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 SWAA2022080833823Floor Panel · pulledFLOORBOARD 241AF HAS MULTIPLE PULLED AND LOOSE COMPOSITE STRANDS ON THE UPPER SURFACE. / [01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241AF USING BMS 4-23TY2 LOT#1496138-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK1KP9159K; APPLIED TAPE AND PARTSDR SWAA2022080833824Floorboard · looseFLOORBOARD 232SF HAS MULTIPLE PULLED AND LOOSE COMPOSITE STRANDS ON THE UPPER SURFACE. / [01] DUE TO THE SEVERITY OF DAMAGE ON FLOORBOARD 232SF THE BOARD WAS REPLACE IAW SRM 51-10-02-0G-0 PAR 9.A. AND AIPC 53-21-00-42A ITEM 210;[02] VERIFIEDSDR SWAA2022080833825Panel · pulledFLOORBOARD 232RF HAS MULTIPLE PULLED AND LOOSE COMPOSITE STRANDS ON THE UPPER SURFACE. / [01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 232RF FROM BMS 4-17TY3 LOT#1430725-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK1KP9159K; PART MARKED AND APPLIESDR SWAA2022080833829Floor Panel · pulledFLOORBOARD 231XF HAS MULTIPLE PULLED AND LOOSE COMPOSITE STRANDS ON THE UPPER SURFACE. / [01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 231XF USING BMS 4-23TY2 LOT#1496138-1; INSTALLED INSERTS USING BMS 5-107 LOT#AK1KP9159K; APPLIED TAPE AND PARTSDR SWAA2022080833830Floorboard · pulledFLOORBOARD 231ZF HAS MULTIPLE PULLED AND LOOSE COMPOSITE STRANDS ON THE UPPER SURFACE. / [01] DUE TO THE SEVERITY OF DAMAGE ON FLOORBOARD 231ZF THE BOARD WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9.A. AND AIPC 53-21-00-42A ITEM 230;[02] VERIFIEDSDR IPXA2024022718706Floor Panel · cracked*** MAJOR REPAIR *** SDR FILED OPEN *** POS 10L - MAIN CARGO COMPARTMENT FLOOR PANEL REPAIR***SM18/LMX6***PANEL NO:251JFF P/N:146T5869-65 1.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.2 WORK INSTRUCTIONS STEP 4-11. 2.CONDITION CHECK IS SATISFACTORYSDR DALA2022072705172None · noneSHIP 661 IN REF TO NRC 00299 CORROSION ON LONG FLOOR SUPPORT 2 RBL BTW STA FS 1320 AND FS 1340 AT AFT CARGO COMPARTMENT, AREA WAS FOUND OUT OF LIMITS PER B757-200 SRM. CORRECTIVE ACTION: SUMMARY OF NRC 00711. FLOOR SUPPORT 2 RBL BTW STA FS 1320 AND FS 1340 WASSDR DALA2022072705171None · noneSHIP 661 CORROSION OUT OF LIMITS IN REF TO NRC 00287 CORROSION ON LH SIDE PLATE BTW STA FS1270 TO FS1310 AFT CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 00729. SIDE PANEL LH (SECTION FROM STA 1270 TO1310) WAS REPAIRED PER B757-200 SRM. (2335035)SDR CALA2022072501868Angle · crackedCRACK FRAME 66 ANS STR23L ANGLE IN PASSENGER CABIN. SEE AEROMAN NON ROUTINE 2022-308749 REMOVED AND REPLACED FRAME 66 AND STR. 23L ANGLE IN PASSENGER CABIN IAW SRM A320 51-72-11 AND DRAWING D53474250, PERFORMED DETAIL VISUAL INSPECTION AFFECTED AREA AND NOT FOSDR CALA2022072501867Angle · crackedCRACK FRAME 68 AND STR23L ANGLE IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-308751 REMOVED AND REPLACED FRAME 68 AND STR 23L ANGLE IN PASSENGER CABIN IAW SRM A320 51-72-11 AND DWG D53474250, PERFORMED DETAIL VISUAL INSPECTION ON AFFECTED AREA AND NOT FOUNSDR SWAA2022082432917Panel · elongatedCABIN PASSENGER FLOOR STRUCTURE STA540 WL208 RBL5 BRAKE HOLES ENLONGATED / [01] REMOVED