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 SWAA2024061175114Floorbeam · corrodedAFT PASSENGER CABIN FLOOR BEAM 947.5 CORRODED IN MULTIPLE AREAS ALONG THE FULL LENGTH OF THE BEAM<[01] ACCOMPLISHED REPAIR AT AFT PASSENGER CABIN CENTER OF FLOOR BEAM 947.5 REF SRM 53-70-51-2R-5.SDR SWAA2024061074942Floorbeam · corrodedCABIN FLOOR BEAM IS CORRODED AT 947.15 NEXT TO RIGHT AFT LAVATORY; OUTBOARD MOUNT.<[01] AFTER FURTHER INSPECTION NO CORROSION WAS FOUND AT CABIN FLOOR BEAM STA 947.5 AT RIGHT AFT LAVATORY O/B MOUNT. CORROSION WAS ONLY FOUND ON ADJACENT ATTACHED INTERCOASTAL ATSDR ASAA2024041549442Floorbeam · corrodedMAIN CABIN FLOOR SUPPORT STA 994 RBL 32 - RBL 44 CORRODED. GROUNDED - YES. CORROSION IS IN AND AROUND HOLE. OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1 DRILLED TO FIT NEW FLOOR SUPPORT IAW B737-800 SRM 51-40-05 AND BAC DWG 147A5700 REV A. FLOOR SUPPORT INSTALSDR AALA202404251311Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FLOORBEAM ASSEMBLY AT STA 540 FROM BL 0 TO RBL 24. REPLACED FLOORBEAM ASSEMBLY PER SRM 51-40-02-0G.SDR SWAA2024051474634Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE STA 540 AND BTW LBL 0.07 TO RBL 24.82 AT PASSENGER CABIN 2024-258064 CRACK ANGLE FLOOR STRUCTURE STA 540 AND BTW BL 0.0 TO RBL 24.82 AT PASSENGER CABIN. REPLACED ANGLE & LOCATED ON FLOOR STRUCTURE IAW SRM 51-40-02 DWG 143A5240; SHESDR AALA202406066010Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS 2 CRACKED FASTENER HOLES AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 3 AT FR 36 AND +Y254. REPAIRED FLOOR BEAM PER 353775SDR SWAA2024052274249Floorbeam · crackedCRACK ON FLOOR SUPPORT AT STA-540 LBL-25 TO BL-0 WL-208<[01] UPDATED MEASUREMENT TABLE;[02] STEP 3 COMPLETE;[03] JOB SUMMARY;FLOOR SUPPORT WAS OUT OF LIMITS DUE TO CRACK AT BS 540 LBL 25 TO BL0 WL208. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0; DWG 143A0060;[0SDR SWAA2024052274250Floorbeam · crackedCRACK ON FLOOR SUPPORT AT STA-540 RBL-25 TO BL-0 WL-208<[01] REMOVED AND REPLACED FLOOR SUPPORT BS 540; RBL 25 - BL 0 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A0060 REV:-;[02] ALL WORK COMPLETE;[03] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.SDR SWAA2024052274251Floorbeam · crackedCRACK ON FLOOR SUPPORT AT STA-540 LBL-45 TO LBL-25 WL-208<[01] UPON FURTHER INVESTIGATION AND VERIFIED BY NDI; FLOOR SUPPORT AT BS 540 LBL 45 TO LBL 25 WL 208 FOUND TO BE CRACK FREE. NO FURTHER ACTION REQUIRED;[02] VERIFIED STEP 1 IS COMPLIED WITH; CARD COMPLESDR HNAA2024051600400Floorbeam · corrodedE032495 FR 20 CROSSBEAM CORRODED AT RH SIDE. : REMOVED AND REPLACED FR 20 CENTER AISLE CROSSBEAM IAW EMB 145 SRM 51-40-02.SDR HNAA2024051400353Floorbeam · corrodedE032382 CROSS SUPPORT BEAM CORRODED AT FR18. RAR THE CROSS SUPPORT BEAM AT FR18 IAW EMB 145 SRM 51-40-02.SDR HNAA2024051400352Floorbeam · corrodedE032381 CROSS SUPPORT BEAM CORRODED AT FR20. RAR CROSS SUPPORT BEAM AT FR20 IAW EMB 145 SRM 51-40-02 AND SRM 51-20-03SDR SWI2024F00455Floorbeam · corrodedL/H FS280 CROSSBEAM CORRODED ON UPPER FLANGE AT