JASC 5315
Service difficulty reports · 44,218
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 SWIA2020021848591Floorbeam · damagedUPOD REMOVAL OF FWD FLOOR SUPPORT ANGLE AT FS280 FOUND L/H AND R/H CLIPS HAS ELONGATED HOLES (C-CHECK) RO 2/14/2020 REMOVED AND REPLACED THE LH AND RH, FS280 FLOOR SUPPORT ANGLE CLIPS REF CRJ 900 SRM AND DWG. SEE CONTINUATION CARD FOR DETAILS. COMPLETESDR REXA2020010720009Floorbeam · corroded"INITIAL INSPECTION: CORROSION ON FLOOR PANEL SUPPORT ANGLE AT FS280.00 LBL9 TO RBL9 (SM)[CPIL].
"SUMMARY ON NRC 00177: CORROSION LEVEL 2, FLOOR PANEL SUPPORT ANGLE AT FS280.00 LBL9 TO RBL9 WAS REPLACED PER CRJ-900SDR SWAA2019122639919Floorbeam · corrodedAFT WET AREA FLOOR STRUCTURE CORRODED AT BS. 986, RBL 43. REPAIRED T-CAP IAW SRM.SDR REXA2019122601731Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 280 BETWEEN STRINGERS 26L TO 26R IN THE MAIN AVIONICS COMPARTMENT. THE CORROSION WAS REMOVED IAW SRM 51-21-06-001-001-A01, PAR 5D, AND THE REWORKED AREA WAS MEASURED AND FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. THE FLOSDR ASAA201912131586Floorbeam · crackedCABIN FLOOR PANEL BREAK STA 540 LBL 2 CRACKED. GROUNDED - YES. REMOVED AND REPLACED PANEL BREAK 143A5240-35 IAW B737-900ER SRM 51-40-02 AND BOEING DWG 143A0060 REV.-.SDR VNAA2019121299905Floor Support · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE AT FS 280. ANGLE CORRODED BEYOND LIMITS IAW CRJ900 SRM FIG 53-00-00-901-803. REMOVED FWD J-ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A01. P/N: CC670-34095-3. NEW SERVICEABLE J-SDR SWAA2019123040016Floorbeam · corrodedFLOOR BEAM AREA CORRODED AT BS. 328, BETWEEN RBL 43 TO RBL 47. REPAIRED THE FLOORBEAM TEE CAP IAW SRM.SDR C77A2019121100001Floorbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON-CONDITION REPAIR OF CORROSION OR OTHER DAMAGE TO THE CENTER FUSELAGE III AFT CABIN LH FLOOR BEAM P/N 170-65669-003. THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIRECT REPLACEMENT OF THE AFFESDR SWIA2020021848587Floorbeam · corrodedAFT ATTACH ANGLE AT FS319.70 ON R/H FLOOR SILL HAS CORROSION. (C-CHECK) RO 2/14/2020 FOUND CORROSION ON RH FLOOR SILL ATTACH ANGLE TO BE BEYOND ALLOWABLE REPAIR LIMITS, REMOVED AND REPLACED THE ATTACH ANGLE REF BOMBARDIER DRAWING AND BOMBARDIER DRAWING ANSDR SWIA2020021848586Floorbeam · corrodedFWD FLOOR SUPPORT ANGLE HAS CORROSION AT FS280 BETWEEN LBL 9 AND RBL 9 (C-CHECK) RO 2/14/2020 RERMOVED AND REPLACED THE FS280 FLOOR SUPPORT ANGLE FROM RBL9-LBL9 REF CRJ 900 SRM. SEE CONTINUE CARD FOR DETAILS. COMPLETED FORM M-337.SDR SWIA2020012147894Floorbeam · cracked*FLIGHT DECK FLOOR SUPPORT FS280.0 O/B OF RBL9 LOWER FRAME HAS SUSPECT CRACK (MARKED). (C-CHECK) RO:1/17/2020REMOVED AND REPLACED CRACKED REPAIR ANGLE REF BOMBARDIER REO. COMPLIED WITH TASK CARD SEE CONTINUATION CARD FOR FULL DETAILS.SDR SWAA2019122339870Floorbeam · corrodedFLOORBEAM CORRODED AT BS 312 BETWEEN LBL 32 TO RBL 22. REPAIRED FLOORBEAM IAW SRM.SDR SIMA2019122010001Floorbeam · corrodedLH CROSSBEAM AT FS 280.00 IS CORRODED IN NUMEROUS AREAS BEWTEEN DRIP TRAY AND THE UPPER L ANGLE.