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 SWAA2023061344751Beam · corroded*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 AROUND 1EA FASTENER HOLE AT LBL 35 WL 208.1<[01] ACCOMPLISHED REPAIR ON STA. 986.5 FROM LBL 5.5 TO LBL 52; PER REF EA 23-153-01510;[02] RII...VERIFIED FINAL CORRECTIVE ACTION.SDR SWAA2023052545298Beam · corrodedCORROSION ON FLOOR BEAM AT STA 927+10; LBL +52- MARKED. FAULT #1137 CLOSED IN ERROR<[01] DRAIN INTERCOSTAL OUT OF LIMITS PER SRM 53-70-51-1A-1;[02] FAULT TO BE RESOLVED ON ANOTHER FAULT. REF TTG8Q00KTSPA;[03] INSPECTED WORK PERFORMEDSDR SWAA2023060144678Floorbeam · corrodedCORROSION ON BS 986 FLOOR BEAM FWD FLANGE LBL 14.5 WL 208.<[01] SRM 53-70-51-1A-1 IS APPLICABLE ALLOWABLE DAMAGE; UPDATED TABLE;[02] REMOVED CORROSION ON 986 FLOORBEAM FWD FLANGE AT LBL 14.5; WL 208 PER SRM 51-10-02-0G-0. MAX MATERIAL REMOVED WAS .011' 1.8' BYSDR SWAA2023060144679Floorbeam · corrodedCORROSION ON BS 986 FLOOR BEAM FWD FLANGE RBL 36-43 WL 208.<[01] SRM 53-70-51-1A-1 IS APPLICABLE ALLOWABLE DAMAGE; UPDATED TABLE;1] LOCATED AND DRILLED REPAIR PARTS ITEM 1 T-CHORD (1EA) ;ITEM 2 ANGLE (2EA);ITEM 3 ANGLE (2EA);ITEM 4 STRAPS (2EA) AND ITEM 7 R/H SDR AALA202305177264Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOORBEAM LOCATED UNDER LAVATORY MOUNT AT BS 947 AND LBL 50. REPAIRED FLOORBEAM PER SRM 53-70-51-2R-5.SDR AALA202305124623Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR BEAM T-CHORD LOCATED UNDER PASSENGER CABIN AFT LAVATORY MOUNT AT BS 947 AND RBL 24. REPAIRED T-CHORD PER SRM 53-70-51-2R-5.SDR SWAA2023061343961Floorbeam · corroded*CORROSION* FLOOR BEAM STA 294.5 AT RBL 7.5 WL 208.1 HAS CORROSION AROUND FASTENER HOLE AS MARKED. 124-008<[01] STARTED REMOVING FASTENERS. REF. SRM. 51-40-02;[02] ACCOMPLISHED FLOOR BEAM UPPER CHORD REPAIR AT STA 294.5 AND BETWEEN LBL22 TO RBL24 IN REF B737-7SDR SWAA2023061344002Beam · corroded*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 AROUND 2EA FASTENER HOLES AT LBL 35 AND LBL 43 WL 208.1 HAS CORROSION AS MARKED. 124-037 CORRECTION ON ORIGINAL FAULT SHOULD READ 1EA FASTENER HOLE AT LBL 43.<[01] ACCOMPLISHED EA 23-153-01510; REF. FAULT TTG8Q00KTES7SDR ASAA2023043043273Floorbeam · corrodedGALLEY MOUNT FITTING @ STATION 947 LEFT SIDE CORRODED. GROUNDED - YES. REMOVED CORROSION ON FLOOR BEAM UNDER GALLEY MOUNT. ORIGINAL THICKNESS 0.180 IAW B737-800 SRM 53-70-51-0I-1. REMAINING THICKNESS 0.100, REMOVED 0.080. OUT OF LIMITS IAW B737-800 SRM 53-70-5SDR SWAA2023060143182Floorbeam · crackedCRACK FLOOR STRUCTURE BEAM LOCATED BETWEEN BS294.5 AND RBL51 AT FWD GALLEY