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 ASOA201100769Floorbeam · corrodedCORROSION ON FLOORBEAM AT FS 349.00 ON RT SIDE. INSTALLED REPAIR PARTS IAW REO 601R-53-21-1268.SDR 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 51-10-4SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 51-3SDR 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.SDR 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.SDR SWAA112615Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 42. REMOVED AND REPLACED BEAM PER SRM.SDR 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-SDR 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 SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR SWIA201126032Floorbeam · corroded(C-CHECK) FS 280 FLOORBEAM CORRODED. REPLACED FS 280 FLOORBEAM.SDR SWAA112704Floorbeam · corrodedDURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CORRODED AT BS 727D+5, LBL 12. REPAIRED BEAM PER SRM AND EA.SDR COMA2011040890005Floorbeam · corrodedFS 280 FLOORBEAM CORRODED LBL9 RBL 27. REMOVED AND REPLACED FS 280 FLOORBEAM IAW REO 690-53-11-092.SDR 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.SDR 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.SDR 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.SDR K11A2011052672403Floorbeam · corrodedFLOORBEAM CORROSION AT STA 1130 LBL 28 AND 43.SDR K11A2011052672402Floorbeam · corrodedFLOORBEAM CORROSION AT STA 1130 LBL 11 AND 18. 2 INCH IN EACH POSITION.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 ISDR V0XR413Y040611015Floorbeam · corrodedFLOORBEAM, STA 280 CORRODED. R & R 280 CROSSBEAM IAW REO 070-53-11-385 & SRM 53-11-10.SDR V0XR413Y040611011Floorbeam · corrodedFS 274.5, LBL 12, FLOORBEAM CRACKED. REPAIRED AREA IAW REO 670-53-11-586.SDR V0XR413Y040611010Floorbeam · crackedFS 274.5, RBL 12 FLOORBEAM IS CRACKED. REPAIRED AREA IAW REO 670-53-11-586.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR SWAA112510Web · crackedDURING SCHEDULED 18Y CHECK, FOUND COCKPIT FLOOR WEB CRACKED AT BS 270, RBL 15. REPAIRED WEB PER ACO.
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