-C/A-COMPLETED LH FS280.00 CROSSBEAM INSTALLATION IAW SRM 53-11-10 AND 51-42-06SDR SIMA2019122010002Floorbeam · corrodedRH CROSSBEAM AT FS 280.00 IS CORRODED IN NUMEROUS AREAS BEWTEEN DRIP TRAY AND THE UPPER L ANGLE.-C/A-RH FS280.00 CROSSBEAM INSTALLATION IAW SRM 53-11-10 AND 51-42-06SDR DALA2019121207261Floorbeam · corroded(LOG 1396172) DURING INSPECTION FOUND CORROSION ON FLOOR STRUCTURE RAILS AT STA 727D+5 , 3.0 RBL AND 3.0 LBL AFT CARGO COMP. FLOOR STRUCTURE RAILS AT STA 727D+5 , 3.0 RBL AND 3.0 LBL AFT CARGO COMP WAS REPAIRED PER ERA 492968-14.SDR QMLA2019121019095Floorbeam · gougedGOUGING FOUND ON RIB UNDERNEATH CABIN FLOOR AT THE RIB BEHIND THE CO PILOTS COLLECTIVE. GOUGING WAS THROUGH THE COMPLETE THICKNESS OF THE RIB. THE DAMAGE WAS APPROXIMATELY 13/32" IN LENGTH AND LOCATED AT THE BEND RADIUS OF THE RIB. ** THIS AIRCRAFT REMAINS OOSSDR DALA2019121007212Floorbeam · corroded(LOG 1394632) DURING INSPECTION FOUND CORROSION ON FLOR SUPPORT ANGLE STA 500I BTW STRINGERS RH 26 TO LH 26 AT FWD CARGO COMPARTMENT. FLOOR SUPPORT ANGLE STA 500I WAS REPLACED PER B737-800 SRM 51-40-02.SDR VNAA2019121099906Floorbeam · crackedWHILE PERFORMING SB670BA-53-041, FOUND RH COCKPIT FLOORBEAM AT RBL 11.00 TO BE CRACKED FWD OF THE ANGLE FITTING. PERFORMED EDDY CURRENT OF CRACKED AREA OF RBL 11/12 FLOORBEAM AND FOUND INDICATIONS EXTENDING BEYOND TYPE III CUTOUT OF SRM CRJ 700 53-11-43-201-0SDR VNAA2019121099905Floorbeam · crackedWHILE PERFORMING SB670BA-53-041, FOUND LH COCKPIT FLOOR BEAM AT LB 11.00 OT BE CRACKED FWD OF ANGLE FITTING. APPLIED PROTECTIVE BARRIER OVER EWIS COMPONENTS BETWEEN FS280 AND FS265 UNDER FLOORBOARDS. VERIFIED ALL APPLIED PROTECTIVE BARRIER OVER EWIS COMPONENSDR VNAA2019121099901Floorbeam · corrodedFS280 IS CORRODED AT LBL 9 AND RBL 9 UNDER TITANIUM CAP. UPON FURTHER INVESTIGATION FOUND BOTH LH AND RH FS280.00 BEAMS TO BE CRACKED AND CORRODED REQUIRES REPLACEMENT OF BOTH. REMOVED BOTH LH AND RH FS280.00 BEAMS AS REQUIRED IAW CRJ 700 SRM 51-42-06-001-0SDR C77A2020012870029Floorbeam · corrodedTHIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON-CONDITION REPAIR OF CORROSION OR OTHER DAMAGE TO THE CENTER FUSELAGE III AFT CABIN LH FLOOR BEAM P/N 170-65669-003. THE PERMANENT REPAIR WILL BE ACCOMPLISHED BY DIRECT REPLACEMENT OF THE AFFESDR SWIA2020010247542Floorbeam · corrodedFS 589.0 BETWEEN LBL9 AND LBL 27 FLOOR SUPPORT HAS POSSIBLE CORROSION (C-CHECK) RO 12/31/2019 DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED AND MANUFACTURED PART PER BOMBARDIER DRAWING. -R PART MARKED "AVMAX P/N 60135031-165" INSTALLED MANUFACTURED PART AT F.S. SDR SWAA2020010240126Floorbeam · corrodedCABIN FLOOR BEAM UPPER SURFACE CORRODED AT BS. 312, LBL 14.5. / REPAIRED FLOOR BEAM PER EA.SDR SIMA2019122309006Floorbeam · crackedLH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.OO-C/A-REPAIRED L/H CENTER COCKPIT FLOOR BEAM AT BL 12.00 JUST FWD OF FS 280.-00 IAW SRM 53-11-43 AND ETN CR-53-088.SDR SIMA2019122309008Floorbeam · crackedRH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF CROSSBEAM AT FS280.OO-C/A-REPAIRED R/H CENTER COCKPIT FLOOR BEAM AT BL 12.00 JUST FWD OF FS 280.