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 USAA2011071900018Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, -Y1292 IAW A319 SRM 51-72-11.SDR USAA2011071900017Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 PLUS 5 INCHES TO FR67 PLUS 15 INCHES, -Y1227. REPLACED FLOORBEAM BETWEEN FR65 PLUS 5 INCHES TO FR67 PLUS 15 INCHES, -Y1227 IAW A319 SRM 51-72-11.SDR USAA2011071900016Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 PLUS 15 INCHES TO FR69, -Y1162.5. REPLACED FLOORBEAM BETWEEN FR67 PLUS 15 INCHES TO FR69, -Y1162.5 IAW A319 SRM 51-72-11.SDR USAA2011071800029Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR67 PLUS 16 INCHES, Y1227. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR67 PLUS 16 INCHES, Y1227 IAW A319 SRM 51-72-11 AIRBUS DRAWING D53472780.SDR USAA2011071800027Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67 PLUS 9 INCHES, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67 PLUS 9 INCHES, -Y465 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472816.SDR USAA2011071800028Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 PLUS 16 INCHES TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR67 PLUS 16 INCHES TO FR69, Y1162 IAW A319 SRM 51-72-11 AIRBUS DRAWING D53472780.SDR USAA2011072100024Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472816.SDR USAA2011071800026Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, Y765 IAW A320 SRM 51-72-11AND AIRBUS DRAWING D534472000.SDR USAA2011071800025Floorbeam · 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.SDR USAA2011071900021Floorbeam · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON CABIN FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765. REPLACED CABIN FLOORBEAM IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.SDR USAA2011071900020Floorbeam · corroded2S CHECK - LEVLE 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR67 + 10 INCHES, Y512. REPLACED FLOORBEAM ASSEMBLY IAW A319 SRM 51-72-11.SDR K11A2012060716007Floorbeam · corrodedMAIN DECK FLOORBEAM HAS CORROSION ON SKIN AND STIFFENER (SEVERAL SPOTS 1X1 INCHES).SDR USAA2011062700022Floorbeam · corrodedBFM - BC3 - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR66, Y1442. REPLACED LONGITUDINAL BEAM AT FR66, Y1442 IAW A320 SRM 51-42-11.SDR VNAA2011062600023Floorbeam · crackedDURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR SWAA114647Floorbeam · crackedDURING SCHEDULED 26Y CHECK, FOUND STUB FLOORBEAM CHORD CRACKED AT BS 639, BETWEEN RBL 48 TO RBL 55. REPAIRED CHORD IAW EA.SDR COMA2011062490006Floorbeam · corrodedFS 280 FLOORBEAM CORRODED AT LBL 9 - RBL 9. REMOVED AND REPLACED CORRODED SECTION OF FLOORBEAM AT FS 280 IAW BOMBARDIER REO 690-53-11-032, 690-53-11-092.SDR FDEA201106232400Floorbeam · gougedFLOORBEAM UPPER FLANGE UPPER SURFACE IS GOUGED STA 950F, RBL 3- RBL 6. CUTOUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR PARTS ON FLOORBEAM UPPER FLANGE IAW SRM 53-10-8 FIG 3.SDR ASAA11410206Floorbeam · corrodedCORROSION ON CABIN FLOORBEAM STA 947 LBL 24 RBL 24. C/W REPAIR OF 947 UPPER CAP IAW EA 400 53EA 05889 REV NEW DATE ISSUED 18 JUL 2011.SDR UIEA2011062200343Floorbeam · crackedDURING THE "C4/A4 CHECK" WHILE COMPLYING WITH SB 747-53A2459 REV 1, CRACK DAMAGE WAS DETECTED AT LBL 68 IN 65B10927-45 FLOORBEAM WEB. REPAIRED CRACK DAMAGED FLOORBEAM WEB IAW SB 747-53A2459 