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 SWAA110378Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 324, RBL 21. REPAIRED BEAM PER SRM.SDR USAA2011022890909Floorbeam · corrodedBFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR16A, -Y1959. REPLACED LONGITUDINAL FLOORBEAM AT FR16A, -Y1959 IAW A330 SRM 51-74-03, 51-42-11 & 51-44-11.SDR USAA2011022890903Floorbeam · corrodedBFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR73, Y1670. REPLACED CABIN FLOOR LONGITUDINAL BEAM AT FR73, Y1670 IAW A330 SRM 51-42-11.SDR DALA1106039857Floorbeam · crackedMAIN PASSENGER CABIN STA 617, BL-0 TO LBL-22 FLOOR PANEL SUPPORT IS CRACKED. REMOVED FLOOR SUPPORT & ANGLE ATTACHED. FOUND ANGLE OUT OF LIMITS IAW SRM 51-30-2 & 53-01, FIG 1. RECEIVED NEW ANGLE AND MAT FOR NEW FLOOR SUPPORT. FABRICATED, DRILLED, DEBURRED ANSDR DALA1104623706Floorbeam · corrodedSTATION 987, FLOORBEAM CORRODED BEYOND LIMITS BETWEEN RBL 30 AND RBL34. ACCOMPLLISHED REPAIR IAW SRM.SDR DALA1113420667Floorbeam · corrodedFWD CABIN FLOORBEAM STN 377.7 HAS CORROSION AT SEVERAL NUT PLATE HOLES AS MARKED BETWEEN LBL 65 TO RBL 25. REPAIRED IAW 53-00-51 FIG 201 REPAIR 3.SDR USAA2011022890908Floorbeam · corrodedBFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM BETWEEN FR75 TO FR78, -Y400. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, -Y400 IAW A330 SRM 53-41-14.SDR USAA2011022890907Floorbeam · corrodedBFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR33, Y=0. REPLACED LONGITUDINAL FLOORBEAM AT FR33, Y=0 IAW A330 SRM 51-42-11.SDR USAA2011022890902Floorbeam · corrodedBFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT BEAM AT FR73 BETWEEN Y1910 TO Y2462.6. REPLACED CABIN FLOOR SUPPORT BEAM AT FR73 BETWEEN Y1910 TO Y2462.6 IAW A330 SRM 51-42-11 & 53-41-14.SDR ASOA201100148Floorbeam · crackedATTACH ANGLE/CLIPS ON FS 280 CROSSBEAM ARE CRACKED AT LBL9 AND RBL9. REMOVED DAMAGED CLIPS, FABRICATED NEW SERVICBLE CLIPS AND INSTALLED IAW REO 601R-53-11-171, REV D. MAJOR REPAIR.SDR ASOA201100146Crossbeam · crackedFS 280 CROSSBEAM CRACKED AT CAP BY MLG ALT EXT CABLE PULLEY SUPPORT. REPAIRED DAMAGE IAW REO 601R-53-11-138, REV A. CLASSIFIED A MAJOR REPAIR.SDR USAA2011022890901Floorbeam · corrodedBFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR SUPPORT BEAM AT FR73 BETWEEN -Y1910 TO -Y2462.5. REPLACED CABIN FLOOR SUPPORT BEAM AT FR73 BETWEEN -Y1910 TO -Y2462.5 IAW A330 SRM 51-42-11 & 53-41-14.SDR SWIA201125524Floorbeam · crackedFS 280 FLOORBEAM CRACKED ON BOTH SIDES. (C-CHECK) REPLACE PER SRM.SDR DALA1104731605Floorbeam · corrodedCORROSION ON FLOORBEAM AT FS 865 AND LBL 33. REPAIRED ON NRC 154.SDR FDEA201101200310Floorbeam · corrodedMAIN CABIN STA 395, RBL 11, WL 208, FLOORBEAM TOP STRAP (PLATE) HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. ORIGNAL MAT THICKNESS .125 AFTER REWORK .108 MAT LOSS .017 AREA OF DAMAGE L(1") X W(1") OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL VI. SDR AALA20110120AFW05Floorbeam · corrodedSTATION 347 FLOOR BEAM AT RIGHT BUTTLINE 30 UPPER CHORD CORRODED. REPAIRED DISCREPANCY PER EA 767-53-014761.SDR CALA2011012000029Floorbeam · corrodedB757-53-3-0443 AFT CABIN FLOORBEAM AT STA 1620 HAS CORROSION AROUND TWO FASTNER HOLES AT LBL 