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 AALA202406069450Floorbeam · noneAIRCRAFT IN BASE MAINTENANCE: VALIDATION OF EXISTING REPAIR TO FORWARD CARGO COMPARTMENT FLOORBEAM FROM STA 443 TO STA 450, LBL 9 REQUIRED. SPLICE REPAIR ACCOMPLISHED PER SRM 53-00-53-2R PROCEDURE 2.SDR SWI2024F00726Floorbeam · corrodedFS280.00 CROSSBEAM UPPER SPLICE STRIP HAS MULTIPLE AREAS OF CORROSION AS MARKED (C-CHECK RO 8/22/2024) REMOVED AND INSTALLED NEW UPPER SPLICE STRIP AT FS280 CROSSBEAM REF-CRJ-700 SRM 51-42-06-001-001 A01, SRM 51-42-13-001-001 A01 AND DWG CC670-34010 RESDR SWAA2024071198731Floorbeam · corrodedCORROSION ON FLOOR BEAM BS 986 BL0-RBL 43 AND LBL 43 WL 208.<[01] REMOVED AND REPAIRED DAMAGE UPPER FLANGES OF THE BS986 T-CHORD LBL50-RBL50 I.A.W SRM 53-70-51-2R-4 REPAIR 4 ; EA-M-24-153-01563-WIP1 CCN TTG8Q00TV85G AND BOEING DWGS 147A5600;147A0000;147A8501 ASDR SWAA2024071098714Floorbeam · crackedCRACKED FLOOR BEAM BS 294 RBL 53 WL 208.<[01] REMOVED DAMAGED SECTION OF UPPER CHORD; REPLACED WITH NEW SECTION OF UPPER CHORD AND INSTALLED REPAIR PARTS AT BS294.5 RBL15-RBL59 WL208 IAW SRM 53-10-51-2R-16 REPAIR 16 AND DWG 141A5502.;[02] VERIFIED COMPLETESDR SWAA2024070102486Floorbeam · corrodedNEED EA TO DEVIATE FROM SRM 53-70-51-2R-5 REPAIR FOR LBL 50 SHIM INSTALL DUE TO STANDOFF INTERFERENCE.<[01] COMPLIED WITH EA 24-153-01528; WIP1 AND WIP2.;[02] 02 - INSPECTED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)];[03] 02 - INSPECTED PER [EA EA-SDR DALA2024061005907Floorbeam · corroded(LOG 0380034) CORROSION AT CABIN FLOOR, TOP SURFACE OF BEAM STA986, RBL38 & RBL44 AT FASTENER HOLES. ACCOMPLISHED ERA 618396-14 REV ORG SECTION 1.SDR DALA2024060605830Floorbeam · corroded(LOG 0378065) CORROSION ON FLOOR BEAM STA STA 947 AND LBL= 53 TO RBL 53 AT PAX CABIN. FLOOR BEAM STA 947 AND LBL=53 TO RBL 53 WAS REPAIRED PER B737-800 SRM 53-70-51-2R PROCEDURE 5 REPAIR 5.SDR SCNA20250501149Floorbeam · corrodedCORROSION ON FLOOR BEAM SUPPORT, AT STA 986.5 & RBL 44 AT PAX CABIN W2. PREVIOUS REPAIR ON FLOOR BEAM SUPPORT, AT STA 986.5 & RBL 44 AT PAX CABIN W2 WAS REPLACED PER B737-800 SRM 51-40-02-0G-0.SDR VNAA202407110024Floorbeam · corrodedSECONDARY NRC FROM NRC 00084': AFTER REMOVAL, CORROSION ON LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. CORROSION ON LH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ-900 SRM 5SDR VNAA202407110023Floorbeam · corrodedCORROSION ON RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00. CORROSION ON RH FLOOR SUPPORT BEAM AT BULKHEAD FS 280.00 WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-10-001-SDR FDEA202406040767Floorbeam · corrodedMAIN CABIN COURIER AREA, STA 346 ALONG TOP SIDE HAS SEVERAL AREAS OF BARE METAL AND CORROSION ON PREVIOSLY BLENDED AREA OF BEAM. PREVIOUS BLEND OUT ON FLOOR BEAM UPPER CHORD AT MAIN CABIN STA 344-346 BETWEEN LBL 7 - LBL 21, AFTER EVALUATION FOUND OUT OF SDR SWIA2024080500603Floorbeam · corrodedFLOORBOARD SILL AS FS569.00 RBL9 HAS SIGNS OF CORROSION AT FASTENER HOLE (C-CHECK RO 7/24/2024) PERFORMED REPAIR ON DAMAGED AREA AT FLOOR BEAM BETWEEN FS569.00 RBL9 IAW REO 670-53-31-889 REV--(P1) DATE: 2024-06-12, 670-53-31-889 REV--(P2) DATE: 2024-06-SDR VNAA202407110005Floorbeam · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LH (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM LH (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-1SDR SWAA2024070998038Floorbeam · crackedCRACK FLOOR BEAM LOCATED STA 328 RBL 20 AT FWD GALLEY AREA 2024-361601<[01] TOOL USED EDDY CURRENT HIGH FREQUENCY INSPECTION P/N: NORTEC600D; S/N: 60009161631; DUE DATE: 11-MAR-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT ; P/N: XRP-3000; S/N: 1859843; DUE DATSDR SWAA2024070998043Floorbeam · corrodedCORROSION FLOOR BEAM LOCATED STA 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361607<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] ON STEP 10 TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DSDR SWAA2024070898045Floorbeam · corrodedCORROSION FLOOR BEAM LOCATED STA 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361606<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] ON STEP 10 TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DSDR ASAA2024060350502Floorbeam · corrodedMAIN CABIN SUPPORT P/N 147A5676-5 STA 947 LBL 25 - LBL 50 CORRODED. GROUNDED - YES. CORROSION IS AROUND SEVERAL FASTENERS HOLE FOUND OUT OF LIMITS ALLOWABLE DAMAGE IAW B737-800 SRM 53-70-51-1A-1 100% MATERIAL LOSS. DRILLED NEW SUPPORT IAW B737-800 SRM 51-40-05SDR ASAA2024060350431Floorbeam · corrodedMAIN CABIN STA 990 RBL 32-43 CORRODED SUPPORT. GROUNDED - YES. CORROSION AT FASTENER HOLES 100% MATERIAL LOSS. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. DRILLED TO FIT NEW SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV.- SUPPORT INSTALLED ON N/SDR IPXA2024061476069Floorbeam · corrodedR/H MCC FLOOR BEAM AT 1200 RBL 0-25 HAS CORROSION. INSTALLED REPAIR PARTS I.A.W SRM 53-00-51-2R-6, DETAIL III STEP 4 O AND P AND SRM 51-40-02-0G.SDR AALA202406104359Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 16 AND +Y765 AT THE LAVATORY MOUNT. REPLACED FLOOR BEAM PER SRM 51-42-11.SDR DALA2024060605807Floorbeam · corrodedSHIP 3275 DISC: CORROSION SUPPORT FLOOR ANGLE LOCATED AT FR 20 -Y1650 AT FWD GALLEY AR EA. C/A: REPLACED FLOOR ANGLE LOCATED AT FR 20 -Y1650 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11,SRM 51-42-11 AND DWG D53112784 ,ISSUE D , RELEASE DATE 28-MAY-98 .TOOK MEASSDR ASAA2024060250427Floorbeam · corrodedMAIN CABIN AFT WET AREA FLOOR STRUCTURE AT STA 951 R/H HAS CORROSION AT FASTENER HOLES UNDERSIDE. GROUNDED - YES. REMOVED AND REPLACED SUPPORT FRAME IAW B737-800 SRM 51-40-02 AND IAW REF'S AIPC 53-42-51.SDR SWAA2024071697352Floorbeam · crackedCRACK ON INTERCOSTAL LOCATED BS 540 BTW BL 0 TO LBL 24.74 AT PASSENGER CABIN 2024-357280<[01] REPLACED INTERCOSTAL LOCATED BS 540 BTW BL 0 TO LBL 24.74 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-40-02-0G-0 ;SRM 51-10-02-0G-0 Ï¿½TEM 9 AND DWG 143A0060 REV-A. SEESDR SWAA2024070197265Floorbeam · corrodedAFT CABIN FLOORBEAM HAS UPPER SURFACE CORROSION STA 947 LBL 23-27 WL 208. MRKD<[01] MEASURED PRE BLENDING DAMAGE AND FOUND OVER 50% MATERIAL LOSS. ORIGINAL PART THICKNESS = .180?; MATERIAL LOSS IS >.090?. DAMAGE IS OUT OF LIMITS PER SRM 53-70-51-1A1.