JASC 5315

Service difficulty reports · 44,220

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 DALA1115890136Floorbeam · corrodedAFT CARGO STA 1219, LBL 35.0 AND LBL 44.0 FLOORBEAM UPPER CHORD FOUND CORRODED. FLOORBEAM UPPER CHORD TRIMMED AT LBL 14 AND REMOVED BET LBL 14 TO LBL 44.0 AND SECTIONAL CHORD REPAIR CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 4 OTIS.Feb 13, 2011 · N136DL · Boeing 767332SDR DALA1115880136Floorbeam · corrodedAFT CARGO STA 1197 AT RBL 6.5 AND RBL 44.0 FLOORBEAM UPPER CHORD FOUND CORRODED. FLOORBEAM UPPER CHORD TRIMMED AT RBL 0 AND REMOVED BET RBL0 TO RBL 44.0 AND SECTIONAL CHORD REPAIR CARRIED OUT IAW SRM 53-00-07, FIG 201, REPAIR 4 OTIS.Feb 13, 2011 · N136DL · Boeing 767332SDR SWIA201125640Floorbeam · crackedFS 280 FLOORBEAM IS CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.Feb 13, 2011 · N773SK · Cndair CL6002C10SDR FDEA201102130553Floorbeam · crackedMAIN DECK FLOORBEAM AT FR 28 BETWEEN SEAT TRACK 2R AND 3R, HAS 1" IN LONG CRACK ON T-CHORD. REMOVED THE DAMAGED SECTION FROM FLOORBEAM AT FR 28 BETWEEN SEAT TRACK 2R AND 3R IAW SRM 53-10-15, STEP 2 PG 394, NDT CHECK COMPLIED WITH IAW NTM 51-10-08, NO CRACK NOFeb 13, 2011 · N674FE · Airbus A300F4605RSDR REXA201100112Floorbeam · corrodedLEFT BUTT LINE 27.0 FS 605.00 TO FS 621.00 OUTBOARD SIDE FLOORBEAM FLANGE HAS CORROSION. REPAIRED IAW BSC EO 601R-53-20572A.Feb 13, 2011 · N8839E · Cndair CL6002B19SDR SWAA110929Floorbeam · crackedDURING SCHEDULED 20Y CHECK, FOUND LONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 669, RBL 24.5. REPAIRED BEAM PER EA.Feb 13, 2011 · N512SW · Boeing 7375H4SDR SWAA110922Floorbeam · corrodedDURING SCHEDULED 6Y CHECK, FOUND AFT CARGO COMPARTMENT FLOORBEAM CORRODED AT BS 767, LBL 8.1. REMOVED AND REPLACED BEAM PER SRM.Feb 13, 2011 · N204WN · Boeing 7377H4SDR SWAA110920Floorbeam · corrodedDURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 312, RBL 19. REPAIRED BEAM PER SRM.Feb 13, 2011 · N726SW · Boeing 7377H4SDR IPXA1B65410Floorbeam · corrodedINSPECTION TYPE:D, M/D FLOORBEAM UPPER CHORD FOUND CORROSION AT STA 980 RBL 75-80. M/D FLOORBEAM AT BS980 BTN RBL55 TO RT MOST OTBD AREA UPR CHORD REPAIRED IAW RS R53-25-36948, REV A & EO B747-5310-41600-A. ORG THICKNESS IS 0.148", BLEND DEPTH REMAINS 0.050" Feb 12, 2011 · N583UP · Boeing 7474R7FSDR IPXA1M64751Floorbeam · damagedFLOORBEAM AND STABILIZATION STRAP HAVE OVERSIZE HOLE THROUGH BOTH. FREEZE PLUG HOLE IN FLOORBEAM AND FABRICATED NEW STRAP IAW EOMD11-5310-41455A.Feb 12, 2011 · N271UP · Doug MD11FSDR DALA1110275530Floorbeam · corrodedFLOORBEAM STA 345, LBL-63 TO RBL-63 HAS CORROSION. COMPLIED WITH ERA 489011-14 REV ORIGINAL. THIS REPAIR IS MAJOR & PERMANENT WITH NO FURTHER INSPECTIONS REQUIRED. INSPECTION COMPLETED.Feb 12, 2011 · N530US · Boeing 757251SDR DALA1110255530Floorbeam · corrodedFLOORBEAM, STA 324, BL 0, RBL 63 HAS CORROSION. REMOVED CORROSION FROM FLOOR BEAM STA 324, BL-0. FOUND OUT OF LIMITS. REMOVED WEB FROM RBL 24, STA 324 TO STA 345. FLOORBEAM REPAIRED IAW ERA 488481-14, REV D AND REINSTALLED WEB AT RBL24 STA 324 TO STA 345 IAFeb 12, 2011 · N530US · Boeing 757251SDR SWAA110857Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 36. REPAIRED BEAM PER EA.Feb 12, 2011 · N347SW · Boeing 7373H4SDR SWAA110835Floorbeam · corrodedDURING SCHEDULED 16Y CHECK, FOUND FLOORBEAM CORRODED AT BS 947.5, LBL 5. REPAIRED BEAM PER SRM.Feb 12, 2011 · N607SW · Boeing 7373H4SDR SWAA110814Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND AFT CARGO FLOORBEAM ANGLE CORRODED AT BS 860, RBL 2. REPAIRED BEAM PER EA.Feb 12, 2011 · N344SW · Boeing 7373H4SDR SWAA110813Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 727E, LBL 3. REPAIRED BEAM PER EA.Feb 12, 2011 · N344SW · Boeing 7373H4SDR SWAA110812Floorbeam · corrodedDURING SCHEDULED 22Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 727E, LBL 17. REPAIRED BEAM PER EA.Feb 12, 2011 · N344SW · Boeing 7373H4SDR SWAA110747Floorbeam · wornDURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM WORN AT BS 887, BETWEEN LBL 22 TO RBL 4. REPAIRED BEAM PER EA.Feb 12, 2011 · N725SW · Boeing 7377H4SDR DALA1116210136Floorbeam · corrodedFWD GALLEY AREA FLOORBEAM AT STA 287 UPPER HORIZ FLANGE UPPER SURFACE FOUND CORRODED AT RBL22 (NRC 0634 ) AND RBL 62 (NRC 0635). CORROSION AT RBL 62 IS ON EXISTING REPAIR. CABIN FLOORBEAM AT STA 287 UPPER HORIZ FLANGE CUT AND TRIMMED BET RBL8 TO RBL45 FROM RFeb 11, 2011 · N136DL · Boeing 767332SDR DALA1112031814Floorbeam · corrodedM/D STA 325 RBL 30 TO RBL 50 FLOORBEAM FOUND CORRODED AND REPAIRED IAW SRM 53-00-51 REPAIR 1 FIG 201.Feb 11, 2011 · N838MH · Boeing 767432ERSDR SWIA201125641Floorbeam · crackedFS 280 FLOORBEAM LOWER FLANGE CRACKED ON RIGHT SIDE. (C-CHECK) REPAIR PER REO. REPLACED PER SRM.Feb 11, 2011 · N866AS · Cndair CL6002B19SDR QXEA2011021400143Floorbeam · damagedC6 CHECK - FS 280 CROSSBEAM RIDING ON, WORKING AGAINST LONGITUDINAL FLOORBEAM CAPS AT RBL 11 AND LBL 11. REMOVED AND INSTALLED NEW 280, WORKED FLOORBEAM LONGITUDINAL CAPS AND COMPLETED REPAIR IAW REO 670-53-11-045, 670-53-11-047, NDTM 51-20-08 AND SRM 51-25-0Feb 11, 2011 · N606QX · Cndair CL6002C10SDR FDEA201102110535Floorbeam · corrodedMAIN DECK, BS 365.25 FLOORBEAM, BETWEEN RBL 45 - 58, UNDERNEATH UPPER CHORD, HAS CORROSION AROUND NUT PLATE HOLES. REMOVED CORROSION BY BLENDING AREA IAW SRM 51-10-02 AREA OUT OF LIMITS. ORIGINAL MAT .125 AFTER REWORK .077 EXCEEDS MAX ALLOWABLE DAMAGE OF 10 PFeb 11, 2011 · N926FD · Boeing 7572S7SDR JR2R2011021100008Floorbeam · corrodedFLOOR SUPPORT TRANSVERSE BEAM CORRODED AT