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 COEA2011040515903Floorbeam · corrodedHEAVY CK COE / MAJOR REPAIR / LEVEL 2 CORROSION: FLOORBEAM 17 IS CORRODED ON THE UPPER AND LOWER SURFACE OF THE UPPER FLANGE BETWEEN LT INBOARD AND LT OUTBOARD SEAT TRACKS.(LENGTH 1.25, WIDTH .300, DEPTH .015 INCH). REMOVED CORROSION, FABRICATED AND INSTALLESDR IPXA11566220Floorbeam · corrodedINSPECTION TYPE:C1, FLOORBEAM FWD FLANGE HAS CORROSION AT FASTENER HOLES BETWEEN 0 - LBL 23 STA 1100. REPAIRED IAW ATS ER 11-02314.SDR SWAA112431Floorbeam · corrodedDURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 20 TO RBL 44. REPAIRED BEAM PER SRM.SDR USAA2011041491496Floorbeam · corrodedMIA - S5 - LEVEL 1 EXFOLIATION CORROSION ON PREVIOUSLY BLENDED CABIN FLOORBEAM BETWEEN FR66 TO FR68, -Y51. REPLACED CABIN FLOORBEAM BETWEEN FR66 TO FR68, -Y51 IAW A320 SRM 51-72-11 & 51-42-11.SDR MALA110082Floorbeam · corrodedFLOOR ANGLE FOR AFT SIDE OF FLOOR PANEL 221ALE AT FS 280 IS CORRODED. R & R FLOOR PANEL FOR AFT SIDE OF FLOOR PANEL IN FLT COMPARTMENT AT FS 280.00 IAW SRM 51-42-06, 51-42-21 AND 51-42-13.SDR SIMA201109501Floorbeam · corrodedDURING MAINTENANCE BASE VISIT FOUND THE TOP FLANGE OF TRANSVERSE FLOORBEAM AT FRAME 280 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE CORROSION IAW EO CR-53MR-219. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR IPXA11566100Floorbeam · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT STA 440, RBL 44, WL 208 FLOORBEAM HAS CORROSION AT FASTENER. SPLICED IN NEW SECTION OF SEAT TRACK IAW SRM 53-00-52-2R-5.SDR SWIA201125925Floorbeam · crackedFS 280 FLOORBEAM CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.SDR IXXA11SMN066SFloorbeam · corrodedDURING ROUTINE C-CHECK INSP, FOUND AFT ACCESSORY COMPARTMENT FLOORBEAM UPPER FLANGE CORRODED AT STA 1420.000 RBL 52. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED ANGLE AND FILLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. ISDR FDEA201104011278Floorbeam · corrodedMAIN CABIN STA 365, BL-0 FLOORBEAM CORRODED UPPER FLANGE. REMOVED CORROSION IAW SRM 51-10-02. ORIGINAL MATERIAL .125 AFTER REWORK .098. EXCEEDED MAX ALLOWABLE DAMAGE REMOVAL OF .107 IAW SRM 53-00-51 FIG 101 DETAIL III. AREA OUT OF LIMITS. REMOVED DAMAGED SDR USAA2011041291449Floorbeam · corrodedBFM - S4 CHECK - CORROSION ON FLOORBEAM AT FR 68, Y1292. REPLACED FLOORBEAM AT FR 68, Y1292 IAW A319 SRM 51-42-11.SDR ASOA201100673Floorbeam · corrodedFLOORBEAM IS CORRODED ACROSS TOP OF UPPER TEE. BLENDED CORROSION IAW SRM 51-21-06. WITHIN SERVICEABLE LIMITS IAW SRM 53-11-06.SDR ASOA201100672Floorbeam · corrodedFS 280, FLOORBEAM IS CORRODED ACROSS TOP OF UPPER TEE. R & R IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-41-02. MAJOR REPAIR.SDR UALA2011040101563Floorbeam · corrodedSTA 365 FLOORBEAM UPPER FLANGE CORRODED. MAJOR REPAIR ACCOMPLISHED: REPAIRED ON SM W-U E9952H PER SRM FROM LBL 8.5 TO RBL 59.SDR EIAA2011034Floorbeam · damagedBS 500 U/D FLOORBEAM CHORD HAS 8 EACH LT AND 8 EACH RT HOLES COMMON TO FRAME LOCATION BEYOND SRM LIMITS. REMOVED DISCREPANT HOLES FABBED AND INSTALLED REPAIRS PER ECRA 471-53-281-2.SDR USAA2011040891380Floorbeam · corrodedPIT - S4 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR68, -Y468.8. REPLACED FLOORBEAM AT FR68, -Y468.8 IAW AIRBUS DRAWING D53472780.SDR F3LA2011040500629Floorbeam · corrodedC-CHECK: NON ROUTINE NR 36930; CABIN FR66, Y-765 FWD OF SPLICE HAS CORROSION AT FLOOR PANEL ON FLOOR SUPPORT. REPLACED CABIN