BREAK STA 540 RBL5 REF. SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW BREAK REF; SRM 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2;[04] OK TO TREAT AND PRIME HOLES;[05] TREATESDR SWAA2022080233084Floor Panel · delaminatedCABIN FLOOR PANEL 242BF IS SEPARATED ON THE EDGE. / [01] CABIN FLOOR PANEL 242BF REPAIRED ON NON-ROUTINE #TTG8Q00DROP7;[02] VERIFIED STEP 1SDR SWAA2022080233082Floor Panel · delaminatedCABIN FLOOR PANEL 241CF IS DELAMINATED. / [01] EVALUATED AND FOUND MISSING PLIES AT FWD EDGE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A; C; E-F.<BR><BR>VERIFIED MATSDR SWAA2022080233083Floor Panel · delaminatedCABIN FLOOR PANEL 242BF IS SEPARATED ON THE EDGE. / [01] EVALUATED DAMAGE; SKIN SEPARATION ON EDGE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1.<BR><BR>VERIFIED REPAIR MATERIALS IAW B737 SRM 53-00-50-2R-1 TABLE 201; FIBERGLASS CLOTH BMS9-3 (A24484); POTTING COMPOUSDR SWAA2022080233085Floor Panel · delaminatedCABIN FLOOR PANEL 232SF IS SEPARATED ON THE EDGE. / [01] EVALUATED PANEL 232 SF AND FOUND DAMAGE TO CORE AT EDGE AT TWO CORNERS. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-10 PAR 1. CLEAN AND PREP FOR REPAIR. IAW B737-700 SRM 53-00-50-2R-10 PAR 3A-D.SDR SWAA2022080233086Floor Panel · peelingCA BIN FLOOR PANEL 232RF HAS PEELED FIBERS. / [01] EVALUATED DAMAGE; PEELED FIBERS ON UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;D; E; AND F. <BR><BR>VERIFIED REPAIRSDR DALA2022072705167None · noneSHIP 661 AFTER REMOVED LH SIDE PLATE, CORROSION ON SUPPORT ANGLE BTW STA FS 1360-FS1380 , STGR 27 AND STGR 26 WAS FOUND AT AFT CARGO, IN REF NRC 00305. CORRECTIVE ACTION: SUMMARY OF NRC 00714: SUPPORT ANGLE BTW STA FS 1360-FS1380 , STGR 27 AND STGR 26 WAS REPLSDR DALA2022072405089None · noneAIRCRAFT 1521, SEAT TRACK -CORROSION FOUND ON THE SEAT TRACK BETWEEM STA850 AND STA927, LBL88.5. CORRECTIVE ACTION: CARRIED OUT THE REPAIR FOR THE SRAT TRACK AS PER B767-300 SRM53-00-52-2R-3 FIG201. (2333134)SDR SWAA2022082231824Floor Panel · crackedAFT CABIN FLOOR PANEL 241ADF AFT O/B CORNER IS CRACKED. / [01] IDENTIFIED FLOOR PANEL 241ADF IAW SRM 53-00-50-0I-1 TABLE 6 FIG 6DAMAGED NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4 DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-6 REMOVED ALLSDR SWAA2022072931953Panel · crackedAFT CARGO FWD BULKHEAD PANEL 142NWB CRACKED / [01] INSTALLED NEW CARGO PANEL 142NWB PER AMM 25-52-09SDR DALA2022072605145None · noneSHIP 661 CORROSION AT INTERCOSTAL BETWEEN FS1400- FS1420 AND STGR 28L-STGR 29, AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00235: INTERCOSTAL BETWEEN FS1400-FS1420 AND STGR 28L-STGR 29, AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2331278SDR DALA2022072605134Shear Plate · corrodedSHIP 3229 CORROSION SHEAR PLATE STR 23L FR69 TO FR70 AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE PER A320 SRM 51-42-11 AND 51-72-11. (2332396)SDR FDEA202207221789Intercostal · corrodedINTERCOSTAL FROM STATION 1500 TO 1520 IN BILGE AREA HAS CORROSION IN 3 AREAS FABRICATED NEW INTERCOSTAL IAW BAC DWG 146N5451-11 REV C & INSTALLED IAW B757 SRM 51-40-02.SDR SWAA2022082231778Floor Panel · brokenFWD CABIN FLOOR PANEL 221BF IS BROKEN ON THE AFT O/B END / [01] IDENTIFIED FLOOR PANEL 221BF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE IS REPAIRABLSDR SWAA2022082231779Floor Panel · pulledFWD CABIN FLOOR PANEL 222DF HAS PULLED THROUGH INSERTS / [01] IDENTIFIED FWD CABIN FLOOR PANEL 222DF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. DAMAGE TO BE REPAIRED IAW SRM 53-00SDR DALA2022072505093None · none(LOG 2330719) AFTER CLEANING SLIDE ANCHOR ( 2EA) (L2, R2 POSITION ) WAS FOUND WITH CORROSION. SLIDE ANCHOR (2EA) (L2,R2 POSITION ) WERE REPLACED PER B737-800, IPC 11-32-01-03.SDR DALA2022072505106None · noneSHIP 661 CORROSION AT UPPER CORD OF FLOOR-LONGITUDINAL BEAM BL0 BETWEEN STA1640-STA1881.8, CABIN PAX. CORRECTIVE ACTION: SUMMARY OF NRC 00439: UPPER CHORD OF FLOOR-LONGITUDINAL BEAM BL0 BETWEEN STA1640-STA1881.8, CABIN PAX WAS REPLACED PER B757-200 SRM. (23296SDR AALA202207255247Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL SUPPORT ANGLE HAS AREAS OF CORROSION AT BODY STA 995 BETWEEN LEFT BUTT LINE 40 AND LEFT BUTT LINE 48. REMOVED AND REPLACED FLOOR PANEL SUPPORT ANGLE PER SRM 51-40-02.SDR DALA2022072105048None · noneSHIP 661 CORROSION ON FLOOR SUPPORT NEXT TO 2L DOOR-LOWER SILL BETWEEN STA700-STA720, CABIN PAX. CORRECTIVE ACTION: SUMMARY OF N.R.C. 00470. FLOOR SUPPORT NEXT TO 2L DOOR-LOWER SILL BETWEEN STA. 700-STA. 720, CABIN PAX, WAS REPLACED. PER. B757-200 SRM. (232960SDR AALA202207213628Floorboard · noneAIRCRAFT WAS NOT GROUNDED: FLOOR BOARD SOFT JUST AFT OF ROW 19 SOFT. REPAIRED PER AARD 53-00-00-3 REPAIR 4A.SDR CALA2022072001845None · corrodedCORROSION FLOOR BEAM -Y765 LOCATED FR21 AT FWD GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA IAW A320 SRM 51-42-11 AND DWG D53112812, D53110984, D53110876, D53112814 AND PERFORMED VISUAL INSPECTION ON AREA NOT FOUNDSDR CALA2022072001842None · missingMISSED DRILL FLOOR BEAM -Y765 LOCATED FR65 TO FR66 AT AFT GALLE Y AREA REMOVED AND REPLACE FLOOR BEAM -Y765 LOCATED FR64 TO FR66 AT AFT GALLEY AREA IAW A320 SRM 51-72-911-001 AND DWG D53472200 AND D4949524 ADD EMP:V939311SDR SWAA2022072531022Floor Panel · crackedAFT CARGO FLOOR PANEL AFT FROM THE FWD PANEL HAS A CRACK APPROX 20 INCHES LONG / [01] R&R AFT CARGO FLOOR PANEL AFT OF FWD FLOOR PANEL REF MM 25-52-10<BR>P/N 453A2610-6SDR DALA2022072005019Stringer · worn(LOG 2326725) DURING INSPECTION FOUND WEAR ON STA 787/STA 807 AND RBL= 3 AT AFT CARGO COMPARTMENT. STGR ON STA 787/STA 807 AND RBL= 3 AT AFT CARGO COMPARTMENT. WAS REPAIRED PER B737-800 SRM 53-00-53-2R PROCEDURE 2 REPAIR 2.SDR DALA2022072005018Rail · worn(LOG 2326721) DURING INSPECTION FOUND WEAR ON FLOOR STRUCTURE RAIL BTW STA 767/STA 787 AND STA 787/STA 807 RBL8 AT AFT CARGO COMPARTMENT. FLOOR STRUCTURE RAIL BTW STA 767/STA 787 AND STA 787/STA 807 RBL8 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 5SDR FDEA202207191765Floor Panel · crackedMAIN DECK CABIN FLOOR PANEL 242QF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242QF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR DALA2022072105047None · noneSHIP 664 DENT ON FRAME STA 1300 BTW S-27R-S26R AND S- 