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 REXA201100300Floorbeam · corrodedLBL 27 FLOORBEAM HAS CORROSION AROUND NUT PLATE HOLES BETWEEN FS 621 AND FS 574. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.SDR SWIA201127475Floorbeam · corrodedFLOORBEAM CORRODED AT OUTBOARD END AND WEB SECTION FS 349 RBL 36. (C-CHECK) REPAIRED PER SRM.SDR MALA110129Floorbeam · corroded900-53-140-509, RT SIDE FS 280 CROSSBEAM IS CORRODED BEYOND ALLOWABLE LIMITS. REPLACED RT FS 280 CROSSBEAM IAW REO 690-53-11-032 AND SRM 51-42-21 AND SRM 51-42-22.SDR MALA110128Floorbeam · corroded900-53-140-509, LT SIDE FS 280 CORRODED IN VARIOUS SPOTS ON THE TOP AFT EDGE. REPLACED LEFT FS 280 CROSSBEAM IAW REO 690-53-11-032 AND SRM 51-42-21 AND SRM 51-42-22.SDR ASOA201100985Floorbeam · corrodedRIGHT FS 349 FLOORBEAM CORRODED ON OTBD END AT SERVICE DOOR ENTRANCE. REPAIRED IAW REO 601R-53-21-1286.SDR COMA2011051770018Floorbeam · corrodedFS 280.00 CROSSBEAM IS CORRODED BEYOND LIMITS. REPLACED FLOORBEAM IAW SRM 51-42-06, 51-42-13 AND 51-42-21.SDR U2RA486DHN030Floor Support · corrodedMAIN PASSENGER CABIN FLOOR SUPPORT BETWEEN BS 1681.8 - 1701 AT RBL 52 CORRODED AT FASTENER HOLE.SDR U2RA486DHN031Floorbeam · corrodedFLOORBEAM STA 1701, RBL 24 CORROED ON UPPER FLANGE.SDR CALA2011051600366Floorbeam · corrodedBS 325 LBL 26 TO 55 FLOORBEAM CORRODED. REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201. HFEC NO CRACK FOUND.SDR DALA1134169866Floor Support · corrodedMAIN CABIN STA 237-302 BL0 FLOOR SUPPORT HAS CORROSION REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-30-05. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1.SDR A6WA201140539Floorbeam · corrodedFS 349 FRAME CAP CORRODED OTBD OF RBL 27 AT LIGHTING PROTECTION PANEL CLIP. FLOOR SUPPORT ANGLE DETERMINED TO BE OUT OF LIMITS, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW SRM 51-11-20, 51-24-16, 51-42-06.SDR DALA1138560627Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER SURFACE CORRODED STA 680 LBL 24 RBL 24. REPAIRED DURING HMV AT SAA ON N/R CARD 187261.SDR DALA1138550627Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED STA 760 LBL 3 TO LBL 22. REPAIRED DURING HMV AT SAA ON N/R CARD 187266.SDR SWAA113389Floorbeam · crackedDURING SCHEDULED 26Y CHECK FOUND, CRACK AT RBL 24.8 LONGITUDINAL FLOORBEAM UPPER CHORD BS 727B. REPAIRED CHORD PER ER.SDR SWAA113384Floorbeam · crackedDURING SCHEDULED OTS CHECK FOUND, CRACK ON LONGITUDINAL FLOORBEAM, AROUND FASTENER, LOCATED UPPER CHORD AFT END AT BS 727B AND LBL 24.8. REPAIRED BEAM PER EA.SDR SWAA113358AFloorbeam · crackedDURING SCHEDULED 24Y CHECK FOUND, CRACKED LONGITUDINAL FLOORBEAM UPPER CHORD AFT END AROUND OF FASTENER BS 727B OF LBL 24.8. REPAIRED CHORD IAW EA.SDR A6WA201140553Floorbeam · crackedFLOORBEAM ANGLE IS CRACKED AT FS 409.00+112 AND LBL 27.0. R & R BRACKET AT FS 409.112, LBL 27.0 INBD SIDE IAW SRM 51-42-06.SDR UALA2011051302371Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED STA 310, RBL 37 TO RBL 41. AFTER CORROSION REMOVAL FOUND T-CHORD TO BE OUT OF LIMITS PER SRM. A PERMANENT REPAIR WAS EXECUTED PER INSTRUCTIONS ON PEMCO PD57-53-121 WITHOUT DEVIATION AND APPROVED BY FAA 8100-9 DATED MAY 6 2011.SDR UALA2011051302370Floorbeam · corrodedMAIN CABIN FLOOR BEAM CORRODED STA 324 RBL 37 TO RBL 60. MAJOR REPAIR PER INSTRUCTIONS ON EA PD 57-53-117 AND UA EVA 80825 WITHOUT DEVIATION.SDR FDEA201105121831Floorbeam · corrodedSTA. 