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 ASAA2023053043566Floor Panel · delaminatedFLOOR PANEL 147A5810-440 INSERTS CORRODED. GROUNDED - YES. REPAIRED FLOOR PANEL 147A5810-440 IAW B737-900ER SRM 53-00-50-2R-0.SDR SWAA2023061453974Floor Panel · pulledDOT A24-10 MID CABIN FLOOR PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MULTIPLE PLIES MISSING ON UPPER SURFACE. TAP TEST GOOD/ FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1SDR SWAA2023061453969Floor Panel · pulledDOT A24-12 MID CABIN FLOOR PANEL 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRMSDR SWAA2023061453973Floor Panel · pulledDOT A24-9 MID CABIN FLOOR PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE TO UPPER AND LOWER SUFACES TO BE REPAIRABLE IAW SRM 53-00-50-2R-2 TABLE 201 REPAIR 2<BR>CLEANED AND PREPPED UPPER AND LOWER SURFACE IAW SRM 53-0SDR SWAA2023061453975Floor Panel · pulledDOT A24-11 MID CABIN FLOOR PANEL 242BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE ON UPPER AND LOWER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 2<BR>CLEANED; PREPPED AND APPLIED POTTING COMSDR SWAA2023061453970Floor Panel · pulledDOT A24-14 MID CABIN FLOOR PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE FULL LENTGTH OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED ASDR SWAA2023061453976Floor Panel · pulledDOT A24-15 MID CABIN FLOOR PANEL 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE FULL LENGTH OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED ANSDR SWAA2023061453988Floor Panel · pulledDOT A24-28 MID CABIN FLOOR PANEL 241AF IS MISSING ALL UPPER COMPOSITE FIBER PLYS AT AFT LH EDGE .<[01] EVALUATED AND FOUND MISSING PLIES EXPOSING CORE WITH NO DAMAGE TO CORE. TAP TEST GOOD AROUND DAMAGE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLESDR SWAA2023061957291Floor Panel · warpedPANEL 211AF WARPED AND DENTED.<[01] REMOVED AND REPLACED PANEL 211AF PER SRM 51-40-02.;[02] VERIFIED PANEL INSTALLED;[03] REMOVED AND REPLACED PANEL 211AF PER SRM 51-40-02.SDR SWAA2023061352876Floor Panel · damagedL/H CABIN FLOOR ACCESS PANEL 231LF LOWER SURFACE HAS (3 EACH) HOLES.<[01] REPAIRED FLOOR PANEL #231LF AT DAMAGED AREA PER B737 SRM 53-00-50-2R-2 PARA J. MATERIAL USED RESIN P/O #1799598; CLOTH P/O #1738579;[02] VERIFIED REPAIRSDR SWAA2023061352875Floor Panel · crackedL/H CABIN FLOOR ACCESS PANEL 231HF LOWER SURFACE HAS (2 EACH) CRACKS.<[01] REPAIRED FLOOR PANEL #231HF AT DAMAGED AREA PER B737 SRM 53-00-50-2R-2 PARA J. MATERIAL USED RESIN P/O #1799598; CLOTH P/O #1738579;[02] VERIFIED REPAIR.SDR FDEA202305260959Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221CFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR.4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260958Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260957Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222BFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260956Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260955Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B. FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260954Floor Panel · dentedMAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222AFF WITH DENTS. MAIN CARGO COMPARTMENT ACCESS FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00- 50-2R PAR. 4.B FIG. 201 SHEET 2 REV. 85 DEC15/2022SDR FDEA202305260953Floorboard · damagedFLOOR BOARD LBL 58.22 STATION 1200-1320 FLOOR BOARD CRACKED DAMAGE. FABRICATED ZONE 250 FLOORBOARD 251 MCI ON VTMAE TRAVELER # T23/1683607 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202305260952Floorboard · damagedMAIN CARGO CABIN RBL 58.22 STATION 900 FLOOR BOARD P/N: 11863182-2 DAMAGED. FABRICATED ZONE 240 FLOORBOARD 242 MCI ON VTMAE TRAVELER # T23/1683606 IAW DWG SRZ- 25-005 REVISION R. MAJOR REPAIRSDR