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 SWAA2022082542273Floor Panel · pulledDOT A-24-02. MID CABIN FLOOR PANEL 231YF HAS PULLED FIBERS ON TOP SIDE OF PANEL / [01] EVALUATED AND FOUND PULLED FIBERS ON UPPER SURFACE. DAMAGE IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1 CLEANED AND PREPPED UPPER SURFACE IAW SRM 5SDR SWAA2022082542277Floor Panel · pulledDOT A-24-03. MID CABIN FLOOR PANEL 231XF HAS PULLED FIBERS ON TOP SIDE OF PANEL / [01] EVALUATED FLOOR PANEL 231XF FOUND WITH IN REPAIRABLE LIMITS OF B737-700 SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED FLOOR PANEL 231XF FOR WET LAY UP IAW B737-700 SRM 53-00-50-2RSDR SWAA2022082542279Floor Panel · pulledDOT A-24-04. MID CABIN FLOOR PANEL 232SF HAS PULLED FIBERS ON TOP SIDE OF PANEL / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD; NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED REPAIR IAW B737 SRM 53-0SDR SWAA2022082542280Floor Panel · pulledDOT A-24-05. MID CABIN FLOOR PANEL 242BF HAS PULLED FIBERS ON TOP SIDE OF PANEL / [01] EVALUATED DAMAGE ON UPPER SURFACE OF FLOOR PANEL 242BF; FOUND WITH-IN LIMITS OF SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED UPPER SURFACE OF FLOOR PANEL 242BF FOR WET LAY-UP IAWSDR SWAA2022082542276Floor Panel · pulledDOT A-24-01. MID CABIN FLOOR PANEL 231ZF HAS PULLED 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.<BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS A;C;E; SDR DALA2022081605540None · noneSHIP 1817 MTC TASK-FWD GALLEY FLOOR BEAM AT STA 347 RBL45 FOUND WITH CORROSION. CORRECTIVE ACTION: CORROSION REMOVED AND ACCOMPLISHED AS PER PRI 601146-14. (2366149)SDR DALA2022081605539None · noneSHIP 1817 FWD GALLEY FLOOR BEAM AT STA 347 RBL45 FOUND WITH CORROSION. CORRECTIVE ACTION: ASSOCIATED ER/A 14-601146 ADDED FOR AC 1817 (2366142)SDR CALA2022081602104Skin · dentedDENT LH FR 28-29 STGR 38-39, REQUIRES EVALUATION AS PER A319 SRM TAS 53-21-11-283-020 REV.141. AS NOTED ON LTPR NR# 5001172215-0010. 53-21-11-205-068. INSPECTION THRESHOLD FROM EMBODIMENT 60000FC & FH. REF SRM 53-21-11-300-087 AND SRI 53-21-11-205-068 FOR REPASDR SWAA2022090641853None · wornAFT CARGO COMP. FWD CENTER BULKHEAD PANEL 142NW WORN OUT / [01] REPLACED AFT CARGO FWD BULKHEAD PANEL 142NW. PANEL WILL BE INSTALLED IN ITEM TTG8Q00DDWXS;[02] VERIFIED STEP 1.SDR DALA2022081705589Web · corroded(LOG 2364205) DURING INSPECTION FOUND CORROSION ON WEB AT STA 986.5 BTW RBL 35 TO RBL 40 AT W2. WEB AT STA 986.5 BTW RBL 35 TO RBL 40 WAS REPLACED PER BOEING DRAWING 147A5712 REV.F AND B737-800 SRM 51-40-02-0G.SDR DALA2022081705588Angle · corroded(LOG 2362974) CORROSION ON ANGLE BTW STA 990 TO 1010 AND LBL 35 AT W2. ANGLE WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR 4.B AND 5B. AND SRM 53-70-51-1A-1.FSDR DALA2022081705587Angle · corroded(LOG 2362962) DURING INSPECTION FOUND CORROSION ON ANGLE AT STA 990 BTW LBL 35 TO LBL 40 AT W2. ANGLE WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR 4.B AND 5B. AND SRM 53-70-51-1A-1.SDR DALA2022081605557None · none(LOG 2362959) DURING INSPECTION FOUND