JASC 5315
Service difficulty reports · 44,218
Reports filed under 5315 · Fuselage Main, Floor Beam, 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 = '5315' 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 = '5315' 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 SWAA2021021541359Floorbeam · crackedFLOOR SUPPORT CRACKED AT BS 540 BL0-RBL25 WL 208 / REMOVED; LOCATED; DRILLED AND INSTALLED A NEW BREAK ASSY AT BS540; BL0-RBL25 WL208 PER SRM 51-40-05-0G-0; REF:BOEING DWG: 143A0060SDR MASA20210201046Floorbeam · corrodedCORROSION ON FLOOR BEAM 27LBL BTW FS1020.00-1040.00 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: FLOOR BEAM 27LBL BTW FS1020.00-1040.00 WAS REPAIRED PER CRJ-900-SRM 53-00-41-201-001-A03. FIG 53-00-41-995-829.SDR FDEA202101120068Floorbeam · crackedFLOOR BEAM INTEGRATION SEGMENT IS CRACKED IN THE AFT RADIUS UNDER THE LBL 45 SEAT TRACK AT STA 580. COMPLIED WITH EA F-5310-T0358814 TITLE: FUSELAGE-MAINFRAME-FLOOR BEAM AT STA 580 AND LBL 45 CRACKED. REPAIR PER DRAWING SR 57-53-004.SDR SWIA202156614Floorbeam · corroded* FS333 FLOOR CROSSBEAM CORRODED AT APPROXIMATELY LBL20 (C-CHECK) RO 3/4/2021 REPAIRED FS333 FLOOR CROSS BEAM AT APPROXIMATELY LBL20 REF REO 690-53-21-1320 REV.-- DATED 2021-02-01 ALL STEPS COMPLETED. COMPLIED WITH 51-900-1002-SKY. SEE CONTINUE CARD FOR DESDR SWIA202156321Floorbeam · damagedFOUND THERE TO BE 1 EA ELONGATED HOLE ON THE RT PRESSURE FLOOR SILL AT FS 559 BETWEEN RBL 36 AND RBL 45. (C-CHECK) RO 2/17/2021. REPAIRED DAMAGE IAW REO 601R-53-41-2847 REV A DATED 2021-01-26. COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM M-337.SDR SWIA202156278Floorbeam · corrodedFOUND CORROSION ON FS280 CROSSBEAM R/H SIDE BETWEEN BL0 AND RBL9 (C-CHECK) RO 2/13/2021 INSTALLED NEW FS280 CROSSBEAM R/H SIDE P/N CC670-34094-2 REF CRJ 700 SRM 51-42-21-001-001-A01, CRJ 700 SRM 51-42-22-001-001-A01, CRJ 700 SRM 51-42-06-001-001-A01 AND DSDR IPXA2021020165141Floorbeam · crackedINSPECTION TYPE: 2C LOWER FWD CARGO FLOOR BEAM IS CRACKED AT STA 6-70, X=57.5 AND Z= -98. REPAIRED CRACKED FLOOR BEAM AT STA 6-70, X=57.5 AND Z= -98 IAW SRM 53-40-51 REPAIR 1 FIG 201. MAJORSDR N6WA2021011101Floorbeam · corroded280 BEAM CTR SPLICE IS CORRODED. R & R 280 CENTER SPLICE, ANGLE ASSEMBLY, IAW CRJ7 SRM 51-42-06 AND 51-42-21.SDR SWIA202156704Floorbeam · corroded*CORROSION ON SUPPORT BRACKET FOR A-BAY FLOORBOARD AFT OF FS280.00 (C-CHECK) RO 3/4/2021 REMOVED OUT OF LIMITS BRACKET AND INSTALLED NEW SUPPORT BRACKET FOR A-BAY FLOORBOARD AFT OF FS280 REF CRJ-900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-21-06-001-001-A0SDR SWAA2021020141445Cargo Track · corrodedCORROSION AFT CARGO FLOOR STRUCTURE TIE DOWN TRACK UPPER SURFACE WITH CORROSION SPOTS AT RBL-13.84 BETWEEN STA-787 TO 847. REMOVED AND REPLACED TIE DOWN TRACK SECTION FROM STA 755 TO 887 RBL 13.85 AS PER REF B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1 ASDR SWAA2021020141448Floorbeam · crackedAFT CARGO FLOOR STRUCTURE RAIL AT RBL-3 AND STA 727E BENT, AFT CARGO FLOOR STRUCTURE RAIL AT STA 727E RBL WAS FOUND CRACKED. PERFORMED FLOOR BEAM REPAIR