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 SWAA2024122772271Floor Panel · corrodedDOT 7L-018: AFT CARGO FLOOR PANEL 140DF IS CORRODED AT FASTENER HOLES<[01] UPON FURTHER INVESTIGATION FOUND A TOTAL OF 42 INCHES OF CORROSION WITH A MAX ALLOWED LENGTH OF CORROSION BEING 3 INCHES FOUND PANEL 140DF TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 RECESDR SWAA2024122772267Floor Panel · corrodedDOT 7L-019: AFT CARGO FLOOR PANEL 140AF IS CORRODED AT FASTENER HOLES<[01] UPON FURTHER INVESTIGATION FOUND A TOTAL OF 30 INCHES OF CORROSION WITH A MAX ALLOWED LENGTH OF 3 INCHES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 RECEIVED REPLACEMENT MATERIAL PNSDR SWAA2024121772383Floor Panel · corrodedCORROSION ON AFT CARGO COMPARTMENT VERTICAL WEB STA 795-797; RBL 21; WL 153-155; O/B SURFACE.<[01] FOUND CORROSION OUT OF LIMITSIAW SRM 53-60-15-1A-1. AND REPLACED VERTICAL WEB STA 795-847; RBL 21; WL 153-155 IAW SRM 51-40-02 AND BOEING DWG# 146A8121 REV:-; ANSDR FDEA202411271745Floor Panel · damagedFLOOR PANEL 222MAF HAS FIBER DAMAGED CRACKED AND PEELED DUE TO REMOVAL OF TAPE. FABRICATED ZONE 220 FLOOR PANEL 222MAF ON VTMAE TRAVELER # T24/1786765 IAW DWG 141N5370 REV. CY MAJOR REPAIRSDR FDEA202411271749Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 252MFF DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MFF ON VTMAE TRAVELER # T24/1787479 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202411271748Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 241MNF DAMAGED. FABRICATED ZONE 240 FLOORBOARD PANEL 241MNF ON VTMAE TRAVELER # T24/1787473 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIRSDR FDEA202411271747Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 232MFF BROKEN FABRICATED ZONE 230 FLOORBOARD PANEL 232MFF ON VTMAE TRAVELER #T24/1787469 IAW DWG 11862181 REV L MAJOR REPAIRSDR FDEA202411271746Floor Panel · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 232MWF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MWF ON VTMAE TRAVELER # T24/1787471 IAW DWG 11862182 REV. H, MAJOR REPAIRSDR DALA2024120311408Fastener · corroded(LOG 0689773) CORROSION ALONG FLOOR MOUNTING STRUCTURE FASTENER HOLES ALONG STA 986.5, WL 208, BETWEEN LBL 45 AND RBL 45. REPAIRED FLOOR BEAM AT STA 986.5 WL 208 BETWEEN LBL 45 TO RBL 45 PER B737-900 SRM 53-70-51-2R-4.SDR DALA2024120211348Pressure Plate · corrodedSHIP 6704 CORROSION AROUND DRAIN HOLE AT EXISTING REPAIR AFT CABIN FLOOR STRUCTURE PRESSURE PLATE APROX' BS.1716 RBL.23. DOT 129-057. CORRECTIVE ACTION: REMOVED EXISTING REPAIR LOCATED AT DECK PLATE BSTA.1716 RBL.23. IAW. B757 SRM .51-40-02-0G, INSTALLATION OFSDR DALA2024120211346Pressure Plate · corrodedSHIP 6704 CORROSION IN AFT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE APROX' BS.1716 RBL.9.5. DOT 129-059. CORRECTIVE ACTION: REMOVED CORROSION FROM AFT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE APROX' BS.1716 RBL.9.5 IAW B757-200-SRM-51-10-02, EVALUATED AREA ASDR DALA2024120211345Plate · corrodedSHIP 6704 CORROSION IN AFT MAIN CABIN FLOOR STRUCTURE PRESSURE PLATE, APROX' BS.1714 RBL.48. DOT 129-060. CORRECTIVE ACTION: REMOVED CORROSION AT AFT MAIN CABIN FLOOR SRUCTURE PRESSURE PLATE BS 1714 RBL 48 IAW B 757 SRM 51-10-02 EVALUATED AREA, FOUND AREA TO BSDR DALA2024120211343Plate · corrodedSHIP 6704 CORROSION IN AFT CABIN FLOOR STRUCTURE PRESSURE PLATE EXISTING REPAIR, APROX' BS.1716 LBL.41. DOT 129-056. CORRECTIVE ACTION: REMOVED IN AFT CABIN FLOOR STRUCTURE PRESSURE PLATE EXISTING REPAIR, APROX' BS.1716 LBL.41 IAW B757 SRM 51-40-02, FABRICATEDSDR DALA2024113011271Beam · corrodedSHIP 3136 CORROSION FLOOR BEAM -Y464.8 AT LEVEL FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED PER A319 SRM 51-42-11, AND SRM 51-72-11. (0681497)SDR SWAA2024123171512Insert · damagedPANEL 222DF HAS A DAMAGED GIRT BAR INSERT.