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 SWAA2024090520997Floor Panel · crackedFWD FLOOR PANEL 221GF O/B FWD CORNER TANG IS CRACKED.<[01] FLOOR PANEL 221GF O/B FWD CORNER TANG WITH CRACK 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] JOB COMPLETE.SDR SWAA2024090521027Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SURFACE OF AFT FLOOR PANEL 241ACF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED.SDR SWAA2024090521030Floor Panel · pulledAFT FLOOR PANEL 242SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242SF AREAS OF PULLED STRANDS ON UPPER SKIN WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION 1.SDR ASAA2024080152093Floor Panel · corrodedAFT CARGO FLOOR PANEL 140DF HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE WITH SURFACE BLEND FOUND TO BE OUT OF LIMITS, LOCATED AND DRILLED NEW FLOOR PANEL IAW B737-9000 SRM 51-40-03-0G-0W= 1.5" O= .071" R= .069" L= 25" D= .002".SDR SWAA2024082721626Floor Panel · delaminatedCABIN FLOOR PANEL 241AF UPPER SKIN DELAMINATED TORN.<[01] RECEIVED LOCETED MATERIAL PN. 4417A4400001CC-10 AD FABRICATED NEW FLOR PANEL 241AF REF. DWG. 144A5810;[02] VERIFIED RECEIVED MATERIAL AND FABRICATED FLOOR PANELSDR AALA202408057997Floor Panel · looseAIRCRAFT IN BASE MAINTENANCE: MAIN E AND E COMPARTMENT FLOOR PANEL LOOSE. RESECURE MAIN E AND E COMPARTMENT FLOOR PANEL. PER B737 MAX8 SRM 51-40-02-0G.SDR IPXA2024080104074Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 814T3538-23 (REPLACE) I.A.W AMM 25-57-05-404-006, AMM 25-58-05-404-052 AND AMM 25-58-01-404-005 REV.142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMALSDR IPXA2024080104102Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL DAMAGE, P/N : 814T3538-27 (REPLACE) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV.142 RESTORED MAIN DECK CARGO HANDLING JOB COMPLETED AND CONDITION CHECK NORMALSDR IPXA2024080104153Floor Panel · damagedFOUND MAIN DECK FLOOR DAMAGE, P/N: 814T3538-30 (REPLACE) THIS REPAIR IS CLASSIFIED AS MAJOR PER GMM 05.04. REPAIR IAW B767-300BCF (REV. 49) SRM 53-00-50-2R-0.SDR IPXA2024080104128Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 657T1126-57 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005, AMM 25-58-04-404-015, AMM 25-57-02-404-016 AND AMM 25-57-06-404-006 REV.142 RESTORED MAIN DECK CARGO HANDLING JOB COMPLETED AND CONDITION CHECK NORMSDR IPXA2024080103230Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL DAMAGE, P/N:814T3538-25 (REPAIR) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMALSDR SWAA2024080919395Floor Panel · delaminatedDOT #114-029. PANEL 193B DELAMINATED ON UNDERNEATH SIDE.<[01] REPAIRED PANEL 193B UNDERNEATH SIDE IAW SRM 51-70-04-2R-6; SRM 51-70-04-2R-0 REPAIR GENERAL AND AMM 51-21-99-300-801.;[02] VERIFIED ITEM 1<BR><BR>AUDIT C/WSDR SWAA2024073018545Floor Panel · crackedAFT CARGO FLOOR PANEL 140BF HAS MUTIPLE CRACKS OVER 3 INCH<[01] CW INSP M-22-125-02598 (CPCP/AD MOC- SWA? 737-700 ? OTHER ? AFT CARGO BILGE AREA RESTORATION AND FLOOR PANEL INSTALLATION) [TTG8Q00UW6GP];[02] INSTALLED AFT CARGO PNL 140BF PER MM 25-52-10SDR IPXA2024072949044Floor Panel · damagedHOLE FOUND IN MAIN CARGO FLOOR AT 4R. REMOVED THE NO-SLIP MATERIAL FROM THE SURFACE OF THE FLOOR PANEL. SECURED THE LOWER PATCH WITH EPOXY ADHESIVE IN THE HOLE LOCATEDIN THE LOWER SKIN PER A300-600F SRM 51-77-10-201SDR SWAA2024090518125Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231XF FLOOR PANEL HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0126.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] JOB COMPLETE.SDR SWAA2024090518126Floor Panel · pulledFLOOR PANEL 231YF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATION OF NEW 231YF FLOOR PANEL HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0124.