CORROSION ON ANGLE AT STA 990 BTW RBL 35 TO RBL 40 AT W2. ANGLE WAS REPLACED PER B737-800 SRM 51-40-02-0G PAR 4.B AND 5B. AND SRM 53-70-51-1A-1.SDR DALA2022081605556None · none(LOG 2362940) DURING INSPECTION FOUND CORROSION ON BEAM STA 986.5 BTW RBL 0 TO RBL 44 AT PAX CABIN. FLOOR BEAM STA 986.5 BTW RBL 0 TO RBL 44 AT PAX CABIN WAS REPAIRED PER B-737-900ER SRM 53-70-51-2R PROCEDURE 4 REP 4.SDR SWAA2022090741413Floor Panel · damagedFLOOR PANEL 222BF HAS TORN PLIES ON UPPER SURFACE IN SEVERAL LOCATIONS (MARKED) / [01] IDENTIFIED MATERIAL IAW SRM 53-00-50-0I-1 TABLE 2 FIG 2.<BR><BR>DAMAGE NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B<BR><BR>DAMAGE TO BE REPAIRED IAWSDR DALA2022081605552None · none(LOG 2362178) DURING INSPECTION FOUND CORROSION ON BEAM ON STA 947.5 BTW RBL 50 TO LBL 27 AT PAX CABIN. FLOOR BEAM ON STA 947.5 BTW RBL 50 TO LBL 27 WAS REPAIRED PER B737-900ER SRM 53-70-51-2R PROCEDURE 5 REPAIR 5.SDR DALA2022081505506Floor Support · corroded(LOG 2361527) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT STA 947.5 AND RBL 24.75. NEW SUPPORT WAS INSTALLED PER B737-900ER SRM 51-40-02-0G.SDR DALA2022081505505Floor Support · corroded(LOG 2361523) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT BTW STA 947.5 TO 958 AND RBL 49 AT PAX CABIN. NEW SUPPORT WAS INSTALLED PER B737-900ER SRM 51-40-02-0G.SDR CALA2022081202056Seat Track · corrodedCORROSION SEAT TRACK -Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359891. REMOVED AND REPLACED SEAT TRACK Y765 LOC.BTW FR12 TO FR24 AT FWD ION ON AREA AND NOT FOUND ADDITIONAL DAMAGE I.A.W. NTM 51-90- 2023. GALLEY AREA IN PASSENSDR CALA2022081202055Seat Track · corrodedCORROSION SEAT TRACK -Y1292 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-359890. REMOVED AND REPLACED SEAT TRACK-Y1292 LOC. BTW FR12 TO FR24 AT DITIONAL DAMAGE I.A.W. NTM 51-90-00. PERFORMED SCEPTRE ENTRY INE 2022-359890. FWD GALLEY ASDR DALA2022081505504Fitting · corroded(LOG 2360593) DURING INSPECTION FOUND CORROSION ON GALLEY 4 FLOOR SUPPORT FITTINGS AT PAX CABIN. FLOOR SUPPORT FITTINGS PAX CABIN WERE REPLACED PER B737-800 SRM 51-40-02-0G.SDR SWAA2022081240190Floor Panel · crackedBREAK PANEL IS CRACKED AT STA 540; BL 0-LBL 25; WL 208. / [01] UPDATED TABLE;[02] REMOVED FLOOR PANEL 231UF PER AMM 53-21-00-000-801;[03] REMOVED BRAKE PANEL AT STA 540 BL0 - LBL 25 WL 208 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW BREAK PANEL AT STA 5SDR CALA2022081002033Angle · crackedCRACK FLOOR STRUCTURE ANGLE LOCATED FR68 LEVEL STRG23L IN PASSENGER CABIN (1 EA) REMOVED AND REPLACED FLOOR STRUCTURE ANGLE AND FASTENERS AND NOT FOUND MORE DAMAGE IAW NTM 51-90-00. PERFORMED LOCATED FR68 AT LEVEL STR 23L IN PASSENGER CABIN IAW A320 SCEPTRE SDR CALA2022081002032Dummy Rail · corrodedCORROSION RAIL DUMMY -Y81 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393815 REPLACED RAIL DUMMY -Y81 AT FWD GALLEY AREA IAW A320 SRM L=2.820 IN, W=2.017IN, D=0.116 IN, TOOL USED: CALIPER P/N: 51-72-11-911-001 AND DRAWING D53110984, PERFORMED DVI ON AREA SDR CALA2022081002021Doubler · inadequateDURING