STA 349 AND RBL 41. REPAIRED FLOOR SUPPORT TRANSVERSE BEAM AT FS 349 RBL 41 IAW RO CRJ-53-2514.Feb 11, 2011 · N77302 · Cndair CL6002B19SDR USAA2011021690763Floorbeam · corrodedPIT - MAJOR REPAIR - C11/SY6 CHECK - 26C22053003/003, LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR 12 - FR 16, Y-81. REPLACED FLOORBEAM AT FR 12 - FR 16, Y-81 IAW A320 SRM 51-72-11.Feb 10, 2011 · N659AW · Airbus A320232SDR DALA1109949873Floorbeam · corrodedMAIN CABIN STA 200, RBL 44 TO 57 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION 11" IAW SRM 51-10-ORIG MAT .060 IAW SRM 53-13-1, FIG 4 AND 51-10-14 S-.22 MAT LOSS REMAINING 53-01, FIG 1. R & R FLOOR SUPPORT 116441. REQUIRED INSP COMPLETED.Feb 10, 2011 · N782NC · Doug DC951SDR DALA1109833274Floorbeam · corrodedFWD CABIN FLOORBEAM -254 IS CORRODED AT FR 18. ORIGINALTHICKNESS .079" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REMOVED FLOORBEAM AND SPLICE IAW SRM 51-42-11. RECEIVED NEW FLOORBEAM AND MACHINED BEAM AFT END TO FIT SPLICE IAW ER/A 489275-14. LOCATED AND DFeb 10, 2011 · N374NW · Airbus A320212SDR UALA2011021100728Floorbeam · corrodedCORROSION ON FLOORBEAM AT LOCATION BS 365 AT RBL 15. MAJOR REPAIR ACCOMPLISHED: CORROSION REMOVAL IS BEYOND LIMITS REQUIRING REPLACEMENT. REPLACED FLOORBEAM IAW SRM. TREATED AND PRIMED AREA.Feb 10, 2011 · N560UA · Boeing 757222SDR AALA20110210TUL01Floorbeam · damagedFLOORBEAM LOWER AFT FLANGE STATION 420 LEFT BUTTLINE 20 HOLE DAMAGED. REPAIRED IAW SRM 53-00-51-2R AND EA B757-53-015076.Feb 10, 2011 · N646AA · Boeing 757223SDR CALA2011032400179Floorbeam · corrodedCABIN: STA 303 LBL 30 TO 40 FLOORBEAM DOUBLER CORROSION FOUND. CABIN: STA 303 LBL 30 TO LBL 40 FLOORBEAM DOUBLER COR BLEND OUT D 0.020"(ORG 0.063") OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND FLOORBEAM UPPER CHORD AND DOUBLER REPAIRED AS PER SRFeb 9, 2011 · N59053 · Boeing 767424ERSDR CALA2011032400178Floorbeam · corrodedCABIN: STA 325 LBL 48 TO 53 FLOORBEAM CORROSION FOUND. CABIN STA 325 LBL 48 TO 53 FLOORBEAM CORRODED BLEND OUT D0.037" (ORG 0.090") OUT OF SRM 53-00-51 ALLOWABLE DAMAGE, FIG 101 LIMIT AND COR FLOORBEAM REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND FORM 44Feb 9, 2011 · N59053 · Boeing 767424ERSDR DALA1121026904Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER FWD FLANGE CORRODED STA 1640 LBL 17-RBL 17. ADDITIONAL CORROSION LBL 55-59 / ACCOMPLISHED ERA 488913-14MA REV ORIGINAL.Feb 9, 2011 · N752AT · Boeing 757212SDR DALA1120126904Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER SURFACE CORRODED STA 345 LBL18. REPAIRED AT SAA DURING HMV ON N/R CARD 175471.Feb 9, 2011 · N752AT · Boeing 757212SDR UALA2011021000687Floorbeam · damagedFLOORBEAM, STA 1681 AT RBL 32 HAS DAMAGE. MAJOR REPAIR ACCOMPLISHED REPAIRED IAW EVA