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.

SDR DALA2025050903615Floorbeam · corroded(LOG 0953940) CORROSION OUT OF LIMITS ON FLOOR BEAM BTW STA312 AND LBL21-LBL23 UPPER/AFT CHORD. FLOOR BEAM BTW STA 312 AND LBL21-LBL23 UPPER/AFT CHORD WAS REPAIRED PERMANENTLY CATEGORY A PER B737-800 SRM 53-10-51-2R PROCEDURE 15, REPAIR 15.May 7, 2025 · N3751B · Boeing 737832SDR AALA202505084688Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540, RBL 3. REPLACED BREAK ASSEMBLY PER SRM 51-40-02-0G.May 7, 2025 · N996NN · Boeing 737823SDR AALA202505080818Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540, LBL 3. REPLACED BREAK ASSEMBLY PER SRM 51-40-02-0G.May 7, 2025 · N996NN · Boeing 737823SDR JJBA20250711011Floorbeam · corrodedLBL 19 FLOOR BEAM CAP CORRODED FRAME 58. REMOVED CORROSION AT LBL 19 FLOOR BEAM CAP FRAME 58, FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED NEW FLOOR BEAM CAP.May 6, 2025 · N13202 · Emb EMB145XRSDR F3LA202505070222Floorbeam · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND CABIN FLOOR BEAM Y254 AT FR20 CORRODED. REQUIRES REPLACEMENT AS PER SRM 51-72-11-911-001 REV 43. FLOOR BEAM Y254 AT FR12-24 REPLACED AS PER SRM 51-72-11-911-001 REV 43. MX ACTMay 6, 2025 · N356FR · Airbus A320251NSDR CALA2025050704525Floorbeam · corrodedCABIN FWD WET AREA FLOOR BEAM AT STA 380 BETWEEN LBL 51 - LBL 64 WITH SURFACE CORROSION SPOT. REMOVED CORROSION AT MAIN CABIN FWD WET AREA FLOOR BEAM 380 LBL 57 IAW SRM 51-10-02-0G-0,& PERFORMED REPAIR PER AAR ESR-WI REV IR #2023385-15-12049,AND UNITED EC/RAMay 5, 2025 · N12225 · Boeing 737824SDR SIMA20250505004Floorbeam · corrodedCROSSBEAM AT FR 17 CORRODED JUST INBD OF CENTER FLOOR BEAM UNDER FLOORBOARD 225ALF. (LEVEL 2 CORROSION) (MAJOR REPAIR) PERMANENTLY REPAIRED IAW ERS-EJ-53MR-4564 PTB.May 5, 2025 · N239NN · Emb ERJ170200LRSDR SWAA2025060967210Floorbeam · crackedCRACK BRAKE PANEL FLOOR STRUCTURE BS 540 FROM LBL45.5 TO LBL64 AT PASSENGER CABIN 2025-297850<[01] REPLACED PLATE OF BRAKE PANEL FLOOR STRUCTURE BS 540 FROM LBL45.5 TO LBL64 AT PASSENGER CABIN IAW SRM B737-700 51-10-02 ITEM 9 AND DWG 143A5240; SHEET: 12 ; REV:May 4, 2025 · N7835A · Boeing 737752SDR SWAA2025060967211Floorbeam · crackedCRACK BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO LBL 24.5 AT PASSENGER CABIN 2025-297852<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO LBL 24.5 AT PASSENGER CABIN IAW B737-700 SRM: 51-40-02 AND DWG: 143A0060; SHEET:May 4, 2025 · N7835A · Boeing 737752SDR SWAA2025060967212Floorbeam · crackedCRACK BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO RBL 24.5 AT PASSENGER CABIN 2025-297851<[01] REPLACED BRAKE PANEL FLOOR STRUCTURE LOCATED STA 540 AND BTW BL 0 TO RBL 24.5 AT PASSENGER CABIN AND FASTENERS IAW B737-700 SRM 51-40-02-0G-0 AND DWGMay 4, 2025 · N7835A · Boeing 737752SDR DALA2025050803579Floorbeam · corroded(LOG 0948600) CORROSION ON FLOOR BEAM UPPER FLANGE STA 328 BTW RBL 48 TO RBL 38 AT (FLOOR STRUCTURE) W1. FLOOR BEAM UPPER FLANGE STA 328 BTW RBL 48 TO RBL 38 AT (FLOOR STRUCTURE) W1 WAS REPAIRED PER B737-800 SRM 53-10-51-2R PROCEDURE 11.May 4, 2025 · N3763D · Boeing 737832SDR DALA2025050703545Floorbeam · corroded(LOG 0948400) SUB THREASHOLD JUST FWD OF R2 DOOR HAS CORROSION. REPAIRED T-CHORD AT STA 947.5 RBL 50 TO