AREA 2023-295235<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC500D; S/N: N500X12101V022240; CAL DUE DATE: 12-MAR-24;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/SDR SWAA2023060143179Floorbeam · corrodedCORROSION FLOOR STRUCTURE BEAM LOCATED BETWEEN BS986.5; WL208.1 AND RBL44 AT AFT GALLEY AREA 2023-295231<[01] EQUIPMENT P/N 45MG; S/N 130063701; DUE DATE 16-JUN-23 WAS USED.;[02] TOOL USED PN:38DL PLUS; SN:120398603; DUE DATE:07-NOV-23;[03] TOOL USED EDDY CURRSDR SWAA2023052641347Beam · corrodedCORROSION FLOOR BEAM LOCATED AT STA312 AND BTW LBL12 AND LBL26.6 TO WL 208.1 AT FWD GALLEY AREA 2023-282627<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: A22046819; DUE DATE: 22-JUN-23;[02] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45 MG; S/N: 130060401; DUESDR CALA2023042601258Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER SURFACE HAS CORROSION STA 947 LBL 51 PERFORMED REPAIR IN MAIN CABIN FLOORBEAM BS 947 LBL 51 IAW B737-80 0 SRM 53-70-51-2R-5.SDR SWAA2023052530836Floorbeam · corrodedCORROSION ON FORWARD EDGE OF STA 947 FLOORBEAM UPPER FLANGE AT LBL 24.75; FORWARD OF AFT LAV INBOARD; AFT TIEDOWN FITTING<[01] REMOVED L/H LAV INBOARD AFT TIEDOWN FITTING TO FOM;[02] REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. FAILEDSDR SWAA2023051530765Panel · crackedCRACKED BREAK PANEL STA 540; BL0- LBL 25; WL 208.<[01] UPDATED MEASUREMENTS. ON BS 540; BL0-LBL25; WL208; BREAK PANEL WILL BE A PART REPLACEMENT IAW SRM 51-10-02 STEP 9. REMOVED BREAK PANEL; AND RECEIVED A NEW BREAK PANEL; LOCATED HOLES; DRILLED; AND DEBURRED SDR SWAA2023051630030Floorbeam · corrodedCORROSION ON 947 FLOORBEAM UPPER SURFACE AT LBL 23; LBL 49; LBL 52; WL 208.<[01] VERIFIED THE APPLICABILY OF SRM 53-70-51-1A-1;[02] EVALUATED CORROSION ON 947 FLOORBEAM UPPER SURFACE AT LBL 23; LBL 49; LBL 52 AND FOUND TO BE OUT LIMITS DUE TO LOSS OF MATERIAL SDR SWAA2023051630011Floorbeam · corrodedCORROSION ON 947 FLOORBEAM UPPER SURFACE AT RBL 27; WL 208.<OUT LIMITS DUE TO LOSS OF MATERIAL EXCEED LIMITS GIVEN PER SRM LBL52 0.750'X0.600' ORIGINAL MATERIAL THICKNESS IS 0.180' REMAINING MATERIAL THICKNESS IS 0.110' ALL I.A.W SRM 53-70-51-1A-1REMOVED ADJACSDR F3LA2023050400050Beam · corrodedDISCREPANCY:REFERENCE NR 5001232178-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION OF AFT CABIN CORRODED FLOOR BEAM FOUND BETWEEN FR.66-70 LH. EVALUATION IS REQUIRED. PERFORMED REWORK MEASUREMENT AS PER A320NEO SRM 51-11-SDR SWAA2023052228886Floorbeam · crackedSUSPECT CRACK AT PASSENGER CABIN FWD SIDE OF FLOOR BEAM STA 294.5 RBL 51 WL 208.1 HAS A CRACK.