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] JOB COMPLETE.SDR SWAA2024090518128Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241BF FLOOR PANEL FABRICATION HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0037.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024090518129Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241DF FLOOR PANEL FABRICATION HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0128.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED JOB COMPLETESDR SWAA2024090518130Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 241EF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024090518131Floor Panel · pulledFLOOR PANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242CF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024090518132Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242DF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024090518127Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] 241AF FLOOR PANEL FABRICATION HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0 AND BOEING DWG: 144A5810 ID: 0008.<BR><BR>ATTACHED CURE SHEET TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024082218160Floor Panel · frayedCABIN FLOOR PNL 242CF UPPER SURFACE FIBERS FRAYED AND PNL PUNCTURED<[01] REPLACED CABIN FLOOR PANEL 242CF WORK TO BE COMPLETED ON CUSTOMER WORK CARD TTG8Q00TTZWE;[02] REMOVED AND REPLACED CABIN FLOOR PANEL 242CF ASPER AMM 53-21-00-000-801 AND AMM 53-21-00-400-SDR SWAA2024082218161Floor Panel · damagedCABIN FLOOR PANEL 241DF UPPER SURFACE FIBERS FRAYED<[01] RECEIVED; LOCATED MATERAL PN.4417A4400001CC-10 AD FABRICATED NEW FLOR PANEL 241DF. REF. DWG. 144A5810;[02] RECEIVED; LOCATED AND DRILLED BOARD PN.4417A4400001CC-10 AND FABRICATED NEW FLOOR PANEL 241DF. RSDR FDEA202407271064Floor Panel · dentedMAIN DECK CARGO COMPATMENT, STA 764 ,241AFF FLOOR PANEL WITH DENTS MAIN DECK CARGO COMPATMENT, STA 764 ,241AFF FLOOR PANEL WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR. 4.B REV. 89 APR 15/2023SDR FDEA202407271060Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, FLOOR WITH DENTS BTW STA 450 AND STA 500 AND LBL 88 AND LBL 33. MAIN DECK CARGO COMPARTMENT, FLOOR 221EFF BTW STA 450 AND STA 500 AND LBL 88 AND LBL 33 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REV:89 APR 15SDR FDEA202407271059Floor Panel · dentedMAIN DECK CARGO COMPARTMENT, FLOOR WITH DENT BTW STA 1115 AND STA 1197 13 AND RBL 88 AND RBL 33. MAIN DECK CARGO COMPARTMENT, FLOOR 252CFF BTW STA 1115 AND STA 1197 13 AND RBL 88 AND RBL 33 WAS REPAIRED IAW B767 SRM 53-00-50-2R PAR 4.B FIG 201 SHEET 2 REVSDR SWAA2024082617272Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE; FABRICATED NEW 231XF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.SDR SWAA2024082617261Floor Panel · pulledAFT FLOOR PANEL 241E UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241E UPPER SKIN STRAND DAMAGE WAS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024082617269Floor Panel · pulledFWD FLOOR PANEL 222BF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] FORWARD FLOOR PANEL 222BF; UPPER SKIN AREAS OF PULLED; STRANDS WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024082617265Floor Panel · brokenFWD FLOOR PANEL 221GF FWD O/B CORNER TANG IS BROKEN.<[01] FWD O/B CORNER TANG ON FWD FLOOR PANEL 221GF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024082617263Floor 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] VERIFIED CORRECTIVE SDR SWAA2024082617273Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241AF WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810-127.;[02] JOB COMPLETE.SDR SWAA2024082218150Floor Panel · deformedAFT CARGO COMPARTMENT FLOOR PANEL 140AF IS WAVY. DOT 102-008<[01] FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140AF ;PER REF AMM25-52-01-201-801;[02] VERIFIED STEP#1SDR SWAA2024082218151Floor Panel · deformedAFT CARGO COMPARTMENT FLOOR PANEL 140BF IS WAVY. DOT 102-009<[01] FABRICATED NEW AFT CARGO COMP. FLOOR PANEL 140BF PER REF. AMM 25-52-01-201-801.;[02] VERIFIED FLOOR PANEL FABRICATION.SDR SWAA2024082218149Floor Panel · delaminatedMID CABIN FLOOR PNL 241AF SURFACE LAMINATED DAMAGED<[01] FABRICATED MAIN CABIN FLOORBOARD 241AF PER SRM DWG 144A5810 AND SRM 51-40-05-0G-0;[02] VERIFIED STEP 1SDR SWAA2024081417184Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241GF HAS UPPER SURFACE DELAMINATION.