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 UALA2011030201016Floorbeam · corrodedCORROSION ALONG FLOOR SUPPORT STA 853, LBL 75 FOUND TO BE BEYOND ALLOWABLE LIMITS. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED T-CAP AND SPLICE ANGLES BTWN STA 853 AND 888 ALONG LBL 75 IAW SRM REPAIR 3. APPLIED TOPCOAT IAW SRM. APPLIED CIC IAW SRM ON PEMar 1, 2011 · N658UA · Boeing 767322SDR UALA2011030201015Floorbeam · corrodedCORROSION ON FLOOR SUPPORT STA 853, LBL 54 BEYOND ALLOWABLE LIMITS IAW SRM. MAJOR REPAIR ACCOMPLISHED: REMOVED AND REPLACED TEE CAP BETWEEN STA 833 AND 920 IAW SRM REPAIR 3. APPLIED TOPCOAT IAW SRM, APPLIED CIC IAW SRM ON PEMCO NR 249N0 0154 BY TECH 600177, Mar 1, 2011 · N658UA · Boeing 767322SDR SWAA111296Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986, BETWEEN LBL 4 TO LBL 44. REMOVED AND REPLACED T-CAP PER SRM.Mar 1, 2011 · N344SW · Boeing 7373H4SDR IPXA1565718Floorbeam · corrodedINSPECTION TYPE:C4, MAIN CARGO COMPARTMENT STA 1681, LBL 42" TO LBL 54" FLOOR HAS CORROSION. REMOVED CORROSION ORIGINAL THICKNESS .071 LOSS .013 WITH .058 REMAINING IS OUT OF LIMITS IAW SRM 53-00-51-1A . ACCOMPLISHED BLEND REPAIR FOR EXTENDED LIMITS IAW EAFeb 28, 2011 · N455UP · Boeing 75724APFSDR USAA2011031891132Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT FR67 + 14 INCHES, Y1292. REPLACED FLOORBEAM AT FR67 + 14 INCHES, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.Feb 28, 2011 · N654AW · Airbus A320232SDR ASOA201100401Floorbeam · corrodedFS 280 FORWARD FLOORBEAM ANGLE IS CORRODED OUT OF LIMITS SRM 53-00-00-101-001-A01. REMOVED FS 280 FWD FLOORBEAM ANGLE PER SRM'S 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. INSTALLED FS 280 FWD FLOORBEAM ANGLE IAW SRM'S 51-42-06-001-001-A01 & 51-42-21-001Feb 28, 2011 · N754EV · Cndair CL6002C10SDR ASOA201100398Floorbeam · corrodedFS 280 FLOORBEAM IS CORRODED. R & R CLIPS IAW SRM 51-42-21.Feb 28, 2011 · N719EV · Cndair CL6002C10SDR ASOA201100397Floorbeam · crackedFS 280 AND LBL 9 AND RBL9 OBD CLIPS CRACKED. R & R CLIPS IAW SRM 51-42-21.Feb 28, 2011 · N719EV · Cndair CL6002C10SDR DALA1114269878Floorbeam · corrodedMAIN CABIN STA 712 BETWEEN RBL-22 AND RBL-44 FLOOR SUPPORT HAS CORROSION AND GOUGED. REMOVED CORROSION AND GOUGES FROM FLOOR SUPPORT STA 712 RBL-22 AND RBL-44 ORG MAT .050 MAT. REMOVED .020 MAT. REMAINING .030 FOUND TO BE OUT OF LIMITS IAW DC9 SRM 53-01Feb 28, 2011 · N787NC · Doug DC951SDR DALA1114259878Floorbeam · corrodedMAIN CABIN STA 674 BETWEEN BL-0 AND RBL-22 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3, SUPPORT OUT OF LIMITS. MATERIAL ID .050 2024T3 IAW SRM 53-18-2 SHEET 2 FIG 4. REMOVED .015 REMAINING .035 IAW SRM 53-01 FIG 1 AND 51-10-3. REMOVED