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 SWAA2022102563668Floor Panel · crackedFWD CARGO PANEL 120CF HAS A CRACK 8 INCHES LONG (FIBERGLASS PANEL) / [01] ACCOMPLISHED A TEMP REPAIR ON FWD CARGO FLOOR PANEL 120CF PER EA 22-125-03161.SDR DALA2022102506876None · none(LOG 2466874) DURING INSPECTION FOUND ELONGATED HOLE ON FLOOR BEAM STA 328 RBL 58 AT CABIN FLOOR STRUCTURE. FLOOR BEAM STA 328 RBL 58 AT CABIN FLOOR STRUCTURE WAS REPAIR PER B 737-900 ER S.R.M. 53-10-51-2R-7.SDR DALA2022102506874Floor Support · corroded(LOG 2466512) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT BTW BSTA 947.5/967 RBL 50. FLOOR SUPPORT WAS REPLACED PER B737-900ER SRM 51-40-02-0G PAR, 7 AND B737-900ER SRM 53-70-51-1A.SDR FDEA202210242649Floor Panel · damagedMAIN CABIN FLOOR PANEL AT STA 480-500 LBL 45 IS DAMAGED REPAIRED FLOOR PANEL IAW B757SRM 53-00-50-2R REPAIR 1SDR FDEA202210242647Floor Panel · delaminatedMAIN CABIN ZONE 240 - FLOOR PANEL 242MCF IS DELAMINATED REPAIRED FLOOR PANEL 242 MCF IAW B757 SRM 53-00-50-2R, REMOVED AND INSTALLED INSERTS IAW B757 SRM 53-00-50-2RSDR DALA2022102606953Membrane · corrodedCORROSION ON CUSP MEMBRANES BTW X=-54-X=-60 AND BTW STA Y=408-427, 506, 525, 598. ORIGINAL THICKNESS IS 0.020 IN AND MINIMUM REMAINING THICKNESS IS 0.010 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00453 AT PAX CABIN. SUMMARY OF NRC 00621: CORROSION LEVSDR DALA2022102606952Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=1024 TO Y=1054 RBL 56 AT RH LAVATORY AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00491: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1024 TO Y=1054 RBL 56 AT RH LAVATORY AFT PASSENGER CABIN WAS REPLACED PER B717-200 SRM 51-41-02SDR CALA2022102402922None · crackedCRACK INDICATION ON FRAME 35 LOWER AND MOST AFT OPEN FASTENER HOLE AT LEVEN OF STGR30RH, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (4 EA) SEE AEROMAN NON ROUTINE 2022-393519 ACCOMPLISHED INTERIM REPAIR PART 1 PER ECRA 5331-02971 ON HOLE # SDR FDEA202210212635Floorboard · crackedMAIN CABIN SEC 46 FLOOR BOARD 251MJF IS CRACKED AT THE FWD OTBD CORNER RPEIARED MAIN CABIN FLOOR BOARD 251MJF IAW B757 SRM 53-00-50-2R, REPAIR 1. ORIG SUBMISSION DATE: 10/24/2022SDR DALA2022102606951Floor Support · corrodedEXFOLATION ON FLOOR SUPPORT STA Y=160-200 X=-44 (CAPX)(W1). SUMMARY OF NRC 00482: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160- 200 X=-44 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND B717-200 SRM 51-41-05-0G. (LP #2462423)SDR DALA2022102606950Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=200 BTW X=-9 AND X=-46 (CAPX)(W1). SUMMARY OF NRC 00472: CORROSION LEVEL 2. FLOOR SUPPORT AT STA Y= 200 BTW X=-9 AND X=-46 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND B717-200 SRM 51-41-05-0G. (LP #2462418)SDR DALA2022102606949Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=1024 TO Y=1055 RBL 48 AT RH LAVATORY AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00492: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA Y=1024 TO Y=1055 RBL 48 AT RH LAVATORY AFT PASSENGER CABIN WAS REPLACED PER DWG 9981474-82 AND B7SDR DALA2022102606948Floor Support · corrodedEXFOLATION ON FLOOR SUPPORT STA Y=180 BTW X=-9 - X=-43 (CAPX)(W1). SUMMARY OF NRC 00481: CORROSION LEVEL 2. SUPPORT STA Y=180 BTW X =-9 - X=-43 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND B717- 200 SRM 51-41-05-0G. (LP #2461817)SDR UIEA2022101801150Floor Panel · corroded***CORROSION*** FWD CARGO COMPT. FLOOR PANEL STA 500D TO 500I, RBL 23 -25, WL 156 (FOUND CORRODED FLOOR PANEL OUT OF LIMITS PER SRM 53-00-53-1A-1 AND FABRICATED NEW FLOOR PANEL PER DWG# 453A1610)SDR DALA2022102406849None · noneSHIP 655 CORROSION ON RH SIDE PLATE BTW STA 1200 TO 1310 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00184: RH SIDE PLATE BTW STA 1200 TO 1310 AT AFT CARGO COMPARTMENT. (C2) REPAIRED PER PER. B757-200 SRM. (2459893)SDR