377 FLOORBEAM CORRODED BL 24 - 45 L. REMOVED CORROSION IAW SRM 51-10-02. AREA OUT OF LIMITS IAW SRM 53-00-51 FIGURE 101 DETAIL III. ORIG. MAT. .125 AFTER REWORK .107 MAT. LOSS EXCEED MAX. ALLOWED. REMOVED FLOORBEAM IAW SRM 51-40-02. FABRICATED NEW FLOOSDR SWAA113339AFloorbeam · corrodedDURING SCHEDULED 20Y CHECK FOUND, FLOOR BEAM CORRODED AT LOWER FLANGE LOCATED ON BS 986.5 AND BETWEEN RBL 27 TO RBL 46.5 UNDER FLOOR OF AFT GALLEY. R&R "T" CHORD IAW SRM.SDR SWAA113337AFloorbeam · crackedDURING SCHEDULED 20Y CHECK FOUND, CRACKED ON LONGITUDINAL FLOORBEAM UPPER CHORD AFT END AROUND FASTENER LOCATED AT RBL 45.5 AND BS 727B. REPAIRED BEAM IAW EA.SDR SWAA113336AFloorbeam · crackedDURING SCHEDULED 20Y CHECK FOUND, CRACKED ON LONGITUDINAL FLOORBEAM UPPER CHORD AFT END AROUND FASTENER HOLE LOCATED AT RBL 24.5 AND BS 727B IN PAX CABIN. REPAIRED BEAM PER EA.SDR USAA2011053100047Floorbeam · corrodedPIT - S5 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR 66, BL -Y1732. REPLACED FLOORBEAM AT FR 66, BL -Y1732 IAW A320 SRM51-72-00 AND AIRBUS DRAWING D53427250.SDR SWAA113680Floorbeam · crackedDURING SCHEDULED 26Y CHECK FOUND, LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM PER ER.SDR AALA20110513AFW05Floorbeam · corrodedCORROSION WAS FOUND AT STATION 325 FLOORBEAM UPPER CAP HORIZONTAL FLANGE UPPER SURFACE AT RIGHT BUTTLINE 41. REMOVED CORROSION AND ACCOMPLISHED DOUBLER REPAIR EA B767-53-016297.SDR COEA2011051104912Floorbeam · corrodedWO 101935 NR 100043 HEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FLOORBEAM 13 HAS AREAS OF BARE METAL & CORROSION BETWEEN STRINGERS 14L & 14R. (DEPTH .012"). REPAIR PER STRUCTURAL REPAIR INSTRUCTIONS & SRAS FROM ATR.SDR EE4Y20110286Floorbeam · corrodedPAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA BETWEEN FR68 AND FR69 -Y52 FLOORBEAM WITH CORROSION. NOTE: THE BEAM CORROSION REQUIRES A MAJOR REPAIR.SDR EE4Y20110285Floorbeam · corrodedPAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA BETWEEN FR67 AND FR68 -Y52 FLOORBEAM WITH CORROSION. NOTE: THE FLOORBEAM CORROSION REQUIRES A MAJOR REPAIR.SDR EE4Y20110284Floorbeam · corrodedPAX CABIN, UPPER REAR FUSELAGE, AFT SERVICE AREA FR66+3" -Y52 FLOORBEAM WITH CORROSION. NOTE: THE BEAM CORROSION REQUIRES A MAJOR REPAIR.SDR EE4Y20110283Floorbeam · corrodedPAX CABIN, UPPER REAR FUSELAGE, RT AFT PASSENGER DOOR LOWER SILL STA 3848 -Y59 FR66 FLOORBEAM WITH CORROSION. NOTE: THE FLOORBEAM CORROSION REQUIRES A MAJOR REPAIR IAW MM INSTRUCTIONS.SDR QXEA2011051300332Floorbeam · corrodedINTERNAL FUSELAGE UNDERFLOOR AT STA 783.102 FLOORBOARD ANGLE GOING FROM STRINGER 25 LT TO 25 RT HAS UPPER SURFACE CORROSION. REMOVED CORROSION REF SRM 51-21-00-00-02. FOUND TO BE WITH IN LIMITS IAW RD 8/4-53-3685. COMPLIED WITH HORIZON TASK CARDS RD 8/4-53-SDR COEA2011051001912Floorbeam · crackedWO 101935 NR 100044 HEAVY CK COE / MAJOR REPAIR: RT LONGITUDINAL FLOORBEAM AT FWD SIDE OF FLOORBEAM 18 IS CRACKED. CUT OUT CRACKED SECTION OF LONGITUDINAL FLOORBEAM BETWEEN FR 17 & 18. FABRICATED AND INSTALLED FLOORBEAM PER EO.SDR DALA1135339880Floorbeam · corrodedFLOORBEAM UPPER CHORD HAS FRETTING WEAR ON REPAIR, STA 294, BETWEEN BL-0 AND RBL-22. REMOVED 2 SHIMS ON FLOORBEAM UPPER CHORD IAW SRM 51-30-5. FABRICATED 2 SHIMS, IAW SRM 53-05 FIG 20, PG 98, PRIMED IAW SRM 51-10-3, PG 31. INSTALLED 2 SHIMS, FLOORBEAM UPPERSDR DALA1135109880Floorbeam · corrodedFLOOR SUPPORT ANGLE