SUFeb 28, 2011 · N787NC · Doug DC951SDR DALA1114249878Floorbeam · crackedMAIN CABIN STA.655 BETWEEN BL-0 AND LBL-22 FLOOR SUPPORT CRACKED AND HAS CORROSION. REMOVED FLOOR SUPPORT DUE TO CRACK IAW SRM 51-30-2. REMOVED CORROSION IAW SRM 51-10-3, FOUND TO BE WITHIN LIMITS MATERIAL ID .050 2024T3 IAW SRM 53-13-02. REMOVED .002 MATERFeb 28, 2011 · N787NC · Doug DC951SDR SWAA111207Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BETWEEN BL 0 TO RBL 24.5. REPAIRED BEAM PER SRM.Feb 28, 2011 · N347SW · Boeing 7373H4SDR A6WA201140237Floorbeam · corrodedLBL 27 FLOORBEAM CAP IN FRONT OF CARGO DOOR CORRODED AROUND NUTPLATE HOLES. REMOVED CORRODED FLOORBEAM CAP AT LBL 27.0 BETWEEN FS 569 IAW SRM 51-42-06 AND 51-42-21. DUPLICATED SERVICEABLE FLOORBEAM CAP IAW SRM 53-61-43 AND INSTALLED SERVICEABLE FLOORBEAM CAPFeb 27, 2011 · N458AW · Cndair CL6002B19SDR MALA110045Floorbeam · corrodedCOCKPIT ENTRY FLOOR PANEL SUPPORT BRACK CORRODED BY 280.00 FRAME. REMOVED AND REPLACED COCKPIT ENTRY FLOOR SUPPORT BRACKET AT FS 280.00 IAW SRM 51-42-06.Feb 26, 2011 · N901XJ · Cndair CL6002D24SDR ASAA1159358Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 986 IS CORRODED. REPAIRED FLOORBEAM IAW B737 800 SRM 53 70 51.Feb 25, 2011 · N548AS · Boeing 737890SDR FDEA201102250768Floorbeam · corrodedFWD CARGO COMPT FLOOR DECK PLATE SUPPORT LT CHANNEL AT STA 740 LBL 10.45 - LBL 16.10 FOUND WITH CORROSION. CORRODED CHANNEL AT STA 740 LBL 10.45 TO LBL 16.10 REMOVED AND REPLACED IAW SRM 51-40-02 REV 102. REPAIR IS CLASSIFIED AS MINOR.Feb 25, 2011 · N947FD · Boeing 757236SDR FDEA201102250767Floorbeam · corrodedFWD CARGO COMPT FLOOR DECK PLATE SUPPORT RT CHANNEL UNDER SURFACE AT STA 740 RBL 10.45 - RBL 16.10 FOUND WITH CORROSION. CORRODED CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR.Feb 25, 2011 · N947FD · Boeing 757236SDR EIAA 2011019Floorbeam · damagedBS 496-535 LEFT BUTTOCK LINE 37 TO 44 WATER LINE 309 FLOORBEAM UPPER CHORD ENLONGATED HOLES AND CORROSION. REMOVED FABRICATED AND INSTALLED NEW UPPER CHORD PER B747 SRM 51-30-02 AND 51-30-05.Feb 25, 2011 · N471EV · Boeing 747273CSDR AALA20110225TUL31Floorbeam · corrodedCORROSION ON AFT FLANGE BOTTOM SIDE OF FLOORBEAM AT STATION 377 LEFT BUTTLINE 60. INSTALLED T-CAP AND DOUBLERS PER SRM 53-00-51-2R 3 AND AARD 53-00-51-01.Feb 25, 2011 · N604AA · Boeing 757223SDR EIAA 2011017Floorbeam · damagedBS 440 UPPER DECK FLOORBEAM WEB HAS DAMAGED FASTENER HOLES AT RIGHT FRAME LOCATION. REMOVED AND REPLACED STA 440 UPPER DECK FLOORBEAM PER B747 SRM 53-10-07 FIG 11.Feb 25, 2011 · N471EV · Boeing 747273CSDR FDEA201102250760Floorbeam · crackedMAIN CABIN FLOORBEAM AT FR 66 BETWEEN 3L AND 4L SEAT TRACKS HAS 2 EACH 0.30 INCH CRACKS, 1 INCH ABOVE