[17] OK TOSDR SWAA2024070197266Floorbeam · corrodedAFT CABIN L/H I/B CREASEBEAM UPPER SURFACE HAS CORROSION STA 988 LBL 46-48 WL 208. MRKD<[01] REMOVED CORROSION STA 988 LBL 46-48; ORIGINAL MATERIAL THICKNESS IS 0.080?; MATERIAL LOSS IS 0.010?; MAX ALLOWED IS 0.008?. FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-SDR SWAA2024070197274Floorbeam · corrodedAFT CABIN FLOOR Z-ANGLE FWD FLANGE HAS CORROSION AT STA 992 RBL 37 AND 44 WL 208. MRKD<[01] LOCATED/DRILLED FASTENER HOLES IN REPLACEMENT Z-ANGLE IAW SRM 51-40-05.;[02] 02 - INSPECTED PER SRM 51-40-02;[03] FAULT RESOLVED ON CARD #TTG8Q00TPRV5.;[04] SEE CARD# TSDR SWAA2024062897275Floorbeam · corrodedAFT CABIN FLOORBEAM STA 947 HAS CORROSION AT LAV. TIE-DOWN FITTING LBL 50-52 WL 208. REPAIRED DAMAGED FLOOR BEAM PER SRM 53-70-51-2R-5; ALTERNATIVE 2 AND EA 24-153-01528; WIP1 AND WIP2.SDR SWAA2024062897276Floorbeam · corrodedAFT CABIN LONGITUDINAL FLOOR SUPPORT CORROSION AT STA 946 LBL 50-52 WL 208 (CORROSION GOING UNDER STA 947 FLOORBEAM UPPER FLANGE.) REMOVED CORROSION AND WAS FOUND TO BE OUT OF LIMITS PER SRM 53-70-15-1A-1. REMOVED AND REPLACED DAMAGED FLOOR SUPPORT PER SRMSDR VNAA202407030009Floorbeam · crackedCRACK ON FLOORBEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR SDR CALA2024060301676Floorbeam · corrodedAFT WET AREA POSSIBLE CORROSION AT FLOOR BEAM STA 947.5 AND RBL 52.SDR DALA2024053005676Floorbeam · corrodedSHIP 6806 CORROSION ON FLOOR BEAM AT STA 1280 RBL 24 AT CPAX. CORRECTIVE ACTION: SUMMARY OF NRC 00478: FLOOR BEAM AT STA 1280 RBL 24 AT CPAX. WAS REPAIRED PER B757-200 S.R.M. (0367369)SDR REXA2024103001163Floorbeam · crackedLBL 12.00 COCKPIT FLOOR BEAM IS CRACKED IN RADIUS AT FS280.00. REMOVED CRACKED BEAM AT LBL 12 FS280. FABRICATED AND INSTALLED NEW L/H FLOOR BEAM P/N CC670-33202-21 IAW CRJ 900 SRM 53-11-43-201-003-A01.SDR DALA2024053005669Floorbeam · corrodedSHIP 3275 DISC: CORROSION FLOOR BEAM -Y1162.5 AT LEVEL FR68 AT AFT GALLEY AREA ( SSI 53 4147). C/A: REPLACED FLOOR BEAM -Y1162.5 AT LEVEL FR68 AT AFT GALLEY AREA ASPER A320 SRM 51-42-11 AND SRM 51-72-11, AS PER DWG # D53472780 RELEASE DATE 26-APR-18 ISSUE K ANSDR DALA2024053005653Floorbeam · inoperative(LOG 0366175) CORROSION AT CABIN FLOOR ANGLE SUPPORT, STA 1030+10, LBL3-LBL 12, WL 208. FLOOR ANGLE SUPPORT FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED NEW ANGLE SUPPORT IAW B737 SRM 51-40-02-0G AND DWG. 147A5701.SDR FDEA202405290741Floorbeam · damagedTO CARRY OUT CRACK REPAIR AS PER E.A.#: 1-5310-T0368267 P2 TITLE: FUSELAGE - MAIN FRAME - MAIN DECK CARGO OVERWING FLOOR BEAM AT STA 1256.750 CRACK REPAIR. REPAIR CARRIED OUT AS PER E.A.#: 1-5310-T0368267 A P2, TITLE: FUSELAGE - MAINFRAME - MAIN DECK CARGOSDR SWAA2024062790927Floorbeam · crackedCUSTOMER REQUEST AAI INSPECTION. PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540 BL0 TO RBL 24.75 2024-341201<[01] REPLACED FLOOR STRUCTURE SUPPORT AT STA 540 BL0 TO RBL 24.75 IAW B737-700 SRM 51-40-02 AND DWG 143A0060 REV -;[02] CORRECTED STEP 1<SDR SWAA2024062790928Floorbeam · crackedCUSTOMER REQUEST AAI INSPECTION PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540 BL0 TO LBL 24.75 2024-341202<[01] REPLACED BREAK PANEL AND FASTENERS LOCATED AT FLOOR STRUCTURE STA 540 BL0 TO LBL 24.75 IAW B737-700 SRM 51-40-02-0G-0 SRM 51-10-02-0GSDR ASAA2024052850504Floorbeam · corrodedAFT