REV 1, DWG 141U0044 SHEET 2 VIEW 1C11 AND EO RS R-53-25-37120 REV A.SDR UIEA2011062200342Floorbeam · damagedDURING THE "C4/A4 CHECK" WHILE COMPLYING WITH SB 747 -53A2459, REV. 1, CRACK DAMAGE WAS DETECTED AT AT LBL 68 IN 65B10927-16 FLOORBEAM CHORD AND DOCUMENTED IAW NRC 50199 (SEE FIGURE 1). COMPLETED THE FLOORBEAM UPPER CHORD SPLICE REPAIR AT BS 340 IAW SRM 53-SDR ASAA1149942Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED AT FASTENER HOLE AT FS 967 LBL 28. REMOVED CORROSION AND REPAIRED FLOORBEAM AT FS 967 LBL 28 IAW B737 400 SRM 53 00 51.SDR CHQA201100258Floorbeam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE CARGO FLOOR STRUCTURE ENTRANCE AREA LOWER BEAM. MAINTENANCE REPLACED THE CARGO FLOOR STRUCTURE ENTRANCE AREA LOWER BEAM WITH NO FURTHER DEFECTS NOTED.SDR UALA2011062303082Floorbeam · corrodedFLOORBEAM AT STA 310.5 RBL 35-39 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. REMOVED CORROSION DAMAGE & ACCOMPLISHED NDT OF CUT-OUT AREA & HFEC SCAN OF FASTENER HOLES COMMON TO REPAIR PER EA PD57-53-135. FABRICATED & INSTALLED TEE SECTION REPAIR, REPAIR ANGLESDR UALA2011062303080Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 324 BL 53R. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED FLOORBEAM, SPLICE ANGLES AND SPLICE STRAPS PER EA PD57-53 -136 AND EVA 80900 ON NR 2673N00125.SDR SWIA201126589Floorbeam · crackedFS 280 FLOORBEAM CRACKED. (C-CHECK) REPLACE PER REO.SDR DALA1141110627Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED STA 377.7 LBL 24 TO RBL 24 TO RBL 24 WITH A GOUGE FROM A CHERRY MAX STEM AT LBL 32. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 187276 W/O 87881700001. PER ER/A 493049-14 REV ORIGINAL.SDR ASOA201101209Floorbeam · corrodedCABIN FLOORBEAM AT FS 349.00 CORRODED AT OTBD END RBL 45. BLENDED MINOR CORROSION, REMOVING .005" D MAX DAMAGE .058" REMAINING WITHIN LIMITS IAW SRM 51-21-06 IAW 53-00-00 AND 53-21-15.SDR ASOA201101208Floorbeam · corrodedCABIN FLOORBEAM AT FS 349.00 BETWEEN RBL 27 AND RBL 45 IS CORRODED AT SEVERAL LOCATIONS ALONG ENTIRE LENGTH. REPAIRED IAW SRM 51-42-10, 51-21-06, IAW 53-00-00 AND 53-21-15. MINOR REPAIR.SDR ASOA201101206Floorbeam · crackedFS 280.00 INBD AND OTBD FLOORBEAM ANGLE CRACKED AT LBL 9 AND RBL 9. REMOVED IAW SRM 51-42-06 AND 51-42-21. INSTALLED IAW SRM 51-42-21.SDR FDEA201106212426Floorbeam · corrodedFLOORBEAM, BS 620, BL0 TO LBL 25 UPPER SURFACE HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 - FLOORBEAM BS 620 BL 0 - LBL 25. CUTOUT DAMAGE AREA FLOORBEAM IAW SRM 53-10-8 - FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG 3. TREATED &SDR USAA2011070100009Floorbeam · corrodedPIT - C11 - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR67 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR67 TO FR68, -Y1292 IAW A320 SRM 51-72-11 AIRBUS DRAWING 18D53472780 & 18D53472816.SDR USAA2011062300015Floorbeam · corrodedBFM - C3 - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR68, -Y765. REPLACED LONGITUDINAL BEAM AT FR68, -Y765 IAW A320 SRM 51-44-11 & SRM 51-42-11.SDR SWAA114549Floorbeam · crackedDURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 636, LBL 45.5. REPAIRED WEB PER ER.SDR FDEA201106202348Floorbeam · corrodedFLOORBEAM CORRODED STA 620 BL 0 TO LBL 24. CUTOUT DAMAGED AREA IAW SRM 51-10-2. FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG 3. TREATED