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 ASOA201001802Floorbeam · crackedLBL 27 FLOORBEAM CAP IS CORRODED AROUND NUTPLATES AT FS 605.00. FLOORBEAM REPAIRED IAW SRM 51-21-11. ACFT RETURNED TO SERVICE.SDR USAA2010120992959Floorbeam · corrodedMCN - C20 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT BS 312 BETWEEN LBL 17 TO LBL 24. REPLACED FLOORBEAM AT BS 312 BETWEEN LBL 17 TO LBL 24 IAW B737 SRM 53-10-51.SDR FDEA201011164396Floorbeam · corrodedAT STA 1681, FLOORBEAM HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE OF FLOOR. REMOVED CORROSION IAW SRM 51-10-01 FOUND FLOOR BEAM OUT OF LIMITS ORIG. MAT 0.150 AFTER BLEND OUT THE WORST SPOT 0.091 IAW SRM 53-00-51 DETAIL VI. REMOVED AND REPLACED FLOORBEASDR SWAA107122Floorbeam · crackedDURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 670, RBL 24.5. REPAIRED BEAM PER EA.SDR SWAA107121Floorbeam · crackedDURING SCHEDULED SPV CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 672, RBL 24.5. REPAIRED BEAM PER EA.SDR FDEA201011164397Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1661, RBL 42, RT SIDE MAIN CABIN. FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 DETAIL II FABRICATED FLOORBEAM 1661 FROM MAT BAC1518-338 BATCH 1915536 LOCATED AND DRILLED IAW SRM 51-40-05. REMOVED AND REPLACED IAW SRM 51-49-0SDR SWAA107086Floorbeam · crackedDURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 727B, LBL 45. REPAIRED CHORD PER EA.SDR SWAA107080Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 26. REPAIRED BEAM PER ER AND EA.SDR SWAA107049Floorbeam · crackedDURING SCHEDULED 10Y CHECK, FOUND NR 4 LONGITUDINAL FLOORBEAM CRACKED AT BS 739A. REPAIRED BEAM PER EA.SDR DALA1032595532Floorbeam · corrodedDURING M-CHECK, FOUND FLOORBEAM STA 365 UPPER CORD FROM BL0 TO RBL 60 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02 DIM. L=44" W=2" D=.065" ORIG MAT .130" FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51, REMOVED FLOORBEAM REPAIR IAW SRM 51-40-02 FABRICATED NEWSDR FDEA201011164398Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1640, FROM RBL 62 TO LBL 62, MAIN CABIN. REMOVED CORROSION AT FLOORBEAM, STA 1640 FROM RBL 62 TO LBL 62, MAIN CABIN IAW SRM 53-00. ORIGINAL MATERIAL .130, AFTER REWORK .095, AMOUNT OF MATERIAL REMOVED TO BE IN OUT OF LIMITS IAW SRMSDR DALA1304116902Floorbeam · damagedDURING HMV, TOOLING DAMAGE WAS FOUND ON BS 580 FLOORBEAM LOCATED AT THE LOWER TEE FORWARD FLANGE. REPAIRED IAW ERA 486838-14.SDR FDEA201011154363Floorbeam · corrodedCABIN STN 345, RBL 25 TO LBL 25, FLOORBEAM SURFACE CORROSION ON BEAM CAP AROUND FLOOR PANEL ATTACHING HOLES. CORRODED FLOORBEAM AT STA 345 REMOVED AND REPLACED IAW SRM 51-40-02 REV.101. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100.SDR WX0A070688Floorbeam · corrodedLEFT AFT LAV FLOORBEAM CORRODED STA 1322, LBL 27 TO RBL 27. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW MD80 SRM 53-05 FIG 79A AND SRM 51-10-4 PAGE 1 AND PARA 6, FIG 3A.SDR WX0A070687Floorbeam · corrodedAFT CARGO PIT AREA CABIN FLOORBEAM IS CORRODED FS 1309, LBL 15 TO LBL 22. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW MD80 SRM 51-70-5 FIG 2.SDR ASOA201001786Floorbeam · corrodedCONTINUED FROM MWC 7107425/100, TOP PLATE ON FLOORBEAM AT RBL9.0 FS 485 TO 581 HAS SEVERAL SPOTS OF CORROSION. REPAIRED IAW REO 670-31-184.SDR UALA2010111604240Floorbeam · crackedBS 770, MID GALLEY FLOOR CENTER RIGHT TRANSITION FLOORBEAM CRACKED. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED TRANSITION BEAM IAW SRM, LOCATED, DRILLED AND DEBURRED NEW BEAM P/N STA 770 MID GALLEY FLOOR. INSTALLED NEW FLOORBEAM IAW SRM.SDR UALA2010111604238Floorbeam · corrodedMAIN CABIN BS 345 FLOORBEAM CORRODED UNDER CLIP NUT AT RBL 12 AND MATERIAL REMAINING AFTER CORROSION REMOVAL EXCEEDS SRM LIMITS. MAJOR REPAIR ACCOMPLISHED: FABRICATED TWO REPAIR ANGLES IAW SRM, NDT INSP OF CUTOUT ACCOMPLISHED WITH NO CRACKS FOUND, ALODINED ASDR SWAA107047Floorbeam · crackedDURING SCHEDULED 14Y CHECK, FOUND FLOORBEAM CRACKED AT BS 668, LBL 24. REPAIRED BEAM PER EA.SDR SWAA106999Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 987, BETWEEN BBL 0 TO RBL 46. REPAIRED BEAM PER SRM.SDR SWAA106988Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 663.75, RBL 24.5. REPAIRED BEAM PER EA.SDR SWAA106987Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, LBL 25. REPAIRED BEAM PER EA.SDR SWAA106986Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 744A, RBL 25. REPAIRED BEAM PER EA.SDR SWAA106984Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 668, LBL 25. REPAIRED BEAM PER EA.SDR SWAA106983Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 664, LBL 25. REPAIRED BEAM PER EA.SDR SWAA106982Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 661, LBL 25. REPAIRED BEAM PER EA.SDR USAA2010121092972Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y168. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y168 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2010120992960Floorbeam · corrodedMCN - C20 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION UPPER SIDE OF FLOORBEAM CHORD AT BS 294.5 BETWEEN LBL 22 TO RBL 60. REPAIRED FLOORBEAM CHORD AT BS294.5 BETWEEN LBL 22 TO RBL 60 IAW B737 SRM 53-10-51.SDR DALA1034705533Floorbeam · corrodedDURING M-CHECK FOUND MAIN CABIN FLOORBEAM CORRODED ON UPPER SURFACE OF REPAIR CHORD EXTENDING ONTO ORIGINAL CHORD ON BOTH ENDS, STA 345, RBL 36 TO LBL 18. REMOVED CORRODED EXISTING REPAIR FLOORBEAM STA 345 CUT OUT FLOORBEAM FROM LBL 53 TO RBL 36, FABRICATESDR USAA2010120192736Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y254. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y254 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2010120192735Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - 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.SDR USAA2010120192734Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 TO FR70, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.SDR USAA2010120192733Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR66 + 1 INCH, Y765. REPLACED FLOORBEAM AT FR66 + 1 INCH, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D534720000.SDR USAA2010120192732Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67, -Y465 IAW A320 SRM 51-72-11.SDR SWAA106980Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 662, RBL 25. REPAIRED BEAM PER ER AND EA.SDR SWAA106974Floorbeam · crackedDURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 24. REPAIRED BEAM PER EA.SDR SWAA106973Floorbeam · crackedDURING SCHEDULED 16Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 727B, RBL 45. REPAIRED BEAM PER EA.SDR DALA1031699853Floorbeam · damagedDURING M CHECK FOUND MAIN CABIN STA 712 LBL 56 FLOORBEAM WEB MISSED DRILLED & PILOT HOLES NOT USED