RBL 21 IAW B737-NG SRM 53-70-51-2R-5 AND INSTALLED NEW INTERCOSTAL P/N 147A5660-22 IAW B737 SRM 51-40-02.May 4, 2025 · N3755D · Boeing 737832SDR AALA202507213544Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CENTER WING BOX FR36 FRONT VERTICAL STRINGER #4 ZONE 1. CRACK DIRECTION AT 12 AND 3 O'CLOCK LOOKING AFT. D: 0.090 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX UPPER BEAM #4 -Y254 IAW EAMay 1, 2025 · N762US · Airbus A319112SDR AALA202507216259Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CENTER WING BOX FR36 FRONT VERTICAL STRINGER #3 ZONE 1. CRACK DIRECTION AT 1 AND 12 O'CLOCK LOOKING AFT. D: 0.090 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX UPPER BEAM #3 Y254 IAW EA#May 1, 2025 · N762US · Airbus A319112SDR AALA202507187563Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CENTER WING BOX FR36 FRONT SPAR VERTICAL STRINGER N5 ZONE 1, CRACK DIRECTION IS 12, 1 AND 3 OCLOCK LOOCKING AFT. CRACK D=0.090 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR (SPLICE REPAIR) ON CENTER WING BMay 1, 2025 · N762US · Airbus A319112SDR AALA202506098898Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y765 LOCATED BTW FR64 AND FR67 AT LEVEL OF STR 23L AT AFT GALLEY AREA, MEASURES OF CORROSION ARE L=1.400 INCH, W=0.800 INCH, D=0.058 INCH. MAINTENANCE REPLACED FLOOR BEAM Y765 LOC. BTW FR64 AND FR67 AT LEVMay 1, 2025 · N762US · Airbus A319112SDR AALA202506033975Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 LOCATED BTW FR64 AND FR67 AT LEVEL OF STR 23L AT AFT GALLEY AREA L: 2.505 INCH, W: 1.899 INCH, D:0.058 INCH, CORRODED AREA. MAINTENANCE REPLACED FLOOR BEAM Y1292 LOC.BTW FR64 AND FR67 AT LEVEL OF STR 23May 1, 2025 · N762US · Airbus A319112SDR SWAA2025060266404Floorbeam · crackedCRACK PANEL BREAK AT THE MID CABIN BS 540 LBL 1<[01] REMOVED AND REPLACED PANEL BREAK AT BS 540; BL0-LBL24 IAW SRM 51-40-02-0G-0 AND DWG 143A0060;[02] COMPLETEMay 1, 2025 · N7860A · Boeing 73779PSDR AALA202505084823Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540, BL 0. REPLACED BREAK ASSEMBLY PER AARD 51-00-05-1.May 1, 2025 · N928NN · Boeing 737823SDR IPXA2025052536184Floorbeam · cracked**SDR FILED OPEN** FAULT: STR-Z200-MDC FLOOR STRUCTURE AT FR75 L/SIDE FLOOR SUPPORT ANGLE HAS 2EA CRACKS (MARKED IN RED). DOT 34-043 ACCOMPLISHED STEP #3 PER EA# A300-5327-27-A3950. NO CRACKS NOTED AT THIS TIME. T95867Apr 30, 2025 · N139UP · Airbus A300F4622RSDR CALA2025050204410Floorbeam · cracked(SDR)-(B757-53-3-0487) NOSE FWD FUSELAGE MAIN DECK FLOOR BEAM CH ANNEL STA 345 BL0 CRACKED. DOT 139-2 REF:124292 SDR/SFR REPORTING ONLY CLOSING FOR SDR REPORTINGApr 30, 2025 · N17126 · Boeing 757224SDR JR2R20250430496Floorbeam · corrodedANGLE ATTACHED TO FLOOR BEAM/INTERCOSTAL AT RBL 11 BETWEEN FRAMES 89 AND 90 IS CORRODED OUT OF LIMITS.Apr 30, 2025 · N88325 · Emb ERJ170200LLSDR JR2R20250430494Floorbeam · corrodedFLOOR BEAM AT RBL BETWEEN FRAME 90 AND 90A IS CORRODED OUT OF LIMITS.Apr 30, 2025 · N88325 · Emb ERJ170200LLSDR REXA2025060900642Floorbeam · corrodedCORROSION ON FLOOR PANEL ANGLE SUPPORT LOCATED BTW FS280.00 AND LBL9.00 TO RBL9.00. CORROSION ON FLOOR PANEL ANGLE SUPPORT LOCATED BTW FS280.00 AND LBL9.00 TO RBL9.