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 SWAA2023092794225Floor Panel · corrodedAFT CABIN FLOOR PANEL 242UF HAS CORRODED INSERTS.<[01] PANEL 242UF WILL BE REPLACED ON ITEM TTG8Q00N353K;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2023092794226Floor Panel · corrodedAFT CABIN FLOOR PANEL 242WF HAS CORRODED INSERTS.<[01] REMOVED AND REPLACED INSERT AT MAIN CABIN FLOOR PANEL # 242WF REF SRM 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2023092794227Floor Panel · corrodedAFT CABIN FLOOR PANEL 242VF HAS CORRODED INSERTS.<[01] PANEL 242VF WILL BE REPLACE ON ITEM TTG8Q00N354J;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2023092794233Floor Panel · corrodedAFT CABIN FLOOR PANEL 241ADF HAS CORRODED INSERTS.<[01] PANEL 241ADF WILL BE REPLACE ON TTG8Q003542;[02] CORRECTION TO STEP 1 SHOULD READ PANEL 241ADF WILL BE REPLACE ON TTG8Q00N3542;[03] VERIFIED CORRECTIVE ACTION.SDR SWAA2023092794229Floor Panel · corrodedAFT CABIN FLOOR PANEL 241AAF HAS CORRODED AND BROKEN INSERTS.<[01] PANEL 241AAF WILL BE REPLACED ON ITEMMTTG8Q00N3549;[02] VERIFIED CORRECTIVE ACTION.SDR SWAA2023092794244Floor Panel · corrodedFWD CABIN FLOOR PANEL 222AF HAS CORRODED INSERTS.<[01] REMOVED AND REPLACED INSERT'S AT MAIN CABIN FLOOR PANEL #222AF REF SRM 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION STEP 1SDR SWAA2023092794238Floor Panel · corrodedFWD CABIN FLOOR PANEL 222DF HAS CORRODED INSERTS<[01] REMOVED AND REPLACED INSERT'S AT MAIN CABIN FLOOR PANEL # 222 DF REF SRM 53-00-50-2R-0;[02] VERIFIED INSERTS INSTALLATIONSDR SWAA2023092794239Floor Panel · corrodedFWD CABIN FLOOR PANEL 221AF HAS CORRODED INSERTS<[01] REMOVED AND REPLACED INSERT'S AT MAIN CABIN FLOOR PANEL #221AF REF SRM 53-00-5-2R-0;[02] VERIFIED CORRECTIVE ACTION STEP 1SDR SWAA2023092794245Floor Panel · corrodedFWD CABIN FLOOR PANEL 221CF HAS CORRODED INSERTS<[01] REMOVED AND REPLACED INSERTS AT MAIN CABIN FLOOR PANEL # 221CF REF SRM 53-00-50-2R-0;[02] VERIFIED STEP 1SDR SWAA2023092794234Floor Panel · corrodedAFT CABIN FLOOR PANEL 241ABF HAS CORRODED INSERTS.<[01] REMOVED AND REPLACED INSERT'S AT MAIN CABIN FLOOR PANEL # 241 ABF REF SRM 53-00-50-2R-0;[02] VERIFIED 1.SDR ASAA2023082744979Floor Panel · damagedAFT CABIN FLOOR PANEL PN 147A5810-398 DAMAGED INSERTS. GROUNDED - YES. REPAIRED AND REPLACED DAMAGED INSERT ON AFT CABIN FLOORPANEL PN 147A5810-398. IAW B737-900 SRM 53-00-50-2R-0 AND DWG 147A5810-398 REV A.SDR ASAA2023082744978Floor Panel · damagedAFT CABIN FLOOR PANEL PN 147A5810-421 TOP LAYER DAMAGED. GROUNDED - YES. REPAIRED AFT CABIN FLOOR PANEL PN 147A5810-421 TOP LAYER. IAW B737-900 SRM 53-00-50-2R-0.SDR ASAA2023082744977Floor Panel · damagedAFT CABIN FLOOR PANEL PN 147A5710-477 TOP LAYER DAMAGED. GROUNDED - YES. REPAIRED AFT CABIN FLOORPANEL PN 147A5810-477 TOP LAYER. IAW B737-900 SRM 53-00-50-2R-0.SDR ASAA2023082744976Floor Panel · damagedAFT CABIN FLOOR PANEL PN 147A5810-440 TOP LAYER DAMAGED. MAJOR REPAIR GROUNDED - YES. REPAIRED TOP LAYER OF AFT