FOUND AFTER REMOVAL OF FRAME REMOVED DAMAGED FLOORBEAM WEB AT STA 712 L/H SIDE LBL 56. FABRICATED NEW FLOORBEAM WEB 7075-T6 .063 IAW DC-9 DWG#19923411. TREATED,SDR F3LA2010111400547Floorbeam · corrodedC-CHECK: NON ROUTINE N0566; MAIN CABIN FLOORBEAM RT SIDE NR4 BETWEEN FRAME 67-69, CORROSION ON BOTTOM SIDE OF FLOORBEAM AT FASTENER HOLE. R & R FLOORBEAM IAW SRM 51-72-11, PAGE 1 AND 2.SDR F3LA2010111400544Floorbeam · corrodedC-CHECK: NON ROUTINE N0557; MAIN CABIN FLOORBEAM, NR 4 LT BETWEEN FRAME 67-68 HAS APPROX 2 SQ IN OF CORROSION AT THE FASTENER HOLES. R & R FLOORBEAM IAW SRM 51-44-11, SRM 51-42-11.SDR USAA2010120892928Floorbeam · corrodedSAL - MAJOR REPAIR - S5 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 +5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 +5 INCHES, -Y765 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53472000.SDR USAA2010120192731Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765 IAW A320 SRM 51-72-11.SDR FDEA201011134340Floorbeam · corrodedFLOORBEAM CORRODED STA 620 LBL 45 TO LBL 25. REMOVED PREVIOUS REPAIR AND CUT-OUT FLOORBEAM DIM. 28.75". FABRICATED AND INSTALLED REPAIR UPPER CHORD AND SPLICES FROM BAC 1505-100617 7075T73511 DIM. 105" LONG, SPLICE FROM BAC 1490-2831 7075T62 DIM. 7.3" LONG, ANSDR FDEA201011134341Floorbeam · corrodedFLOORBEAM CORRODED STA 560, LBL 25 TO LBL 45. CUT-OUT DAMAGED AREA TOP TEE CAP FLOORBEAM BS 560 LBL 36.40 TO 39 APPROX DIM. 2.6" X .90", FABRICATED REPAIR PARTS 2EA ANGLES FROM BAC 1490-2888-7075T6 DIM.19.5" X 0.90" AND 9.6" X .080". REPAIR FILLER FROM 2024SDR FDEA201011134345Floorbeam · corrodedFLOORBEAM CORRODED STA 380, RBL 25 TO RBL 45. CUT OUT DAMAGED AREA DIMS 2.3" X .90". FABRICATED 2 REPAIR ANGLES USING BAC1490- 2888-7075T6 DIMS 13.4" X 2.7" AND 10.2" X 2.6" AND INSTALLED IAW SRM 53-10-8 AND SRM 53-10- 2.SDR FDEA201011134342Floorbeam · corrodedFLOORBEAM CORRODED STA 440, LBL 25 TO BL 0. CUT OUT DAMAGED AREA DIMS 2.5" X 2". FABRICATED UPPER CHORD USING BAC1505-100617-7075T3 DIMS 15.10", SUPPORT ANGLE USING BAC1490-2785-7075T6 DIMS 15.10", SUPPORT ANGLE USING BAC1490-2831-7075T6 DIMS 11.65", REINFORCSDR AALA20101113TUL02Attach Fitting · damagedFLOORBEAM ATTACH FITTING (CASTING) AT STATION 294 LEFT UNDER NUMBER 1 SEAT FLOORBEAM ATTACH FITTING (CASTING) AT STATION 294 LEFT UNDER NUMBER 1 SEAT TRACK HAS DAMAGE ON UPPER AFT SIDE FLANGE. INSTALLED FLOORBEAM FITTING AT STATION 294 LEFT SRM 51-30-05 AND ESDR CALA2010111500538Floorbeam · corrodedAFT WET AREA FLOORBEAM CORRODED STA 1640 AT BL 0. (MARKED) FABRICATED, TREATED, PRIMED,AND INSTALLED REPAIR PARTS (PART 1 CHORD, PART 2 ANGLE, PART 3 ANGLE, PART 4 STRAP AND PART 5 STRAP) FROM LBL 33-RBL 10 AT STA 1640 REF SRM 53-00-51, SRM 51-40-02 AND SRM SDR DALA1031669853Support Angle · crackedDURING M-CHECK FOUND MAIN CABIN STA 712 LBL 45 FLOORBEAM WEB LOWER SUPPORT ANGLE CRACKED. REMOVED DAMAGED ANGLE AT STA 712 LBL 45, FABRICATED NEW SUPPORT ANGLE IAW DC9 DWG 5910464, HEAT TREATED NEW ANGLE PER PEMCO TRAVELER 2281N01724 TREATED, PRIMED, & INSTALSDR DALA1031639853Floorbeam · damagedDURING M- CHECK FOUND MAIN CABIN STA.712 LBL 56 FLOOR BEAM WEB MISSED DRILLED & PILOT HOLES NOT USED FOUND AFTER REMOVAL OF FRAME. REMOVED DAMAGED FLOORBEAM WEB AT STA 712 LT SIDE LBL 56 FABRICATED NEW FLOORBEAM WEB 7075T6 .063 IAW DC9 DWG 19923411. TREATED,
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