AS PER B737-700 SRM 53-00-53-2R-4 REPAIR 4 FIG 201 BETWEEN STA 727E-STA 747 RBL 3.SDR JR2R20210110097Floorbeam · corrodedFLOOR BEAM AT RBL 10 AND FR 87 CORRODED.SDR JR2R20210110103Floorbeam · corrodedFLOOR BEAM LBL 9 AT FR 87 CORRODED.SDR SWIA202156703Floorbeam · corroded*CORROSION NOTED AT COCKPIT FLOOR SUPPPORT BRACKET COMMON TO CROSSBEAM AT FS280.00 (C-CHECK) RO 3/4/2021 COCKPIT FLOOR SUPPORT BRACKET COMMON TO CROSSBEAM AT FS280.00 EVALUATED OUT OF LIMITS AND REPLACED ON CAMP#22159588.SDR SWIA202156268Floorbeam · corroded**CORROSION NOTED AT FS280.00 COCKPIT FLOOR SUPPORT (C-CHECK) RO 2/13/2021 INSTALLED NEW FS280.00 COCKPIT FLOOR SUPPORT BETWEEN LBL9 AND RBL9 REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND DWG. NO. CC670-33052 REV. G. COMPLIED WSDR SWAA2021021540517Floorbeam · corroded***CORROSION*** ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS887 RBL20 TO LBL7 WL168. / PROCURE & REPLACE FLOOR SUPPORT IAW SRM 51-40-02-0G-0 & DWG 147A7500 REV.B AND SRM 51-10-02-0G-0 PARAG 9 59191U 13JAN21SDR SWAA2021051340468Floorbeam · corroded***CORROSION*** ON FLOOR SUPPORT LOWER SIDE OF AFT FLANGE AT BS 947.5+3; RBL 46- RBL 48; WL 207 / CORROSION ON FLOOR SUPPORT BS947.5+3 RBL46-RBL48; WL207 REMOVED IN A 1' X 1' X .015' ORIGINAL THICKNESS .072' FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1 REMOSDR SWAA2021051340467Floorbeam · corroded***CORROSION*** ON FLOOR SUPPORT LOWER SIDE OF AFT FLANGE AT BS 947.5+3; RBL 32- RBL 39; WL 207 / CORROSION ON FLOOR SUPPORT BS947.5+3'; RBL32-RBL39 WL207 FOUND TO BE OUT OF LIMITS 1' X 2' X .018' ORIGINAL THICKNESS .071' PER SRM 53-70-51-1A-1; REMOVED AND REPSDR SWIA202156745Floorbeam · corrodedFLOOR SILL, F.S. 280 TO SERVICE DOOR CUTOUT APPEARS CORRODED. (C-CHECK) RO 3/8/2021 REMOVED CORROSION AT FLOOR SILL AT FS 280 TO SERVICE DOOR CUTOUT REF CRJ 700 SRM 51-21-06-001-001-A01. 100% MATERIAL LOSS OUT OF LIMITS REF CRJ 700 SRM 53-00-45-201-001-A0SDR SWIA202156047Floorbeam · corrodedCOCKPIT AFT FLOOR SUPPORT (ATTACHED TO FWD SIDE OF 280.00) CORRODED. (C-CHECK) RO 2/6/2021 REPLACED COCKPIT AFT FLOOR SUPPORT ASSY ANGLE WITH NEW P/N CC670-34095-1SB ON FWD SIDE OF FS 280.00 REF CRJ 700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 ANSDR IPXA2021020265226Floorbeam · crackedINSPECTION TYPE:2CLOWER FWD. CARGO FLOOR BEAM IS CRACKED AT STA. 6-70 AND X= -57.5.REPAIRED CRACKED FLOOR BEAM AT STA. 6-70 AND X= -57.5 IAW VT-SAA EA 011-5310-01-A8835 REV. I/R AND UPS EO MD11-5340-79191-A. (MAJOR)SDR A6WA202101157546Floorbeam · corrodedFLOOR SUPPORT STRUCTURES AT FS 599, LBL 28 TO LBL 42, AND RBL 28 TO RBL 42 HAND AND RT HAND BLENDED OUT OF LIMITS. AIRCRAFT REMOVED FROM SERVICE. REMOVED RT HAND AND LT HAND FLOOR SUPPORT AT FS 599, LBL 28 TO LBL 42, AND RBL 28 TO RBL 42, IAW CRJ 200 SRM 51 SDR SWAA2021020240618Floorbeam · corroded***CORROSION*** ON FLOOR BEAM UPPER SURFACE AT B.S. 986.5; W.L. 208.1; L.B.L. 27-42. / REPAIRED CORROSION ON THE FLOOR BEAM UPPER SURFACE OF BS 986.5; WL 208.1. WL 27-42. IAW EA 1-A53-8241 REV 3SDR SWAA2021020240619Floorbeam · corroded***CORROSION*** ON FLOOR BEAM