CABIN FLOOR PANEL PN 147A5810-440. IAW B737-900 AMM 53-00-50-2R-0SDR DALA2023083007075Unknown · unknown(LOG 2939510) FWD CARGO COMPARTMENT R/H FLOOR BAFFLE STA 500J-500K CRACKED. REMOVED AND REPLACED R/H BAFFLE STA 500J-STA 500K IAW B737 BOEING DRAWING 143A7505.SDR DALA2023082907044Unknown · unknownSHIP 0669 CRACK ON STABILIZER STRAP STA 1340 RBL 25 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00441: STABILIZER STRAP STA 1340 RBL 25 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM 53-00-51. (2937059)SDR SWIA20231006825Unknown · crackedR/H FLOOR SUPPORT ANGLE COMMON TO COCKPIT FLOOR BEAM AT RBL 12.0 FS 280.0 CRACKED (C-CHECK RO 10/4/2023) REMOVED AND REPLACED WITH NEW R/H FLOOR SUPPORT ANGLE COMMON TO COCKPIT FLOOR BEAM AT RBL 12.0 FS 280.0 REF CRJ700 SRM 51-42-06-001-001-A01 REV. 3SDR SWAA2023092893761Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PANEL 242TF TOP SKIN PEELING OFF SEVERAL AREAS<[01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL 242TF BY OUTSIDE VENDOR (AERO MARINE). REF. DWG 147A5810-94 WITH PO # 2035184. PANEL ASSY WILL BE INSTALLED ON FAULT # TTG8Q00MLQYESDR SWAA2023091993732Floor Panel · pulledPASSENGER CAIN FLOOR PANEL 221AF HAS PULLED STRANDS ON UPPER SURFACE.<[01] PULLED STRANDS ON UPPER SURFACE OF PASSENGER CABIN FLOOR PANEL 221AF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023091993733Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 222BF HAS PULLED STRANDS ON UPPER SURFACE.<[01] UPDATED MEASUREMENT TABLE.;[02] PASSENGER CABIN FLOOR PANEL 222BF WITH PULLED STRANDS ON UPPER SURFACE WAS REPAIRED PER SRM 53-00-20-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[0SDR DALA2023082907041Unknown · unknownSHIP 0692 CORROSION ON LH SIDE PLATE IN AFT CARGO COMPARTMENT, BTW STA 1310 TO 1410. CORRECTIVE ACTION: SUMMARY OF NRC 00552: SIDE PLATE IN AFT CARGO COMPARTMENT, BTW STA 1310 TO 1410 WAS REPLACED AND INSTALLED PER B757-200 SRM 51-40-02. (2936074)SDR AALA202308289667Floor Panel · unknownAIRCRAFT WASD GROUNDED: CABIN FLOOR PANEL 231KF AT SEAT ROW 2 IN AISLE WAS REPORTED AS SPONGY. MAINTENANCE REPAIRED FLOOR PANEL PER EA 347519.SDR SWAA2023092893295Floor Panel · peelingAFT WET AREA FLOOR PANEL 241ABF HAS LOSS LAYERS OF COMPOSITE MATERIAL.<[01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL 241ABF BY OUTSIDE VENDOR (AERO MARINE). REF. DWG 147A5810-88 WITH PO # 2035180. PANEL ASSY WILL BE INSTALLED ON FAULT # TTG8Q00MLPX4;[02]SDR SWAA2023092893297Floor Panel · peelingAFT WET AREA FLOOR PANEL 241AEF HAS LOSS LAYERS OF COMPOSITE MATERIAL.<[01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL 241AEF BY OUTSIDE VENDOR (AERO MARINE). REF. DWG 147A5810-351 WITH PO # 2035182. PANEL ASSY WILL BE INSTALLED ON FAULT # TTG8Q00MLPWX;[02SDR SWAA2023092899215Floor Panel · peelingAFT WET AREA PANEL 242UF HAS LOSS OF SEVERAL LAYERS OF COMPOSITE MATERIAL.<[01] RECIEVED NEW AFT WET AREA FLOOR PANEL 242UF PO#2035176 REF TASK CARD TTG8Q00MLQYA FOR PANEL INSTALLATION;[02] VERIFIED STEP 1.SDR SWAA2023092893293Floor Panel · corrodedAFT WET AREA PANEL 242UF HAS FIFTEEN INSERTS WITH CORROSION.