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 IPXA2023081493905Floor Panel · damagedINSPECTION TYPE:C*** MAJOR REPAIR *** PANEL 132DE IS DAMAGED.FABBED PNL 132DE PER SREO A300-5320-16407.SDR IPXA2023081493904Floor Panel · damagedINSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131SG IS DAMAGED.FABBED PNL 131SG PER SREO A300-5320-16407.SDR SWAA2023080986431Floor Panel · crackedFWD CARGO FIBERGLASS FLOOR PANEL HAS 14 INCH CRACK<[01] REPAIRED FLOOR PANEL IAW AMM 25-52-01 OK FOR CONT SERVICESDR SWAA2023090686331Floor Panel · crackedCRACK FLOOR PANEL 241AEF AT AFT GALLEY AND LAV 2023-490491<[01] TOOL USED CALIPER P/N: 500-197-30 S/N/ B20189527 DUE DATE 26/DEC/23.;[02] TOOL USED: HOT BONDER P/N:HCS9000B-AV S/N:18164925 DUE DATE:22-JAN-24;[03] TOOL USED: CR5200 S/N:8342514510 DUE DATE:13-FESDR SWAA2023082286270Floor Panel · corrodedPNL 120DF HAS CORROSION ALONG THE SIDES.<[01] REPLACED AND INSTALLED NEW FLOOR PANEL PER AMM 25-52-10 SEE TASK TTG8Q00MN032 FOR FLOOR PANEL SEALANT;[02] VERIFIED C/A #1.SDR DALA2023080706423Unknown · unknownSHIP 3118 CRACK FLOOR PANEL 261DF EDGE AREA AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 610344-14 REV. (2903118)SDR SWI2023F00389Unknown · corrodedCABIN - FS 280 FLOOR PANEL SUPPORT ANGLE CORRODED (C-CHECK RO 10/4/2023) REMOVED AND INSTALLED NEW FWD FLOOR SUPPORT ANGLE P/N CC670-34095-1SB. CRJ 700 SRM 51-42-06-001-001-A01, AND DWG #CC670-33052 REV. GCOMPLIED WITH TASK 51-900-1002-SKYSDR SWAA2023090585913Floor Panel · crackedCRACK FLOOR PANEL 211AF AT COCKPIT 2023-477690<[01] REPLACED FLOOR PANEL 211AF AT COCKPIT I.A.W B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9.;[02] REPLACED FLOOR PANEL 211AF AT COCKPIT I.A.W B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9.SDR DALA2023080406342Unknown · unknownSHIP 3126 CORROSION SUPPORT WEB LOCATED BTW FR69 TO F70 AT LEVEL STRG 23 LH. CORRECTIVE ACTION: REPLACED SUPPORT WEB SUPPORT WEB LOCATED BTW FR69 TO F70 AT LEVEL STRG 23 LH AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (2899599)SDR DALA2023080406341Unknown · unknownSHIP 3126 CORROSION SUPPORT WEB LOCATED BTW FR69 TO F70 AT LEVEL STRG 23 RH. CORRECTIVE ACTION: REPLACED SUPPORT WEB AND FASTENER, LOCATED BTW FR69 TO FR70 AT LEVEL STR23 RH AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (2899593)SDR FDEA202308031356Floor Panel · dentedMDC FLOOR PANEL 221CFF WITH DENTS MDC FLOOR PANEL 221CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4B FIG 201. REV APR 15 2023SDR FDEA202308031355Floor Panel · dentedMDC FLOOR PANEL 221DFF WITH DENTS MDC FLOOR PANEL 221DFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4B FIG 101 SHEET 2 REV 86 APR 15 2023SDR FDEA202308031353Floor Panel · dentedMDC FLOOR PANEL 222BFF WITH DENTS MDC FLOOR PANEL 222BFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 101 SHEET 2. REV 86 APR 15 2023SDR FDEA202308031352Floor Panel · dentedMDC FLOOR PANEL 222AFF WITH DENTS MDC FLOOR PANEL 222AFF WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR FIG 201 SHEET 2. REV 86 APR 15 2023SDR FDEA202308031351Floor Panel · dentedMDC FLOOR PANEL 222CFF WITH DENTS MDC FLOOR PANEL 222CFF WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 SHEET 2. REV 