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 DALA2023032802377Unknown · unknownSHIP 658 IN REF TO NRC 211: CORROSION ON FLOOR STRINGERS BTW STA 1450- 1470 LBL 10.45 AT AFT CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 00777: FLOOR STRINGER BTW STA 1450-1470 LBL 10.45 AT AFT CARGO WAS REPLACED PER. B757-200 SRM. (2688129)SDR DALA2023032702351Unknown · unknownAIRCRAFT 3121, CORROSION RAIL DUMMY Y503.2 FR 16 AT FWD GALLEY AREA (SSI 531189). CORRECTIVE ACTION: REPLACED RAIL DUMMY AND FASTENERS LOC BTW FR12 TO FR16 IN FWD GALLEY AS PER A319 SRM 51-72-11 AND DWG D53110984, RELEASE DATE:25-JUN-05, ISSUE C00. (LP 2688011SDR SWAA2023032720960Floor Panel · poppedFLOOR MAKES POPPING NOISE AT ROW 17<[01] C/W EA M-21-153-00794. THIS IS A TIME LIMITED DEFERRAL.SDR DALA2023032702324Floorbeam · damagedDURING INSPECTION FOUND CABIN AFT WET STA 986 FLOOR FRAME UPPER CAP CORRODED LBL0-LBL45. REPAIRED STA 986 FLOORBEAM BETWEEN LBL0-LBL45. REPAIRED STA 986 FLOORBEAM BETWEEN LBL0-LBL45. "SUPPLEMENTAL INFO 10/10/24 OKC REPAIRED PER SRM 53-70-51-2R6 REF WORKCARD 5SDR DALA2023032602318Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-43 TO X=-54. CORRECTIVE ACTION: FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-43 TO X=-54 WERE REPLACED PER B717-200 SRM 51-41-02-0G. (LP 2686942)SDR DALA2023032702364Unknown · unknownSHIP 665 CORROSION ON FLOOR SUPPORTS (4EAS) BTW STA. 660 TO 640 RBL 2, 7,11 AND 16. AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00247 FLOOR SUPPORTS (4EAS) BTW STA. 660 TO 640 RBL 2, 7,11 AND 16. AT FWD CARGO COMPARTMENT WERE REPLACED PER B757-SDR DALA2023032702363Unknown · unknownSHIP 665 CORROSION ON LH SIDE PLATE S27L BTW STA 1200 AND STA 1310 AT AFT CARGO COMPARTMENT FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00284. SIDE PLATE S27L BTW STA 1200 AND STA 1310 AT AFT CARGO COMPARTMENT FLOOR STRUCTURE WAS REPLACED PER B757-200 SSDR DALA2023032702362Unknown · unknownSHIP 665 CRACK ON STRAP OF FLOOR BEAM STA740 RBL 28 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00388 STRAP OF FLOOR BEAM STA740 RBL 28 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2686257)SDR DALA2023032702359Unknown · unknownSHIP 658 SECONDARY NRC: IN REFERENCE TO NRC 00370: CORROSION OUT OF LIMITS ON FLOOR STRINGER LBL 2 STA. 550 (JOGGLE AREA) AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00741: FLOOR STRINGER LBL 2 STA . 