APPROXIMATELY LBL 13 (C-CHECK RO 5/28/2024) (C-CHECK RO 5/28/2024) BLEND CORROSION ON L/H FS 280.0 CROSSBEAM REF CRJ900 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW L/H SDR SWAA2024052074059Floorbeam · corrodedCORROSION ON FLOOR BEAM 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-259089<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] TOOL USED ON STEP 7 UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[03] TOOL USED: ET SDR SWAA2024052074060Floorbeam · corrodedCORROSION ON FLOOR BEAM 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2024-259090<[01] TOOL USED ON STEP 6 UT EQUIPMENT P/N: 45MG; S/N: 130061901; CAL DUE DATE: 09-JUN-24;[02] STEP 11 AND 12 TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 60009161631; DUESDR HNAA2024051600395Floorbeam · corrodedE032068 CORROSION ON LOWER SIDE OF CROSS FLOORBOARD SUPPORT ON LH SIDE IN LAV AREA. REMOVED UNSERVICEABLE AND INSTALLED SERVICEABLE LOWER SIDE OF CROSS FLOORBOARD SUPPORT ON L/H SIDE IN LAV IAW EMB 145 SRM 51-40-02SDR AALA202404165054Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L2 DOOR CUTOUT LOWER SILL BEAM AT THE AFT GIRT BAR FITTING AREA AT FR 68 AND +Y1292. REPAIRED LOWER SILL BEAM PER SRM 53-41-14-203-002 R5.SDR REXA2024102901127Floorbeam · crackedR/H COCKPIT FLOOR BEAM IS CRACKED IN LOWER O/B FWD RADIUS AT FS 280 REPAIRED RIGHT COCKPIT FLOOR BEAM AT RBL12 IAW MHIRJ REO 690-53-11-1716 REV-- DATED 2024-04-08SDR REXA2024102901126Floorbeam · crackedL/H COCKPIT FLOOR BEAM IS CRACKED IN LOWER O/B FWD RADIUS AT FS 280 REPAIRED LEFT COCKPIT FLOOR BEAM AT LBL12 IAW MHIRJ REO 690-53-11-1716 REV-- DATED 2024-04-08SDR SWI2024F00453Floorbeam · crackedCOCKPIT FLOOR BEAM LBL12 CRACKED IN THE OUTBOARD RADIUS AT THE AFT END OF THE BEAM, FS280.00. (MARKED) (C-CHECK RO 5/28/2024) INSTALLED NEW FLOOR BEAM SECTION BETWEEN FS280.00 - FS265 LBL 12 AND INSTALLED -35 INBD UPPER REPAIR ANGLE, -37 INBD LOWER REPAIR SDR SWI2024F00452Floorbeam · corrodedCOCKPIT FLOOR SUPPORT ANGLE ON THE FORWARD SIDE OF THE FS280.00 BEAM IS CORRODED. LBL9 - RBL9. (C-CHECK RO 5/28/2024) FOUND COCKPIT FLOOR SUPPORT ANGLE OUT OF LIMITS REF CRJ900 SRM 53-00-00-101-001-A01 AND CRJ900 SRM 53-11-43-001-001-A01 AND INSTALLED NEWSDR SWI2024F00449Floorbeam · crackedCOCKPIT FLOOR BEAM RBL12, POSSIBLE CRACK IN THE OUTBOARD RADIUS AT THE AFT END OF THE BEAM, FS280.00. (MARKED) (C-CHECK RO 5/28/2024) INSTALLED LOWER ANGLE, UPPER ANGLE AND OUTBOARD WEB ON COCKPIT FLOORBEAM AT RBL 12.00 AND INSTALLED NEW COCKPIT FLOOR SUPSDR AALA202404191117Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR BEAM UPPER CHORD AT BS 986.5, LBL 43. REPAIRED CHORD PER 53-70-51-2R-6 ALTERNATIVE 4.SDR CALA2024041601095Floorbeam · corrodedSUPPORT TASK: MAIN CABIN FLOOR STRUCTURE STA 986 AT RBL 20-30 HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC 9280232. REMOVED AND REPLACED DAMAGED WEB IAW B737-900ER SRM 51-40-02. ORIG THICKNESS .063", REMOVED .016", REMAINING .047 AND FOUND TO BE OUT OF LIMITSDR YENA2024041600586Floorbeam · corrodedDURING HEAVY MAINTENANCE: CORROSION ON FLOOR