SWAA2022112261948Floor Panel · crackedFLOOR PANEL 834DZ IS CRACKED. NEW FLOOR PANEL INSTALLED IAW CARD TTG8Q00EWPU2.SDR SWAA2022111661846Floor Panel · brokenCABIN FLOOR PANEL 221BF, AFT OTBD EDGE WAS BROKEN BS 280. MAIN CABIN FLOOR PANEL 221BF WILL BE REPLACED ON FAULT TTG8Q00FECMR.SDR SWAA2022111561836Floor Panel · delaminatedFLOOR PANEL 232DF HAS THREE SPOTS OF DELAMINATION (STA 430) / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED ON MAIN CABIN FLOOR PANEL 232DF AS PER B737 SRM 53-00-50-2R-1; MATERIALS USED PO#1778544 AND PO#1690463;[03] PERFORMED TAP TEST ON REPAIRSDR SWAA2022111561866Floor Panel · damagedCABIN FLOOR PANEL 242DF;FIBER GLASS IS PEELING (STA 680). / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED ON MAIN CABIN FLOOR PANEL 242DF AS PER B737 SRM 53-00-50-2R-1; MATERIALS USED PO#1778544 AND PO#1690463;[03] PERFORMED TAP TEST ON REPAIREDSDR SWAA2022111561869Floor Panel · damagedCABIN FLOOR PANEL 241AF;FIBER GLASS IS PELLING. / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED WITH A PERMANENT REPAIR ON MAIN CABIN FLOOR PANEL 241AF AS PER B737 SRM 53-00-50-2R-1; MATERIALS USED PO#1778544 AND PO#1690463;[03] PERFORMED TAP TESDR SWAA2022111161428Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242CF FWD I/B EDGE DELAMINATED. PREPARED FOR REPAIR PANEL 242 CF; AS PER B737 SRM 53-00-50-2R-9. VERIFIED STEP 1. OK TO APPLY REPAIR. REPAIRED FLOOR 242 CF; AS PER B 737 SRM 53-00-50-2R-9 MATERIAL USED PO.1473815 AND PO.1783720. VSDR SWAA2022102761933Floorboard · damagedDOT A-24-20 MID CABIN FLOOR BOARD 241BF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAWSDR SWAA2022102761924Floorboard · damagedDOT A-24-21 MID CABIN FLOOR BOARD 241AF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED AND FOUND PULLED FIBERS AND A PUNCTURE ON UPPER SURFACE ARE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPSDR SWAA2022102761926Floorboard · damagedDOT A-24-23 MID CABIN FLOOR BOARD 232SF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED AND FOUND 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 IASDR SWAA2022102761927Floorboard · damagedDOT A-24-24 MID CABIN FLOOR BOARD 232RF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [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>CLEANED; PREPPED; AND POTTED DASDR SWAA2022102761928Floorboard · damagedDOT A-24-26 MID CABIN FLOOR BOARD 231ZF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [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>CLEANED; PREPPED; AND POTTED DASDR SWAA2022102761929Floorboard · damagedDOT A-24-28 MID CABIN FLOOR BOARD 231YF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAWSDR SWAA2022102761930Floorboard · damagedDOT A-24-29 MID CABIN FLOOR BOARD 231XF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED PANEL 231 XF AND FOUND PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53SDR SWAA2022102761931Floor Panel · damagedDOT A-24-30 MID CABIN FLOOR BOARD 242BF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [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>CLEANED; PREPPED; AND POTTED DASDR SWAA2022102761932Floor Panel · damagedDOT A-24-31 MID CABIN FLOOR BOARD 242AF HAS PULLED COMPOSITE FIBERS ON TOP SIDE OF PANEL. / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAWSDR FDEA202210192623Floorboard · delaminatedZONE 20 FLOOR BOARD 222MAF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VT MAE TRAVELER T22/1638358 IAW DWG SRZ- 25-005 REV R. MAJOR REPAIRSDR FDEA202210192622Floorboard · delaminatedZONE 220 FLOOR BOARD 221MBF IS DELAMINATED FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELER T22/1638356 IAW DWG SRZ-25-005 REV R. MAJOR REPAIRSDR FDEA202210192621Floorboard · delaminatedZONE 220 FLOOR BOARD 222AF IS DELIAMINATED FABRICATED ZONE 220 FLOOR BOARD 222AF ON VT MAE TRAVELER T22/1638359 IAW DWG SRZ- 25- 005 REV R. MAJOR REPAIRSDR FDEA202210192619Floorboard · delaminatedZONE 220 FLOOR BOARD 221AF IS DELAMINATED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VT MAE TRAVELER T22/1638355 IAW DWG SRZ- 25- 005 REVISION R. MAJOR REPAIRSDR ASAA2022101840889Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232DF HAS R/H FWD CORNER HAS DELAMINATION. GROUNDED - YES. