JASC 5315
Service difficulty reports · 44,213
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 AALA202507046222Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 2 ZONE 2 RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGH = 0.625 INCH.SDR AALA202505097825Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER T CHORD AROUND LAVATORY MOUNT AT BS 947, RBL 51. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R PROCEDURE 5.SDR FDEA202504240642Floorbeam · crackedINSDIE THE L/H TUNNEL AREA, AT THE FWD FACE OF THE 377 FLOOR BEAM LBL 24, THE FLOOR BEAM SUPPORT THAT RUNS FWD AND AFT IS BUCKLED AND CRACKED. FOUND DURING THE NLG INSTALL. REMOVED BROKEN STRAP, REPLACED WITH FABRICATED STRAP AND REINSTALLED ON FLOOR BEASDR VNAA20250529028Floorbeam · corrodedCORROSION ON FLOOR BEAM LBL 27.00 BTW FS1000-FS1069 AT AFT CARGO COMPARMENT. PAINT ON UPPER FACE OF FLOOR BEAM LBL ON FLOOR BEAM LBL 27.00 BTW FS1000 TO FS1010 AND FS 1069 TO FS1057 AT AFT CARGO COMPARMENT WAS REMOVED PER CRJ900 SRM 51-26-01-001-001-A01, WASDR VNAA20250529021Floorbeam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM RBL 12 TO CROSSBEAM FS280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. COCKPIT FLOOR LONGITUDINAL BEAM RBL 12 TO CROSSBEAM FS280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1987 REV - -SDR VNAA20250529020Floorbeam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LBL 12 TO CROSSBEAM FS280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT . COCKPIT FLOOR LONGITUDINAL BEAM LBL 12 TO CROSSBEAM FS280.00, FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-1988 REV - -SDR ASAA2025042357917Floorbeam · corrodedSTA 947 UPPER T-CAP HAS AREAS OF CORROSION FROM LBL 15 TO RBL 4. GROUNDED - YES. REMOVED DAMAGE AND FOUND OUT OF LIMITS I.A.W. B737-900ER SRM 53-70-51-1A-1, ORIGINAL THICKNESS OF UPPER FLANGES .180, MAT REMOVED .080, MAT REMAINING .100 I.A.W. B737-900ER SRM 53SDR SWAA2025052956945Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA294.5 AND RBL53 WL208.1 AT FWD GALLEY AREA. REPLACED ANGLE (CLIP) FLOOR STRUCTURE LOCATED STA294.5 AND RBL53 WL208.1 AT FWD GALLEY AREA. IAW SRM 51-10-02 AND DWG 141A8310 SHEET 25 REV.SDR CALA2025052704953Floorbeam · corrodedMAIN CABIN AFT WET AREA STA 947.5 RBL 51" FLOOR BEAM PREVIOUS REPAIR CORROSION REF AAR N/R 9963406 ESFR REPORT COMPLETED AND SENT REMOVED PREVIOUS REPAIR AND FABRICATED NEW REPAIR AT INSTALLED AT THE FLOOR BEAM STA 947.5 RBL-25 TO RBL-59 IAW-B-737-SRM-53-7SDR UIEA2025041400466Floorbeam · corrodedUPPER FUSELAGE MAIN CABIN, AT STA 986, BTWN RBL 50 AND LBL50, FLOOR BEAM UPPER FLANGE WITH CORROSION IN SEVERAL PLACES.(<P>REPAIRED FUSELAGE FLOOR BEAM AT STA 986.5, UPPER CHORD SECTION BETWEEN LBL 50" AND RBL 50" I/A/W COOPESA COO-EO-2025-22114-R00 REV:00, DSDR UIEA2025041400467Floorbeam · corrodedUPPER FUSELAGE FWD ENTRY CABIN AREA, STA 312 AT LBL1 AND LBL 8, UPPER CHORD AFT FLANGE WITH CORROSION.(<P>REPAIRED FUSELAGE FLOOR BEAM, STA 312, UPPER CHORD SECTION BETWEEN LBL 21 AND 12.25 I/A/W B-737-800 BCF SRM 53-10-51-2R-12 REPAIR 12 PARAG 1 THRU PARAG 4,SDR UIEA2025041400470Floorbeam · corrodedUPPER FUSELAGE FWD ENTRY CABIN AREA, STA 328 AT RBL 47 , UPPER CHORD FWD FLANGE WITH CORROSION.