<[01] PANEL 222DF DAMAGED INSERTS REMOVED & REPLACED IAW SRM 53-00-50-2R-0;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024123172141Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222AF AT FWD GALLEY AREA. REPLACED FLOOR PANEL 222AF IAW B737-800 AMM 53-21-00-400-801 THE INSTALLATION IS DOCUMENTED ON TASK TTG8Q00WL0W3SDR SWAA2024123172142Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222BF AT FWD GALLEY AREA. REPLACED FLOOR PANEL 222BF AT FWD GALLEY AREA WILL BE INSTALLED ON OTHER TASK CARD SEE TTG8Q00WL0W1.SDR SWAA2024123172143Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222BF AT FWD GALLEY AREA. DELAMINATED FLOOR PANEL 222CF AT FWD GALLEY AREA. REPLACED FLOOR PANEL 222CF AT FWD GALLEY AREA THE INSTALLATION IS DOCUMENTED ON TASK TTG8Q00WL1RS.SDR SWAA2024123172144Floor Panel · delaminatedDELAMINATED FLOOR PANEL 222DF AT FWD GALLEY AREA. REPLACED FLOOR PANEL 222DF AT FWD GALLEY AREA THE INSTALLATION IS DOCUMENTED ON TASK TTG8Q00WL1RQ.SDR SWAA2024123172145Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221CF AT FWD GALLEY AREA. REPLACED FLOOR PANEL 221CF AT FWD GALLEY AREA THE INSTALLATION IS DOCUMENTED ON TASK TTG8Q00WL1S2.SDR SWAA2024123172146Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221BF AT FWD GALLEY AREA 2024-728437<[01] REPLACED FLOOR PANEL 221BF IAW B737-800 AMM 53-21-00-400-801 THE INSTALLATION IS DOCUMENTED ON TASK TTG8Q00WL1S4;[02] REPLACED FLOOR PANEL 221BF IAW B737-800 AMM 53-21-00-400-801 THE INSTALLATIOSDR SWAA2024123172148Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221EF AT FWD GALLEY AREA 2024-728442<[01] REPLACED FLOOR PANEL 221EF IAW B737-800 AMM 53-21-00-400-801 THE INSTALLATION IS DOCUMENTED ON TASK TTG8Q00WL1RY;[02] CERTIFIED WORK PERFORMED. <BR>FOR INSTALLATION SEE TTG8Q00WL1RY.SDR SWAA2024123071527Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024123071522Floor Panel · buckledAFT FLOOR PANEL 242SF O/B AFT CORNER IS BUCKLED. AFT FLOOR PANEL 242SF O/B AFT CORNER WITH BUCKLED WAS REPAIRED IAW SRM 53-00-50-2R-1 AND BDWG D1040M003-301; BDWG 147A5810 ID:0058.SDR SWAA2024123071508Floor Panel · pulledPANEL 222A UPPER SKIN HAS AREAS OF PULLED STRANDS. PANEL 222A UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.SDR SWAA2024123071513Floor Panel · pulledPANEL 231MF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 231MF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.SDR SWAA2024123071526Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241ACF UPPER SKIN HAD AREAS OF PULLED STRANDS REPAIRED IAW SRM 53-00-50-2R-1;[02] VERIFIED RII ITEMS COMPLETE;[03] TASK COMPLETESDR SWAA2024123071506Floor Panel · pulledPANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE. FLOOR PANEL 221EF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2024123071509Floor Panel · pulledPANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221CF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2024123071510Floor Panel · pulledPANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENT OF DAMAGE; FLOOR PANEL 221FF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR SWAA2024123071514Floor Panel · pulledPANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED PER [SRM 53-00-50-2R-0-A00938.SDR SWAA2024123071515Floor Panel · pulledPANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED NEW FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0127.SDR SWAA2024123071516Floor Panel · pulledPANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF ALL OF THE DAMAGE; PANEL 241BF WAS REPLACED WITH A NEWLY FABRICATED PANEL ALL OF THE WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1. PARAGRAPH 4.A.(2); TABLE 204 AND PARAGRAPH 5. SDR SWAA2024123071517Floor Panel · pulledPANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE. PANEL 242AF WAS REPLACED WITH A NEWLY FABRICATED PANEL. ALL OF THE WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A NOTE; PARAGRAPH 4.A.