UPPER SURFACE AT B.S. 986.5; W.L. 208.1; R.B.L. 30-43. / REPAIRED CORROSION ON FLOOR BEAM UPPER SURFACE AT BS 986.5 WL 208.1; RBL 30-43 IAW EA 1-A53-8241 REV 3.SDR DALA2021011500257Floorbeam · corrodedDURING INITIAL INSPECTION MAINTENANCE CORROSION ON FLOOR STRUCTURE RBL 30.0 AND RBL 64.0 AND STA 1640 AT PASSENGER CABIN. BLENDED PER SRM 53-00-51.SDR SWAA2021020239726Floorbeam · corroded***CORROSION*** ON B.S. 328 FLOOR BEAM; UPPER SURFACE; W.L. 208.1; R.B.L. 47. / FLOOR BEAM AT BS 329; UPPER SURFACE; W.L. 208.1; RBL 47 REPAIRED IAW ATS ER 21-01022; REV IR; DATED 18-JAN-2021 AND PER EA NO: 21-153-00121 REV IR. 55981U 19JAN21SDR SWAA2021020239733Floorbeam · crackedFLOOR SUPPORT CRACKED AT BS 663 RBL 63 WL 207 / REMOVED & REPLACED FLOOR SUPPORT AT BS 663 RBL 63 WL 207 P/N 144A5702-6 IAW DRW 144A3701 & SRM 51-40-02-0G-0SDR SWAA2021020239734Floorbeam · crackedFLOOR SUPPORT AT BS 540 BL 0 TO RBL 23 WL 207 CRACKED / REMOVED AND REPLACED FLOOR SUPPORT AT BS 540 BL 0 TO RBL 23 WL 207 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG #143A0060SDR SWIA202156743Floorbeam · crackedSUSPECT CRACK IN THE RADIUS OF THE COCKPIT FLOORBEAM AT LBL12 ON THE FWD SIDE OF THE FS280 BULKHEAD (C-CHECK) RO 3/8/2021 REPAIREDCOCKPIT FLOORBEAM AT LBL 12 FWD OF FS 280 REF CRJ-700 SRM 53-11-43-201-003-A01 REV 38 DATED JUL 25/2020 & CRJ-700 SRM 51-42-SDR REXA2021012200035Angle · corrodedFS 280 J-ANGLE CORRODED. REMOVED AND REPLACED FS 280 J-ANGLE, IAW CRJ 900 SRM'S 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.SDR IPXA2021013065069Floorbeam · corrodedINSPECTION TYPE: C AFT CARGO COMPT FLOOR BEAM LOWER SURFACE IS CORRODED AT FR65 Y805. REPAIRED IAW SRM 53-10-15 FIG 208.SDR A6WA202101257566Angle · crackedFLOOR CROSS MEMBER GAPPED DUE TO FASTENER SWOLLEN BETWEEN STRUCTURES AT FUSELAGE STATION 559.00, LBL 8. AIRCRAFT REMOVED FROM SERVICE. UPON EVALUATION OF DAMAGE OF CROSS MEMBER AT FUSELAGE STATION 559.00, LBL 8. DAMAGE FOUND TO MEASURE 1.78 L X 0.620 W X 0.0SDR AALA202101119031Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON CABIN FLOOR BEAM AT FR 66 AND Y765. REPLACED FLOOR BEAM, PER SRM 51-72-11.SDR AALA202101119030Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON CABIN FLOOR BEAM AT FR 68 AND -Y765. REPLACED FLOOR BEAM, PER SRM 51-42-11.SDR AALA202101119022Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR BEAM AT FR 66 AND -Y1162.5. REPLACED FLOOR BEAM, PER SRM 51-72-11.SDR AALA202101089004Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CABIN FLOOR SUPPORT BEAM AT FR 66 AND +Y765. REPLACED FLOOR SUPPORT BEAM, PER SRM 51-72-11.SDR DALA2020123104348Floorbeam · damagedMISSING MATERIAL ON FLOOR BEAM +Y254 AT LEVEL FRAME 25 IN PASSENGER CABIN. CORRECTIVE ACTION: PERFORMED REPAIR, PER A320 SRM 53-21-14-300-001. OK FOR SERVICE.SDR MASA20201230162Floorbeam · corrodedFS 280 FLOOR BOARD SUPPORT ANGLE CORRODED. R & R FS 280 FLOOR SUPPORT ANGLE PN-CC670-34256-3, IAW SRM-51-42-06-001-001-A01 & 51-42-21-001-001-A01.SDR A6WA202012297521Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 439.