<[01] ACCOMPLISHED DVI ON ADJACENT STRUCTURE AREAS; NO CRACKS; NO CORROSIONS OR OTHER DAMAGES NOTED. REF B737-7 SRM 53-10-51-2R-16 STEP 4.C.(4);[02] OK TO APPLY ALODISDR SWAA2023052228878Floorbeam · corroded*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 BETWEEN LBL 35 AND LBL 44 WL 208.1 HAS CORROSION AROUND FASTENER HOLES AS MARKED. 124-047<[01] CORRECTION ON TABLE STEP 17 REMAINING THICKNESS IS 0.121;[02] VERIFIED CORRECTION;[03] REPAIR AFT CABIN FLOOR BEAM STA 986SDR SWAA2023052228865Floorbeam · corroded*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 BETWEEN RBL 39 AND RBL 44 WL 208.1 HAS CORROSION AROUND FASTENER HOLES AS MARKED. 124-051<[01] REPAIR AFT CABIN FLOOR BEAM STA 986.5 BETWEEN RBL 39 AND RBL 44 WL 208.1 ACCOMPLISHED ON THE ITEM TTG8Q00KJ1J7;[02] CORRECSDR COEA2023050501919Floorbeam · crackedWO 246760 NR 100032 HEAVY CHECK COE/MAJOR REPAIR: INTERNAL FUSELAGE FRAME 22 R/H LONGITUDINAL FLOORBEAM IS CRACKED. CORRECTIVE ACTION: REPLACED FLOORBEAM IAW E.O. 5315-01.SDR A6WA202304188563Floorbeam · corrodedLBL27 FLOOR BEAM IS CORRODED BETWEEN FS569 AND FS621. ******AIRCRAFT REMOVED FROM SERVICE******** INSTALLED LBL27 FLOOR BEAM BETWEEN FS569 AND FS621 IAW CRJ-200 SRM 51-42-21, 51-42-34, AND REO 601R-53-61-3778 REV -B DATED: 2016-1SDR COEA2023060706919Floorbeam · crackedWO 246760 NR 100007 HEAVY CHECK COE/MAJOR REPAIR: R/H LONGITUDINAL FLOORBEAM BETWEEN FRAMES 36-38 IS CRACKED. CORRECTIVE ACTION: REPLACED LONGITUDINAL FLOORBEAM IAW EMPIRE AIRLINES E.O. 5315-01.SDR COEA2023052502919Floorbeam · crackedWO 246760 NR 100005 HEAVY CHECK COE/MAJOR REPAIR: L/H LONGITUDINAL FLOORBEAM BETWEEN FRAMES 29-30 IS CRACKED. CORRECTIVE ACTION: REPAIRED FLOORBEAM PER EMPIRE AIRLINES E.O. 5315-01.SDR CALA2023041901159Panel · corrodedCORROSION FOUND AT END OF RH LATERAL SHEAR PLATE AT FRAME 70, SU SPECTED CORROSION UNDERNEATH PLATE AT FRAME 70 GEN BY V061708 ON HAECO LCQ NR 9298382(34382) REMOVED AND REPLACED CORRODED SHEAR PLATE AT FRM 70, R/H IAW SRM 51-42-11-001 AND SRM 51-72-11-911-001SDR SCNA20230517155Floorbeam · corrodedCORROSION ON FLOOR BEAM UPPER SURFACE LBL 44. REPAIRED BS 986 FLOOR BEAM UPPER CHORD PER B737 SRM 53-70-51-2R-4 LBL 50 TO RBL 11. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS PER B737 SRM 53-70-51-1A-1 PARA. 4 H (2),(B)(1) FIG 104 DETAIL C. CAUSE OF CORROSIOSDR CALA2023041401111Plate · corrodedLH AFT PASS/CREW DOOR CORROSION FOUND ON DOOR SILL PLATE AT FRAME 68 GEN BY V061708 ON HAECO LCQ NR9298380(34380)SDR 7C7A2023041300028Unknown · unknownL/H SEAT TRACK CORROSION BETWEEN STA X202 AND STA X215. REPAIRED