3 TO RBL 3 ( MARKED) . CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53 -00-51 REPAIR 3.SDR FDEA201101200312Floorbeam · crackedMAIN CABIN FLOORBEAM CRACKED IN RADIUS FR36 BETWEEN L2 AND L3 SEAT TRACK. REPAIRED CROSSBEAM AT FR36 BETWEEN SEAT TRACKS 2L AND 3L IAW SRM 53-10-15.SDR SWIA201125909Floorbeam · crackedFS 280 FLOORBEAM IS CORRODED. (C-CHECK) REPLACED FS 280 FLOORBEAM.SDR USAA2011022890906Floorbeam · corrodedBFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR78, -Y1137.1. REPLACED CABIN FLOOR LONGITUDINAL BEAM AT FR78, -Y1137.1 IAW A330 SRM 51-42-11.SDR USAA2011022890900Floorbeam · corrodedBFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, Y400. REPLACED LONGITUDINAL FLOORBEAM BETWEEN FR75 TO FR78, Y400 IAW A330 SRM 51-42-11.SDR USAA2011022590881Seat Track · corrodedBFM - S2 - MAJOR REPAIR - LEVEL 2 CORROSION ON CABIN FLOOR LONGITUDINAL BEAM AT FR16A, -Y953. REPLACED CABIN FLOOR LONGITUDINAL BEAM FROM FR16A, -Y953 IAW A330 SRM 53-42-11.SDR DALA1104009857Floorbeam · crackedMAIN PASSENGER CABIN STA 775, RBL 44, FLOORBEAM SUPPORT IS CRACKED AT BOTTOM OF ANGLE. REMOVED CRACKED FITTING, STA 775, RBL 44, LOCATED, DRILLED NEW FITTING, INSTALLED IAW SRM 51-10-4, 51-30-5, DWG 3925812.SDR COEA2011011815805Floorbeam · damagedHEAVY CK / COE / MAJOR REPAIR: MISDRILLED HOLE ON FLOORBEAM 29 AT RT O/B SEAT TRACK CENTER HOLE (BL -0- 37.82") WAITING FOR STRUCTURAL REPAIR INSTRUCTIONS FROM ATR.SDR DALA1104059857Floorbeam · chafedMAIN PASSENGER CABIN STA 237, RBL 4 -RBL 8, FLOORBEAM CHAFED. BLENDED CHAFE IAW SRM 51-10-3, ORIG MAT .125 IAW SRM 51-10-1, FIG 22, PN 2777897 AND 51-13-2, ITEM 6. REMOVED .040 REMAINING .085 FOUND TO BE OUT OF LIMITS IAW SRM 53-05, FIG 20A. REPAIRED DAMAGESDR UALA2011011900304Floorbeam · corrodedFLOORBEAM AT STA 324, RBL 58 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED: REPAIRED FLOORBEAM T-CHORD PER EA PD 57-53-071 AND UA EVA 80477. MECH P531 INSP Q834 A NEW FAA FORM 8100-9 SHOWING COMPLIANCE TO 14CFR 25.571 AND 26. 43 (D) MUST BE ISSUED WITHIN 24 MONTHSDR USAA2011021490740Floorbeam · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR 64 - FR 66, -Y1292. REPLACED FLOORBEAM AT FR 64 - FR 66, -Y1292 IAW A319 SRM 51-72-11.SDR USAA2011021490735Floorbeam · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR 68 - FR 69, -Y1162. REPLACED FLOORBEAM AT FR 68 - FR 69, -Y1162 IAW A319 SRM 51-72-11.SDR USAA2011021490734Floorbeam · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR 66 - FR 68, -Y1292. REPLACED FLOORBEAM AT FR 66 - FR 68, -Y1292 IAW A319 SRM 51-72-11.SDR USAA2011020790552Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR20 TO FR24, -Y189. REPLACED FLOORBEAM BETWEEN FR20 TO FR24, -Y189 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53111406.SDR USAA2011020790551Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y765. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.SDR USAA2011020790550Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y254. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112816.SDR USAA2011020790549Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR67, -Y318. REPLACED FLOORBEAM BETWEEN FR65 TO FR67, -Y318 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472814.SDR USAA2011020790548Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2011020790547Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 + 10 INCHES TO FR66, -Y765. REPLACED FLOORBEAM BETWEEN FR64 + 10 INCHES TO FR66, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2011020790546Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 + 15 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 + 15 INCHES, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2011020790545Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y254. REPLACED FLOORBEAM AT FR20, -Y254 IAW A319 SRM 51-72-11.SDR USAA2011020790543Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y160. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y160 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2011020790542Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 17 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 + 17 INCHES TO FR70, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2011020790541Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, -Y465 IAW A319 SRM 51-72-11.SDR USAA2011020790540Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR67 + 15 INCHES, Y1162. REPLACED FLOORBEAM AT FR67 + 15 INCHES, Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2011020790539Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, Y765. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.SDR FDEA201101170211Floorbeam · corrodedCORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 560 BL0 TO LBL 25. CUT OUT DAMAGE IAW SRM 53-10-8 FIG 3. LOCATED AND DRILLED NEW UPPER TEE, AND 4 SUPPORT ANGLES AND 4 REINFORCEMENT STRAPS IAW SRM 53-10-8 FIG 3. INSTALLED TEE, SUPPORT ANGLES AND STRAPS IAW SRSDR DALA1104189857Floorbeam · crackedMAIN PASSENGER CABIN STA 775, LBL 44, FLOORBEAM SUPPORT IS CRACKED AT BOTTOM OF ANGLE. REMOVED CRACKED FITTING LOCATED DRILLED DEBURRED NEW FITTING & INSTALLED IAW DWG 392581241, SRM 51-10-4, 51-30-5, 51-30-2, & 51-30-1. REQUIRED INSPECTION COMPLETED.SDR FDEA201101170219Floorbeam · corrodedFLOORBEAM AT STA 780, RBL 45 TO RBL 50 HAS CORROSION ON UPPER CHORD. CORRODED FLOORBEAM AT STA 780, FROM RBL 45 TO RBL 50, R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR.SDR FDEA201101170218Floorbeam · corrodedMAIN DECK FLOOR AT STA 1640, LBL 56, HAS CORROSION ON BOTTOM SIDE OF FLOORBEAM. AT LOWER SIDE OF FWD FLANGE. CORRODED FLOORBEAM AT STA 1640 R & R IAW SRM 51-40-02, REV.101. REPAIR IS CLASSIFIED AS MINOR.SDR SWAA110272Floorbeam · corrodedDURING SCHEDULED 10Y CHECK, FOUND FLIGHT COMPARTMENT FLOOR SUPPORT ANGLE CORRODED AT BS 260, BETWEEN LBL 10 TO RBL 10. REPAIRED FLOORBEAM PER AAR EA.SDR SWAA110269Floorbeam · corrodedDURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 24 TO LBL 45. REPAIRED BEAM PER SRM.SDR USAA2011020990663Floorbeam · corrodedCLT - MAJOR REPAIR - Q1 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 328, RBL 26. REPAIRED FLOORBEAM AT BS 328, RBL 26 IAW B737 SRM 53-00-51.SDR USAA2011020190471Floorbeam · corrodedCLT - Q3 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 986.5 BETWEEN LBL 24 TO LBL 40. REPAIRED FLOORBEAM AT BS 986.5 BETWEEN LBL 24 TO LBL 40 IAW EA 40627A.
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