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE POSITIONS AT FS 439.00, LBL 42. REWORKED DIMENSIONS 2.2 L X 1.8 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMSDR A6WA202001137530Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 461.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 461.00, LBL 42. REWORKED DIMENSIONS 0.6 L X 0.3 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMED HFEC INSDR A6WA202001137526Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 409.00 +128 +11, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 409.00 +128 +11, LBL 42. REWORKED DIMENSIONS 0.720 L X 0.420 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-SDR A6WA202001137535Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS 544.00, RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 544.00, RBL 42. REWORKED DIMENSIONS 1.1 L X 0.7 W, REF REO 601R-53-41-666 REV (C) DATED 2012-11-06. PERFORMED HFEC PRSDR A6WA202101137536Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 473.15 TO FS 473.15 +5 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 473.15 TO FS 473.15 + 5 AND LBL 36 TO LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.070'' L X SDR A6WA202001137537Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS. 484.00, LBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 484.00, LBL 42. REWORKED DIMENSIONS P(1) 1.260 L X 0.640 W, P(2) 1.220 L X 0.710 W, REF REO 601R-53-41-666 REV (C) DASDR A6WA202101137533Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 461.00 + 9 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 461.00 + 9 AND LBL 36 TO LBL 42. BY BLENDING. BLENDED AREA MEASURED (P1) 2.330''L X 0.950''W (P2) 1.160''L X 0SDR A6WA202101137529Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 449.85 AND LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 449.85 AND LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 2.780''L X 1.530''W (P2) 0.920''L X 0.340''W TOOL USED DIGITAL CSDR A6WA202001137534Floorbeam · corrodedPRESSURE FLOOR ANGLE AT FS. 513.00 TO FS. 513.00 + 5, RBL 36 TO RBL 42, HAS CORROSION. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE AT FS 513.00 TO FS 513.00 +5, RBL 36 TO RBL 42. REWORKED DIMENSIONS P(1) 3.0 L X 1.0 W, P(2) 1.SDR A6WA202101137540Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 439.00 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 439.00 RBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.00'' L X 0.720'' W TOOL USED DIGITAL CALIPER S/N 0036003 CAL DUE 04/03/SDR A6WA202101137539Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 484.00 RBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 484.00 RBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.250'' L X 0.800'' W TOOL USED DIGITAL CALIPER S/N 0036003 CAL DUE 04/03SDR A6WA202101137531Floorbeam · corrodedCORROSION ON PRESSURE FLOOR ANGLE FS 513.00 TO FS 513.00 +5 AND LBL 36 TO LBL 42. AIRCRAFT REMOVED FROM SERVICE. REMOVED CORROSION FROM PRESSURE FLOOR ANGLE FS 513.00 TO FS 513.00 +5 AND LBL 36 TO LBL 42 BY BLENDING. BLENDED AREA MEASURED (P1) 1.180'' L X 0
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