HMV VISIT FOUND DOUBLER LOCATED AT FR28-29 STR 38L-39L THAT DOES NOT COMPLY WITH CURRENT SRM. ACCOMPLISHED REPAIR PER SRM 53-21-11-300-090 AND 51-42-11. LOG CREATED FOR DIP REPETITIVE INSPECTION REQUIREMENTS. INSPECTION IAW SRI 53-21-11-205-071 ZONE A.SDR SWAA2022090249508Floor Panel · brokenPANEL 221BF AFT O/B EDGE IS BROKEN. (228-003) / [01] RECEIVED NEW FLOOR PANEL ; PANEL WILL BE INSTALLED ON WORK CARD TTG8Q00DAN6K;[02] VERIFIED STEP 1SDR SWAA2022090249509Floor Panel · brokenPANEL 222DF I/B SIDE AT 23 ' TO THE FWD SIDE IS BROKEN. / [01] RECEIVED NEW FLOOR PANEL ; PANEL WILL BE INSTALLED ON WORK CARD TTG8Q00DAN5K;[02] VERIFIED STEP 1SDR SWAA2022081239495Floor Panel · pulledDOT A-24-1 MID CABIN FLOOR PANEL 241BF HAS PULLED FIBERS ON UPPER SURFACE. / [01] EVALUATED DAMAGE; UPPER SURFACE IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD; NO DELAMINATION. <BR><BR>CLEANED AND PREPPED REPAIR AREA IAW B737 SRM 53-00-50-2R-1 PAR 3SDR SWAA2022081239490Floor Panel · pulledDOT A-24-1 MID CABIN FLOOR PANEL 241CF HAS PULLED FIBERS ON UPPER SURFACE. / [01] EVALUATED AND FOUND DAMAGE TO 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 53-00-50-2R-1 STSDR SWAA2022081239492Floorboard · pulledDOT A-24-1 MID CABIN FLOOR PANEL 242BF HAS PULLED FIBERS ON UPPER SURFACE. / [01] EVALUATED AND FOUND DAMAGE TO 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 53-00-50-2R-1 STSDR SWAA2022081239499Floor Panel · pulledDOT A-24-1 MID CABIN FLOOR PANEL 242AF HAS PULLED FIBERS ON UPPER SURFACE. / [01] EVALUATED PANEL 242AF 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. IAW B737-700 SRM 53-00-50-2SDR SWAA2022081239498Floor Panel · pulledDOT A-24-1 MID CABIN FLOOR PANEL 232RF HAS PULLED FIBERS ON UPPER SURFACE. / [01] EVALUATED AND FOUND DAMAGE TO 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 53-00-50-2R-1 STSDR DALA2022081005464Support Fitting · corroded(LOG 2354770) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT (4EAS) BETWEEN BSTA 951 & 967 AND BETWEEN RBL 25 & 51 / LBL 25 & 51. FLOORS SUPPORTS (4EAS) ON BETWEEN BSTA 951 TO 967 AND BETWEEN RBL 25 & 51 / LBL 25 & 51 ON PASSENGER CABIN WERE REPLACED PER BSDR DALA2022081005462Floorbeam · corroded(LOG 2354711) DURING INSPECTION FOUND CORROSION ALONG OF FLOORBEAMS 312,328 AND 344 AT W1 AREA. FLOORBEAM 312 WAS REPAIR PER. B737-800 SRM 53-10-51-2R REPAIR 17.SDR SWAA2022080939494Floor Panel · pulledMID CABIN FLOOR PANEL 231ZF HAS PULLED FIBERS ON UPPER SURFACE. EVALUATED & FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A, C, E, & F. BSDR SWAA2022080939491Floor Panel · pulledDOT A-24-1 MID CABIN FLOOR PANEL 231XF HAS PULLED FIBERS ON UPPER SURFACE. EVALUATED PANEL 231XF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW 53-00-50-2R-1 PAR 3 A;C;E&F. VERIFIED SDR SWAA2022080939496Floor Panel · pulledMID CABIN FLOOR PANEL 231YF HAS PULLED FIBERS ON UPPER SURFACE. EVALUATED PANEL 231YF & FOUND UPPER FIBER DAMAGE. PANEL IS REPAIRABLE IAW SRM 53-00-50-2R-0 & SRM 53-00-50-2R-1. NO CORE DAMAGE NOTED. CLEANED PANEL IAW SRM 53-00-50-2R-0 PAR. 5E. APPLIED POTTINSDR SWAA2022080939497Floor Panel · pulledMID CABIN FLOOR PANEL 241AF HAS PULLED FIBERS ON UPPER SURFACE. EVALUATED PANEL 241AF & FOUND AREA'S ON UPPER SURFACE TO BE FRAYED. