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 DALA2022072005023Stringer · corrodedSHIP 664 CORROSION ON FLOOR STRINGERS RBL 2.9, RBL 7.55, RBL 10.45, LBL 2.9, LBL 7.55 AND LBL 10.45, BTW STA 1500 TO STA 1520 AT AFT CARGO COMP. CORRECTIVE ACTION: SUMMARY OF NRC 00224-FLOOR STRINGERS RBL 2.9, RBL 7.55, RBL 10.45, LBL 2.9, LBL 7.55 AND LBL 10.SDR DALA2022071804965Support Bracket · bentSHIP 3229 BENT INTERNAL STRUCTURE SUPPORT BRAKET LOC FR30 AT LEVEL BTW STR43L TO STR43R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE SUPPORT BRAKET PER A320 SRM 51-72-11 AND 51-42-11. (2324601)SDR CALA2022071801799Floorbeam · corrodedCORROSION FLOORBEAM +Y1162 LOCATED BTW FR 68 AND FR 69 AT AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM +Y1162 LOCATED BTW FR.68 AND ADDITIONAL DAMAGE ON AREA IAW NTM 51-90-00 FR.69 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472000 TOOL USED CALIPSDR CALA2022071801798Floorbeam · corrodedCORROSION FLOORBEAM +Y160 LOCATED BTW FRAME 68 TO FRAME 70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM +Y160 LOCATED BTW FRAME 68 TO INSPECTION AND FOUND ADDTIONAL DAMAGE IAW NTM 51-90-00 FRAME 70 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG 53472040SDR CALA2022071801797Floorbeam · corrodedCORROSION FLOORBEAM -Y765 LOCATED BTW FR 67 AND FR 70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOOR BEAM -Y765 LOC. BTW FR 67 AND FR S/N 604311, DUE DATE JUL-30-2022. 70 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472040 TOOL USED DIGITAL CALIPER: P/N SDR CALA2022071801796Floorbeam · corrodedCORROSION FLOORBEAM +Y765 LOCATED BTW FR 67 AND FR 70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOORBEAM +Y765 LOC. BTW FR.67 AND FR.70 ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE IAW NTM 51-90-00 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG D53472040, TOOSDR CALA2022071801795Floorbeam · corrodedCORROSION FLOORBEAM +Y512 LOCATED BTW FRAME 64 TO FRAME 70 AT AFT GALLER AREA REMOVED AND REPLACED FLOORBEAM TY512 LOC BTW FR 64 TO FR 70 AREA AND NO FOUND ADDTIONAL DAMAGE IAW NTM 51-90-00 AT AFT GALLEY AREA IAW A320 SRM 51-72-11 AND DWG 53472094000 TOOL USESDR SWAA2022081829992Floor Panel · elongatedELONGATED HOLE FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2022-368380 / [01] REPLACED FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM-25-52-01-201-801 DWG 453A2610; SHEET 7; REV C. MATERIAL USED: GILL COATED 0.070; P/O: 2020 188432;[02] CERTIFIED WSDR SWAA2022081829993Floor Panel · elongatedELONGATED HOLE FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2022-368379 / [01] REPLACED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700MSRM 51-10-02 AND DWG 453A2610; SHEET 11; REV. C. SEE INDIVIDUAL SIGN OF BELOW.;[02] CORRECTED STEP 1. REPLACED FLOOR PSDR FDEA202207161742Floor Panel · crackedMAIN CABIN FLOOR PANEL 241FFF IS DAMAGED 3EA PLACES, STA 855-883, LBL9 TO RBL 9 REPAIRED MAIN CABIN FLOOR PANEL 241FFF IAW B767 SRM 53-00-50-2R, PARA. 4.C. AND 4.D., FIG. 201, SHT. 1.SDR SWAA2022071930046Floor Panel · crackedFWD CARGO BAY AFT FLOOR PANEL HAS MULTIPLE CRACKS THAT ARE OUT