WET AREA STA 947 T-CAP HAS CORROSION AT MOUNT FITTING. GROUNDED - YES. REMOVED CORROSION, ORIGINAL THICK 0.1800 IAW B737-800 SRM 53-70-51-1A-1 AND FLOOR BEAM BAC 1518-1212 REMAINING THICK 0.154 AT RBL 53, 0.026" REMOVE MAT, REMAINING THICK 0.158 AT LBL 4, SDR ASAA2024052850428Floorbeam · corrodedAFT WET STA 986 HAS CORRODED FASTENER HOLES FLOOR BEAM. GROUNDED - YES. REMOVED CORROSION. ORIGINAL THICKNESS 0.150 IAW B737-800 SRM 53-70-51-0I-1 AND BAC 1518-1211. REMAINING THICKNESS AT RBL 34- 0.100, REMOVED 0.050. REMAINING THICK AT LBL43 0.095, REMOVED 0SDR SWAA2024061990721Floorbeam · corrodedFWD PIT AFT BULKHEAD AREA; LOWER SUPPORT ASSY CORRODED APPROX. BS 500I FROM LBL24 TO RBL 24.<[01] REMOVED AND REPLACED SUPPORT PT. #143A9485U35ATSMOR PO#1082214.2 IAW BAC. DWG. 143A9481 REV.A; AND B737-800 SRM 51-40-02;[02] VERIFIED REMOVAL AND INSTALLATION OFSDR SWAA2024061490964Floorbeam · defectiveDURING ACCOMPLISHMENT OF STA 986 FLOOR BEAM REPAIR FAULT TTG8Q00TDFQW REF: SRM 53-70-51-2R-4 DEVIATION IN FASTENERS HOLES LAYOUT AT RBL 22.5' FASTENERS NOT STAGGERED AS PER SRM LAYOUT.<[01] RECEIVED ENGINEERING APPROVAL FOR DEVIATION OF FASTENER HOLES LAYOUT ASDR DALA2024053105701Floorbeam · corroded(LOG 0368239) CORROSION FOUND ON TOP FLANGE OF FLOOR BEAM BS 947 RBL 49. REPAIRED FLOOR BEAM DAMAGED AT STA 947 RBL 38 TO RBL 63 PER B737-900 SRM 53-70-51-2R-5.SDR FDEA202405270731Floorbeam · corrodedMAIN CABIN COURIER AREA, STA 346 ALONG TOP SIDE HAS SEVERAL AREAS OF BARE METAL AND CORROSION ON PREVIOSLY BLENDED AREA OF BEAM. PREVIOUS BLEND OUT ON FLOOR BEAM UPPER CHORD AT MAIN CABIN STA 344-346 BETWEEN LBL 7 - LBL 21, AFTER EVALUATION FOUND OUT OF LISDR HNAA2024070800530Floorbeam · corrodedE040305 CORROSION ON CROSS FLOOR BEAM BETWEEN FRAMES 24-25. BLENDED OUT CORRODED AREAS ON CROSS FLOOR BEAM BETWEEN FRAMES 24-25 IAW EMB145 SRM 51-10-03 AND FOUND REMAINING THICKNESS TO BE WITHIN ALLOWABLE LIMITS IAW EMB145 SRM 53-22-10AD.SDR SWAA2024070189988Floorbeam · crackedCABIN FLOOR SUPPORT STIFFENER CRACKED AT STA 540 BL ZERO TO LBL24<[01] REMOVED AND REPLACED STIFFENER AT STA 540 BL 0 TO LBL 24 PER SRM 51-40-02.;[02] VERIFIED C/A #1.SDR SWAA2024070189987Floorbeam · crackedCABIN FLOOR SUPPORT STIFFENER CRACKED AT STA 540 BL ZERO TO RBL24<[01] REMOVED AND REPLACED FLOOR SUPPORT STIFFENER PER SRM 51-40-02.SDR AALA202406064558Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR SUPPORT BREAK ASSEMBLY AT STA 540 FROM BL 0 TO RBL 24. REPLACED BREAK ASSEMBLY PER AARD 51-00-05-R1.SDR AALA202406051381Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOOR SUPPORT BREAK ASSEMBLY AT STA 540 FROM BL 0 TO LBL 24. REPLACED BREAK ASSEMBLY PER AARD 51-00-05-1 R1.SDR SWAA2024071189898Floorbeam · crackedCRACK FLOOR BEAM LOCATED STA328 AND RBL24.75 WL208.1 AT FWD GALLEY AREA 2024-345526<[01] TOOL USED EDDY CURRENT EQUIPMENT PN:NORTEC 600D;SN:60007161486;DUE DATE:28-JUL-24.;[02] REPAIRED FLOOR BEAM LOCATED STA328 BETWEEN LBL7 TO RBL 65 WL208.1 AT FWD GALLEY ARESDR HNAA2024070800526Floorbeam · corrodedE040111 CORROSION ON CROSS FLOOR BEAM AT FRAME 20. REMOVED AND INSTALLED SERVICEABLE CROSS FLOOR BEAM AT FRAME 20 IAW EMB 145 SRM 51-40-02
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