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 AALA20111018TUL08Floorbeam · corrodedIN THE CABIN AT STATION 1640 THE LATERAL FLOORBEAM IS CORRODED AROUND THE NUT PLATE HOLE ON THE FORWARD SIDE BOTTOM SURFACE RIGHT BUTTLINE 8.5. REMOVED CORROSION, AND REINFORCED LATERAL "I" BEAM "T" CAP PER SRM 53-00-51-2R, REPAIR 3.Oct 18, 2011 · N625AA · Boeing 757223SDR SWAA117172Floorbeam · crackedDURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, RBL 45.5. REPAIRED WEB IAW EO AND EA.Oct 18, 2011 · N619SW · Boeing 7373H4SDR FDEA201110184557Floorbeam · bentBS 580 FLOORBEAM, FOUND BENT. R & R IAW SRM 51-40-02, REV 104. REPAIR IS CLASSIFIED AS MAJOR.Oct 18, 2011 · N940FD · Boeing 757236SDR SWIA201128291Floorbeam · crackedFS 280 FLOORBEAM IS CRACKED. (C-CHECK) REPLACED FS 280 FLOORBEAM PER SRM.Oct 17, 2011 · N613QX · Cndair CL6002C10SDR ZZDA2011885Floorbeam · corrodedCABIN FLOORBEAM BS 180, RBL 9 TO RBL 43, CORROSION. ACCOMPLISHED FLOORBEAM REPLACEMENT PER SRM 51-41-02.Oct 17, 2011 · N997AT · Boeing 717200SDR ZZDA2011887Floorbeam · corrodedCABIN FLOORBEAM BS 200, RBL 9 TO RBL 46, CORROSION. ACCOMPLISHED FLOORBEAM REPLACEMENT PER SRM 51-41-02.Oct 17, 2011 · N997AT · Boeing 717200SDR ZZDA2011882Floorbeam · corrodedCABIN FLOORBEAM BS 200, LBL 5 TO RBL 5, CORRODED. ACCOMPLISHED FLOORBEAM REPLACEMENT PER SRM 51-41-02.Oct 17, 2011 · N997AT · Boeing 717200SDR SWAA117147Floorbeam · corrodedDURING SCHEDULED 16Y CHECK, FOUND UPPER CHORD FLOORBEAM CORRODED AT BS 312, BETWEEN RBL 20 TO RBL 37. REPAIRED BEAM IAW SRM.Oct 17, 2011 · N621SW · Boeing 7373H4SDR SWAA117103Floorbeam · corrodedDURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM UPPER AFT FLANGE CORRODED AT BS 344, LBL 11.Oct 16, 2011 · N329SW · Boeing 7373H4SDR N6WA20111016021Floorbeam · corrodedFS 280 FLOOR SUPPORT ANGLE CORRODED. INSTALLED FS 280 FLOOR SUPPORT ANGLE IAW SRM 51-42-06.Oct 16, 2011 · N169GJ · Cndair CL6002C10SDR FDEA201110154530Floorbeam · corrodedAFT CARGO COMPARTMENT FLOORBEAM BS 1902 IS CORRODED FROM RBL15 TO LBL15. REMOVED DAMAGE IAWSRM 53-00-01 FIG.8 AND SRM 51-31-01. FABRICATED REPAIR ANGLE AND FILLER IAW SRM 53-00-01. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 53-00-01 FIG 8 AND SRM 51-31-01. MOct 15, 2011 · N68054 · Doug MD1010FSDR USAA2011101800059Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, -Y324. REPLACED FLOORBEAM AT FR66, -Y324 IAW A319 SRM 53-42-11.Oct 15, 2011 · N746UW · Airbus A319112SDR USAA2011101800058Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, -Y465. REPLACED FLOORBEAM AT FR66, -Y465 IAW A319 SRM 51-72-11 AND TYPICAL REPAIR 3202528-10-10-0011C.Oct 15, 2011 · N746UW · Airbus A319112SDR SWIA201128292Floorbeam · crackedFS 280 FLOORBEAM CRACKED. (C-CHECK) REPLACED FLOORBEAM PER SRM.Oct 14, 2011 · N742SK · Cndair CL6002C10SDR FDEA201110144506Floorbeam · corrodedFLOORBEAM BS 1640, BL15L-R CORRODED. REMOVED AND REPLACED FLOORBEAM PER SRM 53-60-51, AND DRAWING 146N5180. FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-00-51, FIG.101, DETAIL 3, PAGE 103. MAJOR REPAIR.Oct 14, 2011 · N941FD · Boeing 757225SDR UALA2011101705607Floorbeam · crackedFWD CARGO BAY, BS 700 FLOORBEAM UPPER TEE CRACKED LBL 24 INCHES. REPAIRED IAW EVA 81356.Oct 14, 2011 · N539UA · Boeing 757222SDR USAA2011101800047Floorbeam · corrodedC11 CHECK - CORROSION ON FLOORBEAM BETWEEN FR21 TO FR22, -Y189. REPLACED FLOORBEAM BETWEEN FR21 TO FR22, -Y189 IAW A319 SRM 51-72-11.Oct 14, 2011 · N746UW · Airbus A319112SDR CALA2011101800670Floorbeam · corrodedCABIN FLOOR SUPPORT CORRODED AT STA 326 LBL 30 TO LBL 57. CABIN STA 326 LBL 10 LBL 68 FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIR 1 AND HFEC NIL CRACK FOUND.Oct 14, 2011 · N78060 · Boeing 767424ERSDR