JASC 5315
Service difficulty reports · 44,187
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 CALA2026022614088Floorbeam · corrodedFLOORBEAM BTW BL 0 - RBL 24.75, BS 333.45, CORRODED. REPAIR FABRICATED IAW DWG 141N5160, REV D. REMOVED AND REPLACED, REMOVED 100%, EXFOLIATED BS 333.45 BTW BL 0 - RBL 24.75, APPLIED TREAT AND PRIMER IAW IAW SRM 51-20-01 ; APPLIED TOP COAT IAW AMM 51-21-15SDR DALA2026022401324Floorbeam · corrodedCORRODED FLOORBEAM LOCATED BTW FR 18 - FR 20, -Y 254 AT FWD GALLEY AREA. REPLACED FLOORBEAM, FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, & DWG D53111462. (LP 1464261)SDR IPXA2026031947651Support Bracket · crackedAFT CARGO COMPARTMENT AT FR54 -Y1959, 1EA CEILING BRACKET SUPPORT IS CRACKED. DOT 21-51 INSTALLED NEW SUPPORT BRACKET AT AFT CARGO COMPARTMENT AT FR54 -Y1959 IAW A300 SRM 51-40-21-001 PAR.6SDR CALA2026022614072Floorbeam · corrodedAFT WET AREA FLOORBEAM, BS 947.5, RBL 50 HARD POINT AREA CORRODED IN SPOTS. THE FLOORBEAM WAS REMOVED AND INSTALLED A TEE ANGLE REPAIR IAW SRM SRM-53-70-21-2R-5, SRM 51-40-02-0G-0, & DWG 147A8501.SDR IPXA2026031635090Floorbeam · corrodedMAJOR REPAIR. UPON REMOVAL OF DAMAGED ON DECK PLATE, FOUND FLOORBEAM UPER FLANGE EXFOLIATED BS 1681, LBL 28 - 33. REMOVED THE DAMAGE. CUT OUT THE FLOORBEAM UPPER TEE AND CUT AWAY ANY DAMAGE ON FLOORBEAM VERTICAL WEB AS REQUIRED IAW E.A. 757-5310-01-B0703SDR CALA2026022314011Floorbeam · corrodedCORRODED AFT WET AREA FLOORBEAM UPPER TEE ANGLE, BS 986, BL 0 TO RBL 45 HAD SEVERAL CORROSION SPOTS. THE FLOORBEAM UPPER TEE WAS REMOVED AND INSTALLED A REPAIR IAW SRM 53-70-51-2R-4, SRM 51-40-02-0G-0, & DWG 147A5700.SDR ASAA2026022065116Floorbeam · corrodedMAIN CABIN, AFT WET AREA, FLOORBEAM, BS 986.5 FOUND CORRODED AT MULTIPLE AREAS. GROUNDED - YES. REMOVED THE DAMAGE ON THE FLOORBEAM, BS 986, RBL 20 - LBL 20, FOUND TO BE IN LIMITS IAW SRM 53-70-51-1A-1, REPAIRED THE FLOORBEAM, BS 986.5, RBL20 - RBL30 &SDR IPXA2026031499164Floorbeam · corrodedMAJOR REPAIR, MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION. REMOVED CORROSION AT MAIN DECK FLOOR AREA STA 1600 LBL 49 FLOOR BEAM UNDERNEATH SURFACE REF SRM 51-10-02-0G-0 REPAIRED PER BOEING 757-200PF SRM 53-00-51-2R-6 REPAISDR SWAA2026032472334Floorbeam · crackedCRACKED FLOORBEAM ANGLE BS 695, RBL 24.75. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02-0G-0, AND DWG 273A9110, SHEET 6, REV A.SDR IPXA2026031499075Floorbeam · corrodedMAIN DECK FLOOR AREA STA 1681 LBL 31 METAL PLATE PANEL SURFACE BULGING SIGN OF CORROSION. ACCOMPLISHED REPAIR PER SRM 53-60-51-2R-6 REPAIR 6.SDR IPXA2026022399164Floorbeam · corrodedMAIN DECK FLOOR AREA STA 1600 LBL 49 FLOORBEAM UNDERNEATH SURFACE HAS CORROSION.SDR SWAA2026032371578Floorbeam · crackedCRACKED FLOORBEAM ANGLE, INBD SIDE, BS 695, BL 0. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-10-02, SRM 51-40-02, & DWG 273A9110, SHEET 6, REV A.SDR SWAA2026032371579Floorbeam · crackedCRACKED ANGLE, OTBD SIDE OF FLOORBEAM, BS 695, BL 0. REPLACED THE FLOORBEAM ANGLE IAW SRM 51-40-02, SRM 51-10-02, AND DWG 273A9110, SHEET 6, REV A.SDR CALA2026031214513Floorbeam · crackedAIR CONDITIONING DISTRIBUTION BAY AFT OF FWD CARGO BS 540 CENTER RT FLOORBEAM CRACKED. REF AAR N/R 100007543, R & R THE FLOORBEAM IAW SRM 51-40-02-0G-0 , HOLE SIZES SRM 51-40-05-0G-0.SDR CALA2026022013930Floorbeam · crackedAIR CONDITIONING DISTRIBUTION BAY, AFT OF FWD CARGO BS 540 CENTER LEFT FLOORBEAM CRACKED BS 540 BL 0 - LBL 24. REMOVED AND REPLACED FLOORBEAM ANGLE IAW SRM 51-40-02-0G-0 ,SDR IPXA2026022411434Floorbeam · crackedCRACKED BRACKET, MAIN DECK FLOOR BEAM TO FUSELAGE BRACKET, STA 917 S-21L (AGING INSPECTION) (NO.4736) (REPLACE). INSTALL REPAIR PART -T01 STRINGER CLIP AS SHOWN IN FIGURE 2 AND PER IAI DWG 371-53-00-C4181-001 REQUIREMENTS. ACCOMPLISHED REPAIR I.A.W EO-96668-RSDR CALA2026021813856Floorbeam · corrodedFOUND CORROSION OUT OF LIMITS AT FLOORBEAM, BS 312, LBL 57. REPAIRED THE DAMAGE CORROSION AT THE FWD WET AREA FLOORBEAM IAW ECRA 5310-0879.SDR FDEA202602140200Floorbeam · corrodedMAIN DECK FLOOR BEAM STA 1200 BTW BL 0 RBL 58 CORRODED REMOVED DAMAGE T CAP SECTION INSTALLED T CAP SECTION AND REPAIR SPLICE PARTS MAIN DECK FLOOR BEAM STA 1200 BETWEEN LBL 11 TO RBL 70.5 IAW B757 SRM 53-00-51-2R FIG 201 REP 8.SDR CALA2026021613802Floorbeam · corrodedEXT LOWER MID FUSELAGE STA 900 BL0-RBL5 T- CHORD CORRODED. REF NR: 136283. ESFR REPAIRED AREA AT EXT LOWER MID FUSELAGE STA 900 BTW RBL 25 TO LB L 25 T-CHORD IAW B757-300 SRM 51-70-12-0G FIG 1 AND RESTORED ARE A PROTECTION APPLIED TOP COAT AND APPLIED CIC IAW SDR AALA202602140449Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM TEE AT BS 947, BETWEEN LBL 4 AND RBL 4. REPAIRED THE FLOORBEAM TEE IAW SRM 53-00-51-2R-1.SDR AALA202602148760Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOORBEAM UPPER TEE AT BS 986, BETWEEN RBL 14 AND RBL 23. REPAIRED THE UPPER TEE IAW SRM 53-70-51-2R-4.SDR REXA2026080301390Floorbeam · crackedCRACKED CENTER COCKPIT FLOOR BEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT CENTER COCKPIT FLOOR BEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 670-53-11-2278REV. --SDR CALA2026021213723Floorbeam · corrodedFOUND CORROSION ON THE FLOORBEAM AT BS 333.40, BL 0, SEE BAM N/R 003182031 FOR WORK PERFORMED.SDR AALA202604241668Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N2 FR 36. CRACK L= 0.530 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOOR BEAM Y765 VERTICAL STRINGER #2 AT FR 36 SDR AALA202604226871Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N3 FR 36. CRACK L= 0.550 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM Y254 VERTICAL STRINGER #3 AT FR 36 IAWSDR AALA202604225191Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N5 FR 36. CRACK L= 0.875 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y765 VERTICAL STRINGER #5 AT FR 36 ISDR AALA202604220542Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N4 FR 36. CRACK L= 0.610 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y254 VERTICAL STRINGER #4 AT FR 36 IASDR SIMA20260210006Floorbeam · corrodedCROSSBEAM AT FRAME 14 IS CORRODED AT PREVIOUS REPAIR. PERFORMED PERMANENT REPAIR TO CROSSBEAM AT FRAME 14 IAW ERS-EJ-53MR-5388.SDR CALA2026021213719Floorbeam · corrodedAFT WET AREA FLOORBEAM BS 947.5, LBL 55 HAS CORROSION BELOW FITTING AREAS. FOUND OUT OF LIMITS, PERFORMED A REPAIR TO THE FLOORBEAM UPPER TEE IAW ESR-WI 2024175-70-14516 AND ECRA 5370-01214.SDR VNAA202602090023Angle · corrodedFS 280.00 CROSSBEAM J ANGLE IS CORRODED, CC670-34095-1, J ANGLESDR VNAA202602090039Floorbeam · corrodedLH FS280 CROSSBEAM IS CORRODED AT BL0 ON TOP FWD EDGE. FOUND TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-00-00-101-001-A01 DUE TO DEPTH OF CORROSION AND CORROSION ACROSS MULTIPLE ELEMENTS. REQUIRES REPLACEMENT.SDR VNAA202602090040Floorbeam · corrodedRH FS280 CROSSBEAM IS CORRODED AT RBL6 ON TOP FWD EDGE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 DUE TO DEPTH OF CORROSION AND CORROSION ACROSS MULTIPLE ELEMENTS. REQUIRES REPLACEMENT.SDR SWIA2026020975710Floorbeam · chafedFITTING ON FLOORBEAM RBL27 AT F.S.621 HAS 2EA. CHAFES. REMOVED AND REPLACED FITTING AT FLOORBEAM RBL27 FS621 IAW CRJ 200 SRM 51-42-22 AND REO 601R-53-61-3778 REV-B DATED 2016-12-19 FOR ALTERNATE