ON MILLED GRIP 2 INCH FROM TOP OF FRAME. CUT OUT DAMAGED AREA IAW SRM 53-10-15 FIG 211 PG 389. NDT CHECK COMPLIED WITH FOR INITIAL CRACKS, NO CRACKS FOUND IFeb 25, 2011 · N674FE · Airbus A300F4605RSDR FDEA201102250759Floorbeam · crackedMAIN DECK FLOORBEAM AT FR 64 BETWEEN SEAT TRACKS 4R AND 3R MILLED GRIP ON AFT FACE HAS A 1 INCH CRACK AT 2.25 INCH FROM TOP OF THE BEAM. CUT OUT DAMAGED AREA IAW SRM 53-10-15 FIG 211 PG 389. NDT CHECK COMPLIED WITH, NO CRACKS FOUND IAW NTM 51-10-08. REPAIFeb 25, 2011 · N674FE · Airbus A300F4605RSDR FDEA201102240708Floorbeam · misrepairedCABIN FLOORBEAM WITH BEAM REPAIR AT BS 720, BETWEEN LBL 50.5 TO RT SIDE FRAME JOINT. FLOORBEAM AT STA 720 R & R WITH FABRICATED PART IAW SRM 51-40-02, REV 102. REPAIR IS CLASSIFIED AS MAJOR.Feb 24, 2011 · N948FD · Boeing 757236SDR ASAA1149302Floorbeam · corrodedFLOORBEAM AT BS 986 UPPER CAP PREVIOUS REPAIR IS CORRODED FROM LBL 49 TO RBL 49. REMOVED PREVIOUS "T" CAP REPAIR FABRICATED NEW REPAIR PARTS AND INSTALLED IAW ASA EA 400 53EA 05061.Feb 24, 2011 · N706AS · Boeing 737490SDR IPXA11665159Floorbeam · crackedINSPECTION TYPE:C, FX MAIN EQUIPMENT CTR STA 246, RBL 10, FLOORBEAM ATTACH CLIP FOUND CRACKED. FX MAIN EQUIPMENT CTR STA 246, RBL 10, FLOORBEAM ATTACH CLIP. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 49.Feb 24, 2011 · N316UP · Boeing 76734AFSDR IPXA1665099Floorbeam · crackedINSPECTION TYPE:C, FX MAIN EQUIPMENT CTR STA 246 LBL 25" FLOORBEAM ANGLE FOUND CRACKED. FX MAIN EQUIPMENT CTR STA 246 LBL 25" FLOORBEAM ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 49.Feb 24, 2011 · N316UP · Boeing 76734AFSDR EIAA 2011018Floorbeam · damagedBS 440 UPPER DECK FLOORBEAM WEB HAS DAMAGED FASTENER HOLES AT LEFT FRAME LOCATION. REMOVED AND REPLACED STA 440 UPPER DECK FLOORBEAM WEB PER B747 SRM 53-10-07 FIG 11.Feb 24, 2011 · N471EV · Boeing 747273CSDR DALA1113450667Floorbeam · corrodedAFT CARGO FLOORBEAM UPPER SKIN UNDER NUT CLIPS HAVE SURFACE CORROSION AT STA 1640 BL 0-RBL 50. REPAIRED IAW SRM 53-00-51.Feb 24, 2011 · N667DN · Boeing 757232SDR USAA2011040591331Floorbeam · corrodedCLT - Q5/QX6 - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM T-CAP AT BS 344, S17L BETWEEN BL 0 TO LBL 58. REPAIRED FLOORBEAM T-CAP AT BS 344, S17L BETWEEN BL 0 TO LBL 58 IAW B737 SRM 53-10-51 REPAIR 5.Feb 23, 2011 · N419US · Boeing 737401SDR USAA2011031191027Floorbeam · corrodedMIA - C24 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM UPPER T-CAP AT BS 312, LBL 12. REPLACED FLOORBEAM UPPER T-CAP AT BS 312, LBL 12 IAW B737 SRM 53-10-51 REPAIR 5.Feb 23, 2011 · N316AW · Boeing 7373S3SDR USAA2011031191024Floorbeam · corrodedCLT - Q5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM T-CAP