JASC 5315

Service difficulty reports · 44,220

Reports filed under 5315 · Fuselage Main, Floor Beam, newest first.

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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"

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SDR FDEA201107192823Floorbeam · corrodedSURFACE CORROSION ON TOP OF FLOORBEAM BS 950, RBL 50. REMOVED UPPER TEE CAP IAW SRM 51-30-2. FABRICATED NEW TEE CAP IAW SRM 53-10-2 FIGURE 7 AND SRM 51-30-5. INSTALLED TEE CAP IAW SRM 51-30- 2 AND SRM 51-30-5.Jul 19, 2011 · N257FE · Boeing 727233SDR FDEA201107192818Floorbeam · corrodedSURFACE CORROSION ON FLOORBEAM, LOWER SIDE LBL58, BS 950. FLOORBEAM REPLACED ON NR NOO538.Jul 19, 2011 · N257FE · Boeing 727233SDR FDEA201107192802Floorbeam · corrodedCORROSION TOP TEE ON FLOORBEAM STA 620, LBL 45 - 25. CUT OUT DAMAGE IAW SRM 53-10-8 FIG.3. FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG.3. INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2Jul 19, 2011 · N257FE · Boeing 727233SDR FDEA201107192803Floorbeam · corrodedCORROSION TOP TEE CAP FLOORBEAM STA 380, RBL 25 - RBL 45. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG. 4B. FABRICATED REPAIR PARTS AND REPAIRED TOP TEE CAP OF FLOORBEAM BS 380 IAW SRM 53-10-8 FIG. 3 AND 51-30-2.Jul 19, 2011 · N257FE · Boeing 727233SDR FDEA201107192821Floorbeam · corrodedSURFACE CORROSION TOP OF FLOORBEAM, BS 950F, LBL 18. CUTOUT DAMAGED AREA IAW SRM 53-10-8 FIG 3 AND FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3.Jul 19, 2011 · N257FE · Boeing 727233SDR USAA2011080100034Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, -Y1292. REPLACED FLOORBEAM AT FR16, -Y1292 IAW A319 SRM 51-42-11.Jul 19, 2011 · N732US · Airbus A319112SDR USAA2011080100032Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, Y503.2. REPLACED FLOORBEAM AT FR16, Y503.2 IAW A319 SRM 53-11-14.Jul 19, 2011 · N732US · Airbus A319112SDR USAA2011072900012Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR20, -Y254. REPLACED FLOORBEAM AT FR20, -Y254 IAW A319 SRM 51-42-00.Jul 19, 2011 · N732US · Airbus A319112SDR USAA2011072900002Floorbeam · corrodedC11 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR16 TO FR23, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR23, Y254 IAW A319 SRM 51-42-00.Jul 19, 2011 · N732US · Airbus A319112SDR FDEA201107192814Floorbeam · crackedFLOORBEAM TEE CRACKED THROUGH ALL SIDES AT STA 1156 L29R. REPAIRED CRACKED FLOORBEAM REF SRM 53-30-00 FIG 7. COMPLIED WITH EA 8-5310-147795.Jul 19, 2011 · N68057 · Doug MD1010FSDR ASOA201101351Floorbeam · corrodedCONTINUATION OF MWC 60 TRANSVERSE FLOORBEAM AT FS 349 HAS AREAS OF CORROSION AT LBL 45. EC/TC REQ'D EC/TC REQ'D. REO 601R-53-21-1327, REV HAS BEEN ACCOMPLISHED.Jul 19, 2011 · N873AS · Cndair CL6002B19SDR FDEA201107192820Structure · corrodedSURFACE CORROSION AROUND FASTENERS LOWER SIDE OF FLOORBEAM TOP TEE , BS 930, RBL 60. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1, FIG 4, FABRICATED REPAIR ANGLES IAW EA 7-5310-154104, AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND EA 7-5310-154104.Jul 19, 2011 · N257FE · Boeing 727233SDR FDEA201107192817Floorbeam · crackedFWD CARGO MAIN DECK FLOORBEAM AT FRAME 34 CRACKED AT STIFFENER, BETWEEN SEAT TRACKS 2 & 3 RT SIDE. CUTOUT DAMAGE AT FLOORBEAM IN FWD CARGO COMPARTMENT SUPPORT FR 34 RT SIDE IAW SRM 53-10-15. NDT IAW NTM 51-10-08 SHOW NO CRACK INDICATION AFTER CUTOUT OF DAMAGJul 19, 2011 · N435FE · Airbus A310203SDR FDEA201107192797Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 58, RBL 67 FOUND WITH A 0.25 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15, REV 18, FIG 203 SHT 1 & 2. REPAIR PROFILE FABRICATED AND INSTALLED IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1 & 2. ACCOMPLISHED EA 6-5310-143632. Jul 19, 2011 · N436FE · Airbus A310203SDR FDEA201107192796Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 34, RBL 27 FOUND WITH A 0.25 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15, REV 18, FIG 203, SHT 1. REPAIR PROFILE FABRICATED AND INSTALLED IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1.Jul 19, 2011 · N436FE · Airbus A310203SDR FDEA201107192795Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 37, RBL 27 FOUND WITH 0.25 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR CLASSIFIED ASJul 19, 2011 · N436FE · Airbus A310203SDR FDEA201107192794Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 37, RBL 67 FOUND WITH 0.28 INCH CRACK. FLOORBEAM TRIMMED OUT IAW SRM 53-10-15 REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SRM 53-10-15, REV 18, FIG 203 SHEET 1. REPAIR CLASSIFIED AS MJul 19, 2011 · N436FE · Airbus A310203SDR FDEA201107192793Clevis · crackedMDCC AT FS 54.1 AT SEAT TRACK 3RT CLEVIS ADAPTER MOUNT FITTING CRACK APPROX 2" LONG. R & R CLEVIS IN MDCC AT FR 54.1 ON RT NR 3 TRACK IAW SRM 51-72-10 PARA 5A & 6A. LOCATED, DRILLED & DEBURRED NEW CLEVIS IAW SRM 51-40-44, PG 16.Jul 19, 2011 · N435FE · Airbus A310203SDR FDEA201107192792Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 37, RBL 27 FOUND WITH 0.25 INCH CRACK. TRIMMED OUT IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR Jul 19, 2011 · N436FE · Airbus A310203SDR FDEA201107192791Floorbeam · crackedMAIN DECK FLOORBEAM AT FRAME 36, RBL 27 FOUND WITH 0.25 INCH CRACK. TRIMMED OUT IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR PROFILE AND FILLER FABRICATED AND REPAIR INSTALLED IAW SUPPLEMENT SRM 53-10-15, REV 18, FIG 203, SHEET 1. REPAIR Jul 19, 2011 · N436FE · Airbus A310203SDR SWAA115174Floorbeam · crackedDURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 662, LBL 24.8. REPAIRED CHORD PER EA.Jul 18, 2011 · N689SW · Boeing 7373Q8SDR USAA2011072600014Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR66 TO FR66 - 6 INCHES, -Y465. REPLACED FLOORBEAM BETWEEN FR66 TO FR66 - 6 INCHES, -Y465 IAW A319 SRM 51-72-11.Jul 17, 2011 · N730US · Airbus A319112SDR SWAA115151Floorbeam · crackedDURING SCHEDULED 20Y CHECK, FOUND FLOOR WEB BEAM CRACKED AT BS 639, LBL 45.5. REPAIRED WEB IAW EO.Jul 17, 2011 · N521SW · Boeing 7375H4SDR SWIA201126779Floorbeam · crackedFS 280 FLOORBEAM CRACKED ON AFT SIDE. (C-CHECK) REPAIR PER REO,Jul 17, 2011 · N956SW · Cndair CL6002B19SDR SWAA115104Floorbeam · crackedDURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.5. REPAIRED WEB IAW EA.Jul 17, 2011 · N618WN · Boeing 7373H4SDR USAA2011072600019Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, -Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, -Y254 IAW A319 SRM 51-72-11.Jul 16, 2011 · N730US · Airbus A319112SDR USAA2011072600018Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, Y1292. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, Y1292 IAW A319 SRM 51-72-11.Jul 16, 2011 · N730US · Airbus A319112SDR USAA2011072600017Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR12, -Y50. REPLACED FLOORBEAM AT FR12, -Y50 IAW A319 SRM 51-42-00.Jul 16, 2011 · N730US · Airbus A319112SDR USAA2011072600016Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR14 TO FR20, Y254. REPLACED FLOORBEAM BETWEEN FR14 TO FR20, Y254 IAW A319 SRM 51-72-11.Jul 16, 2011 · N730US · Airbus A319112SDR USAA2011072600015Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR16, Y495. REPLACED FLOORBEAM AT FR16, Y495 IAW A319 SRM 51-72-11.Jul 16, 2011 · N730US · Airbus A319112SDR USAA2011072100020Floorbeam · corrodedC11/SY6 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66 + 6 INCHES, -Y318. REPLACED FLOORBEAM AT FR66 + 6 INCHES, -Y318 IAW EA 200444.Jul 16, 2011 · N730US · Airbus A319112SDR FDEA201107152728Floorbeam · crackedLT GANTRY 4 FOUND CRACKED AT FR 52.A. REPAIRED IAW DRAWING R53810581 AND SRM 51-40-00, AS INSTRUCTED BY EO E6-5310-7-2021PT6Jul 15, 2011 · N723FD · Airbus A300B4622RSDR SWAA115078Floorbeam · corrodedDURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, LBL 24. REPAIRED BEAM PER SRM.Jul 15, 2011 · N734SA · Boeing 7377H4SDR IPXA1568487Floorbeam · corrodedINSPECTION TYPE:C3, CORROSION ON UPPER SURFACE OF THE BS 1200 FLOORBEAM AROUND THE NUTPLATE HOLES AT RBL 5-21 AND RBL 52 WL 208. REPAIRED IAW ATS ER NR11-03560.Jul 14, 2011 · N401UP · Boeing 75724APFSDR USAA2011072500027Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, -Y1292, -Z240. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, -Y1292, -Z240 IAW A320 SRM SRM 51-42-11.Jul 14, 2011 · N604AW · Airbus A320232SDR USAA2011072500026Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 TO FR68, -Y765, -Z240. REPLACED FLOORBEAM BETWEEN FR67 TO FR68, -Y765, -Z240 IAW A320 SRM SRM 51-42-11.Jul 14, 2011 · N604AW · Airbus A320232SDR USAA2011072500025Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR66, -Y1292, -Z240. REPLACED FLOORBEAM AT FR66, -Y1292, -Z240 IAW A320 SRM SRM 51-42-11.Jul 14, 2011 · N604AW · Airbus A320232SDR USAA2011072500024Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR68, Y1292, -Z240. REPLACED FLOORBEAM AT FR68, Y1292, -Z240 IAW A320 SRM SRM 51-42-11.Jul 14, 2011 · N604AW · Airbus A320232SDR USAA2011072500023Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 TO