FDEA202305260943Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 251MF(P/N:152W8601-31) AT STA1798/LBL1.5 FOUND A HOLE. EVALUATED MAIN DECK CARGO FLOOR PANEL 251MF(P/N:152W8601-31) AT STA1798/LBL1.5 A HOLE ,THE HOLE SIZE :LXW=2.0"X1.8" IN UPPER SURFACE ,WITHIN LIMIT AS PER B777 SRM 53-00- 5SDR FDEA202305260942Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 251FF(P/N:152W8601-19) AT STA1656/RBL1 FOUND A HOLE. EVALUATED MAIN DECK CARGO FLOOR PANEL 251FF(P/N:152W8601-19) AT STA1656/RBL1 A HOLE ,THE HOLE SIZE :LXW=1.8"X1.6" IN UPPER SURFACE ,WITHIN LIMIT AS PER B777 SRM 53-00-50-1A SDR SWAA2023070668440Floor Panel · crackedFWD CABIN WET AREA FLOOR PANEL 221BF AFT EDGE 2EA CRACKS AND MISSING INSERTS MKD DOTS<[01] REPLACED NEW FLOOR PANEL#221BF P.N# 141A5810-729 P.O#2012626. THIS PANEL WILL BE INSTALLED IN CUSTUMER CARD N.R# TTG8Q00L1NB1 PER SRM REF 53-00-50-2R-0 PARA 4.;[02] VERISDR SWAA2023062952125Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 CLASS 1 LOT AK2KP8383K-1 RESIN; CURED RESIN UNDER A HEAT LAMP USING THERMOMESDR SWAA2023062952126Floor Panel · pulledFLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL WITH BMS4-23 TYPE II LOT 1525675-1 AND BMS5-107 CLASS 1 LOT AK2KP8383K-1 RESIN; CURED RESIN UNDER A HEAT LAMP USING THERMOMESDR SWAA2023062952127Floor Panel · pulledFLOOR PANEL 242BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 242BF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1526676-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETER ASDR SWAA2023062952128Floor Panel · pulledFLOOR PANEL 241LF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL FROM BMS4-23 TYPE II LOT 1525675-1; DETERMINED INSERT HOLE LOCATIONS; UPSIZED INSERTS HOLES INSTALLED INSERTS WITH BMS5-107 SDR SWAA2023062952129Floor Panel · pulledFLOOR PANEL 241MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL FROM BMS4-17 TYPE VI LOT 1526676-1; DETERMINED INSERT HOLE LOCATIONS; UPSIZED INSERTS HOLES INSTALLED INSERTS WITH BMS5-107 SDR SWAA2023062952130Floor Panel · pulledFLOOR PANEL 241PF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW PANEL FROM BMS4-17 TYPE VI LOT 1526676-1; DETERMINED INSERT HOLE LOCATIONS; UPSIZED INSERTS HOLES INSTALLED INSERTS WITH BMS5-107 SDR SWAA2023062952131Floor Panel · pulledFLOOR PANEL 241RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241RF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5. MOST OF THE UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS OR DELAMINATION. AREAS EXCEED ALLOWABLE DAMAGE LIMITS 53-00SDR SWAA2023062952121Floor Panel · pulledFLOOR PANEL 241SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241SF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5. MOST OF THE UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS OR DELAMINATION. AREAS EXCEED ALLOWABLE DAMAGE LIMITS 53-00SDR SWAA2023062952122Floor Panel · pulledFLOOR PANEL 241TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241TF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5. MOST OF THE UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS OR DELAMINATION. AREAS EXCEED ALLOWABLE DAMAGE LIMITS 53-00SDR SWAA2023062952123Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241UF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1526676-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETER ASDR SWAA2023062952132Floor Panel · pulledFLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241VF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1526676-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETER ASDR SWAA2023062952133Floor Panel · pulledFLOOR PANEL 242NF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 242NF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1526676-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETER ASDR SWAA2023062952134Floor Panel · pulledFLOOR PANEL 242QF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 242QF FLOOR PANEL FROM BMS4-17 TYPE 6 LOT#1526676-1; LOCATED AND INSTALLED INSERTS USING BMS5-107 LOT#AK2KP8383K-1 AND CURED USING HEAT LAMP AND THERMOMETER ASDR IPXA2023112164678Floorboard · damaged*MAJOR REPAIR* MAIN CARGO AREA FLOOR BOARD PANEL P/N 814B6554-273 STATION 2260 LEFT SIDE DAMAGED. AND ONE INSERT MISSING.