PER DHC RD8-53-5623SDR SWAA2023051126747Floorbeam · corrodedMAIN CABIN FWD WET AREA CORROSION AT FLOOR BEAM STA 312 BETWEEN LBL 11'- 50'<[01] MAIN CABIN FWD WET AREA FLOOR BEAM AT STA 312 LBL 11 FOUND OUT OF LIMITS WORK ACCOMPLISHED PER REF EA 23-153-01299-WIP1 AND 23-153-01299-WIP2 SEE TASK CARD # TTG8Q00KKMUZ AND TTGSDR JR2R20230412142Floorbeam · corrodedFLOOR BEAM AT LBL11 CORRODED BETWEEN FR18 THRU FR20SDR JR2R20230412145Floorbeam · corrodedFLOOR BEAM AT RBL11 CORRODED AT FR13SDR ASAA2023041143030Floorbeam · corrodedAFT WET AREA STA 986 FLOOR BEAM HAS SPOT OF CORROSION AT FASTNER HOLE RBL 54. GROUNDED - YES. REPAIRED 986 FLOOR BEAM IAW B737 SRM 53-70-51-2R-6W=2 O=.150 R=.105 L=1 D=.045.SDR ASAA2023041143029Floorbeam · corrodedAFT WET AREA STA 986 FLOOR BEAM HAS AREAS OF CORROSION FROM LBL 8 TO LBL 60. GROUNDED - YES. REMOVED AND REPLACED UPPER CAP WITH NEW FROM LBL8 TO LBL 60 IAW B737 SRM 53-70-51-2R-4W=2 O=150 R=.141 L=1 D=.009.SDR ASAA2023041143017Floorbeam · corrodedAFT WET AREA STA 947 FLOOR BEAM HAS CORROSION NEAR LAV MOUNT FITTING AT LBL 30. GROUNDED - YES. REPAIRED 947 FLOOR BEAM FROM LBL 8 TO LBL 36 IAW B737 SRM 53-70-51-2R-5W=2 O=.180 R=.105 L=1 D=.075.SDR SWAA2023051525340Floorbeam · crackedCRACK ON FLOOR BEAM LOCATED BS 294.5 AT LEVEL STR 17R RBL 53 AT FWD GALLEY AREA 2023-237816<[01] TOOL USED: EDDY CURRENT EQUIPMENT ; P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 27-MAR-24;[02] TOOL USED: RADIOMETER/PHOTOMETER P/N: XRP-3000; S/N:1859843; CAL DUESDR SWAA2023051525337Floorbeam · corrodedCORROSION ON FLOOR BEAM 986.5 RBL 44 WL 208.1 AT AFT GALLEY AREA 2023-237792<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[02] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 RBL44 AND WL208.1 AT AFT GALLEY AREA IAW B73SDR SWAA2023051525336Floorbeam · corrodedCORROSION ON FLOOR BEAM 986.5 LBL 44 WL 208.1 AT AFT GALLEY AREA 2023-237791<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[02] REPAIRED FLOOR STRUCTURE BEAM LOCATED BS986.5 LBL44 AND WL208.1 AT AFT GALLEY AREA IAW B73SDR F3LA2023050500051Floorbeam · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. AFT CABIN - WET AREA - TOP BEAM BETWEEN FLOOR BEAMS C66 TO C68 HAS CORROSION - REF RBL 30.00. FLOORBEAM FR 66 TO 68 RBL 30 AFTER EVALUATION FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-00-14-283-002 ANDSDR SWAA2023050524370Floorbeam · corrodedAFT WET AREA FLOOR BEAM AT 986 44 INCHES RIGHT BUT LINE UPPER 'T' CORD IS CORRODED AFT WET AREA FLOOR BEAM AT 986.5 44 INCHES RIGHT BUT LINE UPPER 'T' CORD IS CORRODED.