<[01] PANEL WILL BE REPLACED ON TASK TTG8Q00N1DPC;[02] VERIFIED PANEL WILL BE REPLACED ON TC TTG8Q00N1DPC.;[03] CORRECTION TO STEP 1: PANEL WILL BE REPPLACED ON TASK CARD TTG8Q00N1DPH;[04] CORRECTION SDR SWAA2023092898338Floor Panel · corrodedAFT WET AREA PANEL 241AAF HAS FOURTEEN INSERTS WITH CRROSION.<[01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL 241AAF BY OUTSIDE VENDOR (AERO MARINE). REF. DWG 147A5810-8 WITH PO # 2035177. PANEL ASSY WILL BE INSTALLED ON FAULT # TTG8Q00MLPX6;[02] INSP./VERSDR SWAA2023092893294Floor Panel · corrodedAFT WET AREA FLOOR PANEL 241ABF HAS SEVEN INSERTS WITH CORROSION.<[01] DUPLICATE ITEN - THIS FAULT WAS ACCOMPLISHED ON FAULT # TTG8Q00N1DQT;[02] VERIFIED STEP 1SDR SWAA2023092893296Floor Panel · corrodedAFT WET AREA FLOOR PANEL 241AEF HAS THREE INSERTS WITH CORROSION.<[01] DUPLICATE ITEN - THIS FAULT WILL BE ACCOMPLISHED ON FAULT # TTG8Q00N1DRD;[02] VERIFIED STEP 1SDR SWAA2023092693400Floor Panel · brokenCABIN FLOOR PANEL 242WF IS BROKEN.<[01] CABIN FLOOR PANEL 242WF WITH BROKEN LOWER SKIN O/B EDGE WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023092693298Floor Panel · corrodedAFT WET AREA FLOOR PANEL 241ACF HAS FOUR INSERTS WITH CORROSION.<[01] REMOVED AND REPLACED SEVERAL INSERTS AT CABIN AFT WET AREA FLOOR PANEL 241ACF PER B737-700 SRM 53-00-50-2R-1;[02] VERIFIED STEP 1SDR ASAA2023082444881Floorboard · delaminatedFWD WET AREA BOARD DELAM P/N 141A5810Y183. GROUNDED - YES. EVALUATED & ACCOMPLISH PERMANENT REPAIR TO FWD WET AREA FLOOR BOARD P/N 141A5801Y183 IAW B737-800 SRM 53-00-50-1A-1, 53-00-50-2R-01, 53-00-50-2R-6.SDR SWAA2023092192648Floor Panel · frayedMAIN CABIN FLOOR PANEL 221CF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL AND WILL BE INSTALLED ON T/C TTG8Q00MKT4J;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 221CF AND WILL BE INSTALLED ON T/C TTG8Q00MKT4J;[03] VERIFIED; STEP # 2.SDR SWAA2023092192649Floor Panel · frayedMAIN CABIN FLOOR PANEL 222BF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 222BF AND WILL BE INSTALLED ON T/C TTG8Q00N0FKV;[02] VERIFIED STEP 1SDR SWAA2023092192650Floor Panel · frayedMAIN CABIN FLOOR PANEL 221AF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL AND WILL BE INSTALLED ON T/C TTG8Q00MKT4N;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 221AF AND WILL BE INSTALLED ON T/C TTG8Q00MKT4N;[03] VERIFIED; STEP # 2.SDR SWAA2023092192651Floor Panel · frayedMAIN CABIN FLOOR PANEL 221DF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 221DF AND WILL BE INSTALLED ON T/C TTG8Q00MKT4G;[02] VERIFIED STEP 1SDR SWAA2023092192652Floor Panel · frayedMAIN CABIN FLOOR PANEL 242TF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL AND WILL BE INSTALLED ON T/C TTG8Q00MKT3N;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 242TF AND WILL BE INSTALLED ON T/C TTG8Q00MKT3N;[03] VERIFIED; STEP # 2.SDR SWAA2023092192653Floor