-00 IAW SRM 53-11-43 AND ETN CR-53-088.SDR R61A201912181406Doubler · corrodedWHILE IN HEAVY CHECK FOUND R/H FLOOR SUPPORT AT FR.16 CORRODED AS MARKED. REPLACED RH FLOOR DOUBLER PER SRM 51-40-08. APPLIED TOP COAT TO FASTENERS REF SRM 51-23-06SDR SWAA2019121039496Floorbeam · damagedCABIN FLOOR STRUCTURE BREAKAWAY INTERCOSTAL BROKEN AT BS. 540, BETWEEN RBL 24 TO RBL 45. / R&R INTERCOSTAL PER SRM.SDR DALA2019121007205Floorbeam · corroded(AIRCRAFT 5645, L/P 1393944) CORROSION ON FLOOR BEAM UPPER CHORD AREA STA 365 BTW BL=0 AND RBL=64 TO 365 AT PASSENGER CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: CORROSION LEVEL 2. BEAM REPAIRED PER B757-200 SRM 53-00-51-2R-10 REPAIR 10. REPLACED BOX BEAM PER LOSDR SWIA2019120946840Floorbeam · corroded* CROSS BEAM TOP CAP FS 559+112 LBL 27 TO SILL HAS CORROSION (C-CHECK) RO 12/6/2019 REMOVED CORROSION AND EVALUATED REPAIRS. REPAIRS FOUND TO BE WITHIN LIMITS AND RESTORED REPAIR TO ORIG. FINISH. IAW SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.SDR SWIA2019120946839Floorbeam · corroded* CROSS BEAM TOP CAP FS 559+80 RBL 27 TO THE SILL HAS CORROSION (C-CHECK) RO 12/6/2019 BLENDED CORROSION FROM CROSS BEAM TOP CAP FS 559+80 RBL 27 TO THE SILL. THE AREA IS FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL IAW SRM.SDR SWIA2019120946838Floorbeam · corroded* CROSS BEAM TOP CAP FS 559+80 RBL 9 TO RBL 27 HAS CORROSION (C-CHECK) RO 12/6/2019 CROSS BEAM TOP CAP FS 559+80 RBL 9 TO RBL 27 IS BLENDED, FOUND TO BE WITHIN LIMITS AND RESTORED TO ORIGINAL FINISH IAW SRM.SDR REXA2019123081809Floorbeam · corrodedCORROSION FOUND ON THE FLOORBEAM ANGLE AT BS 280, BETWEEN STRINGERS 26L - 26R IN THE MAIN AVIONICS COMPARTMENT. THE FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-42-06-001-001-A01.SDR RAIA2019122708030Floorbeam · corrodedCENTER OMEGA BEAM HAS CORROSION AT FR 59 BETWEEN UPPER DIGITAL & FLOOR BEAM AROUND NUTPLATE HOLE- PERFORMED CUT OUT OF CORROSION AROUND THE NUTPLATE AT FR 59 ON THE CENTER OMEGA BEAM. MANUFACTURED DOUBLER FOR THE CENTER OMEGA BEAM REPAIR AT FR 59 & INSDR DALA2019121097204Floorbeam · corroded(AIRCRAFT 5645, L/P 1392588) CORROSION ON FLOOR SUPPORT FITINGS ON STA 335, LBL=20 AND LBL=40 AT PASSENGER CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 51-40-05-0G AND 51-40-02-0G PAR. 7.SDR DALA2019121097202Floor Support · corroded(AIRCRAFT 5645, L/P 1392488) CORROSION ON FLOOR SUPPORT BL=0 BTW STA 365 TO 377 AT PASSENGER CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: REPLACED PER B757-200 SRM 51-40-05-0G AND SRM 51-40-02-0G PAR 4, 7.SDR ASAA2019121371585Floorbeam · crackedCABIN FLOOR PANEL BREAK STA 540 RBL 2 BROKEN. GROUNDED - YES. REMOVED AND REPLACED PANEL BREAK 143A-5240-36 IAW BOEING DWG 143A-0060 REV.