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.

SDR ASOA201100769Floorbeam · corrodedCORROSION ON FLOORBEAM AT FS 349.00 ON RT SIDE. INSTALLED REPAIR PARTS IAW REO 601R-53-21-1268.Apr 13, 2011 · N884AS · Cndair CL6002B19SDR DALA1125809871Floorbeam · crackedMAIN CABIN FS 598, LBL 0-22 FLOOR SUPPORT IS CRACKED. REMOVED CRACKED FLOOR SUPPORT IAW SRM 51-30-05. FAB NEW FLOOR SUPPORT. MAT ID .050 2024 T3 IAW SRM 53-12-2 FIG 4. CUT, RIMMED, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED FLOOR SUPPORT IAW SRM 51-10-4Apr 13, 2011 · N780NC · Doug DC951SDR DALA1125670688Floorbeam · corrodedCORROSION ON UPPER SURFACE OF BS 324 FLOORBEAM FROM BL 0 TO RBL 64. COMPLIED WITH PERMANENT REPAIR IAW ERA 490258-14, REV 0 RG.Apr 13, 2011 · N688DL · Boeing 757232SDR USAA2011042691652Floorbeam · corrodedPIT - SY6 CHECK - C11 CHECK - LEVEL 2 INTERGANULAR CORROSION ON CORROSION ON FLOORBEAM AT FR 66, -Y765. REPLACED FLOORBEAM AT FR 66, -Y765 IAW AIRBUS DRAWING D53472816 AND EA 117675.Apr 12, 2011 · N107US · Airbus A320214SDR FDEA201104121447Crossbeam · corrodedUPPER SUPPORT CROSSBEAM GOT CORROSION AT FR86 STG R12L. REPLACED THE DAMAGED CROSSBEAM BY NEW ONE IAW SRM 51-40-21. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MINOR.Apr 12, 2011 · N426FE · Airbus A310203SDR FDEA201104121446Floorbeam · corrodedUPPER SUPPORT STRUCTURE GOT MINOR CORROSION AT FR86 STG 12R. REMOVED THE CORRODED CROSS BEAM. FABRICATED A NEW CROSS BEAM I.A.W. DRAWING NO.: A53988624201. INSTALLED THE NEW CROSS BEAM FOR REPLACING.Apr 12, 2011 · N426FE · Airbus A310203SDR UALA2011041301780Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 367, RBL 5 THRU 65. MAJOR REPAIR ACCOMPLISHED, REPAIRED FLOORBEAM STA 365.25 T-CAP FROM LBL 8.5 TO RT FRAME JOINT AND REPAIRED FLOORBEAM WEB RBL 57.9 PER PEMCO EA PD57-53-104 ON PEMCO NR 2486N00275.Apr 12, 2011 · N562UA · Boeing 757222SDR DALA1125569871Floorbeam · corrodedFLOORBEAM AT STA 389, RBL 52 CORRODED AND CRACKED AT NUTPLATE. CUT OUT DAMAGED AREA 1" X 2". DAMAGE CONTAINED IAW NDT 06-01-10. 001. FABRICATED REPAIR ANGLE FROM MATERIAL ID 60-377707376571. MILLED ANGLE ON NR 2504NO1510. INSTALLED REPAIR ANGLE IAW SRM 51-3Apr 12, 2011 · N780NC · Doug DC951SDR LR7A2011041900175Fitting · corrodedDURING SCHEDULED C-9 CHECK, FOUND BELLY FLOORBEAM RT END FITTING WITH EXFOLIATION CORROSION AT FS557, RBL62, WL144. REPAIR ACCOMPLISHED BY REPLACING END FITTING IAW SMP583, CHAP 51-60 & 51-70.Apr 11, 2011 · N405LC · Lkheed 382GSDR ASOA201100737Floorbeam · corrodedFLOORBEAM TEE AT FS 589 BETWEEN LBL 9 AND RBL 9 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06. FOUND WITHIN LIMITS IAW SRM 53-00-00. ALODINED, PRIMED AND PAINTED IAW SRM 51-22-00.Apr 11, 2011 · N870AS · Cndair CL6002B19SDR SWAA112615Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 42. REMOVED AND REPLACED BEAM PER SRM.Apr 11, 2011 · N350SW · Boeing 7373H4SDR F3LA2011041300633Floorbeam · corrodedC-CHECK: NON ROUTINE 30064; FLOORBEAM ON FRAMES 66-68 HAS CORROSION AT FASTENER HOLES, BLENDED CORROSION, MEASURED OUT OF LIMITS. ORIGINAL THICKNESS .100", REMAINING .078". SRM 53-41-14 4A(1)AND 53-00-14 4B, FIG 102. LOCATED AND DRILLED NEW BEAM. IAW SRM 51-Apr 11, 2011 · N949FR · Airbus A319112SDR F3LA2011041300632Floorbeam · corrodedC-CHECK: NON ROUTINE NR 30063; FLOORBEAM ON FRAMES 66- 68 HAS CORROSION AT FASTENER HOLES, BLENDED CORROSION, MEASURED OUT OF LIMITS. ORIGINAL THICKNESS .100", REMAINING .080". SRM 53-41-14 4A(1)AND 53-00-14 4B, FIG 102. LOCATED AND DRILLED NEW BEAM. IAW SRM Apr 11, 2011 · N949FR · Airbus A319112SDR V0XR413Y041111003Floor Support · corrodedFWD FUSELAGE FLOOR SUPPORTS NEXT TO MAIN PASSENGER DOOR KICK PLATE CORRODED. REMOVED AND INSTALLED NEW KICKPLATE ANGLE ON FWD FUSELAGE FLOOR SUPPORT NEXT TO PASSENGER DOOR IAW SRM 53-21-23, SRM 51-42-06, SRM 51-40-11.Apr 11, 2011 · N166GJ · Cndair CL6002C10SDR A6WA201140292Floorbeam · corrodedFLOORBEAM AT FS 589.00 OTBD NEXT TO FLOOR LEDGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-12-00 AND SRM 51-11-00 ALODINED, PRIMED, TOPCOATED.Apr 10, 2011 · N415AW · Cndair CL6002B19SDR USAA2011041991537Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR68, Y1292. REPLACED FLOORBEAM AT FR68, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.Apr 9, 2011 · N677AW · Airbus A320232SDR USAA2011041991536Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472816 & D53472780.Apr 9, 2011 · N677AW · Airbus A320232SDR USAA2011041991535Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, -Y1292. REPLACED FLOORBEAM AT FR66, -Y1292 IAW A320 SRM 51-72-11 & EA 117648.Apr 9, 2011 · N677AW · Airbus A320232SDR USAA2011041991534Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1292 IAW A320 SRM 51-72-11.Apr 9, 2011 · N677AW · Airbus A320232SDR USAA2011041991533Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A320 SRM 51-72-11, EA 117648, AIRBUS DRAWING D53472816 & D53472780.Apr 9, 2011 · N677AW · Airbus A320232SDR USAA2011041991532Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1292 IAW A320 SRM 51-72-11, EA 117648 & AIRBUS DRAWING D53472780.Apr 9, 2011 · N677AW · Airbus A320232SDR CALA2011041100277Floorbeam · corrodedSUPPORT TASK - MAIN CABIN FLOORBEAM 1681 FWD FLANGE HAS CORROSION UNDER NUT PLATE RBL 47. INSTALLED REPAIR AT MAIN CABIN FLOORBEAM STA 1681 RBL 47 REF EC RA 5310-05373 STEPS 1 THROUGH 12.Apr 9, 2011 · N21108 · Boeing 757224SDR USAA2011041991531Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, -Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, -Y254 IAW A320 SRM 51-72-11.Apr 8, 2011 · N677AW · Airbus A320232SDR USAA2011041991530Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR17, Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR17, Y1292 