FLOOR SUPPORT FR66, Y-765 IAW A319 SRM 51-42-11, PARA 5 AND 6.D AND PARA 5A. AND B.SDR ASOA201100669Floorbeam · corrodedFLOORBEAM AT LBL 27, FS 621 TO FS 574 HAS CORROSION AROUND FASTENER HOLES. WHILE COMPLYING WITH LT ELEV CONTROL CABLE RIG FOUND RT ELEV FUSE CABLE TENSIONS LOW. RETENSIONED RT ELEV CONTROL CABLES IN FUSE IAW AMM 27-31-00-830-808.SDR DALA1123389871Floorbeam · chafedMAIN CABIN STA 579 BETWEEN BL-0 AND LBL-20 FLOORBEAM CHAFED ON TOP SIDE BLENDED CHAFED AREA 5EA 1"X 1.50". ORIG THICK MAT .125 REMOVED.030, REMAINING .095 FOUND TO BE OUT OF LIMITS. REC MAT .025 TY301 1/7. FAB 5EA WEAR STRIP. INSTALLED 5EA WEAR STRIPS IASDR CALA2011033100244Floorbeam · corrodedFLOOR SUPPORT HAS CORROSION AT STA 377 AT LBL 2 TO 24. AS MARKED INSTALLED REPAIR AT STA 377 FLOORBEAM FROM LBL-8 TO LBL 54 REF SRM 53-00-51.SDR CALA2011040100253Floorbeam · corrodedCABIN - FLOORBEAM CORRODED AT STA 303 LBL 11 - 55 CABIN STA 303 FLOORBEAM UPPER BEAM LBL 11 TO 55 REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NIL CRACK FOUND ATT MAINT WORK SHEET FORM 44.0008 ITEM 1 TO 19 ACCOMPLISHED.SDR CALA2011040100252Floorbeam · corrodedFLOORBEAM CORRODED AT STA 324 LBL 20-LBL 55 CABIN - STA 324 LBL 19 TO RBL 59 FLOORBEAM UPPER CHORD. REPAIRED AS PER SRM 53-00-51. REPAIR 1 FIG 201 AND HFEC NIL CRACK FOUND ATT MAINTENANCE WORKSHEET FORM44.0008 ITEM 1 TO 19 ACCOMPLISHED.SDR SWAA112344Floorbeam · corrodedDURING SCHEDULED 8Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 804, RBL 18. REPAIRED BEAM PER SRM AND BAC DWG.SDR ASAA1149480Strap · brokenFLOORBEAM CENTER STRAP BROKEN STA 312. REMOVED BROKEN STRAP FABRICATED REPLACEMENT AND INSTALLED IAW B737 400 SRM 51 40 02.SDR USAA2011041891511Strap · crackedMCN - C1 - CRACK ON FLOORBEAM STABILIZATION STRAP AT BS 1620, RBL 24.75. REPAIRED FLOORBEAM STABILIZATION STRAP AT BS 1620, RBL 24.75 IAW B757 SRM 51-70-13.SDR USAA2011041191398Floorbeam · corrodedPIT- S4 CHECK - CORROSION ON FLOORBEAM, FR 67 - FR 68, -Y765. REPLACED FLOORBEAM, FR 67 - FR 68, -Y765 IAW A319 SRM 51-42-00.SDR USAA2011040891389Floorbeam · corrodedPIT - S4 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, Y495. REPLACED FLOORBEAM AT FR16, Y495 IAW A319 SRM 51-72-11.SDR USAA2011040891373Floorbeam · corrodedPIT - S4 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, Y1292. REPLACED FLOORBEAM AT FR66, Y1292 IAW A319 SRM 51-42-00.SDR SWIA201125926Floorbeam · crackedFS 280 FLOORBEAM CRACKED ON BOTH LEFT AND RIGHT SIDES. (C-CHECK) REPLACE PER SRM.SDR DALA1129080137Floorbeam · corrodedAFT CARGO FLOORBEAM AT STA 1197, INNER CHORD FOUND CORRODED AT LBL 13.0 AND LBL 42.0. AFT CARGO FLOORBEAM AT STA 1197 INNER CHORD TRIMMED BETWEEN BL 0 TO LBL 44 AND REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 4, OTIS.SDR USAA2011041291456Floorbeam · corrodedSAL - S5 CEHCK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR 67 + 15, Y1155. REPLACED FLOORBEAM AT FR 67 + 15", Y1155 IAW A320 SRM 51-72-11.SDR USAA2011040891376Floorbeam · corrodedPIT - S4 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y765. REPLACED FLOORBEAM AT FR66, -Y765 IAW A319 SRM 53-41-11.SDR USAA2011040891375Floorbeam · corrodedPIT - S4 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR65, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR65, -Y1292 IAW A319 SRM 53-41-11.SDR USAA2011040891374Floorbeam · corrodedPIT - S4 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A319 SRM 53-41-14.SDR USAA2011040891371Floorbeam · corrodedPIT - S4 