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 FDEA202302080222Track · chafedCABIN - SEAT TRACK STATION 1671, X = -47.50 CROWN AREA CHAFFING MARKS. REMOVED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1651 TO STATION 16SDR FDEA202302080221Track · damagedCABIN - SEAT TRACK STATION 1325, X = 8.50 CROWN AREA DAMAGED. CABIN Ï¿½ AT SEAT TRACK STATION 1325, X = 8.5, CROWN DAMAGED AREA EVALUATED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CROWN DAMAGED SEAT TRACK REPAIRED BY SESDR FDEA202302080220Track · corrodedCABIN - SEAT TRACK STATION 1149, X = -47.50 CORROSION. CABIN Ï¿½ CORROSION AT SEAT TRACK STATION 1149, X = -47.5 EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SSDR DALA2023020901045Unknown · unknown(LOG 2620270) DURING H MAINTENANCE VISIT AT AEM (SAL) ON A/C 3958 (LN 5070), WHILE EXECUTION OF JIC 5300-2594-B3, SEVERAL DAMAGES WERE FOUND ON FRAME P/N: 143A1261-4#A AT BSTA STA500K BETWEEN S-22L AND S-26L AT FORWARD CARGO COMPARTMENT. MAINTENANCE REPAIRED DSDR SWAA2023030900386Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PANEL #241ABF TOP SKIN FIBERGLASS PEELING OFF<[01] FABRICATED PASSENGER CABIN FLOOR PANEL #241ABF PER DRWG #147A5810 BY OUTSIDE VENDOR PO#2006646. THIS PANEL WILL BE INSTALLED ON FAULT #TTG8Q00GQ33Y PER B737-700 AMM 53-21-00-400-8SDR SWAA2023030900390Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL #221BF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS<[01] FABRICATED MAIN CABIN FLOOR PANEL #221BF BY OUTSIDE VWENDOR (AERO MARINE) WITH PO #2006745 REF. DRAWING 141A5810. PANEL 221BF BY OUTSIDE VENDOR;[02] VERIFIED STEP 1.SDR SWAA2023030900392Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL #221DF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS<[01] FABRICATED MAIN CABIN FLOOR PANEL #221DF BY OUTSIDE VWENDOR (AERO MARINE) WITH PO #2006750 REF. DRAWING 141A5810. PANEL 221DF WILL BE INSTALLED ON FAULT #TTG8Q00HPPNPSDR SWAA2023030800116Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PANEL #242UF TOP SKIN FIBERGLASS PEELING OFF<[01] FABRICATED PASSENGER CABIN FLOOR PANEL #242UF PER DRWG #147A5810 BY OUTSIDE VENDOR PO#2006660. THIS PANEL WILL BE INSTALLED ON FAULT #TTG8Q00GQ3EY PER B737-700 AMM 53-21-00-400-801SDR SWAA2023030800117Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PANEL #242TF TOP SKIN FIBERGLASS PEELING OFF<[01] FABRICATED PASSENGER CABIN FLOOR PANEL #242TF PER DRWG #147A5810 BY OUTSIDE VENDOR PO#2006738. THIS PANEL WILL BE INSTALLED ON FAULT #TTG8Q00GQ3F2 PER B737-700 AMM 53-21-00-400-801SDR SWAA2023030800394Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #241KF TOP SKIN FIBERGLASS PEELING OFF SEVERAL AREAS<[01] PREPARED FOR REPAIR PANEL 241 KF; AS PER B737 SRM 53-00-50-2R-1;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED PANEL 241KF AS PER B737 SRM 53-00-50-2R-1.MATERIAL USDR FDEA202302070211Track · corrodedCABIN Ï¿½ SEAT TRACK STATION 6 - 35, X = - 47.50 CORROSION. EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CORRODED SEAT TRACK REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 6-60 TO EXISTINSDR DALA2023020800988Unknown · unknownAIRCRAFT 3122, BENT FLOOR STRUCTURE CROSS BEAM LOCATED BETWEEN FR26 AND STR38L TO STR42R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REMOVED FLOOR STRUCTURE CROSS BEAM LOCATED