86 APR 15 2023SDR SWIA2023082202Unknown · corrodedCORROSION, AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CENTER AND RH SHEAR PANELS. (C-CHECK RO 8/18/2023) REMOVED AND REPLACED RH LONGITUDINAL FLOOR BEAM AFT WET AREA REF EMB SRM 51-40-08. SEE CONTINUATION CSDR SWIA202300801Unknown · crackedL/H COCKPIT FLOOR BEAM AT BL12.0 CRACKED IN LOWER RADIUS AT FS 280.0 (C-CHECK RO 9/13/2023) PERFORMED A SPLICE REPAIR TO REMOVE DAMAGED FLOOR BEAM BY REMOVING CRACKED FLOOR ANGLE AT L/H COCKPIT FLOOR BEAM AT BL12.0 FS 280.0 REF CRJ700 SRM 51-42-06-001-0SDR SWAA2023083184767Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #242RF; UPPER SURFACE DELAMINATED DOT 223-AW242RF.<[01] RECEIVED NEW FLOOR PANEL# 242RF. THIS PANEL WILL BE INSTALL ON FAULT# TTG8Q00M6ZT2.;[02] FINAL INSPECTION. RECEIVED NEW FLOOR PANEL# 242RF. THIS PANEL WILL BE INSTALL ONSDR SWAA2023083184612Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #241ACF; UPPER SURFACE DELAMINATED DOT 223-AW241ACF.<[01] RECEIVED PANEL 241ACF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 241ACF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00MSDR SWAA2023083184611Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #241AEF; UPPER SURFACE DELAMINATED DOT 223-AW241AEF.<[01] RECEIVED PANEL 241AEF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 241AEF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00MSDR SWAA2023083184610Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #241ADF; UPPER SURFACE DELAMINATED DOT 223-AW241ADF.<[01] RECEIVED NEW FLOOR PANEL# 241ADF. PANEL WILL BE INSTALL ON FAULT# TTG8Q00M6ZAL.;[02] FINAL INSPECTION. RECEIVED NEW FLOOR PANEL# 241ADF. PANEL WILL BE INSTALL ON FAULTSDR SWAA2023083184609Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL #242WF; UPPER SURFACE DELAMINATED DOT 223-AW242WF.<[01] RECEIVED PANEL 242WF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 242WF WILL BE COMPLETED ON ROUTINE CARD TTG8Q00M6ZSS.;[02] SDR SWAA2023083184613Floor Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #242UF; UPPER SURFACE DELAMINATED UPPER SURFACE DELAMINATED DOT 223-AW242UF.<[01] RECEIVED PANEL 242UF FABRICATED BY OUTSIDE VENDOR AND ATTACHED CERTS IN MAINTENIX. FINAL INSTALLATION OF FLOOR PANEL 242UF WILL BE COMPLETED ONSDR SWAA2023083184606Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL #232SF; UPPER SURFACE DELAMINATED DOT 223-CP232SF.<[01] RECEIVED MAIN CABIN FLOOR PANEL 232SF (P/N 144A5810-161); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZCA.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 232SF (P/N 144ASDR SWAA2023083184608Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL #231ZF; UPPER SURFACE DELAMINATED DOT 223-CP231ZF.<[01] RECEIVED NEW PANEL 231ZF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZD4;[02] VERIFIED STEP 1. COMPLETESDR SWAA2023083184607Access Panel · delaminatedPASSENGER CABIN FLOOR ACCESS PANEL #241DF; UPPER SURFACE DELAMINATED DOT 223-CP241DF.<[01] RECEIVED NEW PANEL 241DF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZAA;[02] VERIFIED STEP 1. COMPLETESDR SWAA2023081684385Floor Panel · corroded(A204 DOT 59) FWD CARGO FLOOR PANEL 120DF HAS LIGHT SURFACE CORROSION ALONG RH EDGE ON UPPER AND LOWER SURFACE.