BEAM, FILLER, LOCATED ON FR17, STGR 17R, HAS CORROSION THAT IS BEYOND LIMITS. NOTE: THERE IS NO SPECIFIC SRM LIMIT FOR THIS SPECIFIC PART, THEREFORE IT WAS DETERMINED TO REPLACE IT; REMOVED AND REPLACED FLOOR-BEAM FSDR YENA2024041600585Floorbeam · corrodedDURING HEAVY MAINTENANCE: CORROSION ON FLOOR-BEAM, UPPER SURFACE, LOCATED ON FR 17, + .617, STGR 17R, IS BEYOND ALLOWABLE E190 SRM LIMITS; REMOVED AND REPLACED FLOOR-BEAM (P/N: 170-03263-001, TRACK, RIGHT-FLOOR, FWD.) LOCATED BTW FR 12 AND FR 20, PER E190 SRM:SDR YENA2024041600552Floorbeam · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / FORWARD FUSELAGE / FLOOR STRUCTURE CROSS BEAM @ FR14 / CORROSION - PERMANENT REPAIR. (CONSIDERED A MAJOR REPAIR)SDR DALA2024041604477Floorbeam · corrodedCORROSION ON FLOORBEAM AT WL-208, STA-344, FROM RBL-2 TO RBL-9. C/W ER/A 617081-14 REV. ORIGINAL.SDR CALA2024041201055Floorbeam · corrodedCORROSION ON MAIN DECK FLOORBEAM STA 986, BL 8 RBL 43 ON TOP CHORD UPPER & LOWER SURFACESDR REXA2024070800507Floorbeam · corrodedFOUND LH FS 280 CROSSBEAM TO HAVE CORROSION. REMOVED AND REPLACED LH FS 280 CROSSBEAM PN: CC670-34094-1 IAW CRJ 900 SRM 51-42-06-001-00-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01, 51-40-11-001-001-A01. PAINTED LH FS 280 CROSSSDR SWAA2024052073066Floorbeam · corrodedMAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM HOLE STA 986.5 LBL 45'<[01] ACCOMPLISHED REAPAIR AT MAIN CABIN AFT WET AREA FLOOR BEAM STA 986.5 AT LBL 45' REF SRM 53-70-51-2R-6; ALTERNATIVE 4;[02] PERFORMED SME INSPECTION OF REPAIR PASSED.;[03] LATE ENTRY: ACSDR SWAA2024050973440Floorbeam · corrodedCORROSION ON 986 FLOOR BEAM LBL 45 WL 208 AROUND FASTENER HOLE<[01] ACCOPLISHED REPAIR PER SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4SDR SWAA2024050973441Floorbeam · corrodedCORROSION ON 986 FLOOR BEAM RBL 45 WL 208 AROUND FASTENER HOLE<[01] REPAIRED CORROSION ON 986 FLOOR BEAM; RBL 45; WL 208; IAW EA 24-153-00997.;[02] JOB COMPLETE.SDR SWAA2024050973377Floorbeam · corrodedCORROSION ** AFT CABIN WET AREA FLOOR SUPPORT BEAM UPPER CAP FASTENER HOLE STA 986.5 RBL 45.5 MKD DOT<[01] INSTALLED REPAIR AT AFT CABIN WET AREA FLOOR SUPPORT BEAM STA 986.5 RBL 45.5. REF EA 24-153-01013 WIP 1;[02] RII...VERIFIED CORRECTIVE ACTION.SDR AALA202405016985Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AND CRACK IN PASSENGER CABIN FLOORBEAM UPPER CHORD AT STA 947, LBL 53. REPAIRED CHORD PER SRM 53-70-51-2R-5.SDR SWAA2024042673165Floorbeam · crackedPASSENGER CABIN FLOOR PANEL SUPPORT TRANSVERSE CHANNEL AT STA 540; LBL 3 HAS CRACK.(MARKED) NOTE: PHOTO ATTACHED.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)]SDR SWAA2024050272964Floorbeam · corrodedSTA 986.5 FLOOR BEAM UPPER FLANGE HAS CORROSION AROUND FLOOR PANEL ATTACH HOLE AT LBL 30.5.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. ORIGINAL THICKNESS=.150?; REMAINING THICKNESS=.125?.;[02] BLENDSDR SWAA2024050272963Floorbeam · corrodedSTA 986.5 FLOOR BEAM UPPER FLANGE HAS CORROSION AROUND NUTPLATE HOLE AT LBL 43.