(2); TABLE 204 AND SDR SWAA2024123071518Floor Panel · pulledPANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] PANEL 241UF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0; DWG 146A5810 ID:0054.;[02] JOB COMPLETE.SDR SWAA2024123071519Floor Panel · pulledPANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231ZF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0160.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR SWAA2024123071520Floor Panel · pulledPANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF ALL OF THE DAMAGE, PANEL 241EF WAS REPLACED WITH A NEWLY FABRICATED PANEL WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A NOTE; PARAGRAPH 4.A.(2); TABLE 204 AND PARAGRAPH 5. (1); SDR SWAA2024123071521Floor Panel · pulledPANEL 242CF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO THE EXTENT OF ALL OF THE DAMAGE; PANEL 242CF WAS REPLACED WITH A NEWLY FABRICATED PANEL. WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 1.A NOTE; PARAGRAPH 4.A.(2); TABLE 204 AND PARAGRAPH 5. (1)SDR SWAA2024123071524Floor Panel · buckledAFT FLOOR PANEL 242XF IS BUCKLED IN MIDDLE OF PANEL. DUE TO EXTENT OF DAMAGE; FLOOR PANEL 242XF WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A (1).SDR FDEA202411261763Angle · crackedAVIONICS COMPT FLOOR CROSSBEAM PICK UP ANGLE CRACK AT FR10, Y403 POSITION. REPLACED AVIONICS COMPT FLOOR BEAM PICK UP ANGLE WITH NEW ONE AT FR10, Y403 POSITION. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B~23. THIS REPAIR IS CSDR DALA2024120211327Support · corroded(LOG 0680029) CORROSION ON FLOOR SUPPORTS (LOWER SILL AREA BTW LOWER SILLSTA360,RBL60 AND LBL60 AT CPAX. FLOOR SUPPORTS LOWER SILL BTW STA270 STA360, RBL60 AND LBL60 AT CPAX WERE REPLACED PER B737-800 SRM 51-40-02-0G.SDR DALA2024120111296Plate · corrodedSHIP 6704 CORROSION ON TOP OF AFT CABIN FLOOR STRUCTURE ATTACH PLATE, BS.1681 BL.0. DOT 129-049. CORRECTIVE ACTION: SUMMARY OF-REMOVED ATTACH PLATE FROM TOP OF AFT CABIN FLOOR STRUCTURE BS.1681 BL.0. IAW B757-200-SRM-51-40-02, FABRICATED, LOCATED AND DRILLED NSDR LR7A2024112603673Floor Support · crackedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5211, FOUND CARGO RAMP ZEE FLOOR SUPPORT CRACKED AT RS2, RBL49. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0523. / PSE# 52-60-01, AD 2012-06-09SDR LR7A2024112603653Floor Panel · dentedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5211, FOUND CARGO RAMP FLOOR PANEL DENTED AT RS08 TO RS10 LBL10 TO RBL10. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0471. / PSE# 52-60-01, AD 2012-06-09SDR LR7A2024112603652Floor Panel · dentedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5211, FOUND CARGO RAMP FLOOR PANEL DENTED AT RS06 TO RS08, LBL45. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0470. / PSE# 52-60-01, AD 2012-06-09SDR LR7A2024112603615Floor Panel · crackedDURING SCHEDULED C-10 CHECK UNDER JOB CARD HC5211, FOUND CARGO RAMP CENTER FLOOR PANEL SKIN CRACKED AT RS2, LBL2,. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0167. / PSE# 52-60-01, AD 2012-06-09SDR SWAA2024122771469Floor Panel · corrodedDOT 7L-009: FWD CARGO FLOOR PANEL 120CF HAS CORROSION AT FATENER HOLES<[01] EVALUATED AREA ON FLOOR PANEL 120CF; DAMAGE REMOVED HAS A MORE THAN 3 INCHES IN LENGHT; MORE OF THE LIMITS PERMITTED; THEREFORE IS OUT OF THE LIMITS I.A.W. SRM 53-00-53-1A-1<BR><BR>FABSDR SWAA2024122771471Floor Panel · corrodedDOT 7L-010: FWD CARGO FLOOR PANEL 120DF HAS CORROSION AT FASTENER HOLES<[01] EVALUATED ALLOWABLE LIMITS: DAMAGE IS MORE THE MAXIMUN LENGTH PERMITTED (MAXIMUN 3.0 IN) FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1 ITEM 5 B AND FABRICATED NEW FLOOR PANEL AMM 50-10-04SDR ASAA2024112554534Floorboard · damagedMAIN CABIN FLOORBOARD DELAME P/N 141A5810-454. GROUNDED - YES. PREFORMED PERMANT REPAIR TO MAIN CABIN FLOORBOARD 141A5810-454 DELAMINATION IAW B737-900ER SRM 53-00-50.SDR ASAA2024112554306Floorboard · delaminatedMAIN CABIN FLOORBOARD DELAM P/N: 141A5810-155. GROUNDED - YES. PREFORMED PERMANT REPAIR TO MAIN CABIN FLOORBOARD 141A5810-155 DELAMINATION IAW B737-900ER SRM 53-00-50.
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