IAW AIRBUS DRAWING D53110920.Apr 8, 2011 · N677AW · Airbus A320232SDR USAA2011041991529Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, -Y1292. REPLACED FLOORBEAM AT FR16, -Y1292 IAW A320 SRM 51-72-11, 51-40-00 & 51-43-00.Apr 8, 2011 · N677AW · Airbus A320232SDR USAA2011041991528Floorbeam · corrodedPIT - C11-SY6 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, Y254 IAW A320 SRM 51-72-11.Apr 8, 2011 · N677AW · Airbus A320232SDR SWIA201126032Floorbeam · corroded(C-CHECK) FS 280 FLOORBEAM CORRODED. REPLACED FS 280 FLOORBEAM.Apr 8, 2011 · N611SK · Cndair CL6002C10SDR SWAA112704Floorbeam · corrodedDURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D+5, LBL 12. REPAIRED BEAM PER SRM AND EA.Apr 8, 2011 · N663SW · Boeing 7373Q8SDR COMA2011040890005Floorbeam · corrodedFS 280 FLOORBEAM CORRODED LBL9 RBL 27. REMOVED AND REPLACED FS 280 FLOORBEAM IAW REO 690-53-11-092.Apr 8, 2011 · N678CA · Cndair CL6002D24SDR UALA2011040701692Floorbeam · corrodedFLOORBEAM CAP AT STA 324 RBL 36 HAS MULTIPLE AREAS OF CORROSION. MAJOR REPAIR ACCOMPLISHED: ACCOMPLISHED REPAIR OF FLOORBEAM AT STATION 324 RBL 36 PER EVA 80737 AND PD 57-53-101.Apr 7, 2011 · N561UA · Boeing 757222SDR USAA2011041291433Floorbeam · corrodedBFM - S2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR 33, +Y450 TO -Y450. REPAIRED FLOORBEAM AT FR 33, +Y450 TO -Y450 IAW EA 134433.Apr 7, 2011 · N272AY · Airbus A330323SDR USAA2011041191399Floorbeam · corrodedMIA - S5 CHECK - CORROSION ON FLOOR SUPPORT BEAM AT FR67, LBL31. REPLACED FLOOR SUPPORT BEAM AT FR76, LBL 31 IAW A320 SRM 51-72-11 AND 51-42-00.Apr 7, 2011 · N658AW · Airbus A320232SDR K11A2011052672403Floorbeam · corrodedFLOORBEAM CORROSION AT STA 1130 LBL 28 AND 43.Apr 6, 2011 · N724CK · Boeing 727225SDR K11A2011052672402Floorbeam · corrodedFLOORBEAM CORROSION AT STA 1130 LBL 11 AND 18. 2 INCH IN EACH POSITION.Apr 6, 2011 · N724CK · Boeing 727225SDR USAA2011041491498Floorbeam · corrodedMIA - S5 - LEVEL 1 EXFOLIATION CORROSION ON PREVIOUSLY BLENDED CABIN FLOOR BEAM BETWEEN FR66 TO FR67, -Y20. REPLACED CABIN FLOORBEAM BETWEEN FR66 TO FR67, -Y20 IAW A320 SRM 51-72-11 & 51-42-11.Apr 6, 2011 · N658AW · Airbus A320232SDR USAA2011041491497Floorbeam · corrodedMIA - S5 - LEVEL 1 EXFOLIATION CORROSION ON PREVIOUSLY BLENDED CABIN FLOORBEAM AT FR68, 8 INCHES INBOARD OF L2 DOOR. REPLACED CABIN FLOORBEAM AT FR68, 8 INCHES INBOARD OF L2 DOOR IAW A320 SRM 51-72-11 & 51-42-11.Apr 6, 2011 · N658AW · Airbus A320232SDR USAA2011041191400Floorbeam · corrodedCLT - S5 CHECK - FILIFORM CORROSION ON FLOOR SUPPORT BEAM AT FR66, RBL 30. REPLACED FLOOR SUPPORT BEAM AT FR66, RBL 30 IAW A320 SRM 51-72-11 AND 51-42-11.Apr 6, 2011 · N658AW · Airbus A320232SDR COEA2011040617903Floorbeam · crackedHEAVY CK COE / MAJOR REPAIR: FLOORBEAM 22 UPPER FLANGE IS CRACKED OUTBOARD OF THE RT OUTBOARD SEAT TRACK. REPAIRED