BETWEEN FR26 AND STRINGER 38L TO STRINGER 42R IN FWD CARGO COMPARTMENT AS PER A319 SDR DALA2023020800983Not Reported · not reportedSECONDARY NRC 00428: FLOOR SUPPORT STA Y=180 AND X=-9 TO X=-43 HAS CORROSION. ORIGINAL THICKNESS IS 0.070 IN AND MINIMUM REMAINING THICKNESS IS 0.020 IN, THEREFORE THE AREA CORROSION IS OUT LIMITS AT PAX CABIN. (CPAX)(W1). SUMMARY OF NRC 00489: CORROSION LEVELSDR DALA2023020800982Not Reported · not reportedCORROSION ON FLOOR SUPPORTS (3 EA) STA Y=196 TO 200 FROM X=16 TO X=55.5 AT PAX CABIN FLOOR STRUCTURE. CPAX. SUMMARY OF NRC 00435: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA) AT STA Y=196 TO 200 FROM X=16 TO X=55.5 WERE REPLACED PER B717-200 SRM 51-41-05 PAR 8, 51SDR DALA2023020700937Not Reported · not reported(LOG 2618087) DURING INSPECTION FOUND CORROSION ON FLOOR BEAM STA 947.5 AT SETTLEMENT AREA OF LH/RH AFT LAVATORIES FITTINGS. FLOOR BEAM STA 947.5 BTW LBL 54 TO LBL 54 WAS REPAIRED PER B737-900ER SRM 53-70-51-2R REPAIR 5.SDR DALA2023020700933Not Reported · not reportedSHIP 1201 FOUND OUT FWD CARGO DOOR CUTOUT SUPPORT CORROSION AT STA562, REF TO CPCP TASK 53-458-00. CORRECTIVE ACTION: FWD CARGO DOOR CUT OUT SUPPORT AT STA562 CORROSION REMOVED AND MEASURED: THE MINIMUM REMAINING THICKNESS IS 0.075" , THE BLEND OUT AREA PERFORSDR SWI2023F00025Unknown · crackedAT R/H FS280 AFT FLOOR ANGLE FOUND RBL 9.0 INBD AND OUTBD CLIPS CRACKED (C-CHECK RO 3/11/2023) REMOVED AND INSTALLED NEW INBOARD AND OUTBOARD CLIPS AT RBL9 / FS280 BEAM. REF: REO 601R-53-11-171, REV: D, 13 FEB 07 FOR FASTENER TYPE AND LOCATION.C/W 51-90SDR SWI2023F00024Unknown · unknownAT R/H FS280 AFT FLOOR ANGLE FOUND RBL 9.0 SPLICE ANGLE 601R-53-11-136-4 CRACKED (C-CHECK RO 3/11/2023) REPAIRED R/H FS280 AFT FLOOR ANGLE RBL 9.0 SPLICE ANGLE 601R-53-11-136-4 REF REO 601R-53-11-136, REV: A 2007-11-01.C/W 51-900-1003-SKYSDR SWI2023F00022Unknown · crackedAT R/H FS280 AFT FLOOR ANGLE FOUND RBL 9.0 INBD AND OUTBD CLIPS CRACKED (C-CHECK RO 3/11/2023) REMOVED AND INSTALLED NEW INBOARD AND OUTBOARD CLIPS AT RBL9 / FS280 BEAM. REF: REO 601R-53-11-171, REV: D, 13 FEB 07 FOR FASTENER TYPE AND LOCATION.C/W 51-90SDR SWI2023F00021Unknown · unknownAT R/H FS280 AFT FLOOR ANGLE FOUND RBL 9.0 SPLICE ANGLE 601R-53-11-136-4 CRACKED (C-CHECK RO 3/11/2023) REPAIRED R/H FS280 AFT FLOOR ANGLE RBL 9.0 SPLICE ANGLE 601R-53-11-136-4 REF REO 601R-53-11-136, REV: A 2007-11-01.C/W 51-900-1003-SKYSDR SWAA2023031099852Floor Panel · peelingCABIN FLOOR PANEL 221AF SURFACE IS PEELING.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR><BR>FOUND 2 AREAS OF UPPER SURFACE SKIN DAMAGE; BOTH AREAS ARE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B.<BR><BR>REPAIRS TO BESDR SWAA2023031099851Floor Panel · brokenCABIN FLOOR PANEL 221BF IS BROKEN AT TAB.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.<BR><BR>FOUND DAMAGE AT 2EA LOCATIONS ON PANEL; AREA #1 AT AFT O/B CORNER ON LOWER SURFACE WHERE TAB IS BROKEN; AREA #2 IS 14.5' FROM FWD AND 10' FROM SDR SWAA2023031099850Floor Panel · corrodedCABIN FLOOR PANEL 241ABF HAS CORRODED INSERTS AND SURFACE PLYS PEELING.<[01] IDENTIFIED 241ABF PANEL IAW SRM 53-00-50-OI-1 PARA FIGURE 6; TABLE 6.