DALA1158440955Floorbeam · corrodedSDR - CORROSION ON FLOORBEAM RBL 7 FS 160-200 MCF 04. SAA102 CORROSION. FABRICATED FLOORBEAM TRACK FROM MATERIAL S3932140 BATCH # 0002110433 PER SRM DC9/MD88 SRM 53-14-1 FIG 11 SHT 2 ITEM 64. INSTALLED FLOORBEAM AT MAIN CABIN STA 160-200 RBL 7 PER SRM 51-30-Oct 14, 2011 · N955DL · Doug MD88SDR U2RA20111014067Floorbeam · corrodedBS377 LBL45 - 62, HEAVY CORROSION ABOVE AND BELOW FLOORBEAM, AREA DAMAGE CUT-OUT 85 INCHES.Oct 14, 2011 · N763CA · Boeing 7572Y0SDR U2RA201110140066Floorbeam · corrodedBS377 LBL 45-62, HEAVY CORROSION ABOVE AND BELOW FLOORBEAM. AREA DAMAGE CUT-OUT 85 INCHES.Oct 14, 2011 · N763CA · Boeing 7572Y0SDR USAA2011110100021Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, Y512. REPLACED FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, Y512 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011110100020Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR16 TO FR24, -Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR24, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011110100017Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y462. REPLACED FLOORBEAM BETWEEN FR64 TO FR67+10 INCHES, -Y462 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472816.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102800014Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66+5 INCHES, Y1292 IAW A320 SRM 51-72-11, SRM 51-42-11 & AIRBUS DRAWING D53472831.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102600030Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR67 PLUS 16 INCHES & BETWEEN Y1292 TO Y1162. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR67 PLUS 16 INCHES & BETWEEN Y1292 TO Y1162 IAW A320 SRM 51-72-11, 51-42-11 AND AOct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102600020Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53472780.Oct 13, 2011 · N117UW · Airbus A320214SDR FDEA201110134464Floorbeam · corrodedAFT CARGO COMPARTMENT FLOORBEAM TEE CORRODED UNDERNEATH 1R ROLLER TRACK AT FR 62R. REPLACED TEE IAW SRM 51-40-24.Oct 13, 2011 · N748FD · Airbus A300B4622RSDR USAA2011102500001Floorbeam · corrodedDURING 2S CHECK FOUND LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR65 TO 66, Y1500. REPLACED FLOORBEAM IAW SRM 51-72-11 & DRAWING D53474250.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102500007Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 PLUS 16 INCHES TO FR69 PLUS 5 INCHES, Y1162. REPLACED FLOORBEAM BETWEEN FR67 PLUS 16 INCHES TO FR69 PLUS 5 INCHES, Y1162 IAW A320 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53472780.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102500006Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68 & BETWEEN Y254 TO Y165. REPLACED FLOORBEAM BETWEEN FR66 TO FR68 & BETWEEN Y254 TO Y165 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102500005Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 PLUS 16 INCHES TO FR69 PLUS 5 INCHES, -Y1162. REPLACED FLOORBEAM BETWEEN FR67 PLUS 16 INCHES TO FR69 PLUS 5 INCHES, -Y1162 IAW A320 SRM 51-72-11, 51-42-11 AND AIRBUS DRAWING D53472780.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102500004Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, Y165. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, Y165 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102500003Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, -Y292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, -Y292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472816.