JASC 5315
Service difficulty reports · 44,220
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 DALA1031345523Floorbeam · corrodedDURING L-CHECK FOUND CORROSION ON FLOORBEAM UPPER CAP AT BS 1640 RBL 53 TO BL 0. REPAIRED PER ERA 486850-14 REV 0.SDR USAA2010120892931Floorbeam · corrodedSAL - MAJOR REPAIR - S5 - LEVEL 2 GALVANIC CORROSION ON RAIL SEAT BEAM BETWEEN FR64 TO FR66, Y1292. REPLACED RAIL SEAT BEAM BETWEEN FR64 TO FR66, Y1292 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING 53472000.SDR USAA2010120892930Floorbeam · corrodedSAL - MAJOR REPAIR - S5 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR 66 +5 INCHES TO FR67 +15 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR 66 +5 INCHES TO FR67 +15 INCHES, Y1292 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING 53472000.SDR USAA2010120292770Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM RAIL BETWEEN FR64 TO FR66, -Y1292. REPLACED FLOORBEAM RAIL BETWEEN FR64 TO FR66, -Y1292 IAW A320 SRM 51-72-11 AIRBUS DRAWING D53472000.SDR USAA2010120192742Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2010120192741Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAWA320 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2010120192740Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR68 +1 INCH, Y1292. REPLACED FLOORBEAM AT FR68 +1 INCH, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2010120192739Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y765. REPLACED FLOORBEAM AT FR20, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110920.SDR USAA2010120192738Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y254. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y254 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53111462.SDR USAA2010120192737Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR16 TO FR23, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR23, Y254 IAW A320 SRM 51-72-11.SDR DALA1034325533Floorbeam · corrodedDURING M-CHECK FOUND RT NLG W/W TUNNEL, STA 365, LBL 24 TO RBL 24, FLOORBEAM HAS CORROSION. FABRICATED REPLACEMENT CHORD, 02 EA REPAIR ANGLES, AND 02 EA REPAIR STRAPS, TO FLOORBEAM 70 IAW SRM 53-00-51, REPAIR 3, PAGE 203, FIG 201. TREATED AND PRIMED REPLACEMESDR V0XR413Y111210014Floor Support · corrodedFS 280, FLOOR SUPPORT CHANNEL BETWEEN LBL-9 AND RBL-9 CORRODED BEYOND REPAIR. FABRICATED FLOOR SUPPORT CHANNEL IAW SRM 53-11-10.SDR V0XR413Y111210002Floorbeam · corroded(V0XR) STA 280, FLOORBEAM CORRODED BEYOND REPAIR. R & R STA 280 FLOORBEAM IAW REO 670-53-11-047, REV E, W/C 1042.SDR ASOA201001776Floorbeam · crackedFLOORBEAM ANGLE AT FS 280 RBL 9 IS CRACKED. R & R ANGLE FLOORBEAM IAW SRM 51-40-06 AND 51-42-21. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.SDR SWAA106914Floorbeam · crackedDURING SCHEDULED 18Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, RBL 24. REPAIRED BEAM PER EA.SDR GTIA1000151Floorbeam · corrodedUPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA BETWEEN +Y55 AND +Y74 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP AT UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA 2884 BETWEEN +Y55 AND +Y74 DUE TO CORROSION IAW SRM 51-72-11, PAR 4 AND 6.SDR GTIA1000146Floorbeam · corrodedUPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA 2884 BETWEEN +Y13 AND -Y13 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP AT UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA 2884 BETWEEN +Y13 AND -Y13 IAW SRM 51-72-11 PAR 4 AND 6 DUE TO CORROSIOSDR GTIA1000145Floorbeam · corrodedUPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA 2884 BETWEEN -Y20 AND -Y44 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP AT UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA 2882 BETWEEN -Y20 AND -Y44 DUE TO CORROSION IAW 51-72-11 PAR 4 AND 6.SDR GTIA1000144Floorbeam · corrodedUPPER FUSELAGE CABIN AFT ENTRANCE AREA STA 2884 BETWEEN -Y49 AND -Y73 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP AT UPPER FUSELAGE PAX CABIN ENTRANCE AFT AREA STA 2884 BETWEEN -Y49 AND -Y73 DUE TO CORROSION IAW SRM 51-72-11, PAR 4 AND 6.SDR GTIA1000143Floorbeam · corrodedUPPER FUSELAGE PAX CABIN ENTRANCE AREA STA 2884 BETWEEN -Y80 AND -Y112 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP AT UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA 2884 BETWEEN -Y80 AND -Y112 DUE TO CORROSION IAW A319 SRM 51-72-11 PAR 4 ASDR GTIA1000140Floorbeam · corrodedUPPER FUSELAGE PAX CABIN ENTRANCE AREA STA 2884 BETWEEN +Y80 AND +Y112 FLOOR SUPPORT STRAP WITH CORROSION. REPLACED FLOOR SUPPORT STRAP AT UPPER FUSELAGE PAX CABIN AFT ENTRANCE AREA STA 2884 BETWEEN +Y80 AND +Y112 DUE TO CORROSION IAW SRM 51-72-11 PAR 4 AND 6SDR USAA2010112292637Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, -Y1170. REPLACED FLOORBEAM AT FR68, -Y1170 IAW A320 SRM 51-42-11.SDR USAA2010112292636Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR67, -Y1250. REPLACED FLOORBEAM AT FR67, -Y1250 IAW A320 SRM 51-42-11.SDR USAA2010112292635Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y1297. REPLACED FLOORBEAM AT FR66, -Y1297 IAW A320 SRM 51-42-11.SDR USAA2010112292634Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR67, Y1250. REPLACED FLOORBEAM AT FR67, Y1250 IAW A320 SRM 51-20-11.SDR FOTR2016911107Floorbeam · corrodedAFT CARGO BAY FLOORBEAM BS 1183 IS CORRODED AT LBL 16- RBL 3. REPAIRED ON NR 11107 FASI W/O 20169.SDR USAA2010121092974Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON SUPPORT FLOOR BEAM BETWEEN FR19 + 7 INCHES TO FR20, -Y1292. REPLACED SUPPORT FLOOR BEAM BETWEEN FR19 + 7 INCHES TO FR20, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112089.SDR USAA2010121092973Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOORBEAM BETWEEN FR18 + 5 INCHES TO FR20, -Y765. REPLACED SUPPORT FLOOR BEAM BETWEEN FR18 + 5 INCHES TO FR20, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112089.SDR USAA2010121092971Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR67 + 19 INCHES, Y1155. REPLACED FLOORBEAM AT FR67 + 19 INCHES, Y1155 IAW A320 SRM 51-72-11.SDR UHLA2010110900242Floorbeam · corrodedLEVEL 2 CORROSION FLOORBEAM FR14 AT RIGHT END IN FRONT OF FORWARD SERVICE DOOR. INSTALLED DOUBLER IAW EMB ETD 2010-170/10545.SDR ASOA201001743Floorbeam · corrodedLBL 27, FLOORBEAM CAP IS CORRODED AROUND NUTPLATES AT FS 605.00. BLENDED CORROSION ON FLOORBEAM & FOUND TO BE OUT OF LIMITS IAW SRM 53-61-43, 53-00-00 FIG 101. REMOVED FLOORBEAM CAP IAW SRM 51-42-06, 51-42-21. LOCATED AND DRILLED FLOORBEAM CAP IAW REO 601R-SDR SWAA106895Floorbeam · crackedDURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 665.75, LBL 24.5. REPAIRED CHORD PER EA.SDR DALA1030965532Floorbeam · corrodedDURING M-CHECK FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 377 LBL 60. REPAIRED PER SRM 53-00-51 FIGURE 201, SRM 51-40-05, SRM 51-20-01 & SRM 51-40-02.SDR AALA20101202TUL09Floorbeam · corrodedFLOORBEAM