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR67 +12 INCHES, -Y1292. REPLACED FLOORBEAM AT FR67 +12 INCHES, -Y1292 IAW A319 SRM 53-41-14.SDR CALA2011032900235Floorbeam · corrodedMAIN CABIN FLOORBEAM 1661 HAS CORROSION FROM BL-0 TO LBL-27 (MARKED). REPAIRED STA 1681 FLOORBEAM BL 0 LBL 21 REF SRM 53-00-51 FIG 201.SDR USAA2011040691339Floorbeam · corrodedPIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, S23L. REPLACED FLOORBEAM AT FR66, S23L IAW A320 SRM 51-42-11.SDR USAA2011040691338Floorbeam · corrodedPIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, Y1160. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, Y1160 IAW A320 SRM 51-72-11.SDR USAA2011040691337Floorbeam · corrodedPIT - C11/SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, Y1160. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, Y1160 IAW A320 SRM 51-72-11.SDR UALA2011033001536Floorbeam · corrodedFLOORBEAM CAP AT STA 365.25 HAS CORROSION FROM RBL 2 TO RBL 50. MAJOR REPAIR ACCOMPLISHED: FLOORBEAM CAP HAS PREVIOUS REPAIR WHICH IS ALSO CORRODED. CORR OUT OF LIMITS, CUT OUT DAMAGE, FABBED T-CHORD, 2 EA ANGLES, 2 EA. STRAPS & INSTALLED PER AMM'S.SDR FDEA201103291234Seat Track · damagedSEAT TRACK INSTL SEC46 UNABLE TO INSTALL 657N3311-1 SPLICE FITTING AT STA 1280 LBL 45.50, EXISTING FASTENER HOLES ON FLOORBEAM WEB ARE NOT POSITIONED ON DWG 657N3311, SH 5 AND SEAT TRACK 657N3318-7 REQ TO TRIM FWD EDGE FLANGE .300 APPROX TO MAINTAIN .10SDR DALA1130920623Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED STA 720 LBL 12 / ACCOMPLISHED ERA PER SRM 53-00-51 REPAIR 3 PG 201 FIG 201.SDR USAA2011042991709Floorbeam · corrodedSAL - S4 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR20 TO FR21, -Y189. REPLACED FLOORBEAM BETWEEN FR20 TO FR21, -Y189 IAW EA 133471.SDR USAA2011042191599Floorbeam · corrodedSAL - S4 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR16, Y765. REPLACED FLOORBEAM AT FR16, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110984, D53112812 & D53110920.SDR USAA2011042191598Floorbeam · corrodedSAL - S4 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y254. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53111462.SDR USAA2011042191597Floorbeam · corrodedSAL - S4 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, -Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, -Y1732 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474250.SDR USAA2011041291474Floorbeam · corrodedSAL - S4 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 10 INCHES TO FR67 + 18 INCHES, Y1295. REPLACED FLOORBEAM BETWEEN FR66 + 10 INCHES TO FR67 + 18 INCHES, Y1295 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2011041291466Floorbeam · corrodedSAL - S4 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 + 18 INCHES TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR67 + 18 INCHES TO FR69, Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2011041291464Floorbeam · corrodedSAL - S4 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 10 INCHES TO FR67 + 18 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 + 10 INCHES TO FR67 + 18 INCHES, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2011041291463Floorbeam · corrodedSAL - S4 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67 + 10 INCHES, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67 + 10 INCHES, -Y465 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472305.
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