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL; USING BMS4-17TYVI LOT 1557541-1 AND BMS5-107CL1TY1 LOT 1540837-1 ADHESIVE; CURED THE ADHESIVE; UNDER A HEAT LSDR SWAA2024081417187Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231GF HAS UPPER SURFACE DELAMINATION<[01] REMOVED AND REPLACED FLOOR PANEL 231GF PER AMM 53-21-00-400-801;[02] CORRECTED MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION 1SDR SWAA2024081316400Floor Panel · pulledAFT FLOOR PANEL 241D UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] AFT FLOOR PANEL 241D UPPER SKIN WAS REPAIRED IAW SRM 53-00-50-2R-1;[02] JOB COMPLETE.SDR SWAA2024081316391Floor Panel · pulledFWD FLOOR PANEL 221BF HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] 221BF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 141A5810 ID: 0729.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEMSDR SWAA2024081316393Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AN AREA OF PULLED STRANDS. (MARKED)<[01] 221DF FLOOR PANEL UPPER SURFACE DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1 AND BOEING DWG: 141A5810 ID: 0303.<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] JOB COMPLETE.SDR SWAA2024081316396Floor Panel · damagedFWD FLOOR PANEL 222CF ALONG THE O/B EDGE AND 11' FROM AFT EDGE HAS AN AREA OF MISSING CORE AND LOWER SKIN.<[01] FWD FLOOR PANEL 222CF ALONG THE O/B EDGE AND 11' FROM AFT EDGE HAD AN AREA OF MISSING CORE AND LOWER SKIN REPAIRED IAW SRM 53-00-50-2R-1;[02] JOB COSDR SWAA2024081316397Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREAS OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222DF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR IXXA20240725003Floor Panel · corrodedCORROSION ON THE UPPER SURFACE OF THE SUBFLOOR, FROM STA.276 TO 340, LBL85, UNDER THE COMPSITE FLOOR PANEL LOCATED JUST INSIDE OF THE L1 DOORSDR DALA2024072407440Floor Panel · damagedSHIP 3146 FWD CARGO PANEL 131 DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED FWD FLOOR CARGO PANEL 131 IAW A319 AMM 53- 22.SDR SWAA2024081415750Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241TF HAS UPPER SURFACE DELAMINATION.<[01] PASSENGER CABIN FLOOR PANEL 241TF WITH UPPER SURFACE DELAMINATION 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 CORSDR SWAA2024081415751Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242HF HAS UPPER SURFACE DELAMINATION.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242HF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] REMOVED AND REPLACED FLOOR PANEL 242HF PER AMM 53-21-SDR FDEA202407231046Floorboard · damagedAFT MAIN CABIN FLOOR PNL #252 MWF HAS DAMAGE AND MISSING SHALLOW INSERTS, DOT 4-123 PANEL RACK L/H FABRICATED ZONE 250 FLOORBOARD PANEL #252 MWF ON VTMAE TRAVELER # T24/1767887 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR.SDR SWAA2024082915396Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241AF HAS DELAMINATION<[01] PASSENGER CABIN FLOOR PANEL 241AF WITH DELAMINATION WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.SDR SWAA2024081415547Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 242DF HAS UPPER SURFACE HEAT DAMAGE AND DELAMINATION.<[01] DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242DF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] REMOVED AND REPLACED FLOOR PANEL 242D
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