<[01] STARTED FABRICATION AFT WET FLOOR BEAM UPPER CHORD STA 986.5 BETWEEN RBL-38 TO RBL-47 SDR IPXA2023050393104Floorbeam · crackedINSPECTION TYPE:3CFWD CARGO R/H SIDE AT STA 6-70 HAS A FLOOR BEAM TEE FITTING THAT IS CRACKED 58 INCH FROM CL.REMOVED, FABRICATED, REPLACED CRACKED TEE FITTING AT FWD CARGO R/H SIDE AT STA 6-70 IAW SRM 51-31-01 (MINOR)SDR A6WA202304018620Flange · unknownTWO FLANGES UNDERFLOOR PANEL 271ALF AT FS559.00+16 BLO 0 ARE NOT INSTALLED. AIRCRAFT REMOVED FROM SERVICE. DURING EVALUATION FOUND 13 OVERSIZED HOLE EFFECTING RBL 9 BL 0 AND LBL 9 ON FLOOR BEAM FLANGES AND INSTALLED NEW FLANGES PN 6010R31025-23 AND PN 601SDR AALA202304128290Splice · wornAIRCRAFT IN BASE MAINTENANCE FORWARD CABIN FLOOR BEAM INBOARD SPLICE HAS ELONGATED FASTENER HOLES AT FR 24 AND -Y1292. REPLACED SPLICE PER SRM 51-72-11.SDR AALA202304121557Splice · wornAIRCRAFT IN BASE MAINTENANCE FORWARD CABIN FLOOR BEAM OUTBOARD SPLICE HAS ELONGATED FASTENER HOLES AT FR 24 AND -Y1292. REPLACED SPLICE PER SRM 51-72-11.SDR ASAA2023033043019Floorbeam · corrodedCORROSION AT 947 BEAM LBL 45. GROUNDED - YES. REPAIRED FLOOR BEAM SEGMENT IAW B737-700 SRM 53-70-51-2R-5W=3 O=.180 R=-.147 L=3 D=.033.SDR ASAA2023033043018Floorbeam · corrodedCORROSION AT 947 BEAM RBL 45. GROUNDED - YES. REPAIRED FLOOR BEAM SEGMENT IAW B737-700 SRM 53-70-51-2R-1W=3 O=.180 R=.150 L=3 D=.030.SDR SWAA2023041822464Floorbeam · crackedFLOOR BEAM IS CRACKED AT BS 294 RBL 55 WL 208<[01] FORMED 2 EA -2 ANGLES FROM 7075T0#0.080' CLAD LOT# 1462657-1 IAW SRM 53-10-51-2R-16 REPAIR 16;[02] VERIFIED CORRECTIVE ACTION 1.;[03] FLOOR BEAM CRACK AT BS 294 RBL55 WL 208 WAS REPAIRED IAW EA 23-153-01078;[0SDR SIMA20230330002Floorbeam · corrodedLH OTBD "BEAM" BETWEEN FR 19-20 CORRODED AT NUT PLATE HOLE. (UNDER LH OTBD FLOOR SILL BETWEEN FR 19-21.) (LEVEL 2 CORROSION) -C/A-REMOVED LH OUTBD BEAM BETWEEN FR 19-20 IAW EMB 170 SRM 51-40-08 AND FABRICATED AND INSTALLED REPLACEMENT BEAM IAW EMB-170 SRM 51-4SDR SWAA2023042721295Floorbeam · corrodedCORROSION ON 328 FLOORBEAM UPPER FWD FLANGE AT RBL 21; RBL 40; RBL 48; WL 208.<REMOVED CORROSIONS BY 2.0'X1.5'X.025' ON FLOOR BEAM BS 328; RBL21; RBL40; RBL48; WL208 FOUND TO BE OUT OF LIMITS BECAUSE EXCEEDED 15% ORIGINAL MATERIAL THICKNESS WAS .125' IS NOW .1SDR SWAA2023042621276Floorbeam · corrodedCORROSION ON 947 FLOORBEAM UPPER SURFACE (FWD EDGE) AT RBL 52; WL 208;<FOUND TO BE OUT OF LIMITS; IAW SRM 53-70-51-1A-1 TRIMMED OUT DAMAGE UPPER CHORD OF THE FLOOR BEAM BS 947 RBL60 TO LBL39 PER SRM 53-70-51-2R-5 PAR. 4 C. FLAP PEENED CUT EDGE AREA PER SRM 53-
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