AT BS 328 BETWEEN LBL 55 TO RBL 55. REPLACED FLOORBEAM T-CAP AT BS 328 BETWEEN LBL 55 TO RBL 55 IAW B737 SRM 53-10-51 & BOEING DRAWING 65-45812.Feb 23, 2011 · N419US · Boeing 737401SDR IPXA1165047Floorbeam · crackedINSPECTION TYPE:10YR, MAIN CARGO COMPARTMENT OVER THE WING BOX, THE FLOOR SUPPORT BEAM AT FR 51 BETWEEN FLOOR PANEL 242ZJ AND PANEL 242EK IS CRACKED. R & R FLOOR SUPPORT BEAM REF A300-600, SRM 51-40-21, PARA 5, PG 7.Feb 23, 2011 · N129UP · Airbus A300F4622RSDR UALA2011022400936Floorbeam · corrodedCORROSION ON FLOORBEAM BS 1640, RBL 30, RBL 19, RBL 13, AND RBL 10. MAJOR REPAIR ACCOMPLISHED: FOUND TO BE OUT OF LIMITS, R & R DAMAGED SECTION IAW SRM.Feb 23, 2011 · N560UA · Boeing 757222SDR EIAA 2011015Floorbeam · crackedUPPER DECK FLOORBEAM WEB AT BS 400 HAS CRACKED HOLE COMMON TO LT FRAME FAILSAFE CHORD FASTENER. FABBED AND INSTALLED REPAIR BS 400 UPPER FLOORBEAM WEB LBL 24 TO LBL 90 PER B747 SRM 53-100-07 PG 47-48.Feb 23, 2011 · N471EV · Boeing 747273CSDR IPXA1565717Floorbeam · corrodedINSPECTION TYPE:C4, MAIN DECK FLOOR STRUCTURES LT SIDE STA BS 1681.8 BETWEEN LBL 45. 5 TO LBL 54.9 HAS CORROSION. REMOVED CORROSION ORIGINAL THICKNESS .07K LOSS .025 WITH .046 REMAINING IS OUT OF LIMITS IAW SRM 53-00-51-1A . ACCOMPLISHED BLEND REPAIR FOR EFeb 22, 2011 · N455UP · Boeing 75724APFSDR IPXA11565548Floorbeam · corrodedINSPECTION TYPE:C4, MAIN DECK FLOOR STRUCTURE LT SIDE STA 1600 BETWEEN LBL 45.5 TO L BL 54.9 HAS CORROSION AROUND SEVERAL FASTENER HOLES. REPAIRED PER EA 110184 REV IRFeb 22, 2011 · N455UP · Boeing 75724APFSDR FDEA201102220676Floorbeam · corrodedCORROSION ON TOP TEE CAP FLOORBEAM, MAIN CABIN, STA 1030, RBL 45 TO RBL 61. CUT AND REMOVED DAMAGED AREA OF FLOOR BEAM IAW SRM 53-10-8 FIG 3 FABRICATED NEW UPPER TEE, 2 REPAIR ANGLES AND 2 REINFORCEMENT STRAPS IAW SRM 53-10-8 FIG 3. INSTALLED UPPER TEE, Feb 22, 2011 · N485FE · Boeing 727227SDR FDEA201102220681Floorbeam · corrodedCORROSION ON TEE CAP TOP FLOORBEAM MAIN CABIN, STA 680, LBL 45 TO LBL 25. REMOVED CORROSION FROM FLOORBEAM TEE CAP IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIG 4B. FABRICATED 1 TEE CAP 16" LONG, SUPPORT ANGLE 16" LONG, SUPPORT ANGLE 11" LOFeb 22, 2011 · N485FE · Boeing 727227SDR FDEA201102220686Floorbeam · corrodedCORROSION ON FLOORBEAM TEE, STA 1110, RBL 25 TO RBL 45. CUT OUT DAMAGED AREA, FABRICATED FILLER, 2 REPAIR ANGLES AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-8 FIG 8, 51-30-5 AND 51-30-2.Feb 22, 2011 · N571FE · Doug MD1010FSDR FDEA201102220677Floorbeam · corrodedCORROSION ON TEE CAP FLOORBEAM, STA 620, BL 0 TO RBL 25. REMOVED CORROSION. EVALUATED AREA; ORIGINAL THICKNESS .125" MATERIAL LOSS .015" MATERIAL REMAINING .110" FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED AREA APPROX DIM 100". FABRICATED TEE CAP & FILLEFeb 22, 2011 · N485FE · Boeing 727227SDR FDEA201102220678Floorbeam · corrodedCORROSION ON FLOORBEAM TEE CAP, STA 720D, BL 0 TO LBL 25. CUT-OUT DAMAGED AREA AT FLOORBEAM TEE CAP, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 53-10-8 FIG 8.Feb 22, 2011 · N485FE · Boeing 727227SDR FDEA201102220682Floorbeam · corrodedCORROSION ON FLOORBEAM TEE, STA 680, BL 0 TO LBL 25. CUT-OUT DAMAGED AREA, FABRICATED FILLER, 2 REPAIR ANGLES, AND INSTALLED IAW SRM 53-10-8 FIG 8.Feb 22, 2011 · N485FE · Boeing 727227SDR FDEA201102220679Floorbeam · corrodedSTA 377, FLOORBEAM, LBL-60 HAS CORROSION ON LAWER SIDE OF UPPER FLANGE AROUND NUT PLATE HOLES. REMOVED CORROSION AND CHECK LIMITS ORIG MAT. 0.125 AFTER REWORK 0.050. FOUND OUT OF LIMITS IAW SRM 53-00-51 DET III. R & R FLOORBEAM IAW SRM 51-40-02 WITH MAT PFeb 22, 2011 · N926FD · Boeing 7572S7SDR FDEA201102220668Floorbeam · crackedMAIN CARGO COMPARTMENT FLOORBEAM HAS A 0.25 INCH CRACK AT FR 31 BETWEEN SEAT TRACKS Y1456 AND Y1959. BLENDED CRACKED VERTICAL STIFFNER IAW SRM 53-10-15, FIG 212. NDT CHECK COMPLIED IAW NTM 51-10-08 VERIFIED ELIMINATION OF CRACK. REPAIRED CROSSBEAM AT R31Feb 22, 2011 · N674FE · Airbus A300F4605RSDR USAA2011031691080Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y1292. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y1292 IAW A320 SRM 51-72-11.Feb 21, 2011 · N105UW · Airbus A320214SDR USAA2011031691079Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 + 18 INCHES TO FR66 + 4 INCHES, -Y465. REPLACED FLOORBEAM BETWEEN FR65 + 18 INCHES TO FR66 + 4 INCHES, -Y465 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472816.Feb 21, 2011 · N105UW · Airbus A320214SDR USAA2011031691078Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR16, Y1379.5. REPLACED FLOORBEAM BETWEEN FR12 TO FR16, Y1379.5 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112831.Feb 21, 2011 · N105UW · Airbus A320214SDR USAA2011031691077Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR20 TO FR24, Y189. REPLACED FLOORBEAM BETWEEN FR20 TO FR24, Y189 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53111406.Feb 21, 2011 · N105UW · Airbus A320214SDR USAA2011031691076Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 + 18 INCHES TO FR67, -Y318. REPLACED FLOORBEAM BETWEEN FR65 + 18 INCHES TO FR67, -Y318 IAW A320 SRM 51-72-11.Feb 21, 2011 · N105UW · Airbus A320214SDR USAA2011031691075Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y765. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y765 IAW A320 SRM 51-72-11.Feb 21, 2011 · N105UW · Airbus A320214
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