FLOORBEAM 22 IAW ATR72 SRM.Apr 6, 2011 · N903FX · Aerosp ATR42320SDR REXA201100213Floorbeam · corrodedFLOORBEAM CRACKED AND CORRODED AT FS 280 RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0110.Apr 6, 2011 · N8869B · Cndair CL6002B19SDR CALA2011040600267Floorbeam · crackedSUPPORT TASK EA5310-04445 REV D OP1 STEP 33.19 INSTALL CHIP FOUND THE FLOORBEAM WEB ONE HOLE CRACKED AT BS 246 RBL 74 CABIN BS 246 RBL 74 FLOORBEAM WEB. REPAIRED AS PER ECRA 5310-05368 REV- AND HFEC NIL CRACK FOUND ATTACH MAINTENANCE WORK SHEET FORM 44.0008 IApr 6, 2011 · N73152 · Boeing 767224SDR V0XR413Y040611015Floorbeam · corrodedFLOORBEAM, STA 280 CORRODED. R & R 280 CROSSBEAM IAW REO 070-53-11-385 & SRM 53-11-10.Apr 6, 2011 · N162GJ · Cndair CL6002C10SDR V0XR413Y040611011Floorbeam · corrodedFS 274.5, LBL 12, FLOORBEAM CRACKED. REPAIRED AREA IAW REO 670-53-11-586.Apr 6, 2011 · N162GJ · Cndair CL6002C10SDR V0XR413Y040611010Floorbeam · crackedFS 274.5, RBL 12 FLOORBEAM IS CRACKED. REPAIRED AREA IAW REO 670-53-11-586.Apr 6, 2011 · N162GJ · Cndair CL6002C10SDR V0XR413Y040611006Floorbeam · corrodedSTA 280 FLOOR SUPPORT ANGLE AT LBL 9 & RBL 9 ARE CORRODED. REMOVED CORROSION ORIGINAL THICKNESS .063, REMOVED .003 TO CLEAN UP CORROSION, REMAINING THICKNESS OF PART IS .060 IAW SRM 51-42-10.Apr 6, 2011 · N162GJ · Cndair CL6002C10SDR V0XR413Y040611005Floorbeam · crackedSTA 280 FLOOR SUPPORT LBL9 TO RBL 9 IS CRACKED. R & R FLOOR SUPPORT ANGLE STA 280.00, LBL 9.00 TO RBL 9.00 IAW SRM 51-42-06.Apr 6, 2011 · N162GJ · Cndair CL6002C10SDR ASAA1149599Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED AT STA 986 RBL 30 AT FASTENER HOLE. REMOVED DAMAGED FLOORBEAM LOCATED DRILLED TREATED PRIMED AND INSTALLED REPAIR PARTS IAW ASA EA 400 53EA 05335.Apr 5, 2011 · N791AS · Boeing 737490SDR USAA2011041491500Floorbeam · corrodedMIA - S5 - LEVEL 2 EXFOLIATION CORROSION ON CABIN FLOORBEAM AT FR66, 30 INCHES INBOARD OF L2 DOOR. REPLACED CABIN FLOORBEAM AT FR66, 30 INCHES INBOARD OF L2 DOOR IAW A320 SRM 51-72-11 & 51-42-00.Apr 5, 2011 · N658AW · Airbus A320232SDR USAA2011041491499Floorbeam · corrodedMIA - S5 - LEVEL 1 EXFOLIATION CORROSION ON PREVIOUSLY BLENDED CABIN FLOORBEAM AT FR68, Y48. REPAIRED CABIN FLOORBEAM AT FR68, Y48 IAW A320 SRM 53-41-14.Apr 5, 2011 · N658AW · Airbus A320232SDR UALA2011040601657Floorbeam · corrodedCORROSION ON TOP OF FLOORBEAM AT STA 1640 RBL 24. MAJOR REPAIR ACCOMPLISHED: AFTER REMOVING CORROSION FOUND TO BE OUT OF LIMITS PER SRM. REMOVED TOP CHORD AT 1640 LB 10 THRU RBL 68. FABRICATED REPLACEMENT T-CHORD, ANGLES AND STRAPS FROM 7075-T6511 PER SRM.Apr 5, 2011 · N561UA · Boeing 757222SDR SWAA112510Web · crackedDURING SCHEDULED 18Y CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BS 270, RBL 15. REPAIRED WEB PER ACO.Apr 5, 2011 · N360SW · Boeing 7373H4
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