(<P>REPAIRED FUSELAGE FLOOR BEAM STA 328, UPPER CHORD SECTION BETWEEN RBL 32 AND RBL 64 I/A/W B-737-800 BCF SRM 53-10-21-2R-7, REPAIR 7 PARAG, FIG 204 DETAIL A SHEETSDR UIEA2025041600482Floorbeam · crackedUPPER FUSELAGE FWD ENTRY AREA, AT STA 303.9 AND LBL 60, FLOOR ANGLE WITH CRACK.(<P>REPAIRED INNER CHORD ANGLE AT FWD ENTRY DOOR LOWER SILL, STA 303.9 WL 208, LBL 60 I/A/W COOPESA COO-EO-2025-22069-R00 REV:00 DATED: MAR-27-25, DOCUMENTED ON F.A.A FORM 8110-3. NSDR SWAA2025052956927Floorbeam · crackedCRACK FLOOR BEAM LOCATED STA328 AND RBL21 FWD GALLEY AND LAV 2025-274263 <[01]. TOOL USED RADIOMETER/PHOTOMETER KIT P/N : XRP-3000 ; S/N : 1753759 ; DUE DATE: 30/JUN/25; [02] TOOL USED ON STEP 18: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 240525411; DUE DASDR VNAA20250529027Floorbeam · corrodedCORROSION ON FLOOR BEAM LBL 9.00 BTW FS1000-FS1069 AT AFT CARGO COMPARMENT. PAINT ON UPPER FACE OF FLOOR BEAM LBL 9.00 BTW FS 1000 TO FS 1010 AND FS 1069 TO FS 1056 AT AFT CARGO COMPARMENT WAS REMOVED PER CRJ900 SRM 51-26-01-001-001-A01, WAS EVALUATED, AFTERSDR VNAA20250529026Floorbeam · corrodedCORROSION ON CROSSBEAM SECTION (FS280) BTW LBL 9.00 / RBL 9.00. CROSS BEAM FS.280 R/H WAS CLEANED AND NOT DAMAGED WAS FOUND PER CRJ-900 SRM 51-26-00-001-001-A01, EVALUATED WAS DUE EXCESSIVE CORROSIÓN ON LH CROSS BEAM FS.280 AT COCKPIT CABIN FLOOR WAS FOUND OFSDR VNAA20250529006Floorbeam · corrodedCORROSION ON FLOORBEAM FS280 BTW LBL9.00 / RBL9.00 AT PILOTS CABIN STRUCTURE. EXCESSIVE CORROSION ON FLOORBEAM FS280 BTW LBL9.00 / RBL9.00 WAS EVALUATED PER CRJ-900 SRM 53-00-00-101-001-A01 AND REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 5SDR AALA202507214424Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FROM ZONE 1 RADIUS LOCATED AT CENTER WING BOX FRONT S PAR VERTICAL STRINGER AT FRAME 36 AND Y765 LEVEL AT FWD CARGO COMPARTM ENT. CRACK LENGTH IS 0.170 INCH. MAINTENANCE PERFORMED REPAIR LOCATED AT CENTER WING BOXSDR AALA202507211260Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FROM ZONE 1 HOLE LOCATED AT CENTER WING BOX FRONT SPAR VERTICAL STINGER AT FRAME 36 AND Y-254 FWD CARGO COMPARTMENT L= 0.141 INCH. MAINTENANCE PERFORMED REPAIR (SPLICE REPAIR) LOCATED AT CENTER WING BOX FRONT SPARSDR AALA202505163463Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER CHORD (T-CAP) OF PASSENGER CABIN FLOOR BEAM AT BS 328, RBL 52. REPAIRED FLOOR BEAM UPPER CHORD PER SRM 53-10-51-2R-7 ALTERNATIVE 2.SDR AALA202505113797Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 947, RBL 14. REPAIRED CHORD PER SRM 53-70-51-2R-5 AND EA 364121.SDR AALA202505066972Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR SUPPORT AT BS 950 FROM RBL 16 TO RBL 24. REPLACED FLOOR SUPPORT PER AARD 51-00-05-1.SDR FDEA202504180660Floorbeam · corrodedMAIN DECK FLOOR FOUND FLOOR BEAM CORROSION AT FR12A PLUS 16" Y740 REPLACED THE DAMAGE SUPPORT BY NEW ONE WITH RIVETS I.A.W. A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA .6, PAGE,7B~PAGE,23.THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAISDR AALA202504215826Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT BS 540, LBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-40-02-0G.SDR AALA202504211161Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT BS 540, RBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-40-02-0G.SDR UIEA2025032800413Floorbeam · puncturedAFT CARGO COMPT RH STA 1880 RBL 36 FLOOR BEAM SUPPORT WEB FOUND PUNCH(<P>WEB REPAIRED AS PER RI-53-65-17515 REV A. NO FURTHER DEFECTS NOTED</P>)SDR J6B2025F00005Floorbeam · crackedF.S280.00 FLOOR BEAM IS CRACKED RH SIDE. REPAIRED AFT FLOOR BEAM ANGLE ON BULKHEAD FS280.00 BETWEEN LBL 20.75 TO RBL 20.75 IAW CRJ200 MHIRJ REO 601R-53-11-3994 REV.-- DATE 2025/06/04 AND MHIRJ REO 601R-53-11-926 REV -B 2006/05/10.SDR CALA2025051904772Floorbeam · corrodedSUPPORT TASK- MAIN CABIN FLOOR BEAM AT STA 947 AND RBL 51 HAS SIGNS OF CORROSION. REMOVED DAMAGE, ORIG .180 REF BAC DWG BAC1518-1212 REV-. MAT LOSS .080, REMAINING .100 FOUND TO BE OUT OF LIMITS REF B737- 800 SRM 53-70-51-1A-1 FIG 104 DETAIL C. CUT OUT DAMASDR CALA2025051904771Floorbeam · corrodedSUPPORT TASK- MAIN CABIN FLOOR BEAM HAS SIGNS OF CORROSION AT STA 986.5 AND RBL 43. REMOVED DAMAGE, ORIG .150 REF BAC DWG BAC1518-1211 REV-. MAT LOSS .055, REMAINING .095 FOUND TO BE OUT OF LIMITS REF B737- 800 SRM 53-70-51-1A-1 FIG 104 DETAIL C. CUTOUT DAMSDR CALA2025051904770Floorbeam · corrodedSUPPORT TASK- MAIN CABIN FLOOR BEAM AT STA 986.5 AND LBL 43 HAS SIGNS OF CORROSION. REMOVED DAMAGE, ORIG .150 REF BAC DWG BAC1518-1211 REV-. MAT LOSS .060, REMAINING .090 FOUND TO BE OUT OF LIMITS REF B737- 800 SRM 53-70-51-1A-1 FIG 104 DETAIL C. CUTOUT DAMASDR CALA2025051904769Floorbeam · corrodedSUPPORT TASK- MAIN CABIN FLOOR BEAM STA 947 AND LBL 51 HAS SIGNS OF CORROSION. REMOVED DAMAGE, ORIG .180 REF BAC DWG BAC1518-1212 REV-. MAT LOSS .020, REMAINING .160 FOUND TO BE OUT OF LIMITS REF B737- 800 SRM 53-70-51-1A-1.REMOVED DAMAGE TO FORM FLAT SURFACSDR DALA2025042103059Floorbeam · corrodedAFT CABIN FLOOR STRUCTURE HAS CORROSION STA 947.5 LBL 50. MAIN CABIN FLOORBEAM REPAIR AT STA 947.5 WAS ACCOMPISHED ON N/R 00326. MAIN CABIN FLOOR BEAM STATION 947.5 WAS REPAIRED AS PER B737 SRM 53-70-51-2R REPAIR 5.SDR VNAA202504170069Floorbeam · corrodedFRAME 349 IS CORRODED BETWEEN STRINGER 27 AND 26R CORRECTIVE ACTION: FRAME 349 IS CORRODED BETWEEN STRINGER 27 AND 26RSDR VNAA202504170068Floorbeam · corrodedDISCREPANCY: F.S. 295 BETWEEN STGR 26L & 26R PREVIOUS REPAIR IS CORRODED.SDR VNAA202504170064Floorbeam · corrodedLBL 27 FLOOR BEAM IS CORRODED BETWEEN FS 1000 AND FS 1069. CORRECTIVE ACTION: REPAIRED AND REPLACED WITH NEW FLOOR BEAM LBL27 FS1000-1069 P/N MM670-35302-035 IAW SRM 53-00-41-201-001-A01 MM670-35302-035SDR SWI2025F00928Floorbeam · crackedCOCKPIT FLOOR FRAME RBL 9 CRACKED IN THE RADIUS WHERE THE FRAME ATTACHES TO THE FS 280 BULKHEAD. REMOVED AND INSTALLED NEW COCKPIT FLOORBEAM RBL 9 IAW SRM 53-11-43-201-003-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.SDR SWAA2025052025713Floorbeam · crackedFLOOR SUPPORT CROSSBEAMS AT MID CABIN ABOVE FWD SPAR CRACKED - BS 539; LBL 1 AND RBL 1.