550 WAS REPLACED PER B757-200 SRM. (2685667)SDR DALA2023032702357Unknown · unknownSHIP 658 CORROSION ON FLOOR STRINGERS BTW STA 1495- 1520, RBL 11.40, RBL 7.55 AND LBL 2.90; LBL 7.55 , LBL 11.40 AT AFT CARGO COMPT. CORRECTIVE ACTION: SUMMARY OF NRC 00196: FLOOR STRINGERS ON STA 1495-1548 RBL 11.40, STA 1495-1550 RBL 7.55, STA 1495-1530 LBL SDR DALA2023032702343Unknown · unknownSHIP 3352 CORROSION FLOOR BEAM +Y1456 LOCATED BTW FR35 TO FR37.1 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED NEW SECTION FLOOR BEAM Y1456 LOC. BTW FR31 AND FR37.1 IN PASSENGERS CABIN. (2686439)SDR DALA2023032702336Unknown · unknownSHIP 1601 FOUND FWD CARGO DOOR CUT OUT LOWER SUPPORT CORROSION AT STA 552 AND RBL 40. CORRECTIVE ACTION: FWD CARGO DOOR CUT OUT LOWER SUPPORT CORROSION AT STA 552 AND RBL 40 REMOVED AND REPAIRED AS PER PRI 606682-14 REV 0. COMPARED AND COMPLIED WITH ER/A 60668SDR DALA2023032602311Unknown · unknownAIRCRAFT 3121, ELONGATED HOLE FLOOR STRUCTURE SPLICE FRAME 24 Y1292 IN PASSENGER CABIN (2 EA). CORRECTIVE ACTION: REPLACED SPLICE (2EA) AND FASTENERS LOC FR24 Y1292 IN FWD GALLEY AS PER A319 SRM 51-72-11 AND DWG D 53111225 RELEASE DATE05-JUN-12 ISSUE A. (LP 26SDR DALA2023032602310Unknown · unknownAIRCRAFT 3121, CORROSION FLOOR BEAM +Y1292 ON FR 16 AT FWD GALLEY AREA (SSI 531189). CORRECTIVE ACTION: REPLACED FLOOR BEAM AND FASTENERS LOC BTW FR12 TO FR24 Y1292 IN FWD GALLEY AS PER A319 SRM 51-72-11 AND DWG D53110920 RELEASEDATE 28-APR-21 ISSUE E00 RII. (SDR DALA2023032402308Unknown · unknownAIRCRAFT 9513, CORROSION ON DIAPHRAGM STA Y=200 RBL45 - 55 (UNDER R1) VIEW FROM E/E COMPARTMENT. CORRECTIVE ACTION: REPAIR ON DIAPHRAGM STA Y=200 RBL45 - 55 (UNDER R1) VIEW FROM E / E COMPARTMENT WAS PERFORMED PER B-717-200 SRM 51-70-10 REPAIR 2 PAR. 4 FIG. 20SDR DALA2023032402304Unknown · unknownAIRCRAFT 9513, CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-9 TO X=-42. CORRECTIVE ACTION: FLOOR SUPPORTS WERE REPLACED PER DWG 9936534 REV. BW AND PER B717-200 SRM-51-41-02-0G PAR. 4. (LP 2685485)SDR SWAA2023041920361Floor Panel · crackedCRACK FLOOR PANEL 242UF AT AFT GALLEY AND LAV 2023-191953<[01] TOOL USED: CALIPER: P/N: 500-193-30 ; S/N: 0000288 ; DUE DATE: 27-DEC-23.;[02] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18185847 DUE DATE: 24/SEP/23;[03] TOOL USED: SCALE PN: SPX621 SN: 8340225441SDR DALA2023032402292Unknown · unknownSHIP 6706 BROKEN STABILIZATION STRAP IN STA365.25 AND LBL 24.75 THROUGH ACCESS PANEL 119BL. CORRECTIVE ACTION: SUMMARY OF NRC 00016: STABILIZATION STRAP IN STA 365.25 AND LBL 24.75 WAS REPAIRED PER B-757-200 SRM. (2683744)SDR DALA2023032402275Unknown · unknownSHIP 3352 CORROSION FLOOR STRUCTURE LOC. -Y1552.5 BTW FR33 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1552.5 LOC BTW FR31 TO FR37.1 ON PASSENGER CABIN AS PER A330 SRM 51-72-11-801. (2684989)SDR DALA2023032402274Unknown · unknownSHIP 3328 CORROSION FLOOR BEAM -Y381 BTW FR 75 TO FR 78 AT AFT GALLEY AREA. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM -Y381 BTW FR75 TO FR78 AT AFT GALLEY AREA AS PER A330 SRM 51-42-11-801. (2684856)SDR DALA2023032402272Unknown · unknown(LOG 2684871) DURING INSPECTION FOUND AFT CARGO FLOOR STRUCTURE RH TRANSITION PNL HAS CORROSION AT FASTENER HOLE BETWEEN STA 767- STA 787. REPAIRED TRANSITION PANEL IAW ERA 606727-14 REV ORIGINAL.SDR DALA2023032402271Intercostal · corroded(LOG 2684967) DURING INSPECTION FOUND CORROSION FLOOR BEAM LOCATED BS947.5 AT LEVEL LBL 24.5. PASSENGER CABIN. INSTALLATION OF INTERCOSTAL LOC BTW BS 947.5- BS967 AND LBL 24.5 TO LBL 48.SDR DALA2023032402269Unknown · unknown(LOG 2685079) DURING INSPECTION FOUND CORROSION FLOOR BEAM LOCATED BS986.5 AND FROM LBL44 TO RBL42 AT PASSENGER CABIN. PERFORMED REPAIR INSTRUCTIONS CORROSION FLOOR BEAM LOCATED BS986.5 AND FROM LBL44 TO RBL42 AT PASSENGER CABIN AS PER ER/A 605883-14 REV. ORIGSDR SWAA2023050319989Structure · crackedCRACK ANGLE FLOOR STRUCTURE FWD POSITION BS 695 AND BL 0 CENTER SECTION 2023-208571<[01] REPLACED ANGLE FLOOR STRUCTURE FWD POSITION BS 695 AND BL 0 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG:273A9110 SHEET:6 REV:A <BR>SEE INDIVIDUAL SIGNSOSDR SWAA2023042519830Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF AFT O/B CORNER (TANG) IS BROKEN<FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.B.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-6.<BR>REMOVED 3EA INSERTS TO FACILITATE REPAIR IAW SRM 53-00-50-2R-6 PARA 3.B.SDR DALA2023032302266Unknown · unknownAIRCRAFT 3121, CORROSION FLOOR BEAM -Y765 LOCATED AT LEVEL FR 68 AT AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOCATED BTW FR66 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG #D53472000 RELEASES DATE06/JAN/03 ISSUESDR DALA2023032302224Unknown · unknownSHIP 658 REFERENCE TO NRC 315: CORROSION ON FLOOR STRINGERS LBL 7 AND 10 BTW STA. 680-688 ALSO LBL 16 BTW STA 635-710 AT FWD CARGO COMPARTMENT FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00737: FLOOR STRINGERS LBL 7, LBL 10 LBL 16 BTW STA 635-710 AT FWDSDR F3LA2023040700038Threshold · corrodedDISCREPANCY: REFERENCE NR 5001226088-0020 UPON REMOVAL FOR ACCESS ON INSPECTION FOUND 261LG PANEL CORRODED AND REQUIRES REPLACEMENT.
