLETE.SDR DALA2023122110455Unknown · unknown(LOG 0117377) PANEL BREAK AT STA 540 CABIN FLOOR AREA IS CRACKED BETWEEN BL0-RBL22. REMOVED AND REPLACED PANEL BREAK AT STA 540 BL0-RBL22 IAW BOEING 737-800 SRM 51-40-02.SDR AALA202312217190Floorboard · delaminatedAIRCRAFT IN BASE MAINTENANCE: PASSENGER CABIN FLOORBOARD AT SEAT 1A, 2A DELAMINATED. REPLACED FLOORBOARD PER AMM B787-A-53-01-01-02A-520A-A/720A-A.SDR DALA2023122010424Unknown · unknownSHIP 3120 PUNCTURE ON FLOOR PANEL IN AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED PER ER/A 613976-14. (0117425)SDR SWAA2024020633230Floor Panel · delaminatedMAIN CABIN FLOOR PANEL FWD CORNER DELAMINATED @ STA 767 RBL 25<[01] FOUND MAIN CABIN FLOOR PANEL AT STA 767 RBL 25 (242MF) OUT LIMITS PER B737-700 SRM 53-00-50-2R-1. REMOVED AND REPLACED MAIN CABIN FLOOR PANEL 242MF PER B737-700 AMM 53-21-00-000-801 AND 53-21-SDR AALA202401041620Floor Panel · crackedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO FLOOR PANEL 151LF CRACKED AT RIGHT HAND OUTBOARD CORNER. SUPPLEMENTAL REPORT FOR AALA202312191620: MAINTENANCE REPLACED FLOOR PANEL.** (CLOSED)SDR AALA202312191620Floor Panel · crackedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO FLOOR PANEL 151LF CRACKED AT RIGHT HAND OUTBOARD CORNER. SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)SDR SWAA2024011632520Floor Panel · pulledFLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF 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 COMPLETESDR SWAA2024011632521Floor Panel · pulledFLOOR PANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231MF 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 COMPLETESDR SWAA2024011632522Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241UF 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 COMPLETESDR SWAA2024010432086Floor Panel · debondedFLOOR PANEL 242AF UPPER SKIN HAS AN AREA OF DISBOND NEAR CENTER OF PANEL. (MARKED)<[01] FLOOR PANEL 242AF WITH DISBOND IN UPPER SKIN WAS REPLACED BY FABRICATING NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG NO. 144A5810 ID:0037;[02] VERIFIED CORRECTIVE ACTION ITEM 1SDR SWAA2023121532103Floor Panel · loosePASSENGER CABIN AISLE FLOOR IS LOOSE AND POPPING WHEN WALKED ON AT ROW 8.R&R PANEL ASSY. 143A5240-63;AND PANEL 143A5240-64 IAW SRM 51-40-02. INSTALLED CENTER AISLE FLOOR PANEL IAW AMM 53-21-00. INSTALLED FWD CARGO AFT CENTER WALL IAW SRM 51-40-02.SDR SWAA2024012331960Floor Panel · pulledCABIN FLOOR PANEL #222BF DELAMINATED.<[01] RECEIVED FLOOR PANEL $222BF P.N# 141A5810-507; WILL BE INSTALLED ON N/R: TTG8Q00PUEQR.;[02] VERIFIED.SDR SWAA2024012331965Floor Panel · delaminatedCABIN FLOOR PANEL #221CF DELAMINATED.<[01] RECEIVED NEW PANEL #221CF INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00PUHD5;[02] VERIFIED 1.SDR SWAA2024012331966Floor Panel · delaminatedCABIN FLOOR PANEL #221EF DELAMINATED.<[01] RECEIVED NEW PANEL #221EF ; INSTALLATION WILL BE ACCOMPLISH ON TTG8Q00PUACN;[02] VERIFIED 1.SDR SWAA2024012331967Floor Panel · delaminatedCABIN FLOOR PANEL #242VF DELAMINATED.<[01] RECEIVED PANEL #242 VF P.N#147A5810-309; WILL BE INSTALLED ON N.R# TTG8Q00PUGRN.;[02] RECEIVED PANEL #242 VF P.N#147A5810-309; WILL BE INSTALLED ON N.R# TTG8Q00PUHAC.;[03] VERIFIED 2. CORRECTION TO STEP 1.SDR SWAA2024012331963Floor Panel · delaminatedCABIN FLOOR PANEL #241ADF DELAMINATED.<[01] RECEIVED PANEL #241 ADF P.N#147A5810-362; WILL BE INSTALLED ON N.R# TTG8Q00PUGRN.;[02] VEIFIED 1.SDR SWAA2024012331969Floor Panel · delaminatedCABIN FLOOR PANEL #242UF DELAMINATED.<[01] RECEIVED PANEL #242 UF P.N#147A5810-389; WILL BE INSTALLED ON N.R# TTG8Q00PUHAK.;[02] VERIFIED 1.SDR SWAA2024012331971Floor Panel · delaminatedCABIN FLOOR PANEL #242AF DELAMINATED.<[01] RECIEVED FLOORPANEL 242 AF P.N#144A5810-190 WILL BE INSTALLED ON N/R: TTG8Q00PUH74.;[02] VERIFIED 1.SDR SWAA2024012331972Floor Panel · delaminatedCABIN FLOOR PANEL #241AF DELAMINATED.<[01] RECIEVED FLOORPANEL 241 AF P.N#144A5810-127 WILL BE INSTALLED ON N/R: TTG8Q00PUGRC.;[02] VERIFIED 1.SDR SWAA2024012331973Floor Panel · delaminatedCABIN FLOOR PANEL #241DF DELAMINATED.