OF LIMITS. / [01] R+R FLOOR PANEL PER AMM 25-52-10.SDR FDEA202207161745Floor Panel · crackedMAIN CABIN FLOOR PANEL 242HFF IS DAMAGED 2EA PLACES, STA 888, RBL 78 REPAIRED MAIN CABIN FLOOR PANEL 242HFF IAW B767 SRM 53-00-50-2R, PARA. 4.C., FIG. 201, SHT 1SDR FDEA202207161744Floor Panel · crackedMAIN CABIN FLOOR PANEL 242GFF IS DAMAGED 4EA PLACES, STA 881-884, RBL 57-72 REPAIRED MAIN CABIN FLOOR PANEL 242GFF IAW B767 SRM 53-00-50-2R, PARA. 4.C., FIG. 201, SHT. 1SDR FDEA202207161743Floor Panel · crackedMAIN CABIN FLOOR PANEL 241WFF IS CRACKED 2EA PLACES, STA 1040, LBL 4 TO RBL 4 REPAIRED MAIN CABIN FLOOR PANEL 241WFF IAW B767 SRM 53-00-50-2R, PARA. 4.B., FIG. 201, SHT. 1SDR FDEA202207161741Floor Panel · crackedMAIN CABIN FLOOR PANEL 241ZFF IS DAMAGED 4EA PLACES, STA 1010-1018, LBL 66-72 REPAIRED MAIN CABIN FLOOR PANEL 241ZFF IAW B767 SRM 53-00-50-2R, PARA. 4.D., FIG. 201, SHT. 1.SDR DALA2022071504927Plate · corrodedAIRCRAFT 0664, CORROSION ON LH SIDE PLATE AT AFT CARGO COMPARTMENT FROM STA 1280-1283. CORRECTIVE ACTION: CORROSION LEVEL 2-AREA OUT OF LIMITS ON LH SIDE PLATE AT AFT CARGO COMPARTMENT FROM STA 1280-1283 WAS REPAIRED PER PER B757-200 SRM 51-70-13-0G. (2321011)SDR DALA2022071804944Plate · corroded(LOG 2321551) DURING INSPECTION FOUND CORROSION ON RH SIDE PLATE BTWN STA 727/STA 767 AND RBL= 21 AT AFT CARGO COMPARTMENT. SIDE PLATE BTWN STA 727/STA 767 AND RBL=21 AT AFT CARGO COMPARTMENT. WAS REPLACED PER B737-800, SRM 51-40-02-0G.SDR FDEA202207151735Floor Panel · damagedMAIN CABIN FLOOR PANEL 251MVF IS DAMAGED REPAIRED MAIN CABIN FLOOR PANEL IAW B757 SRM 53-00-50-2R FIG. 201 REPAIR 1.SDR CALA2022071501771Seat Track · corrodedCORROSION SEAT TRACK LOCATED FR21 Y-1292 IN PASSENGER CABIN REMOVED AND REPLACED SEAT TRACK Y-1292 AND FASTENER LOC. BTW 500-196-30, S/N: A21033544, DUE DATE; OCT 09 2022 ,DEPTH FR12 TO FR24 IN PASSENGER CABIN AND SPLICE (1EA) LOC. GAGES P/N; 20915A22, S/N 003SDR SWAA2022082229381Floor Panel · deterioratedFWD CARGO COMPARTMENT FLOOR PANEL 120AF DETERIORATED / [01] FABRICATED NEW FLOOR PANEL #120AF AT FWD CARGO COMPARTMENT IN REF AMM 25-52-01-201-801;[02] VERIFIED STEP 1SDR SWAA2022082229382Floor Panel · deterioratedFWD CARGO COMPARTMENT FLOOR PANEL 120CF DETERIORATED / [01] FABRICATED NEW FLOOR PANEL # 120CF AT FWD CARGO COMPARTMENT IN REF AMM 25-52-01--201-801;[02] VERIFIED STEP 1.SDR SWAA2022082229542Floor Panel · crackedAFT CARGO COMPARMTENT FLOOR PANEL 140AF CRACKED. / [01] FABRICATED AFT CARGO COMPARTMENT FLOOR PANEL 140 AF REF AMM 25-52-01-201-801;[02] VERIFIED STEP 1.SDR SWAA2022082229545Floor Panel · crackedAFT CARGO COMPARMTENT FLOOR PANEL 140BF CRACKED. / [01] FABRICATED NEW AFT CARGO FLOOR PANEL 140 BF PER REF. AMM 25-52-01-201-801; USING REMOVED FLOOR AS TEMPLATE;[02] VERIFIED STEP 1.SDR SWAA2022082229543Floor Panel · crackedAFT CARGO COMPARMTENT FLOOR PANEL 140DF CRACKED. / [01] FABRICATED NEW AFT CARGO FLOOR PANEL 140 DF; PER REF AMM 25-52-01-201-801;USING REMOVED FLOOR AS TEMPLATE;[02] VERIFIED STEP 1.SDR DALA2022071504930None · noneTHE F/A REPORTS THAT THE 1R DOOR GIRT BAR KEEPS SLIPPING OUT WHEN IN THE ARMED POSITION DURING FLIGHT. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REPLACED THE DOOR 1R RH GIRT BAR FITSDR DALA2022071504900None · none(LOG 2320279) DURING INSPECTION FOUND CORROSION ON FLOOR BEAM STA 947.5 RBL 5. FLOOR BEAM STA 947.5 RBL 5 WAS REPAIRED PER B-737-800 SRM 53-70-51-2R REPAIR 5.SDR CALA2022071501759Skin · damagedDURING A MAINTENANCE HMV-4 CHECK PRODUCTION REPORTED A MILLED DOUBLER ON THE FUSELAGE SKIN AT FR34/STR43 WHILE PERFORMING THE REQUIRED INSPECTION PER UAL EA 5300-02120 REV C OP 001. BETWEEN STGR44 AND STGR42HR PER PART-2 OF THE LATEST REVISION OF ECRA 5321-020SDR SWAA2022082229153Floor Panel · crackedFLIGHT COMPARTMENT PANEL 211CW FWD/UPPER CORNER IS CRACKED. / [01] REPAIRED DAMAGED AREA AT FLIGHT COMPARTMENT PANEL 211CW REF B737-700 SRM51-70-04-2R-13 PARAGRAPH 4. MATERIAL USED RESIN PO#:1753794.;[02] VERIFIED STEP 1SDR SWAA2022081828557Floor Panel · frayedAFT FLOOR PANEL 242VF UPPER SKIN FRAYED AT SEVERAL PLACES / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 6 TABLE 6.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F.<BR>DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>RSDR SWAA2022081828555Floor Panel · frayedAFT FLOOR PANEL 241ADF UPPER SKIN FRAYED AT SEVERAL PLACES / [01] IDENTIFIED AFT FLOOR PANEL 241ADF IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-1.<SDR DALA2022071504897None · none(LOG 2318005) DURING INSPECTION FOUND CORROSION ON RH SIDE PLATE BTW STA 420 TO STA 500C RBL 24. AT FWD CARGO COMPARTMENT. SIDE PLATE RH SIDE BTW STA 420 TO STA 500C RBL 24. AT FWD CARGO COMPARTMENT WAS REPLACE PER. B737-800, SRM 51-40-02-0G.SDR DALA2022071404885None · noneAIRCRAFT 0664, CORROSION ON STRINGER LBL 7.55 STA 1470 AT AFT CARGO COMPARTMENT. (C2) CORRECTIVE ACTION: SUMMARY OF NRC 00297-CORROSION LEVEL 2-STRINGER LBL 7.55 STA 1470 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM 53- 00-53-2R PROCEDURE 1. (2319396SDR SWAA2022082328040Floor Panel · frayedMAIN CABIN FLOOR PNL 241RF FIBERGLASS FRAYED ON TOP SKIN. / [01] MEASUREMENTS;[02] PREPARED FOR REPAIR DAMAGE AREA AT CABIN FLOOR PANEL #241RF AS PER BOEING737 SRM53-00-50-2R-0;[03] REPAIRED DAMAGE AREAS AT CABIN FLOOR PANEL 3241RF AS PER BOEING 737 SRM 53-00-SDR SWAA2022082328042Floor Panel · frayedMAIN CABIN FLOOR PNL 241LF FIBERGLASS FRAYED ON TOP SKIN / [01] MEASUREMENTS;[02] PREPARED DAMAGED AREA ON FLOOR PANEL #241LF FOR REPAIR PER B737 SRM 53-00-50-2R-1 PARAG 3.F;[03] VERIFIED STEP # 1 AND # 2;[04] REPAIRED FLOOR PANEL #241LF AT DAMAGED AREA PER B7SDR SWAA2022081828214Floor Panel · elongatedELONGATED HOLE FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2022-381266 / [01] FABRICATED AND REMPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW TO B737 -700 SRM 51-10-02 DRW 4531610 REV C SEE INDIVIDUAL SIGN OFFS BELOW;[02] FABRICATED AND REMPLACED FLOOR SDR DALA2022071504896None · none(LOG 2317793) DURING INSPECTION FOUND CORROSION ON LH SIDE PLATE BTWN STA 727/STA 847 AND LBL= 21 AT AFT CARGO COMPARTMENT. LH SIDE PLATE BTWN STA 727/ STA 847 AND LBL= 21 AT AFT CARGO COMPARTMENT WAS REPLACED PER B737-800 SRM 51-40-02-0G.SDR IPXA2022071284100Floor