***SM20/LMX8*** VERIFIED INSTALLATION OF FLOOR PANEL PER SREO-42648-REQ1 STEPS 1-13SDR SWAA2023070652751Floor Panel · loosePANEL 241DF SHOWS UPPER SURFACE LOOSE FIBERS<[01] APPLIED REPAIR ON FLOOR PANEL 241 DF; AS PER B737 SRM 53-00-50-2R-1 MATERIAL USED PO 1473815 AND PO.1783720;[02] VERIFIED AND INSPECTED APPLIED REPAIR ON FLOOR PANEL 241 DF; AS PER B737 SRM 53-00-50-2R-1 MATERISDR SWAA2023070668432Panel · loosePANEL 222BF HAS SURFACE FIBERS LOOSE<[01] RECEIVED NEW FLOOR PANEL #222BF. PANEL TO BE INSTALLED ON ITEM #TTG8Q00L1MF8. AS PER B 737 AMM 53-21-00-400-801;[02] VERIFIED RECEIVED NEW FLOOR PANEL #222BF. AND VERIFIED #TTG8Q00L1MF8.SDR SWAA2023070668435Floor Panel · loosePANEL 242D SHOWS UPPER SURFACE LOOSE FIBERS<[01] RECEIVED NEW FLOOR PANEL (242D) P/N: 147A5810-345; PO# 2012626. REF TASK CARD: TTG8Q00L1MP3 FOR PANEL INSTALLATION.;[02] VERIFIED RECEIVED NEW FLOOR PANEL (242D)SDR SWAA2023070668436Panel · loosePANEL 242UF SHOWS UPPER SURFACE LOOSE FIBERS<[01] REPLACED NEW FLOOR PANEL #242UF P.N#147A5810-136 P.O #2012626. THIS PANEL WILL BE INSTALLED IN CUSTUMER CARD N.R# TTG8Q00L1N8Y PER SRM 53-00-50-2R-0.;[02] VERIFIED REPLACEDSDR SWAA2023070668437Floor Panel · loosePANEL 241XF HAS LOOSE FIBERS ON TOP SURFACE<[01] REPLACED NEW FLOOR PANEL # 241XF; P.N#147A5810-18 PO#2012626. THIS PANEL WILL BE INSTALLED IN COSTUMER CARD N.R# TTG8Q00L 1MP9 PER SRM REF 53-00-50-2R-0 PARA 4.;[02] VERIFIED REPLACEDSDR IPXA2023070560210Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 231XCF DAMAGE. VERIFIED COMPLETION OF FABRICATED PANEL 231XCF. SRM 53-00-50-2R-1 REVIEWED.SDR SWAA2023062951868Floor Panel · brokenAFT CABIN FLOOR PANEL 241ADF HAS A BROKEN AFT O/B CORNER<[01] IDENTIFIED PANEL IAW SRM 53-00-50-0I-1 FIGURE 6. DAMAGE TO THE PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.B AND WILL BE REPAIRED IAW SRM 53-00-50-2R-4. REMOVED AN APPROX. 1.7SDR AALA202305253066Floor Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 241MF CRACKED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.SDR FDEA202305240931Floorboard · damagedCTR CARGO FLOORBOARD 183EB HAS EVIDENCE OF IMPACT DAMAGE FABRICATED FLOORBOARD 183EB REF FEDEX DWG SRZ-25-005 MAJOR REPAIRSDR DALA2023052504154Unknown · unknownSHIP 3356 CORROSION FLOOR BEAM -Y380 BTW FR75/FR78 AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y380 LOC. BTW FR75/78 AT AFT GALLEY AREA. RII INSPECTION COMPLETE. (2782283)SDR ASAA2023052344956Floor Panel · delaminatedAFT WET AREA FLOOR PNL 261AC DELAMINATED GROUNDED - YES. FABRICATED NEW FLOOR PANEL 261AG IAW A320 SRM 53-02-00-300-011 AND GILL CORPORATION MANUAL TGC IRM 9701-REV L FH: 47561:57, FC:15607,WTV:010SDR SWAA2023070563486Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL#241AF FOUND WITH DELAMINATION.<[01] APPLIED THE GLASS FABRIC REPAIR PLIES AT DAMAGED AREA ON PASSENGER CABIN FLOOR PANEL#241AF. REF B737 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPHG 3. MATERIAL USED GLASS FABRIC REPAIR PLIES PO#: 1738579 ASDR DALA2023052504172Unknown · unknown(LOG 2780732) FLOOR SUPPORT IS CORRODED STA 967-986.5 LBL 16. REMOVED PART, LOCATED & DRILLED NEW PART AND INSTALLED IAW BOEING 737-800 SRM 51-40-05, 51-40-02.SDR AALA202305252946Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR PANEL 241GF DELAMINATED. REPLACED FLOOR PANEL PER SRM 53-02-00-300-011.
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