<[01] RECIEVED FLOORPANEL 241 DF P.N#144A5810-128 WILL BE INSTALLED ON N/R: TTG8Q00PUGRN.;[02] VERIFIED 1.SDR SWAA2024011631806Floor 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] PANEL REPLACED. JOB SDR SWAA2024011631807Floor 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] PANEL REPLACED. JOB SDR SWAA2024011631815Floor Panel · pulledFWD FLOOR PANEL 221GF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221GF 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 SWAA2024011631812Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222CF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2024011631816Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241DF HAS PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE ON PASSENGER CABIN FLOOR PANEL 241DF FABRICATED NEW PANEL FROM BMS4-17 TYPE 6 LOT#1544951-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK3BA2380A/A; CURED USING HEAT SDR SWAA2024011631820Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241FF HAS PULLED STRANDS.<[01] VERIFIED STEP 1;2 AND THE MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 241FF WITH PULLED STRANDS WAS BEYOND ECONOMICAL REPAIR. PANEL WAS REPLACED BY FABRICATING A NEW ONE IAW SRM 53-00-50-2R-0 ASDR SWAA2024011631818Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 242CF HAS PULLED INSERT.<[01] VERIFIED STEP 1;2 AND THE MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 242CF WITH A PULLED INSERT WAS BEYOND ECONOMICAL REPAIR. PANEL WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0SDR SWAA2024011631821Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AAF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS BEYOND ECONOMICAL REPAIR. A NEW PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0 AND BOEING DWG 147A5810 ID: 0008.;[02] VERIFIED COSDR SWAA2024011631823Floor Panel · pulledAFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ADF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 241ADF WAS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.SDR SWAA2024011631824Floor Panel · pulledAFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 242TF REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETE.SDR SWAA2024011631827Floor Panel · pulledAFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242UF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] VERIFIED FLOOR PANEL 242UF WAS REPAIRED PER SRM 53-00-50-2R-1.;[03] WORKSCOPE COMPLETESDR SWAA2024011631828Floor 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] VERIFIED FLOOR PANEL 242VF WAS REPAIRED IAW SRM 53-00-50-2R-1.SDR SWAA2024011631956Floor Panel · corrodedCORROSION FLOOR PANEL 221BF INSERT AT PASSENGER CABIN 2023-756820<[01] FLOOR PANEL 221BF WILL BE REPLACED BY ANOTHER MAINTENANCE PROCEDURE AT PASSENGER CABIN AND WORK WILL BE DOCUMENTED ON ?TTG8Q00QA4MY?;[02] CORRECTED STEP 1. <BR>FLOOR PANEL 221BF WILL BE REPSDR SWAA2024011631949Floor Panel · corrodedCORROSION FLOOR PANEL 221BF SLEEVE AT PASSENGER CABIN 2023-756821<[01] FLOOR PANEL 221BF WILL BE REPLACED BY ANOTHER MAINTENANCE PROCEDURE AT PASSENGER CABIN AND WORK WILL BE DOCUMENTED ON ?TTG8Q00QA4MS?;[02] CORRECTED STEP 1.<BR>FLOOR PANEL 221BF WILL REPLACESDR SWAA2024011631955Floor Panel · crackedCRACK FLOOR PANEL 221BF AT PASSENGER CABIN 2023-756819<[01] REPLACED FLOOR PANEL 221BF AT PASSENGER CABIN IAW B737-700 AMM 53-21-00-400-801 <BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED FLOOR PANEL 221BF AT PASSENGER CABIN IAW B737-700 AMM 53-21-00-400-801 <SDR SWAA2024011231795Panel · crackedAFT CARGO PANEL 141PW INSTALLATION AREA WITH BRACKET PN 149A8109-114 CRACKED.<[01] REMOVED AND REPLACED BRACKET ON AFT CARGO PANEL 141PW INSTALLATION AREA PER REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.SDR ASAA2023121348793Floor Panel · delaminatedLESSOR ITEM 537: CABIN FLOOR PANEL L3 DOOR 3 OFF DENTS. PANEL 261LG GROUNDED - YES. EVALUATED AND RECEIVED NEW FLOOR PANEL 261LG, P/N: E5367180500000 TO BE INSTALLED ON NON-ROUTINE 32105 (HAECO) CUST. CARD NO: G1871105SDR ASAA2023121348163Floor Panel · delaminatedCABIN FLOOR PANEL 251RF TOTALLY DE-LAMINATED. GROUNDED - YES. EVALUATED 251RF CABIN FLOOR PANEL AS BEYOND REPAIRABLE LIMITS AND REQUIRES REPLACEMENT IAW A320-200 SRM 53-02-000-283-001 TABLE 002 FIG 2 FH 35266:10, FC 11749, WV 015. RECEIVED NEW FLOOR PANEL 251R
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