Panel · puncturedMDC FLOOR PANEL 242FK HAS PUNCTURE.REPAIRED MDC FLOOR PANEL 242FK NEEDED IAW EO:A300-5320-42722-FSDR DALA2022071304869None · noneSHIP 3229 CORROSION FLOOR BEAM -Y1292 FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2317807)SDR DALA2022071304868None · noneSHIP 3229 CORROSION WEB INTERNAL STRUCTURE FR 69 TO FR 70 AND STR 23L AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB PER A320 SRM 51-42-11, AND 51-72-11. (2317297)SDR DALA2022071304867None · noneSHIP 3229 CORROSION ANGLE WEB FLOOR STRUCTURE FR 69 TO FR 70 AND STR 23R AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED ANGLE WEB PER A320 SRM 51-72-11. (2317290)SDR DALA2022071304866None · noneSHIP 3229 CORROSION SHEAR PLATE FR 69 TO FR 70 AND STR 23R AT AFT GALLEY. CORRECTIVE ACTION: REPLACED SHEAR PLATE PER A320 SRM 51-72-11. (2317289)SDR DALA2022071304865None · noneSHIP 3229 CORROSION FLOOR BEAM BETWEEN Y 254 TO Y 160 FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2317282)SDR DALA2022071304864None · noneSHIP 3229 CORROSION FLOOR BEAM -Y1292 FR 20 TO FR 21 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11 AND 51-42-11. (2317272)SDR DALA2022071304863None · noneSHIP 3229 CORROSION FLOOR BEAM -Y765 FR 20 TO FR 21 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11 AND 51-42-11. (2317267)SDR SWAA2022080227734Floor Panel · crackedFWD CABIN WET AREA L/H O/B FWD LAV.FLOOR PANEL 221BF HAS 2EA CRACKS @ FWD EDGE INB MKD DOT / [01] RECEIVED NEW FLOOR PANEL 221BF PANEL INSTALLATION WILL BE ACCOMPLISHED ON WORK CARD TTG8Q00D9YWM;[02] VERIFIED 1;COMPLETESDR SWAA2022072227915Floor Panel · pulledCABIN FLOOR PANEL 242AF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED FLOOR PANEL 242AF FOUND WITHIN REPAIRABLE LIMITS OF SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED FLOOR PANEL 242AF FOR WET LAY-UP REPAIR IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-K);[SDR SWAA2022072227921Floor Panel · pulledCABIN FLOOR PANEL 231ZF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED FLOOR PANEL 231ZF FOUND WITHIN REPAIRABLE LIMITS OF SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED FLOOR PANEL 231ZF FOR WET LAY-UP REPAIR IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-K);[SDR SWAA2022072227920Floor Panel · pulledCABIN FLOOR PANEL 241CF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED FLOOR PANEL 241CF FOUND WITHIN REPAIRABLE LIMITS OF SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED FLOOR PANEL 241CF FOR WET LAY-UP IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEPS 3 (A-K);[03] VERSDR SWAA2022072227916Floor Panel · pulledCABIN FLOOR PANEL 241BF UPPER SURFACE HAS PULLED FIBERS / [01] EVALUATED FLOOR PANEL 241BF FOUND WITH IN REPAIRABLE LIMITS OF SRM 53-00-50-2R-1 REPAIR 1;[02] PREPPED FLOOR PANEL 241BF FOR WET LAY-UP REPAIR IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1 STEP 3 (A-K);[SDR SWAA2022072127917Floor Panel · pulledCABIN FLOOR PANEL 231YF UPPER SURFACE HAS PULLED 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 53-00-50-2R-1 STEP A; C; E-F.
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