<[01] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1.;[02] BLENDED CORROSION PER SRM 51-10-02. DAMAGE REMOVAL FOUND TO BE OUT OF SDR CALA2024041601088Floorbeam · corrodedCABIN AREA FLOOR STRUCTURE AT STATION 286 HAS CORROSION LEFT SIDE, MARKED WITH STREAMER 3257. REPLACED WEB IAW B767 SRM 51-40-02 PARAGRAPH 7 PART D.SDR CALA2024041501079Floorbeam · corroded(B737-05-3-0049) CORROSION ON MAIN DECK FLOOR SUPPORT ON EDGES AT STA 951, RBL 27-49. FLOOR SUPPORT DAMAGED WAS REMOVED AND INSTLLED NEW ONE P/N:147A5 676U6 PER B737-700 SRM 51-40-02-0G-0 PAR 7.SDR CALA2024041501066Floorbeam · corrodedCORROSION ON MAIN DECK FLOOR BEAM STA 947, RBL 37-54. UPPER CHORD UPPER SURFACE AND LOWER SURFACE. PERFORMED REPAIR ON MAIN DECK FLOOR BEAM STA 947 60 RBL - 60 LBL IAW B737-700 SRM 53-70-51-2R REPAIR 5 SECTION 47 PAR 4.SDR DALA2024041204375Floorbeam · corrodedSHIP 180 AFT CARGO FLOOR UPPER CHORD FOUND CRACK AT STA1219, RBL22. CORRECTIVE ACTION: THE CRACK FLOOR UPPER CHORD AT STA1219 RBL22 REPAIRED AS PER B767-300 SRM 53-00-07. (0284596)SDR DALA2024041204374Floorbeam · corrodedSHIP 180 FOUND FWD CARGO FLOOR BEAM UPPER CHORD LOWER SURFACE CORROSION AT STA 654+44 AND LBL6 TO LBL 8, CORRECTIVE ACTION: THE DAMAGED UPPER CHORD REPAIRD AS PER B767-300 SRM 53-00-07 (0284583)SDR SWAA2024052072112Floorbeam · crackedDURING INSPECTION OF THE WN CENTER SECTION FOUND; 1.5' CRACK; BELOW CABIN FLOOR; AT STA 540' LBL 1 INCH; OF 1.5' LONG APROX. ON UPPER SPAR CHORD. SEE DOT # 3.<[01] REMOVED AND REPLACED PANEL BREAK AT STA 540 LBL IAW SRM 51-40-02-0G-0 AND IPC 53-42-11-66.;[02] SDR SWAA2024052072113Floorbeam · crackedDURING INSPECTION OF THE WN CENTER SECTION FOUND; 1' CRACK; BELOW CABIN FLOOR; AT STA 540' RBL 1 INCH; ON UPPER SPAR CHORD. SEE DOT # 2.<[01] REMOVED AND REPLACED PANEL BREAK AT STA 540 RBL IAW SRM 51-40-02-0G-0.;[02] CORRECTION OF STEP 1: REMOVED AND REPLACEDSDR SWAA2024051572067Floorbeam · crackedCRACK FLOOR BEAM LOCATED STA 294.5 AND RBL 52 AT FWD GALLEY AREA 2024-253238<[01] TOOL USED ON STEP 7;8 AND 9. EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022235; DUE DATE: 07-SEP-24;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 14SDR DALA2024041204346Floorbeam · corroded(LOG 0286878) CORROSION ON FLOOR SUPPORT AT WL-208, STA-947+4.5, BETWEEN LBL-29 AND LBL-48. REMOVED AND REPLACED FLOOR SUPPORT AT WL 208 STA 947+4.5 BETWEEN LBL 29 AND LBL 48 IAW B737 SRM 51-40-02-0G AND BOEING DWG 147A5650.SDR AALA202404128154Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM AT FR 68 AND +Y1292. REPLACED FLOOR BEAM PER SRM 51-42-11.SDR SWIA202405290407Floorbeam · corrodedFS280 FLOOR BEAM HAS CORROSION BETWEEN LBL 9.0 AND RBL9.0 FOUND DURING REMOVAL OF COCKPIT FLOOR SUPPORT ANGLE P/N CC670-34095-1 CAMP # 28042337 (C-CHECK RO 5/25/2024) REPLACED L/H SIDE F.S. 280.00 FLOOR BEAM WITH NEW ONE FROM F.S. 280.00 BULKHEAD BETWEEN LSDR SWAA2024052071740Floorbeam · corrodedCORROSION FLOOR BEAM LOCATED STA 986.5 RBL 43 AND WL 208.1 AT AFT GALLEY AREA 2024-253189<[01] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL
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