<[01] FABRICATED NEW FLOOR PANEL C/W;[02] FABRICATED NEW FLOOR PANEL C/W;[03] AUDIT C/W.SDR SWAA2023080184156Floor Panel · crackedAFT CARGO FFIBER GLASS FLOOR PANEL HAS 14 CRACK AND 2 FAR FROM THE EDGE /FASTENER.<[01] INSPECTED AND REPAIRED THE AFT CARGO FLOOR PANEL IAW AMM 25-52-00SDR DALA2023080106211Unknown · unknownCORROSION ON GENERATION FLOOR ACCESS PANELS 221SF, 222EF, 221NF, 222AWF, AND 222SF. SUMMARY OF NRC 00283: CORROSION LEVEL 2. FLOOR ACCESS PANELS 222EF AND 222SF WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2, FLOOR PANELS 221SF AND 221NF WERE FSDR SWAA2023090583797Floor Panel · crackedCRACK FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2023-477507<[01] REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02 AND DWG# 453A1610 REV C. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED<BR>SEE INDIVIDUAL SIGN OFF BELOWSDR SWAA2023083184100Floor Panel · delaminatedFWD CABIN WET AREA FLOOR PANEL NO- 221EF UPPER SKIN SURFACE DELAMINATED MKD DOT<[01] RECEIVED MAIN CABIN FLOOR PANEL 221EF (P/N 141A5810-249); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZUJ.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 221EF (P/N 141SDR SWAA2023083184101Floor Panel · corrodedFWD CABIN WET AREA FLOOR PANEL NO-221BF UPPER SURFACE SKIN BULGING ;DELAMINATED AREAS MKD DOT<[01] RECEIVED NEW PANEL 221BF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZUS;[02] FINAL INSPECTION; RECEIVED NEW PANEL 221BF ; THIS PANEL WILL BE INSTALL ON FAUSDR SWAA2023082383807Floor Panel · damagedFWD CABIN FLOOR PANEL 231CF UPPER SKIN SURFACE CHIPPING AT EDGE.<[01] REMOVED AND REPLACED FWD CABIN FLOOR PANEL 231CF UPPER SKIN ASPER AMM 53-21-000-801 AND 53-21-00-400-801;[02] VERIFIED REMOVED AND REPLACED FWD CABIN FLOOR PANEL 231CF.SDR SWAA2023082383806Floor Panel · peelingR/H FWD CABIN FLOOR 232AF UPPER SKIN SURFACE PEELING.<[01] RECEIVED R/H FWD CABIN FLOOR 232AF UPPER SKIN SURFACE WILL BE CLOSED ON TTG8Q00LYLAQ ASPER DWG#141A5810;[02] VERIFIED 1.SDR SWAA2023083183687Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 231GF. 8-64<[01] RECEIVED NEW FLOOR PANEL 231GF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZTU;[02] FINAL INSPECTION; RECEIVED NEW FLOOR PANEL 231GF ; THIS PANEL WILL BE INSTALL ON FAULT # TTG8Q00M6ZTUSDR SWAA2023083183680Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING RF. 8-66 PANEL FLOOR 241RF<[01] RECEIVED NEW PANEL 241RF ; THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00M6Z9S;[02] VERIFIED STEP 1. COMPLETESDR SWAA2023083183679Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 241UF. 8-67<[01] RECEIVED MAIN CABIN FLOOR PANEL 241UF (P/N 146A5810-470); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6YE6.