<[01] REMOVED AND REPLACED 2EA PANEL BREAK. P/N: 143A5240U33 LOT: 1602183-5 AND P/N: 143A5240U34 LOT: 1591872-1 AND 2EA PLATE P/N 143A5240U12 LOT: 1598027-6 AND P/N: 143A524SDR SWAA2025051456818Floorbeam · corrodedCORROSION ON BS986 FLOOR BEAM AT NUTPLATE HOLES AT RBL 27.5; RBL31.5; RBL35.5 AND RBL 43 WL208.1<[01] REPAIRED PASSENGER CABIN FLOOR BEAM BS 986 IAW SRM 53-70-51-2R-4 REPAIR-4;[02] COMPLETE;[03] VERIFY JOB COMPLETE;[04] COMPLETESDR QXEA2025042300128Floorbeam · corrodedFR74 STR29L-29R CENTER FLOORBEAM CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-08 2 EA.SDR DALA2025042103051Floorbeam · corroded(LOG 0917257) CORROSION ON RH SIDE AFT OF R2 DOOR. ACCOMPLISHED REPAIR AT MAIN CABIN STA 986.5 AFT WET AREA FLOORBEAM IAW B 737 SRM 53-70-51-2R REPAIR 4.SDR CALA2025041803997Floorbeam · corrodedAFT PASSENGER COMPARTMENT FLOOR STRUCTURE IN WET AREA AT STA 987 FLOORBEAM UPPER CAP HAS CORROSION. REMOVED CORRODED T-CAP AND REPAIRED WITH T-CHORD ANGLES AND STRAPS IAW B737-800 SRM 53-70-51-2R-4.SDR SWI2025F00938Floorbeam · corrodedAVIONICS BAY FLOORBEAM ANGLE AT FS280 HAS SPOTS OF CORROSION. INSTALLED NEW FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REV-K. COMPLIED WITH 51-900-1002-SKYSDR SWAA2025051956495Floorbeam · crackedCRACKED PANEL BREAK AT MID CABIN BS540 LBL1 WL208.<[01] REMOVED AND REPLACED PANEL BREAK AT MID CABIN BS540 LBL1 WL208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060;[02] VERIFIEDSDR SWAA2025051956496Floorbeam · crackedCRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208. MARKED<[01] REMOVED AND REPLACED PANEL BREAK AT MID CABIN BS540 RBL1 WL208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060;[02] COMPLETESDR IPXA2025050222871Floorbeam · corrodedMDC, STA 1100, BETWEEN RBL 45 AND RBL 60, BEHIND FLOOR PANEL 242XJF, FLOOR BEAM HAS 2EA SPOTS WITH CORROSION. NO DOT. REMOVED RH SIDE RAIL FROM STA 1100-1200 TO FOM I.A.W AMM 25-56-12-004-001.REMOVED 1EA CARGO LOCK AT STA 1140 TO FOM I.A.W AMM 25-56-05-024-022SDR ASAA2025041557461Floorbeam · damagedPANEL BREAK AT STA 540 IS DAMAGED. GROUNDED - YES. REMOVED AND REPLACED 2EA PANEL BREAKS IAW B737-800 SRM 51-40-02-0G-0.SDR ASAA2025041557460Floorbeam · damagedPANEL BREAK AT STA 540 IS DAMAGED. GROUNDED - YES. REMOVED AND REPLACED 2EA PANEL BREAKS IAW B737-800 SRM 51-40-02-0G-0.SDR UIEA2025041400465Floorbeam · corrodedCORROSION - MFOUND M/D FLOOR BEAM CORROSION AT STA 2240 RBL 57 TO RBL 85.(<P>1. REMOVE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 103. 2. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 103 W/S 50176 AND EI NO: T2025A53M-546 REV 1. 3. INSTALL FASTNERS IAW SRM 5SDR UIEA2025041400468Floorbeam · corrodedCORROSION - FOUND M/D FLOOR BEAMS TOP SURFACE CORROSION STA 1500 BETWEEN LBL 55 TO LBL 75.92.(<P>1. REMOVE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 103. 2. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 103, W/S NO: 50169 AND EI NO: T2025A53M-4SDR SWAA2025051456759Floorbeam · corrodedCORROSION ON BS986 FLOOR BEAM AT NUTPLATE HOLE RBL 43; WL 208.1<[01] THE FLOOR BEAM REPAIR WILL BE COMPLETED ON COSTUMER CARD # TTG8Q00ZWBA6;[02] CORRECTIVE ACTION COMPLETED.;[03] CHANGED MEASUREMENTS FIELD ON RII TO NO AND MAJOR REPAIR TO NO DAMAGE REPAIRED O
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