JASC 5315
Service difficulty reports · 44,187
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 CALA2026052816583Floorbeam · corrodedCORROSION IN VARIOUS LOCATIONS ON TOP SIDE OF FLOORBEAM, BS 328, RBL13, RBL21, RBL27, RBL 38, AND RBL46. REMOVED CORRODED TEE SECTION FROM PREVIOUS REPAIR AT STA 328 BETWEEN RBL 2 AND RBL65, FABRICATED AND INSTALLED NEW TEE SECTION WITH SAME LENGHT AND SHAPESDR DALA2026052003087Floorbeam · corrodedCORROSION FOUND AFFECTING THE UPPER CHORD OF AN EXISTING REPAIR AT FLOORBEAM BS 947.5, RBL 53. FLOOR PANEL ATTACHMENT HOLE. REPAIRED FLOORBEAM IAW 53-70-51-2R PROCEDURE 5. (LOG 1597210 - AIRCRAFT WAS GROUNDED).SDR CALA2026051816349Floorbeam · corrodedMAIN CABIN AFT WET AREA, FLOOR BEAM REPAIR HAS CORROSION ON UPPER SURFACE AT BS 947.5 APPROX RBL51. TRANSCRIBED FROM AAR GSO NRC 9288256. ACCOMPLISHED ESFR ACCOMPLISHED REPAIR PER UNITED ECRA 5375-01022 REO- A/C 0255 FLOOR BEAM STATION 947.50 BETWEEN RBL30 ANDSDR 4VAA202605150030Floorbeam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE FLOOR BEAM FRAME IN SERVICE (AFT) DOOR AREA. THE FRAME WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060705.SDR 4VAA202605150029Floorbeam · crackedDURING INSPECTION, CORROSION AND A CRACK WAS FOUND ON THE FLOOR BEAM FORWARD ENTRANCE AREA. THE BEAM WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060702.SDR 4VAA202605150011Floorbeam · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE FLOORBEAM AT THE ENTRANCE. THE BEAM WAS REPLACED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060702.SDR DALA2026051903057Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 1016 AT RBL35. PERFORMED FLOORBEAM STRAP REPAIR AT BS 1016 RBL 35 IAW B737-900 ERA 634321-14. (LOG 1595076 - AIRCRAFT WAS GROUNDED).SDR DALA2026051903056Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 1016 AT LBL 35. PERFORMED FLOORBEAM REPAIR STRAP AT BS 1016 LBL 35 IAW ERA 634321-14. (LOG 1595064 - AIRCRAFT WAS GROUNDED).SDR SWAA2026071398474Floorbeam · corrodedAFT CABIN FLOORBEAM UPPER FLANGE HAS EVIDENCE OF CORROSION AT BS 947, RBL 51, JUST BELOW LAV ATTACH FITTING. MEASURED CORROSION TO BE 0.060, DEEP REMAINING THICKNESS IS 0.120, FLOORBEAM UPPER FLANGE IS OUT OF LIMITS IAW SRM 53-70-51-1A-1. CUT AND REMOVED TSDR SWAA2026071398475Floorbeam · corrodedAFT CABIN FLOORBEAM UPPER FLANGE HAS EVIDENCE OF CORROSION AT BS 947, RBL 25. JUST BELOW LAV ATTACH FITTING, TTG8Q01C6CMA. MEASURED CORROSION TO BE 0.020 DEEP REMAINING THICKNESS IS 0.160 FLOORBEAM UPPER FLANGE IS OUT OF LIMITS IAW SRM 53-70-51-1A-1. REPAISDR SWAA2026071302952Floorbeam · corrodedFWD WET AREA FLOORBEAM BS 328, RBL 40, AFT FLANGE CORROSION ON UPPER SURFACE ADJACENT TO RIVET HEAD. BLENDED CORROSION ON UPPER CHORD; AFT FLANGE OF THE TRANSVERSE FLOORBEAM AT BS 328, RBL 40 IAW SRM 51-10-02. REMOVED .027 OF MATERIAL. REMAINING THICKNESS IS SDR SWAA2026071302951Floorbeam · corrodedFWD WET AREA FLOORBEAM BS 328 RBL 39; FWD FLANGE; CORROSION AT FLOOR PANEL ATTACH HOLE UPPER AND LOWER SURFACE. BLENDED CORROSION ON UPPER CHORD, FWD FLANGE OF THE TRANSVERSE FLOORBEAM AT BS. 328; RBL 39 IAW SRM 51-10-02. REMOVED .026 OF MATERIAL. REMAININGSDR AALA202606163971Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT BS 947 AND LBL 50. REPAIRED CHORD PER SRM 53-70-51-2R-5 ALTERNATIVE 2.SDR AALA202606051660Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT BS 947 AND LBL 25.5. REPAIRED CHORD PER SRM 53-70-51-2R-5.SDR JR2R20260514222Floorbeam · corrodedFWD WET AREA LH FR17 CROSSBEAM FLOOR SUPPORT CORRODED. REPLACEDSDR SWAA2026061700968Floorbeam · corrodedCORROSION ON FLOORBEAM BS 344, RBL 7, WL 208.1 IN THE FWD GALLEY AREA. PERFORMED REPAIR CATEGORY A LOCATED ON FLOORBEAM BS 344 AND BTW LBL10 TO RBL 20 IAW SRM 53-10-51-2R-10, REPAIR 10, AND EA 26-153-01400.SDR AALA202606055487Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT BS 947 BETWEEN BL 0 AND RBL 16. REPAIRED CHORD PER SRM 53-70-51-1-1A-1 .SDR MASA20260529133Floorbeam · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII, FLOOR STRUCTURE CORROSION FOUND ON CROSSBEAM AT FR 84 LBL08_ CROSSBEAM AT FR 84 LBL08 HAS BEEN REPAIRED IAW ETD2026-170-008647.SDR JR2R20260513885Floorbeam · corrodedFWD WET AREA RH FR16 CROSSBEAM FLOOR SUPPORT CORRODED. REPLACEDSDR SWAA2026061897994Floorbeam · corrodedCORRODED FLOORBEAM BS 947.5, LBL 25, WL 208.1 AT AFT GALLEY AREA. THIS REPAIR HAS BEEN ACCOMPLISHED IAW SRM 53-70-51-2R-5 ALTERNATIVE 2 WITH A MINOR DEVIATION CONSIDERED ACCEPTABLE AS PER EA 26-153-01390.SDR SWAA2026061897990Floorbeam · corrodedCORRODED FLOORBEAM, BS 947.5, LBL 53, WL 208.1 IN THE AFT GALLEY AREA. REPAIRED THE UPPER TEE FLOORBEAM WILL BE INSTALLED ON FAULT TTG8Q01C5CAC IAW SRM 53-70-51-2R-5, REPAIR 5.SDR SWAA2026061897869Floorbeam · corrodedCORRODED FLOORBEAM, BS 986.5, LBL 43, WL 208.1 IN THE AFT GALLEY AREA. PERFORMED REPAIR ON FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.SDR SWAA2026061897870Floorbeam · corrodedCORROSION FLOORBEAM, BS 986.5, RBL43, WL 208.1 IN THE AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON THE FLOORBEAM IAW SRM 53-70-51-2R-6, REPAIR 6.SDR IPXA2026061144531Floorbeam · corrodedWHILE WORKING FAULT T3F18E008T21R FOUND CORROSION ON FLOORBEAM UPPER SURFACE AT STA. 1200 LBL 45.5 TO 62.2. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97555-REQ1 AND VT-SAA EA 757-5360-01-B0745, REV IRSDR MASA20260529121Floorbeam · corrodedDURING HEAVY CHECK INSPECTIONS ON FWD FUSELAGE, FLOOR STRUCTURE, CORROSION FOUND ON FLOORBEAM UPPER FLANGE AT FR 17 RBL 19. FLOORBEAM UPPER FLANGE REPAIRED IAW SRM 53-00-10 REP 03 REV 49.SDR IPXA2026052044531Floorbeam · corrodedWHILE WORKING FAULT T3F18E008T21R FOUND CORROSION ON FLOORBEAM UPPER SURFACE AT STA. 1200 LBL 45.5 TO 62.2.SDR VNAA20260512024Floorbeam · corrodedCORROSION ON BRACKETS FLOOR BEAM AT FS 284.00 RBL16 AND RBL36, ON BRACKET FLOOR BEAM FS 295.00 AND RBL 5 OF THE FUSELAGE FLOOR STRUCTURE. FLOORBEAM TEE REMOVED PER SRM 51-21-06-001-001-A01 AND AREAS IS OUT LIMITS PER CRJ700 SRM 53-21-43-101-001-A01 AND SRM 53SDR SCNA20260529221Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 986.5, RBL 42.5 AND LBL 42.5 ON PAX CABIN. :CORROSION ON FLOORBEAM AT STA 986.5, RBL 42.5 AND LBL 42.5 ON PAX CABIN WERE REPAIRED PER B737-800 53-70-51-2R-6, REPAIR 6, ALTERNATIVE 4SDR IPXA2026052627817Floorbeam · corrodedAFT OF BULK CARGO COMPARTMENT FLOOR BEAM ASSY UPPER FLANGE HAS 4 EA NUT PLATE CORRODED APPROX AT BS 1681.8, BTW BL 0 AND RBL 50, ID STICKER NUM. (085-015) ATA 53-10. INSTALLED 2EA NEW NUT PLATE STRAPS ASSY AT AFT OF BULK CARGO COMPARTMENT FLOOR BEAM ASSY UPPESDR IPXA2026052129933Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, APPROX BTW BS 1400 AND BS 1420, RBL 45.50,SDR IPXA2026052129850Strap · corrodedUPON REMOVAL OF CEILING DECOMPRESSION PANEL FOUND STABILIZATION STRAP CORRODED, BTW BS 1560 AND BS 1580, LBL 45.50,SDR IPXA2026051226988Floorbeam · crackedMCD FLOORBOARD SUPPORT BRACKET AT STA 900 BETWEEN RBL 24-45 IS DAMAGED. 33-010. INSTALLED FLOORBOARD PLATE SUPPORT AT MCD FLOORBOARD SUPPORT BRACKET AT STA 900 BETWEEN RBL 24-45 PER SRM 51-40-02-0G. REVIEWED.SDR R61A2026060300152Floorbeam · corrodedCABIN FLOOR CROSSBEAM AT FR 17 HAS CORROSION, REPAIRED CROSSBEAM PER SRM 53-00-10/REPAIR 03P.SDR CALA2026052916618Floorbeam · damagedFOUND TEE ANGLE AT FWD SIDE OF STA 947.5 AND WL208.1 WITH OUT OF ROUND HOLES. REMOVED AND REPLACED TEE ANGLE AT FLOOR STRUCTURE ON FRAME 947.5 WL 208.1 IAW SRM 51-40-02-0G-0 AND DWG 147A0000 REV-.SDR CALA2026052916616Floorbeam · dentedFLIGHT DECK FLOOR STRUCTURE STA 270 FROM RBL10 TO LBL20 HAVE DENT AT MULTIPLE PLACES. REMOVED DAMAGE, FABRICATED, LOCATED, DRILLED REPAIR PARTS, INSTALLED AND RESTORED COATINGS IAW UAL ECRA 5315-01234 REV- AND AAR REO-G25899 REV IR. THIS IS A CATEGORY 'A' RESDR AALA202605277606Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT BS 947 AND LBL 24. REPAIRED CHORD PER SRM 53-70-51-2R-5.SDR AALA202605268593Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT STA 986.5 AND LBL 43. REPAIRED CHORD PER SRM 53-70-51-2R-6.SDR AALA202605266264Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT BS 947.5 AND LBL 16. REPAIRED THE FLOORBEAM PER SRM 53-70-51-2R-5'SDR MASA20260512103Floorbeam · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FUSELAGE FLOOR STRUCTURE, CORROSION AT CFIII, FR 84, RBL 9, LBL 13, LBL 29, CROSS BEAM UPPER FLANGE. REPAIRED IAW ETD 2026-170-007729, REV:/, HFC AND