HAS LIGHT CORROSION STA 200 BETWEEN RBL 22 TO RBL 44 RL017. BLENDED OUT CORROSION OUT OF LIMITS, IAW SRM 53-01, FIG 1. REMOVED SUPPORT ANGLE IAW SRM 51-30-5, PG 1. REPLACED WITH NEW SUPPORT ANGLE IAW DC9 DWG S2652479, LOCATED AND DRILLEDSDR DALA1135099880Floorbeam · corrodedCABIN FLOOR SUPPORT ANGLE HAS CORROSION BS 200 BETWEEN RBL 22 AND BL 0 RL018. BLENDED OUT CORROSION MAIN CABIN FLOOR SUPPORT ANGLE IAW SRM 51-10-3 PARA 26, FOUND OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED AND REPLACED SUPPORT ANGLE DWGS2652479 BATCH 000203SDR DALA1134919880Floorbeam · corrodedCABIN FLOORBEAM ANGLE HAS CORROSION STA 237 BETWEEN BL-0AND LBL-22 BLENDED CORROSION OUT OF LIMITS PER SRM 53-01, FIG 1, SHEET 3, FORMED NEW FLOORBEAM PER SRM 53-01-2, TREATED AND PRIMED PER SRM 51-10-3, PARA 14 AND 21, REMOVED AND INSTALLED NEW FLOORBEAM PER SDR ASOA201100942Floorbeam · crackedLEFT TEE BRACKET FOUND CRACKED LBL 9 AND FS 280. R & R LT TEE BRACKET IAW SRM 51-42-21-001-001 AND 51-42-22-001-001. MINOR REPAIR.SDR AALA20110509TUL02Floorbeam · corrodedSTATION 365 RIGHT BUTTLINE 62 CORROSION ON FRAME. INSTALLED UPPER CHORD T-ANGLE PER SRM 53-00-51-2, R 3 AND BOEING DWG LOR5L53005.SDR DALA1132959866Attach Bracket · damagedMAIN CABIN STA 218 RBL 46 HAS DRILL START IN FLOORBEAM ATTACH BRACKET. REMOVED FLOORBEAM ATTACH BRACKET FROM MAIN CABIN STA 218 RBL 46 IAW DC9 SRM 51-30-06. FABRICATED, LOCATED, DRILLED AND DEBURRED NEW BRACKET PER DRAWING NR 3912075 USING EXTRUSION 2911391.SDR QXEA2011051100331Floorbeam · crackedRT FLOORBEAM AT STA X683 IS CRACKED. REMOVED RT FLOORBEAM IAW SRM 51-42-05-02-01. PREPARED AND INSTALLED NEW FLOORBEAM IAW SRM 51-42-05-02-01.SDR SWIA201126251Fitting · crackedFS 280 FLOORBEAM CLIP CRACKED. (C-CHECK) REPLACED PER REO.SDR SWIA201126226Floorbeam · corrodedFS 280 FLOORBEAM IS CORRODED. (C-CHECK) REPLACE FLOORBEAM PER SRM.SDR USAA2011051291841Floorbeam · crackedFORWARD PRESSURE BULKHEAD - CRACK IN FLOORBEAM UPPER TEE AT BS 665, LBL 0.7.SDR USAA2011050991803Floorbeam · corrodedCWF - S4 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR12 TO FR16, S23R, -Y81. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, S23R, -Y81 IAW A319 SRM 51-42-11.SDR DALA1131955531Floorbeam · corrodedFLOORBEAM AT STA 324 RBL 43-61 UPPER SURFACE HAS CORROSION. REMOVED CORROSION OUT OF LIMITS PER SRM 53-00-51. REMOVED TEE CHORD SRM 51-40-02. FABRICTED NEW TEE CHORD AND REP SPLICES ON STAM TRAVELER, FABRICATED REPAIR STRAPS PER ER/A 491292-14. DRILLED TEESDR ASAA1149780Floorbeam · corrodedTOP OF FLOORBEAM AT BS 360 CORRODED AT FASTENER HOLE LBL 10. REPAIRED FLOORBEAM IAW ASA EA 400 53EA 05459.SDR USAA2011060300003Floorbeam · corrodedPIT - S4 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR65 TO FR65 + 22 INCHES, -Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR65 + 22 INCHES, -Y1732 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472750.SDR ASAA1149704Floorbeam · corrodedFLOORBEAM STA 312 CORRODED BETWEEN LBL 12 TO RBL 12. REMOVED CORRODED UPPER CHORD, FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW UPPER CHORD REPAIR IAW B737 400 SRM 53 10 51 FIG 201 REPAIR 5.SDR ASAA1149705Floorbeam · corrodedFLOOR BEAM CORRODED STA 294 BETWEEN BL 0 AND RBL 12. REMOVED UPPER CHORD. FABRICATED TREATED PRIMED TOP COATED AND INSTALLED NEW UPPER CHORD IAW B737 400 SRM 53 10 51 FIG 201 REPAIR 5.
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