27L-S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00251: DENT ON FRAME STA 1300 BTW S-27R-S26R AT AFT CARGO COMPARTMENT. (C2) WAS REPAIRED PER PRI 600676-14 REV 3 AND ERA 600676-14AD REVSDR DALA2022072105060None · noneSHIP 664 DENT ON FRAME STA 1300 BTW S-27R-S26R AND S- 27L-S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00251: DENT ON FRAME STA 1300 BTW S-27L-S-26L AT AFT CARGO COMPARTMENT. (C2) WAS REPAIRED PER PRI 600675-14 REV 1 AND ERA 600675-14AD RESDR FDEA202207181761Floor Panel · crackedMAIN DECK CABIN FLOOR PANEL 242PF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242PF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202207181759Floor Panel · crackedMAIN DECK CABIN FLOOR PANEL 242LF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242LF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202207181758Floor Panel · crackedMAIN DECK CABIN FLOOR PANEL 242KF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 242KF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202207181757Floor Panel · crackedMAIN DECK CABIN FLOOR PANEL 241QF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241QF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR CALA2022072001812Floorbeam · misinstalledMISSED DRILL FLOORBEAM -Y1292 LOCATED FR65 TO FR66 AT AFT GALLE Y AREA REMOVED AND REPLACED FLOORBEAM -Y1292 AND FASTENERS LOC FR64 TO FR66 AT AFT GALLEY AREA IAW SRM A320 51-42-11 AND DWG D5347220 ADD EMP:V939315SDR FDEA202207181756Floor Panel · crackedMAIN DECK CABIN FLOOR PANEL 241UF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241UF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202207181755Floor Panel · crackedMAIN DECK CABIN FLOOR PANEL 241MF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241MF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202207181754Floor Panel · crackedMAIN DECK CABIN FLOOR PANEL 241PF FOUND CRACK. MAIN DECK CABIN FLOOR PANEL 241PF REPAIRED PER B777 SRM 53-00-50-2R . REPAIR 1, REV41.0, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR CALA2022071801806None · noneMISSED DRILL FLOOR BEAM -Y1292 LOCATED FR65 TO FR66 AT AFT GALLEY AREA. REMOVED AND REPLACED FLOOR BEAM -Y1292 AND FASTENERS LOC FR64 TO FR66 AT AFT GALLEY AREA.SDR SWAA2022082330270Floor Panel · crackedCABIN FLOOR PANEL 231UF FWD RIGHT CORNER CRACKED / [01] CLEANED FLOOR PANEL 231UF REMOVE DAMAGE PLIES AND PREPARE AREA FOR REPAIR ON TOP SURFACE R/H FWD. CORNER AS PER B737 SRM 53-00-50-2R-9;[02] VERIFIED STEP 1. OK TO INSTALL REPAIR.;[03] REPAIRED DAMAGE FWD.SDR DALA2022072005027Stringer · corrodedSHIP 664 CORROSION ON PREVIOUS REAIR ON STRINGER S- 28L BTW STA 1500 TO STA 1520 AT AFT CARGO COMP. CORRECTIVE ACTION: SUMMARY OF NRC 00226: PREVIOUS REAIR ON STRINGER S-28L BTW STA 1500 TO STA 1520 AT AFT CARGO COMP. WAS REPLACED PER B757-200 SRM. (2324450)SDR DALA2022072005026Frame · dentedSHIP 664 DENT ON FRAME STA 1260 BTW S-27R-S25R AND S- 27L-S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00244-DENT ON FRAME STA 1260 BTW S-27L-S-26L AT AFT CARGO COMPARTMENT WAS REPAIRED PER PRI 600777-14 REV.0 AND ERA 600777-14AD REV. ORIG
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