UT INSPECTION C/O, NO FAULT FOUND. SEE AWS AND NDT REPORT TWO47SDR MASA20260512102Floorbeam · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FUSELAGE FLOOR STRUCTURE, CORROSION AT CFIII, FR 84, RBL 9, LBL 13, LBL 29, CROSSBEAM UPPER FLANGE. REPAIRED IAW ETD 2026-170-007729, REV:/, HFC AND UT INSPECTION C/O, NO FAULT FOUND. SEE AWS AND NDT REPORT TWO473SDR AALA202605226128Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT STA 986 AND RBL 54. REPAIRED CHORD PER SRM 53-70-51-2R-6.SDR SWIA2026050676923Floorbeam · abnormalCOMPLY WITH REO 601R-53-41-1116, REPAIR & REINFORCEMENT FOR BS 559 LWR CAP ANGLES BL 9.00 & 18.00 LT & RT. COMPLIED WITH REO 601R-53-41-1116, REV- C. REPAIR AND REINFORCEMENT FOR BS 559 LWR CAP ANGLES, BL 9.AND 18. LT & RT. COMPLIED WITH TASK CARD 51-900-100SDR REXA2026060400917Floorbeam · corrodedCORROSION ON CROSSBEAMS ON FS349 BTW LBL9 TO RBL9 AT FLOOR STRUCTURE PASSENGER. CROSSBEAMS ON FS349 BTW LBL9 TO RBL9 AT FLOOR STRUCTURE PASSENGER WAS REPAIRED PER REO 690-53-21-2136 REV.--SDR CALA2026050716058Floorbeam · crackedMAIN CABIN FLOORBEAM CRACKED AT RBL1 TO RBL 24 STA 540. REPAIR ACCOMPLISHED IAW SRM 51-40-02-OG-0 PAGE 1-40 FIGURE 14 AND SRM 51-40-05-0G-0 PAGE 1-20 FIGURE 6.SDR CALA2026050716056Floorbeam · crackedMAIN CABIN FLOORBEAM CRACKED AT LBL1 TO LBL 24 STA 540. REPAIR ACCOMPLISHED IAW SRM 51-40-02-OG-0 PAGE 1-40 FIGURE 14 AND SRM 51-40-05-0G-0 PAGE 1-20 FIGURE 6SDR REXA2026070301051Floorbeam · corrodedCORROSION ON FLOOR CROSSBEAM FS1051 BTW RBL27 AND RBL47 AT AFT BAGGAGE COMPARTMENT FLOOR CROSSBEAM FS1051 BTW RBL27 AND RBL47 AT AFT BAGGAGE COMPARTMENT WAS REPAIRED PER EA NO. CRJ953-22332 REV IRSDR SWIA2026050576407Floorbeam · corrodedLT CROSSBEAM AT FS 280 HAS CORROSION. REMOVED AND REPLACED CORRODED LT CROSSBEAM AT FS280.00 WITH NEW LT CROSSBEAM AT FS 280 USING ALL NEW FASTENERS IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01 AND DWG CC670-34010 REV -K. SDR VNAA202606120009Floorbeam · crackedDURING D.I OF THE TASK CARD: 53-10-219B CRACK WAS DETECTED ON UNDER FLOORBEAM AT F.S 280.00 RBL 12. FLOORBEAM AT F.S 280.00 RBL 12. WAS REPAIRED PER REO 690-53-11-2187 REV.- -SDR DALA2026050602865Tee Angle · corrodedCORROSION ON "T" EXTRUSSION AT STA950 AND RBL27 AT INTERCOSTAL ATTACHMENT. LOCATED AND DRILLED NEW "T" EXTRUSION. APPLIED TREAT, PRIME, AND INSTALLED IAW B737-900 SRM 53-70-51-1A-1, 51-40-02-06, 51-40-05-06, 51-20-01-06. (LOG 1577327 - AIRCRAFT WAS GROUNDED).SDR SWIA2026050475992Floorbeam · damagedOUTBOARD FLOORBEAM REF SRM 53-51-43 ITEM 24 PN 601R31117-35. AT RBL 9, BS 559+64 - 559+80 HAS ELONGATED HOLE IN FLANGE JOINING CROSS MEMBER. COMPLIED WITH REO 601R-53-51-741 DATED: 2026-05-28 REV- STEPS: 3A, 3B AND 3C BY INSTALLING A FREEZE PLUG FOR THE ELO
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