FASTENERS COMPLETED TASK CARD 51-900-1003-SKY .SDR VNAA202603140008Floorbeam · corrodedCORROSION WAS FOUND ON CROSSBEAM FS 280 RH SIDE. RH CROSSBEAM FS280 AT COCKPIT CABIN WAS REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01, CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-10-001-001-A01SDR VNAA202603140007Floorbeam · corrodedCORROSION WAS FOUND ON FLOORBEAM BS 280 LT. CORROSION WAS FOUND ON CROSSBEAM FS 280 LH WAS EVALUATED DUE EXCESSIVE CORROSION PER CRJ-900 SRM 53-00-01-101-001-A01 AND REPLACED IAW SRM 51-42-13-001-001-A01 AND SRM 51-42-06-001-001-A01.SDR AALA202603122572Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD AT STA 986, LBL 1. REPAIRED CHORD PER SRM 53-70-51-2R-4 ALTERNATIVE 2 AND EA 372764.SDR AALA202603092770Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 986, RBL 34. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 1.SDR AALA202603098419Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 986, RBL 30. REPAIRED UPPER CHORD PER SRM 53-70-51-2R-4.SDR AALA202603091949Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 986, RBL 38. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 1.SDR AALA202603097440Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 986, RBL 44. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 1.SDR AALA202602121139Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CHORD) AT BS 947, RBL 52. REPAIRED UPPER CHORD PER SRM 53-70-51-2R-5.SDR AALA202603126670Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 986.5, RBL 48. REPAIRED CHORD PER SRM 53-70-51-2R-6.SDR AALA202603098225Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 AT LEVEL FR66 AT AFT GALLEY AREA. MEASURES L = 2.732 IN, W = 1.17 IN, D = 0.0210 IN. MAINTENANCE REPLACED FLOOR BEAM +Y1292 LOC. BTW FR64 AND FR66 AT AFT GALLEY AREA IAW A320 SRM 51-42-11-801 AND DWG D5SDR AALA202603038853Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: AIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM -Y765 BTW FR64 AND FR66 AT AFT GALLEY AREA. (MEASURES L: 1.250 IN, W: 1.026 IN D: 0.029 IN). MAINTENANCE REPLACED FLOOR BEAM -Y765 BTW FR64 AND FR66 AT AFT GALLEY AREA. IAW A320 SSDR AALA202603039183Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM Y765 BTW FR64 AND FR66 AT AFT GALLEY AREA. (MEASURES L: 1.250 IN, W: 1.026 IN D: 0.029 IN). MAINTENANCE REPLACED FLOOR BEAM Y765 BETWEEN FR64 THRU FR66 AT AFT GALLEY AREA. IAW A320 SRM 51-42-11-801, DWG D53142SDR AALA202603025272Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT BS 947, LBL 24. REPAIRED UPPER CHORD PER SRM 53-70-51-2R-5 ALTERNATIVE 2.SDR AALA202603024283Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON PASSENGER CABIN FLOOR BEAM UPPER CHORD (T-CAP) AT STA 986.5, LBL 48. REPAIRED CHORD PER SRM 53-70-51-2R-6 ALTERNATIVE 4.SDR ABXA20260212061Floorbeam · not reportedDURING C6 CHECK, ON WO 15843154, ACCOMPLISHED ABX-REA-5300-65992-00 (MODIFY - STA 390 TO 720 MAIN DECK FLOORBEAMS AND LOWER DECK CEILING, FQIS WIRE SEPARATION PROVISION, B767). C6 CHECK COMPLETED AND AIRCRAFT RETURNED TO SERVICE.SDR VNAA202603130008Floorbeam · corrodedCORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT. CORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01 AND FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBLSDR VNAA202603130007Floorbeam · corrodedCORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT. CORROSION ON FLOOR ACCESS PANEL SUPPORT ANGLE BTW LBL 9 TO RBL 9 AT COCKPIT WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 53-00-01-101-001-A01 AND FLOOR ACCESS PANEL SUPPORT ANGLE BTW LB
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