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-00-00-101-001-A01 AND WAS REPLACED PER CRJ900 Apr 29, 2025 · N903XJ · Cndair CL6002D24SDR SWAA2025051965155Floorbeam · crackedCABIN FLOOR INTERCOSTAL STA-540 BL-0 TO RBL-24 CRACKED AT RBL-1 (MARKED)<[01] REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.;[02] INSPECTION COMPLETED FOR WORK ACCOMPLISHED; REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02.;[03] INSPECTION COMPLETED FOR WApr 29, 2025 · N8691A · Boeing 7378H4SDR AALA202505062822Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT BS 540, RBL 2. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.Apr 29, 2025 · N964AN · Boeing 737823SDR DALA2025050103350Floorbeam · corrodedSHIP DISC: CORROSION FLOOR BEAM +Y254 LOCATED AT FR 16 AT FWD GALLEY AREA ( SSI 531189). C/A: REPLACED FLOOR BEAM Y254 AND FASTENERS LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG: D53110984, DWG: D53112816, DWG: D531Apr 29, 2025 · N342NB · Airbus A319114SDR AALA202507020055Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 20 AND +Y1292. REPLACED FLOOR BEAM PER SRM 51-42-11.Apr 28, 2025 · N182UW · Airbus A321211SDR AALA202506303175Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM AT FR 20 AND +Y765. REPLACED FLOOR BEAM PER SRM 51-72-11.Apr 28, 2025 · N182UW · Airbus A321211SDR SWAA2025060365339Floorbeam · corrodedCORROSION ON FILLER OF FLOOR BEAM AT BS 986 RBL 45 WL 208 MARKED<[01] REMOVED; FABRICATED AND REPLACED FILLER AS SHOWN PREVIOUS REPAIR RECORD ON CCN TTG8Q00L09BK SRM 53-70-51-2R-6 FIG 205 I.A.W SRM 51-40-02-0G-0 WITHOUT ANY DEVIATION.Apr 28, 2025 · N288WN · Boeing 7377H4SDR SWI2025F01092Floorbeam · corrodedSTR 18R IS CORRODED FS629 €“ 645 (C-CHECK RO 8/21/2025) COMPLIED WITH ALL THE STEPS OF THE REO 690-53-31-1023 REV -- DATE:2025-06-25 .INSTALLED HI-LITES AND SOLID RIVETS PER SRM, ENSURED HOLE SIZE ARE WITHIN SRM LIMITS, WET INSTALLED ALL PARTS, FILL GAApr 27, 2025 · N804SK · Cndair CL6002D24SDR SIMA20250427007Floorbeam · corrodedSSI 53-10-027 LH CTR FLOOR BEAM HAS CORROSION LOCATED AROUND SEAT TRACK FWD END. (MAJOR REPAIR) (LEVEL 2 CORROSION). REMOVED AND REPLACED LH CTR FLOOR BEAM BETWEEN FR 12-21 IAW EMB 175 SRM 51-40-08.Apr 27, 2025 · N203NN · Emb ERJ170200LRSDR REXA2025050100535Floorbeam · corrodedFS280 RH FLOOR CROSSBEAM IS CORRODED. REPAIRED IAW BOMBARDIER GREO 670-53-11-579, REV. B DATE: 2013/05/01.Apr 27, 2025 · N379CA · Cndair CL6002C10SDR SWIA2025082500426Floorbeam · corrodedINTERNAL STRUCTURE, CROSS BEAM FS1031, BETWEEN LBL27 AND LBL9 HAS CORROSION, HN00238049 (C-CHECK RO 8/21/2025) INTERNAL STRUCTURE, CROSS BEAM FS1031, BETWEEN LBL27 AND LBL9 HAS CORROSION PERFORMED A REPAIR PER THE REO 690-53-61-1586 REV. --. DATED 20Apr 26, 2025 · N804SK · Cndair CL6002D24SDR AALA202506025180Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947.5, RBL 50. REPAIRED UPPER CHORD PER SRM 53-70-51-2R-5.Apr 26, 2025 · N928NN · Boeing 737823SDR AALA202505226260Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 947.5, FROM RBL 4 TO RBL 24. REPAIRED UPPER CHORD PER SRM 53-70-51-2R-5.Apr 26, 2025 · N965AN · Boeing 737823SDR AALA202505227281Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER CHORD (T-CAP) AT STA 986, RBL 48. REPAIRED UPPER CHORD PER SRM 53-70-51-2R-4.Apr 26, 2025 · N965AN · Boeing 737823SDR AALA202505209478Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 