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1<BR><BR>WILL PERFORM WORK IAW SRM 53-00-50SDR SWAA2023021599596Floor Panel · pulledDOT A-24-04 CENTER CABIN FLOOR PANEL 231ZF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED PANEL 231ZF 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 53-0SDR SWAA2023021599594Floor Panel · pulledDOT A-24-02 CENTER CABIN FLOOR PANEL 231YF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[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 AREA FOR REPAIR IAW SRM 53-00-50SDR SWAA2023021599597Floor Panel · pulledDOT A-24-05 CENTER CABIN FLOOR PANEL 231XF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00SDR SWAA2023021599598Floor Panel · pulledDOT A-24-06 CENTER CABIN FLOOR PANEL 241AF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00SDR SWAA2023021599599Floor Panel · pulledDOT A-24-07 CENTER CABIN FLOOR PANEL 232SF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED PANEL 232SF AND FOUND AREA'S OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1. CLEAN AND PREP FOR REPAIR. IAW B737-SDR SWAA2023021599600Floor Panel · pulledDOT A-24-08 CENTER CABIN FLOOR PANEL 242AF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE THE LENGTH OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PSDR DALA2023021401130Unknown · unknownAFT LOWER CARGO COMPARTMENT LINERS METAL TRANSITION STRIP BENT UP. MCC FCP DEFERRAL TO MEL 25-50-01, FLIGHT CREW PLACARD INSTALLED. LOWER COMPARTMENT LINERS BINS 3-4. INSTALLED SIDEWALL PANELS PUSHED OUT. FOUND PNL 181HF BENT UP AND WILL NEED REPLACED REF IPC SDR DALA2023021001065Unknown · unknownSHIP 1200 THE CABIN FLOOR BEAM UPPER SURFACE CORROSION AT STA 347 AND RBL 11 TO 54.7;REF TO CPCP TASK 53-400-00. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER PRI 605190-14 (2616528)SDR SWAA2023020800068Panel · crackedFWD BIN C AND B HAVE CRACK IN FLOOR STA 190 AND STA 205<[01] REPAIRED IAW 25-52-01 AMM OK FOR SVCSDR AALA202302081098Floor Panel · delaminatedAIRCRAFT WAS NOT GROUNDED: FORWARD CARGO COMPARTMENT FLOOR PANEL 131EF DELAMINATED. MAINTENANCE REPLACED FLOOR PANEL PER AMM 53-22-14.SDR AALA202302081765Floor Panel · delaminatedAIRCRAFT WAS NOT GROUNDED: FORWARD CARGO COMPARTMENT FLOOR PANEL 131HF DELAMINATED. MAINTENANCE REPLACED FLOOR PANEL PER AMM 53-22-14.SDR DALA2023020700936Floor Support · corroded(LOG 2617732) DURING INSPECTION FOUND CORROSION AT FLOOR SUPORT LBL 52 BTW STA 947 AND STA 967 LH CPAX (W2). FLOOR SUPORT LBL 52 BTW STA 947 AND STA 967 LH CPAX (W2) WAS REPLACED PER B737-900ER SRM 51-40-02-0G.SDR DALA2023020700935Floor Support · corroded(LOG 2617673) DURING INSPECTION FOUND CORROSION ON FLOOR SUPPORT UPPER FACE BETWEEN STA: 947 AND STA: 967 RBL 52. FLOOR SUPPORT UPPER FACE BETWEEN STA: 947 AND STA: 967 RBL 52 WAS REPLACED PER B737-900ER SRM 51-40-02-0G.SDR SWI2023F00020Unknown · crackedPILOT'S SIDE POST CRACKED AT UPPER BARREL NUT AS MARKED (C-CHECK RO 3/11/2023) REMOVED AND REPLACED PILOT SIDE POST. REF. CRJ200 SRM 51-42-21, SRM 51-41-02 AND DWG# 601R33007 REV. UCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURASDR SWI2023F00019Unknown · crackedFS280 AFT CENTER COCKPIT FLOOR SUPPORT IS CRACKED (C-CHECK RO 3/11/2023) REPAIRED FS280 AFT CENTER COCKPIT FLOOR SUPPORT REF DWG 600-34017, REV: AD, CRJ200 SRM 51-42-06, REVISION 39: MAR 10/2021.C/W 51-900-1003-SKYSDR SWI2023F00018Unknown · crackedPILOT'S SIDE POST CRACKED AT UPPER BARREL NUT AS MARKED (C-CHECK RO 