CORRODED STATION 927 RIGHT BUTTLINES 50 TO 53 ON TOP SURFACE. ACCOMPLISHED T-CAP REPAIR PER EA B737-53-014129.SDR AALA20101202TUL10Floorbeam · corrodedFLOORBEAM STATION 947 CORRODED AT RIGHT BUTTLINE 52 TOP SURFACE. ACCOMPLISHED T-CAP REPAIR PER SRM 53-70-51-2R 5.SDR SIMA201031502Floorbeam · corrodedDURING MAINTENANCE BASE VISIT FOUND THE RIGHT AND LEFT PORTION OF BEAM 280 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT AND LEFT BEAM 280 IAW CRJ 700 SRM 51-42-06 AND 51-42-21 AND AE EO CR-53MR-219. THE AIRCRAFT WAS RETURNSDR SWAA106862Floorbeam · crackedDURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708.5, LBL 24.5. REPAIRED BEAM PER EA.SDR SWAA106835Floorbeam · brokenDURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM UPPER FLANGE BROKEN AT BS 312, RBL 21. REPAIRED BEAM PER SRM.SDR SWAA106827Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER ER AND EA.SDR U2RA227DHN036Floorbeam · corrodedMAIN PASSENGER CABIN-FLOORBEAM, STA 345 TOP HAT SECTION HAS CORROSION BETWEEN LBL 8-16 AROUND FASTENER HOLES.SDR FDEA201011084284Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD HAS CORROSION BS 345 BLENDED UPPER CHORD STA 345 IAW SRM 51-10-02, ORIGINAL MATERIAL .125 AFTER REWORK .106 OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. EXCEEDS MAX MAT LOSS OF 10 PERCENT OF ORIGINAL MASDR USAA2010112392648Floorbeam · corrodedCWF - C2 - MAJOR REPAIR - CORROSION ON AUXILIARY FLOOR BEAM AT FR76, -Y1447.8. REPLACED AUXILIARY FLOORBEAM AT FR76, -Y1447.8 IAW A330 SRM 51-42-11 & 53-41-14.SDR SWIA201025145Floorbeam · crackedFS 280 FLOORBEAM CRACKED. (C-CHECK) REPAIR PER REO.SDR DALA1030705523Floorbeam · corrodedDURING L-CHECK FOUND CORROSION ON MAIN CABIN FLOORBEAM UPPER CAP UNDER FLOOR PANEL 104C AND 107A FROM BL 0 TO RBL 53. REPAIRED PER SRM 53-60-51 DETAIL 111 PAGE 7, DWG 148N216, SRM 51-40-02 PAGE 7.SDR C8GA2010000072Floorbeam · corrodedDURING HEAVY MX INSP, IT WAS NOTED THAT THE FLOORBEAM FLANGE AT STA 1110 LBL 64. REMOVED CORROSION AND FABRICATED REPAIR ANGLES FROM 7075 T6, .090" DIM 13.5" X 4", 10.5" X 4" AND 4" X 1" FILLER INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SSDR C8GA2010000066Floorbeam · corrodedDURING HEAVY MX IT WAS NOTED THAT THE MAIN CARGO FLOORBEAM IS CORRODED AT STA 1110 LBL 35. CORROSION WAS REMOVED, FABRICATED DOUBLER FROM 7075 T6 .090", FILLER FROM 7075 T6 .125. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000065Floorbeam · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STAT 1010, LBL 10 IS CORRODED. CUT OUT DAMAGE, FABRICATED REPAIR PARTS FROM 7075 T6 .063" DIM 18" X 3", STRAP FROM 7075 T6 .100" DIM. 18" X 2" FILLER FROM BAC1505-100797 DIM. 7.25" X 2.25" AND INSTSDR C8GA2010000064Floorbeam · corrodedDURING HEAVY MX INSP IT WAS NOTED THAT THE AFT CARGO FLOORBEAM STA 1030, RBL 20 IS CORRODED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR ASOA201001725Floorbeam · corrodedUPON REMOVAL OF RT 280 CROSSBEAM FOUND RT LOWER WEB TO BE CORRODED BEYOND REPAIRABLE LIMITS. REMOVED WEB IAW SRM 51-42-06-001-001-A01. INSTALLED WEB IAW SRM 53-11-10-99-805.SDR UALA2010110504122Floorbeam · corrodedBS 324 FLOORBEAM HAS CORROSION ON TEE AT RBL 58. MATERIAL REMAINING AFTER BLENDOUT EXCEEDS LIMITS OF SRM. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED TEE AND FABRICATED A REPLACEMENT T-CHORD AND INSTALLED PER PEMCO EA PD 57-53-052 AND UAL EVA 80278 ON NON ROU
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