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN FLOOR PANEL 232DF AT FR20 IAW A320 SRM ADL 53-12-00-283-005 FIG 001 AND SRM 53-12-00-300-002 RV 142 01 AUG 2022.SDR SWAA2022111561257Floor Panel · damagedMAIN CABIN AFT WET AREA FLOOR PANEL #242UF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS / [01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL #242UF BY OUTSIDE VENDOR WITH R.O #1792601 REF.DRAWING #147A5810. AND AMM 53-21-00-400-801. PANEL ASSY WILL BE INSTALSDR SWAA2022111561262Floor Panel · damagedMAIN CABIN AFT WET AREA FLOOR PANEL #241ABF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS / [01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL #241ABF BY OUTSIDE VENDOR WITH R.O #1792603 REF.DRAWING #147A5810. AND AMM 53-21-00-400-801. PANEL ASSY WILL BE INSTSDR IXXA2022101808Roller Tray · damagedUPPER CARGO ROLLER AT RBL 30.0 IS CUT.SDR AALA202210257016Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: SEAT ROW 7D SMALL CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-32-12.SDR AALA202210241033Floor Panel · delaminatedAIRCRAFT IN BASE MAINTENANCE: SEAT ROW 7C SMALL CABIN FLOOR PANEL IS DELAMINATED. MAINTENANCE REPAIRED FLOOR PANEL PER AARD 53-02-00-2 REPAIR 3.SDR SWIA202266734None · corrodedCORROSION ON RH COCKPIT FLOOR DOUBLER AS MARKED AT FR10-FR12 AND FR08-FR09. (C-CHECK RO 11/3/2022) PERFORMED CUTOUT, FABRICATED REPAIR SPLICES AND SHIMS, AND INSTALLED REPAIR DOUBLER ON RH COCKPIT FLOOR DOUBLER REF ETD2022-170-031813. SEE CONTINUATION CSDR SWAA2022111760102Floor Panel · pulledFLOOR PANEL 241AF UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS. / [01] IDENTIFIED FLOOR PANEL 241AF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.E(2). DAMAGE TO FLOOR PANEL IS BEYOSDR SWAA2022111760098Floor Panel · pulledFLOOR PANEL 241DF UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS. / [01] IDENTIFIED FLOOR PANEL 241DF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE TO FLOOR PANEL IS BEYOND SDR SWAA2022111760094Floor Panel · pulledFLOOR PANEL 231XF UPPER SURFACE HAS LARGE AREAS OF PULLED STRANDS. / [01] IDENTIFIED FLOOR PANEL 231XF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.E(2). DAMAGE TO FLOOR PANEL IS BEYOSDR SWAA2022111660339Floor Panel · crackedCRACK FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT. FABRICATED A NEW FLOOR PANEL IAW AMM 25-52-01-201-801 AND DWG 453A2610 SHEET 18 REV B, SRM 51-10-02 ITEM 9. REPLACED THE FLOOR PANEL 140CF IAW AMM 25-52-01-201-801 AND DWG 453A2610 SHEET 18 REV B, SRM 51-1SDR DALA2022101806715None · noneSHIP 195 AFT CARGO INNER CHORD AT STA 1197,LBL 7 FOUND CORROSION . CORRECTIVE ACTION: AFT CARGO INNER CHORD AT STA 1197,LBL7 CORROSION AREA REMOVED AND REPAIRED AS PER PRI 602625-14 REV 0. (2452965)SDR DALA2022101406644Plate · corroded(LOG 2450952) DURING INSPECTION FOUND CORROSION SEVERAL AT ZEE PLATE FWD CARGO RBL 23, STA500L TO STA490. ZEE PLATE ON STA 490 TO STA 500L WAS REPLACED PER B737-900ER SRM 53-00-53-2R PROCEDURE 6 REPAIR 6.SDR IXXA2022101401Floor Panel · crackedBILGE FLOOR PANEL CRACKEDSDR DALA2022101706686None · noneSHIP 655 CRACK STABILIZATION STRAP STA 1440 LBL-25 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00261: STABILIZATION STRAP STA 1440 LBL-25 AT AFT CARGO COMPARTMENT. (C2) WAS REPAIRED PER B757-200 SRM. (2450731)SDR DALA2022101706685None · noneSHIP 655 DENTS ON FRAMES STA 1500 BTW S-27L - S-24L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00262:FRAME STA 1500 BTW S-27L - S-24L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2450714)
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