FR68, -Y1292, -Z240. REPLACED FLOORBEAM AT FR66, -Y1162, -Z240 IAW A320 SRM SRM 51-42-11.Jul 14, 2011 · N604AW · Airbus A320232SDR USAA2011072500022Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR66, -Y1162, -Z240. REPLACED FLOORBEAM AT FR66, -Y1162, -Z240 IAW A320 SRM SRM 51-42-11.Jul 14, 2011 · N604AW · Airbus A320232SDR UALA2011071503586Floorbeam · corrodedCABIN FLOORBEAM HAS CORR STA 1661, LBL 5 - 8. MAJOR REPAIR ACCOMPLISHED: CUT OUT DAMAGED T-CAP AND INSTALLED REPAIR. REF COAIR N-R 9946383. RPR T-CAP AND DOUBLER ANGLES INSTALLED.Jul 14, 2011 · N580UA · Boeing 757222SDR SWAA115065Floorbeam · crackedDURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 986.5, BETWEEN BBL 0 TO LBL 43. REPAIRED BEAM IAW EA AND E.Jul 14, 2011 · N618WN · Boeing 7373H4SDR SWAA115064Floorbeam · crackedDURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED BETWEEN BS 656 T0 BS 686, LBL 24.5. REPAIRED BEAM IAW EA AND E.Jul 14, 2011 · N618WN · Boeing 7373H4SDR FDEA201107132682Floorbeam · corrodedFLOORBEAM TEE BETWEEN RBL 41-62 BS 324 CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-08. ORIGINAL MATERIAL .0125 AFTER REWORK .110. R & R TEE IAW SRM 51-40-01. MAJOR REPAIR.Jul 13, 2011 · N996FD · Boeing 7572Q8SDR USAA2011080500023Floorbeam · corrodedC4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT BS 1640, LBL 55. REPLACED FLOORBEAM AT BS 1640, LBL 55 IAW B757 SRM 53-00-51 & 53-00-51.Jul 13, 2011 · N203UW · Boeing 75723NSDR IPXA11668181Floorbeam · corrodedINSPECTION TYPE:C, M/D BELOW FLOOR BS 1518, LBL 80 FLOORBEAM FOUND CORROSION. REPAIRED IAW RS R-53-65-37175 REV A & EO B767-5310-43604-A ORIG MAT IS BAC1506-4177-0775T6511 EXTRUSION, TOP FLANGE THICKNESS IS 0.0150, CORROSION BLENDED AREA IS 0.063" DEPTH, 1" Jul 13, 2011 · N307UP · Boeing 76734AFSDR IPXA11668179Floorbeam · corrodedINSPECTION TYPE:C, M/D BELOW FLOOR BS 1540 LBL 75 FLOORBEAM FOUND CORROSION. REPAIRED IAW HX RS R-53-65-37170 REV A & EO B767-5310-43603-A. ORIG MAT IS BAC1506-4177-7075T6511 EXTRUSION, TOP FLANGE THICKNESS IS 0.150, CORROSION BLENDED AREA IS 0.050" DEPTH, 1Jul 13, 2011 · N307UP · Boeing 76734AFSDR UALA2011071403547Floorbeam · corrodedCORROSION ON FLOOR BEAM AT STATION 365 RBL 60. MAJOR REPAIR. AFTER BLENDING CORROSION FOUND FLOORBEAM TO BE OUT OF LIMITS PER SRM. REMOVED DAMAGE IAW SRM, FABRICATED REPAIR PART ANGLES. FABRICATED STRAP & BEAM. INSTALLED ALL PARTS IAW SRM 53-00-51.Jul 13, 2011 · N579UA · Boeing 757222SDR UALA2011071403582Floorbeam · corrodedMAIN CABIN FLOORBEAM AT STA 1660 CORRODED AROUND FLOORBOARD MOUNT HOLES BL 0 TO LBL 30. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS OF SRM. ORIGINAL MATERIAL THICKNESS IS .125, REMOVED .011, AND REMAINING MATERIAL THICKNESS IS .1 14. ALODINED AND PRIMEDJul 13, 2011 · N571UA · Boeing 757222SDR ASOA201101328Floorbeam · corrodedTRANSVERSE FLOORBEAM AT FS 310 HAS A AREA OF CORROSION AT LBL 45. REMOVED MINOR CORROSION IAW SRM 51-21-06.Jul 13, 2011 · N873AS · Cndair CL6002B19
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