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 241UF (P/N 146A5810-470); PANEL WILL BE CLSDR SWAA2023083183682Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 231XF. 8-62<[01] RECEIVED NEW FLOOR PANEL PANEL 231XF ; THIS FLOOR WILL BE INSTALL ON FAULT #TTG8Q00M6ZE0;[02] FINAL INSPECTION; RECEIVED NEW FLOOR PANEL PANEL 231XF ; THIS FLOOR WILL BE INSTALL ON FAULT #TTG8Q00M6ZE0.SDR SWAA2023083183678Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 231KF. 8-63<[01] RECEIVED MAIN CABIN FLOOR PANEL 231KF (P/N 143A5810-580); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZTN;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 231KF (P/N 143A5810-580); PANEL WILL BE CLOSDR SWAA2023083183677Floor Panel · peelingCABIN FLOOR PANEL UPPER SURFACE PEELING 231DF. 8-65<[01] RECEIVED MAIN CABIN FLOOR PANEL 231DF (P/N 143A5810-513); PANEL WILL BE CLOSED ON TASK CARD TTG8Q00M6ZU0.;[02] FINAL INSPECTION; RECEIVED MAIN CABIN FLOOR PANEL 231DF (P/N 143A5810-513); PANEL WILL BE CLSDR SWAA2023081683649Floor Panel · corroded185-010 AFT CARGO FLOOR PANEL 140DF HAS CORROSION ON BOTH SIDE OF DOOR OPENING<[01] REMOVED CORROSION AT AFT CARGO FLOOR PNL 140DF VERIFIED MATERIAL LOSS ;LOSS IS OVER 3.0 IN LENGTH IS OUT OF LIMITS I/A/W SRM 53-00-53-1A-1 STEP 5 A.B;[02] VERIFIED STEP 1;[03] SDR DALA2023080106201Unknown · unknownCORROSION ON FLOOR PANEL 211AMF AT COCKPIT. SUMMARY OF NRC 00299: CORROSION LEVEL 2. PANEL (SKIN) OF FLOOR PANEL 211AMF AT COCKPIT WAS FABRICATED AND REPLACED PER DWG 9957826 REV AA, B717-200 SRM 51-20-05-0G AND 51-41-02-0G. (LP #2891380)SDR AALA202307312639Floor Panel · damagedAIRCRAFT WAS GROUNDED: FLIGHT ATTENDANT REPORTS THAT THE FLOOR PANEL AT SEAT ROW 17 IS VERY SOFT. MAINTENANCE REPLACED FLOOR PANEL PER AMM 53-22-12.SDR AALA202308091300Floor Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN BREAK ASSEMBLY LOCATED AT BS 540 FROM BL 0 TO LBL 18. REPLACED BREAK ASSEMBLY PER AARD 51-00-05-1.SDR AALA202308096259Floor Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN BREAK ASSEMBLY LOCATED AT BS 540 FROM BL 0 TO RBL 18. REPLACED BREAK ASSEMBLY PER AARD 51-00-05-1.SDR DALA2023080106215Panel · corroded(LOG 2889784) FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL UPPER SURFACE HAS AREAS OF CORROSION BETWEEN BS 500 AND BS 500A. REMOVED AND REPLACED TRANSITION PANEL IAW B737 SRM 51-40-02-0G AT FWD CARGO COMPT RH FLOOR BETWEEN BS 500 AND BS 500A.SDR DALA2023080106214Panel · corroded(LOG 2889771) FORWARD CARGO COMPARTMENT RH FLOOR TRANSITION PANEL HAS AREAS OF CORROSION AT BS 430 TO BS 440. REMOVED AND REPLACED NEW TRANSITION PANEL AT FWD CARGO COMPARTMENT AT BS 430 TO 440 RH IAW B737 SRM 51-40-02, SRM 51-40-05 AND 53-00-53-1A-2.SDR SWAA2023082390330Floor Panel · crackedLEFT FLIGHT COMPARTMENT CONTROL STAND ACCESS PANEL # 211B CRACKED.<[01] APPLIED TOPCOAT ON LEFT FLIGHT COMPARTMENT CONTROL STAND ACCESS PANEL #211B REF B 737 AMM 25-00-00-370-801;[02] CORRECTION TO STEP 1: REPAIRED DAMAGE AREA ON LEFT FLIGHT COMPARTMENT CONTROSDR SWAA2023080882928Floor Panel · pulledDOT A24-26 MID CABIN FLOOR PANEL 232SF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] CLEANED UPPER SURFACE OF FLOORBOARD 232SF IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 5A(1);[02] VERIFIED ITEM 1;[03] FABRICATED NEW BOARD FROM SAMPLE IAW SRM 53-00-50-2R-0SDR SWAA2023080882932Floorboard · pulledDOT A24-23 MID CABIN FLOOR PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] FABRICATED NEW BOARD FROM SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 4; BOEING DRW. 144A5810 AND BAC5085 STEP 8.4.2.<BR>CURED ADHESIVE WITH HEAT LAMP AND DIGIT
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