CORRECTIVE ACTION: REPAIRED 261LG PANEL AS PER EA# N2-53R-37571 REV. ORIG REV DATE. N/A
TASK SUBJECT TO RII. THE EMBODIED REPSDR DALA2023032202170Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT BTW STA Y= 200 TO STA Y=218 AND X=-11 AT CABIN PAX. CORRECTIVE ACTION: FLOOR SUPPORT BTW STA Y= 200 TO STA Y=218 AND X=-11 AT CABIN PAX WAS REPLACED PER B717-200 SRM 51-41-05-0G. PAR.8. (LP 2681442)SDR DALA2023032202157Unknown · unknownSHIP 3354 CORROSION FLOOR BEAM Y953 BTW FR32 TO FR37 PLUS 10 INCHES IN PASSENGER CABIN. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR BEAM Y953 LOCATED BTW FR26 TO FR37.4 IN PASSENGER CABIN AS PER A330 SRM 51-72-11-911-001 AND 51-42-11-801. (2681886)SDR SWAA2023041819092Floor Panel · pulledCABIN FLOOR PANEL 222BF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTBFU (LINE 410 ).;[02] C/W INSPECTION.;[03] C/W INSPECTION.SDR SWAA2023041819113Floor Panel · pulledCABIN FLOOR PANEL 222AF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTBFW (LINE 412 ).;[02] C/W INSPECTION.SDR SWAA2023041819114Floor Panel · pulledCABIN FLOOR PANEL 232BF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTBTA (LINE 786 ).;[02] C/W INSPECTION.SDR SWAA2023041819094Floor Panel · pulledCABIN FLOOR PANEL 232AF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTBTC (LINE 788 ).;[02] C/W INSPECTION.SDR SWAA2023041819117Floor Panel · pulledCABIN FLOOR PANEL 222DF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTC32 (LINE 1110 ).;[02] C/W INSPECTION.SDR SWAA2023041819095Floor Panel · pulledCABIN FLOOR PANEL 221GF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTC36 (LINE 1114 ).;[02] C/W INSPECTION.SDR SWAA2023041819096Floor Panel · pulledCABIN FLOOR PANEL 221FF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTC38 (LINE 1116 ).;[02] C/W INSPECTION.SDR SWAA2023041819100Floor Panel · pulledCABIN FLOOR PANEL 221EF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTC3A (LINE 1118 ).;[02] C/W INSPECTION.SDR SWAA2023041819103Floor Panel · pulledCABIN FLOOR PANEL 221DF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTC3C (LINE 1120 ).;[02] C/W INSPECTION.SDR SWAA2023041819105Floor Panel · pulledCABIN FLOOR PANEL 221CF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTC3E(LINE 1122 ).;[02] C/W INSPECTION.SDR SWAA2023041819121Floor Panel · pulledCABIN FLOOR PANEL 221BF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTC3G (LINE 1124 ).;[02] C/W INSPECTION.SDR SWAA2023041819122Floor Panel · pulledCABIN FLOOR PANEL 221AF HAS DENTS & PULLED FIBERS.<[01] REMOVED AND REPLACED FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00. PANEL WILL BE INSTALL ON ROUTINE CARD TTG8Q00HTC3J (LINE 1126 ).;[02] C/W INSPECTION.SDR SWAA2023041018825Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF IS BROKEN AT OUTBOARD AFT END.<[01] RECEIVED NEW FLOOR PANEL 221BF PANEL WILL BE INSTALLED ON WORK CARD TTG8Q00HVFN4;[02] VERIFIED STEP 1; COMPLETESDR FDEA202303200470Support · crackedCENTER CARGO BELOW FLOORPANEL 183HB FOUND LOWER SUPPORT CRACKED AT STATION 1841. CENTER CARGO BELOW FLOOR PANEL 183HB LOWER SUPPORT CRACKED AT STATION 1841 REMOVED AND REPLACED PER SRM 51-31-01-0G. SUPPORT FABRICATED PER DOUGLAS DRAWING AGA7170 REVISION SDR SWAA2023033019165Floor Panel · pulledDOT A24-25 CENTER CABIN FLOOR PANEL 241CF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 241CF AND FOUND DAMAGE TO UPPER SURFACE PLIES. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-SDR SWAA2023033019164Floor Panel · pulledDOT A24-24 CENTER CABIN FLOOR PANEL 231ZF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] FOUND AREAS OF PULLED FIBERS ON UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-SDR SWAA2023033019163Floor Panel · pulledDOT A24-23 CENTER 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 SDR SWAA2023033019173Floor Panel · pulledDOT A24-22 CENTER CABIN FLOOR PANEL 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 231XF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP FOR REPAIR. IAW BSDR SWAA2023033019172Floor Panel · pulledDOT A24-21 CENTER CABIN FLOOR PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 241AF AND FOUND PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50SDR SWAA2023033019171Floor Panel · pulledDOT A24-20 CENTER CABIN FLOOR PANEL 232SF 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
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