947.5, LBL 25. REPAIRED CHORD PER SRM 53-70-51-2R -5.Apr 26, 2025 · N928NN · Boeing 737823SDR AALA202505202530Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 947.5, LBL 51. REPAIRED CHORD PER SRM 53-70-51-2R -5.Apr 26, 2025 · N928NN · Boeing 737823SDR AALA202505121142Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM AT BS 986, LBL 44. REPAIRED FLOOR BEAM PER SRM 53-70-51-2R-6.Apr 26, 2025 · N928NN · Boeing 737823SDR AALA202505162768Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD FLANGE AT STA 947, RBL 43. REPAIRED CHORD PER SRM 53-70-51-2R PROCEDURE 6 ALTERNATIVE 4 AND EA 364364.Apr 25, 2025 · N928NN · Boeing 737823SDR SWAA2025051456877Floorbeam · crackedMAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75.<[01] REMOVED AND REPLACED NEW PANEL BREAK ASSY P/N 143A5240-64 LOT 1601361-1 AT STA 540; BL 0 TO RBL 24.75 IAW SRM 51-40-02-0G-0 AND DWG 143A0060 REV: -.;[02] UPDATED MEASUREMENTS TABApr 25, 2025 · N293WN · Boeing 7377H4SDR SWAA2025051456875Floorbeam · crackedMAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75.<[01] REMOVED AND REPLACED NEW PANEL BREAK ASSY P/N 143A5240-63 LOT 1602100-2 AT STA 540; BL 0 TO LBL 24.75 IAW SRM 51-40-02-0G-0 AND DWG 143A0060 REV: -.;[02] UPDATED MEASUREMENTS TABApr 25, 2025 · N293WN · Boeing 7377H4SDR DALA2025042803271Floorbeam · corrodedSHIP 6712 CORROSION AND PREVIOUS BLENDS FOUND ON CABIN FLOOR SUPPORT BEAM UPPER SURFACE TRANSITIONING TO THE LOWER SURFACE OF THE TOP FLANGE @ STA 1640 LBL 15 TO RBL 12. RED STREAMER AND TAG # 14361 ATTACHED. CORRECTIVE ACTION: REMOVED AND REPLACED NEW FABRICAApr 25, 2025 · N6712B · Boeing 757232SDR 2025FA0000331Floor Support · corrodedMAIN DECK FLOOR STRUCTURE, -Y794.3 (RH SIDE) FROM FR72 TO FR80 FOUND MULTIPLE SPOTS OF CORROSION (LEVEL 2).Apr 25, 2025 · Airbus A330243SDR AALA202603183710Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS CRACKED ZONE 1 FASTENER HOLE AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 6 AT FR 36 AND -Y1292. REPAIRED FLOOR BEAM PER EA 364302.Apr 24, 2025 · N760US · Airbus A319112SDR AALA202603183720Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR BEAM HAS CRACKED ZONE 2 FASTENER HOLE AT THE CENTER WING BOX FRONT SPAR COMMON TO VERTICAL STRINGER 6 AT FR 36 AND -Y1292. REPAIRED FLOOR BEAM PER EA 364302.Apr 24, 2025 · N760US · Airbus A319112SDR AALA202507044428Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 5 ZONE RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGH = 0.25 INCH. MAINTENANCE ACCOMPLISHED INTERIM REPAIR (SPLICE REPAIR) LOC. ON CENTER WINGBOX UPPER BEAM -Y765 PApr 24, 2025 · N760US · Airbus A319112SDR AALA202507044674Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 4 ZONE 2 RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGH = 0.687 INCH. MAINTENANCE ACCOMPLISHED INTERIM REPAIR (SPLICE REPAIR) LOC. ON CENTER WINGBOX UPPER BEAM -Y254Apr 24, 2025 · N760US · Airbus A319112SDR AALA202507048878Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND AT BEAM LAYER POSITION 3 ZONE 2 RADIUS BACK SIDE OF THE SPAR VERTICAL STRINGER FR 36. CRACK LENGH = 0.937 INCH. MAINTENANCE ACCOMPLISHED INTERIM REPAIR (SPLICE REPAIR) LOC ON CENTER WINGBOX UPPER BEAM Y254 PApr 24, 2025 · N760US · Airbus A319112
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