AND PRIMED NEW PARTS IAW SRM 51-10-2. INSTALLED NEW PARTS IAW SRM 51-30-2.SDR UIEA2011062000346Floorbeam · crackedDURING THE "C4/A4 CHECK" WHILE COMPLYING WITH SB-53A2459 REV. 1, CRACK DAMAGE WAS DETECTED AT AT RBL 72 IN 65B10928-58 FLOORBEAM WEB. REPAIRED DAMAGED IAW REPAIR SRM 53-10-07, FIG 11.SDR UALA2011062103038Floorbeam · crackedSTA 700 FLOORBEAM CRACKED FWD FACE TO UPPER CHORD RADIUS AT LBL 24.75 AND LBL 45.5. MAJOR REPAIR ACCOMPLISHED: REPAIRED ON SMB W-US C1389M AND S8433M, PER EVA 80930 AND SRM 53-00-51 FIG 201, RPR.3. CUT DAMAGE, HFEC CUTOUT AND HOLES, INSTALLED DOUBLERS, FILLSDR SWAA114526Floorbeam · crackedDURING SCHEDULED SPV CHECK, FOUND FLOORBEAM LOWER T-CHORD CRACKED AT AIR STAIR FWD STOP FITTING FWD HOLE. REPAIRED T-CHORD PER ER AND EA.SDR USAA2011062300013Floorbeam · corrodedBFM - C3 - LEVEL 2 EXFOLIATION CORROSION ON LONGITUDINAL BEAM AT FR66 -Y1292. REPLACED LONGITUDINAL BEAM AT FR66 -Y1292 IAW A320 SRM 53-00-14, 51-74-00, 51-42-11 & 51-75-12.SDR USAA2011062300012Floorbeam · corrodedBFM - C3 - LEVEL 2 WIDESPREAD EXFOLIATION CORROSION ON LONGITUDINAL BEAM BETWEEN FR66 TO FR68, Y765. REPLACED LONGITUDINAL BEAM BETWEEN FR66 TO FR68, Y765 IAW A320 SRM 53-00-14, 51-74-00, 51-42-11 & 51-75-12.SDR SWAA114501Floorbeam · crackedDURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, LBL 45. REPAIRED WEB PER EA.SDR SWAA114500Floorbeam · crackedDURING SCHEDULED 14Y CHECK, FOUND LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 639, RBL 45. REPAIRED WEB PER EA.SDR SWAA114485Angle · crackedDURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM ANGLE CRACKED AT BS 639, LBL 45.5. REPAIRED ANGLE PER EA.SDR ASAA11410002Strap · brokenFLOORBEAM STRAP BROKEN AT FS 312. FABRICATED, DRILLED, TREATED AND INSTALLED REPAIR IAW B737 400 SRM 53 10 51. FIG.201.SDR EE4Y20110413Floorbeam · crackedLOWER FUSELAGE, FR28-STA 1163 BETWEEN STRINGER 38LT AND STRINGER 38RT, FWD CARGO COMPARTMENT FLOOR SUPPORT PLATE WITH CRACK. NOTE: THE PLATE CRACK REQUIRES A MAJOR REPAIR IAW ENGINEERING GUIDELINES.SDR SWAA114495Floorbeam · corrodedDURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, BETWEEN RBL 53 TO RBL 56. REMOVED AND REPLACED ANGLE PER SRM.SDR DALA1142166803Floorbeam · corrodedCORROSION DAMAGE WAS FOUND TO THE UPPER CHORD OF THE STA 324 FLOORBEAM FROM RBL 33 TO THE O/B END. THE SUBJECT CHORD WILL BE REMOVED AND A NEW SECTION WILL BE SPLICED IN. THE SUBJECT CHORD IS MADE FROM 7075-T6511 ALUMINUM EXTRUSION PER AND 10136-2409.SDR EIAA2011058Floorbeam · corrodedFWD CARGO FLOORBEAM BS 640 LBL HAS CORROSION UNDER NUT PLATE FWD SIDE OF T-CHORD. REMOVED CORROSION REPLACED T-CAP INSTALLED REPAIR ANGLES PER B747 SRM 51-40-04 FIG 2.SDR DALA1140480627Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED STA 1640 BL 0 TO RBL 23. C/W AT SAA/SAT AS PER ER/A 493040-14 REV, ORIGINAL. ON NONROUTINE 194594 W/O 87878960001.SDR USAA2011062100021Floorbeam · corrodedPIT - GALLEY MAT - CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPAIRED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW EA 200142.SDR USAA2011062100020Floorbeam · corrodedPIT - GALLEY MAT - CORROSION ON UPPER CAP OF FLOORBEAM BETWEEN FR66 TO FR68 + 3 INCHES, -Y765. REPAIRED UPPER CAP OF FLOORBEAM BETWEEN FR66 TO FR68 + 3 INCHES, -Y765 IAW A320 53-00-14 & EA 200143.
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