- AND B737-900ER SRM 51-40-02.SDR COEA2020020612811Floorbeam · corrodedWO 209669 NR 100019 HEAVY CHECK COE/MINOR REPAIR: FLOORBEAM 36 UPPER SURFACE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED RH OB SECTION PER SRM 530000-300-857-A01.SDR COEA2020020611811Floorbeam · corrodedWO 209669 NR 100016 HEAVY CHECK COE/MINOR REPAIR: FLOORBEAM 30 UPPER SURFACE HAS MULTIPLE AREAS OF LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED WITH OEM PART.SDR SWIA2020010247538Floorbeam · corrodedCROSS BEAM FLOOR SUPPORT AT 559.0 BETWEEN LBL 27 TO LBL 32.0 CORRODED (C-CHECK) RO 12/31/2019 BLENDED PER SRM. FOUND TO BE OUT OF LIMITS. REMOVED LH STRAP PN 601R31025-29, FS 559.00 LBL27-LBL42. FABRICATED REPLACEMENT STRAP PER DRAWING FROM 0.050 7075 T6. MARSDR SWIA2020010247536Floorbeam · corrodedCORROSION FOUND ON 280 BEAM FLOOR SUPPORT AT STATION FS 280 AND BL0.00 (C-CHECK) RO 12/31/2019 CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED NEW 280 BEAM FLOOR SUPPORT ANGLE. ALODINED, PRIMED AND PAINTED. WET INSTALLED ALL FASTENERS. IAW CRJ200 SRM.SDR SWIA2020010247535Floorbeam · crackedFS 559.0 AT RBL 27 TO SILL PLATE CROSS BEAM FLOOR SUPPORT CORRODED (C-CHECK) RO 12/31/2019 BLENDED PER SRM. FOUND OUT OF LIMITS. REMOVED STRAP PN 601R31025-29 FS 559.00, RBL 27-RBL 42 PER SRM. FABRICATED REPLACEMENT STRAP FROM 0.050" 7075 T6 PER DRAWING 601R3SDR SWIA2020010247533Floorbeam · crackedCRACK FOUND ON CLIP AT STA FS280 LBL 8.0. CRACK FOUND ON CLIP AT STA FS 280 LBL 10.0 CRACK ON 280 BEAM AT STATION FS 280+LBL 11.0. CRACK FOUND ON OB CLIP AT STATION FS 280 RBL 10.0 (C-CHECK) RO 12/31/2019 PERMANENTLY REPAIRED. CUT-OUT DAMAGED AREA AND INSTALSDR SWAA2020010740171Strap · corrodedAFT CARGO COMPARTMENT FLOOR BEAM STRAP CORRODED AT BS. 887, BETWEEN LBL 9 TO RBL 21. / R&R STRAP PER SRM.SDR FDEA201912043175Splice · crackedFUSELAGE MAINFRAME STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK AT LBL 45.5. COMPLIED WITH EA F-5310-T0351218 P1 TITLE: FUSELAGE-MAIN FRAME- STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE AND SHEAR WEB CRACK REPAIR.SDR FDEA201912043173Floorbeam · crackedCRACK FLOORBEAM T CAP STA 580 LBL 45.5. COMPLIED WITH EA F-5310-T0351069 P1. TITLE : FUSELAGE - MAINFRAME - STA 580 FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR.SDR SWAA2019121239588Floorbeam · crackedFLOOR SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO RBL 25. / R&R FLOOR SUPPORT PER SRM & DWG.SDR AALA2019120659025Floorbeam · misrepairedAIRCRAFT IN BASE MAINTENANCE: FLOOR BEAM "T" CAP HAD COUNTER SUNK HOLE UNDER THE LAVATORY MOUNT AT BS 947 AND RBL 52. REPAIRED FLOOR BEAM "T" CAP PER EA 301009.SDR DALA2019120647106Floorbeam · corroded(AIRCRAFT 5645, L/P 1386127) POINTS OF CORROSION ALONG FLOOR BEAM UPPER CHORD STA 1640 FROM RBL20 TO LBL45 AT PAXCABIN FLOOR STRUCTURE. CORRECTIVE ACTION: LEVEL CORROSION 2. FLOOR BEAM UPPER CHORD STA 1640 FROM LBL 60 TO RBL60 WAS REPAIRED PER B757-200 SRM 53-SDR EE4Y2019120410389Floorbeam · corrodedLOWER FUSELAJE FWD C/C FLOOR SUPPORT FITTINGS CORRODED, LOCATED AT FR28 BTWN S-26L AND S-26R, AT FR31 BTWN S-26L AND S-26R AND AT FR35 AT S-26R. NOTE: SINCE THAT ALLOWABLE LIMITS NOT WERE FOUND, THE PARTS DAMAGED WERE REPLACED PER EMBRAER FABRICATION INSTRUCTISDR SWAA2022041132665Cap · corrodedAFT CABIN FLOOR BEAM UPPER SURFACE STA 986 LBL43 WL208 HAS CORROSION AROUND DOME NUT FASTENERS / ACCOMPLISHED FLOOR BEAM T-CAP REPAIR AT STA 986 LBL 43 WL 208 I.A.W SRM 53-70-51-2R-6 REV 68
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