3/11/2023) REMOVED AND REPLACED PILOT SIDE POST. REF. CRJ200 SRM 51-42-21, SRM 51-41-02 AND DWG# 601R33007 REV. UCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURASDR SWIA2023003150011Unknown · crackedFS280 AFT CENTER COCKPIT FLOOR SUPPORT IS CRACKED (C-CHECK RO 3/11/2023) REPAIRED FS280 AFT CENTER COCKPIT FLOOR SUPPORT REF DWG 600-34017, REV: AD, CRJ200 SRM 51-42-06, REVISION 39: MAR 10/2021.C/W 51-900-1003-SKYSDR SWAA2023030699304Floor Panel · brokenBROKEN FLOOR PANEL 242UF AT AFT GALLEY AND LAV 2023-99277<[01] TOOL USED; CALIPER; P/N:500-197-30 S/N:B20189526; DUE DATE: 20/DEC/23.;[02] TOOL USED: HOT BONDER P/N: HCS9000B-AV S/N: 18164925 DUE DATE: 22-JAN-24?;[03] TOOL USED: SCALE P/N: SPX621 S/N: 83402254SDR DALA2023020600911None · noneAIRCRAFT 3122, CORROSION SEAT TRACK +Y1292 BTW FR 65 AND FR 66 AT AFT GALLEY. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 LOC. BTW FR64 TO FR65 AT AFT GALLEY. LP 2615952SDR DALA2023020600910None · noneAIRCRAFT 3122, CORROSION FLOOR BEAM -Y765 BTW FR 66 AND FR 68 AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 BTW FR 66 AND FR 68 AFT GALLEY AREA AND FASTENERS AS PER A319 SRM 51-42-11 AND DWG D53472000 RELEASEDATE 06/JAN/23. LP 2615SDR DALA2023020700967None · noneSHIP 3327 CORROSION FLOOR STRUCTURE FR75 TO FR76 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED NEW FLOOR STRUCTURE AND FASTENERS BTW FR75 TO FR76 IN PASSENGER CABIN AS PER A330 SRM 51-42-11 SRM 51-72-11. (2615762)SDR SWAA2023030698661Floor Panel · elongatedELONGATED HOLE FLOOR PANEL 221GF AT PASSENGER CABIN 2023-99171<[01] TOOL USED: CALIPER P/N: 500-196-30 S/N: A21033535 DUE DATE: 29-OCT-23;[02] TOOL USED ULTRASONIC FLAW DETECTOR PN. EPOCH 650; SN. 190859705; DUE DATE. 16-SEP-23;[03] REPLACED FLOOR PANEL 221GF SDR SWAA2023030698660Floor Panel · crackedCRACK FLOOR PANEL 221BF AT PASSENGER CABIN 2023-99170<[01] REPLACED FLOOR PANEL 221BF AT PASSENGER CABIN IAW BOEING 737-700 AMM 53-21-00-000-801 AND AMM 53-21-00-400-801 SEE BELOW INDIVIDUAL;[02] CORRECTED STEP 1 <BR>REPLACED FLOOR PANEL 221BF AT PASSENGER CABSDR SWAA2023021697987Floor Panel · damagedNEED TO RELOCATE FLOOR PANEL #241FF INSERT (1 EACH) DUE TO REPAIRED INSTALLED ON THE FLOORBEAM AT BS727+6 LBL 45.57.<[01] FABRICATED NEW FLOOR PANEL 241FF USING BMS 4-17TY6 LOT#1514505-1; INSTALLED ALL INSERTS EXCEPT P12 TO BE RELOCATED USING BMS 5-107 LOT#AK2SDR DALA2023020400866Not Reported · not reportedSHIP 3308 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FLOOR BEAM WEB AROUND THE COLLAR OF THE REINFORCEMENT STRAP ATTACHMENT FASTENERS BTW FR75 TO FR79 IN PASSENGER CABIN. CORRECTIVE ACTION: EXISTING ALTERATION INSTALLED PER EO 5320-01135. STC IS APPROVED FOSDR DALA2023020600888Not Reported · not reported(LOG 2610414) DURING INSPECTION FOUND CORROSION AT FLOOR STRUCTURE SUPPORTS LBL 13 BTW STA.294.5 AND STA.303.9 CPAX (W1). INTERCOSTAL LBL 13 BTW STA.294.5 AND STA.303.9 CPAX (W1) WAS REPLACED PER B737-900ER SRM 51-40-02-0G.SDR DALA2023020600886Web · corroded(LOG 2610235) DURING INSPECTION FOUND CORROSION ON WEB AT FLOOR STRUCTURE BETWEEN STA.787 AND STA.847 RBL 20 APRROX OF AFT CARGO COMPARTMENT. WEB AT FLOOR STRUCTURE BETWEEN STA.787 AND STA.847 RBL 20 APRROX OF AFT CARGO COMPARTMENT WAS REPLACED PER B737-900ER
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