Panel · frayedMAIN CABIN FLOOR PANEL 242UF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 242UF AND WILL BE INSTALLED ON T/C TTG8Q00MKT3L;[02] VERIFIED STEP 1SDR SWAA2023092192654Floor Panel · frayedMAIN CABIN FLOOR PANEL 241XF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 241XF AND WILL BE INSTALLE ON T/C TTG8Q00MKSX0;[02] VERIFIED; STEP # 1.SDR SWAA2023092192655Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ZF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR 241ZF AND WILL BE INSTALLED ON T/C TTG8Q00MKSY3;[02] VERIFIED STEP 1SDR SWAA2023092192656Floor Panel · frayedMAIN CABIN FLOOR PANEL 241AAF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 241AAF AND WILL BE INSTALLED ON T/C TTG8Q00MKSY1;[02] VERIFIED; STEP # 1.SDR SWAA2023092192657Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ABF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 241ABF AND WILL BE INSTALLED ON T/C TTG8Q00MKSXZ;[02] VERIFIED STEP 1SDR SWAA2023092192646Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ACF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL AND WILL BE INSTALLED ON T/C TTG8Q00MKSXX;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 241ACF AND WILL BE INSTALLED ON T/C TTG8Q00MKSXX;[03] VERIFIED; STEP # 2.SDR ASAA2023082245715Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231XF IS DELAMINATED GROUNDED - YES. EVALUATED AND REPAIRED DELAMINATED AREA OF FIBERGLASS TOP LAYER ON MAIN CABIN FLOOR PANEL 231XF IAW A320-200 SRM REV 146 53-02-00-283-001 AND A320-200 SRM 53-02-00-300-013 THIS IS A CATEGORY A PERMSDR ASAA2023082245697Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231KF IS DELAMINATED GROUNDED - YES. EVALUATED AND REPAIRED 2EA AREAS OF DELAMINATED FIBERGLASS TOP LAYER ON MAIN CABIN FLOOR PANEL 231KF IAW A320-200 SRM 53-02-00-283-001 AND A320-200 SRM 53-02-00-300-013. FH-48745:53 FC-18418 WV-010SDR SWAA2023092192639Floor Panel · frayedMAIN CABIN FLOOR PANEL 222CF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 222CF AND WILL BE INSTALLED ON T/C TTG8Q00MKT48;[02] VERIFIED STEP 1SDR SWAA2023092192643Floor Panel · crackedMAIN CABIN FLOOR PANEL 221GF FWD O/B END CRACKED<[01] RECEIVED MAIN CABIN FLOOR PANEL 221GF AND WILL BE INSTALLED ON T/C TTG8Q00MKT4A;[02] VERIFIED STEP 1SDR FDEA202308221477Floor Panel · crackedAFT CARGO FLOOR PANEL 154GF BROKEN. AFT CARGO FLOOR PANEL 154GF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR.4.B FIG.201 SHEET 2 REV.87 AUG 15/2023SDR UIEA2023082200791Unknown · unknownCRACK - STRINGER OF FUSELAGE STA 980 + 160 S12L(<P>1) REPAIRED DAMAGE AREA IAW SRM 53-20-03-2R-1 REV 40 AND DWG 142U3312 SH 8 REV C. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR SWAA2023092191973Floor Panel · corrodedFWD CABIN FLOOR PANEL 221CF HAS CORRODED INSERTS.<[01] NEW FLOOR FANEL INSTALLED ON FAULT TTG8Q00N0FKT;[02] CORRECTION TO STEP #1: NEW FLOOR PANEL INSTALLED ON FAULT TTG8Q00N0FKT.;[03] VERIFIED STEP 2
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