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1, PAR 1A. CLEAN AND PREP. IAW SRM 53-00-50-2R-1 PAR 3 A, C, E & F. BONDED REPAIR SDR SWAA2022080939493Floor Panel · pulledMID CABIN FLOOR PANEL 232SF HAS PULLED FIBERS ON UPPER SURFACE. EVALUATED & FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A, C, E, & F. ASDR SWAA2022082339225Floor Panel · damagedPASSENGER CABIN FLOOR PANEL 241ABF HAS 3 EACH INSERTS THAT DOES NOT ALIGN WITH HOLES IN STRUCTURE=R/H SIDE; AFT INBOARD AFT 3 HOLES / REMOVED DAMAGE FROM UPPER SURFACE MEASURING 13'X3' APPLIED BMS5-28 TY19 LOT#AK2DP3091K POTTING COMPOUND TO (3EA) FASTENER HOLESDR SWAA2022082239226Floor Panel · out of positionPASSENGER CABIN FLOOR PANEL 241AAF HAS 1 EACH INSERT THAT DOES NOT ALIGN WITH HOLE IN STRUCTURE=L/H SIDE; AFT OUTBOARD CORNER HOLE / [01] IDENTIFIED FLOOR PANEL 241AAF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. FLOOR PANEL PROVIDED FROM STOCK WAS BAD. THSDR SWAA2022082239227Floor Panel · misalignedDUE TO REPAIR OF BS 986 FLOORBEAM; AT SPLICE LOCATION;PASSENGER CABIN FLOOR PANEL 242VF HAS 2 EACH INSERTS THAT DOES NOT ALIGN WITH HOLES IN STRUCTURE= FWD EDGE OF PANEL-MARKED / [01] IDENTIFIED PANEL 242VF IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6<BR><BR>DAMAGEDSDR DALA2022080905431None · none(LOG 2353869) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT BEAM AT SEVERAL AREAS AT BSTA 947 BETWEEN LBL 13 & RBL 48. FLOOR SUPPORT BEAM AT BSTA 947 BETWEEN LBL 13 & RBL 48 WAS REPAIRED PER B737-800 SRM 53-70-51-2R REPAIR 5.SDR FDEA202208061906Floor Panel · dentedMAIN DECK FLOOR PANEL AT STA 1100-1200 BL0 TO LBL24.75 HAS DENT REMOVED, FABRICATED AND INSTALLED NEW PANEL IAW FEDEX REPAIR DWG SRZ-25-005 AND AMM 25-55-04-4SDR FDEA202208061905Floor Panel · dentedMAIN DECK FLOOR PANEL AT STA 1100-1200 BL0 TO RBL24.75 HAS DENT REMOVED, FABRICATED AND INSTALLED NEW PANEL IAW FEDEX REPAIR DWG SRZ-25-005 AND AMM 25-55-04-4SDR IPXA2022092042019Floor Panel · debondedFAULT - FOUND MAIN DECK FLOOR PANEL 241AG DISBOND, STA 1220 - 1264, LBL 97 - 117 (REPAIR) REVIEWEDSDR IPXA2022092042007Floor Panel · debondedFAULT - FOUND MAIN DECK FLOOR PANEL 241DG DISBOND, STA 1260 - 1300, LBL 33 - 76 (REPAIR) REVIEWEDSDR IPXA2022092042041Floor Panel · debondedFAULT - FOUND MAIN DECK FLOOR PANEL 241XF DISBOND, STA 1220 - 1260, LBL 11 - 33 (REPAIR) REVIEWEDSDR DALA2022080905428Plate · corrupted(LOG 2351114) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT BTW STA 947.5 TO 967 AND RBL 52 AT W2. FLOOR SUPPORT BTW STA 947.5 TO 967 AND RBL 52 AT W2 (CPAX) WAS REPLACED PER B737-800 S.R.M. 51-40-02-0G.SDR DALA2022080805395None · none(LOG 2351090) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT BTW STA 947.5 TO 967 AND RBL 25 AT W2. FLOOR SUPPORT BTW STA 947.5 TO 967 AND RBL 25 AT W2 (CPAX) WAS REPLACED PER B737-800 S.R.M. 51-40-02-0G.
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