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102500002Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR67 PLUS 16 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR67 PLUS 16 INCHES, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.Oct 13, 2011 · N117UW · Airbus A320214SDR USAA2011102300010Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Y765 IAW A320 SRM 51-72-1 & AIRBUS DRAWING 53472816.Oct 13, 2011 · N117UW · Airbus A320214SDR DU4R20111013016Floorbeam · corrodedDURING SCHEDULED INSPECTION, CORROSION ON FLOORBEAM BS 344 AND BL0, LBL 1, LBL 8.Oct 13, 2011 · N19638 · Boeing 737524SDR USAA2011101400023Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR66, -Y765. REPLACED FLOORBEAM AT FR66, -Y765 IAW A319 SRM 51-72-11 & 51-42-00.Oct 13, 2011 · N746UW · Airbus A319112SDR SWAA117049Floorbeam · crackedDURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CRACKED AT BS 294.5, LBL 55.5. REPAIRED BEAM IAW SRM.Oct 13, 2011 · N619SW · Boeing 7373H4SDR SWAA117048Floorbeam · corrodedDURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, BETWEEN BL 0 TO LBL 24.5. REPAIRED BEAM IAW SRM.Oct 13, 2011 · N619SW · Boeing 7373H4SDR A6WA201141025Floorbeam · crackedFLOORBEAM STRUCTURE AT FS 589 UNDER BAGGAGE DOOR SILL CRACKED IN 2 EA AREAS. REPAIRED FLOORBEAM STRUCTURE AT FS 589 IAW REO 601R-53-61-4229.Oct 12, 2011 · N422AW · Cndair CL6002B19SDR A6WA201140903Floorbeam · crackedCLIPS ON FS 280 FLOORBEAM AT LBL9 AND RBL9 ARE CRACKED. REMOVED UNSERVICEABLE CLIPS ON FS 280 FLOORBEAM AT LBL9 AND RBL9. INSTALLED SERVICEABLE CLIPS ON FS280 FLOORBEAM AT LBL9 AND RBL9 IAW SRM 51-42-21, SRM 53-21-43, SRM 51-24-16, SRM 51-40-11.Oct 12, 2011 · N467AW · Cndair CL6002B19SDR FDEA201110124432Floorbeam · corrodedCABIN FLOORBEAM BS 344 UPPER AFT. FLANGE LBL 24 TO 44 HAS CORROSION. UPPER TEE REPAIR ACCOMPLISHED ON NR NOO585.Oct 12, 2011 · N213FE · Boeing 7272S2FSDR FDEA201110124427Floorbeam · corrodedFLOORBEAM BS 344, LBL 24- RBL24 CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW B727 SRM 51-10-6 AND 53-10-1 FIG.5. REMOVED UPPER TEE SECTIONS AND SPLICE REPAIR PARTS IAW SRM 51-30-2. FABRICATED NEW TEE SECTIONS IAW SRM 53-10-8 FIG. 9. TEATED, PROct 12, 2011 · N213FE · Boeing 7272S2FSDR ASOA201101957Floorbeam · corrodedCORROSION ON FLOORBEAM RBL 9 AROUND FASTENER HOLE AT FS 621.00. REMOVED CORROSION IAW REO 601R-53-00-005. .014" MATERIAL REMOVED. .014" FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005, FIG 2. REMOVED FLOORBEAM CAP IAW SRM 51-42-06 & 51-42-21. LOCATED ANOct 12, 2011 · N876AS · Cndair CL6002B19SDR ASOA201101956Floorbeam · corrodedCORROSION ON FLOORBEAM AT LBL 9 AROUND FASTENER HOLES AT FS 605.00. REMOVED CORROSION IAW REO 601R-53-00-005.Oct 12, 2011 · N876AS · Cndair CL6002B19SDR C77A20111012003Floorbeam · corrodedCORROSION ON LT FLOOR TRACK, REPLACEMENT PERM REPAIR.Oct 12, 2011 · N606CZ · Emb ERJ170200LRSDR FDEA201110114431Floorbeam · corrodedFLOORBEAM WEB CORRODED BS 880, LBL 45 TO LBL 62. REMOVED CORROSION IAW SRM 51-10-6. NDT INSPECTED AFFECTED AREA IAW EA 7-5310-152465. TREATED AND PRIMED AFFECTED AREA IAW SRM 51-10-2, AND EA 7-5310-152465.Oct 11, 2011 · N213FE · Boeing 7272S2FSDR IPXA11669985Floorbeam · corrodedINSPECTION TYPE:8C, M/D STA 1540 LBL 75.25" TO LBL 78" FLOORBEAM FWD FACE UPPER CHORD FOUND CORROSION. REPAIRED IAW HX RS NR R-53-65-37243 REV A & EO B767-5310-44767-A, ORIGINAL THICKNESS IS 0.150", CORROSION BLENDED OUT AREA IS DEPTH 0.084" X WIDTH 2" X LENGOct 11, 2011 · N314UP · Boeing 76734AFSDR IPXA11669984Floorbeam · corrodedINSPECTION TYPE:8C, M/D STA 1518 LBL 80.75, FLOORBEAM AFT FACE UPPER TEE FOUND CORRODED. REPAIRED IAW HX RS NR R53-65-37241 REV A & EO B767-5310-44765-A, ORIGINAL THICKNESS AT FWD FLANGE IS 0.150" & AFT FLANGE IS 0.180", CORROSION BLENDED OUT AREA AT FWD FLOct 11, 2011 · N314UP · Boeing 76734AF
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