UA-EVA-80549B.Feb 9, 2011 · N565UA · Boeing 757222SDR FDEA201102090517Floorbeam · crackedMAIN DECK CARGO FLOORBEAM LOWER CHORD AT STA 1761, "X" = -107 FOUND DEFORMED, CRACKED. REPAIRED AS PER E.A. 1-5310-143855, PART 1, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100, REVISION 111.Feb 9, 2011 · N614FE · Doug MD11FSDR FDEA201102090516Floorbeam · crackedMAIN CARGO COMPARTMENT FLOORBEAM HAS CRACK AT FRAME 64 BETWEEN SEAT TRACK R-4 AND R-5 ( -Y1456 AND -Y1858) .5 IN LONG CUT OUT DAMAGED AREA IAW SRM 53-10-15, FIG 211, PG 389. TRIMMED FLOORBEAM IAW 53-10-15, PG 391-392. NDT CHECK FOR CRACKS IAW IAW NTM 51-10-0Feb 9, 2011 · N674FE · Airbus A300F4605RSDR CALA2011020900076Floorbeam · corrodedCABIN STA 325 LBL 30 TO 51 FLOORBEAM DOUBLER CORROSION FOUND. CABIN STA 325 LBL 30 TO 51 FLOORBEAM DOUBLER CORROSION BLEND OUT D:0.018 (ORG 0.063) OUT OF SRM 53-00-51 ALLOWABLE DMG 1 FIG 101 LIMIT AND DOUBLER REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 WORKFeb 9, 2011 · N59053 · Boeing 767424ERSDR CALA2011020900075Floorbeam · corrodedCABIN STA 303 LBL 51 TO 55 FLOORBEAM UPPER CHORD CORROSION FOUND. STA 303 LBL 51 TO 55 FLOORBEAM UPPER CHORD CORROSION BLEND OUT D:0.036 (ORG 0.090") OUT OF SRM 53-00-51 ALLOWABLE DMG FIG 101 LIMIT AND FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIRFeb 9, 2011 · N59053 · Boeing 767424ERSDR CALA2011020900074Splice Plate · corrodedCABIN STA 325 RBL 38 TO 41 FLOORBEAM SPLICE PLATE CORRODED. STA 325 RBL 38 TO 41 FLOORBEAM SPLICE PLATE CORROSION BLEND OUT D:0.019" (ORG.063") OUT OF SRM 53-00-51 ALLOWABLE DMG 1 FIG 101 LIMIT AND SPLICE PLATE REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 WOFeb 9, 2011 · N59053 · Boeing 767424ERSDR DALA1133301608Floorbeam · corrodedCABIN-STA 1480 LBL 50 FLOORBEAM FOUND CORRODED AND REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201.Feb 8, 2011 · N1608 · Boeing 767332SDR ASOA201100244Angle · crackedFS 280.090, RBL 9.0, OTBD ANGLE IS CRACKED. REMOVED CRACK ANGLE IAW SRM 51-42-21. FABRICATED AND INSTALLED ANGLE IAW REO 601R-53-11-638, REV A, STEP 4.Feb 8, 2011 · N835AS · Cndair CL6002B19SDR DALA1109453274Floorbeam · corrodedFWD CABIN FLOORBEAM +Y1292 IS CORRODED AT FR 16 BLENDED OUT CORRODED AREA IAW SRM 51-74-00, L=7.0" W=1.5" D=0.045", ORIGINAL MATERIAL THICKNESS 0.079", FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. REMOVED FLOORBEAM IAW SRM 51-42-11. INSTALLED NEW FLFeb 8, 2011 · N374NW · Airbus A320212SDR COMA2011020850014Floorbeam · crackedFS 280 FLOOR SUPPORT CRACKED AT LBL 9 AND RBL 9. REMOVED AND REPLACED DISCREPANT FLOORBEAM IAW SRM 51-42-06 AND 51-42-21.Feb 8, 2011 · N369CA · Cndair CL6002C10SDR V0XR413Y020811002Floorbeam · corrodedFLOOR SUPPORT 280 LBL 9 TO RBL 9 IS CORRODED. R & R FLOOR CHANNEL SUPPORT FS 280.00 LBL 9 TO RBL 9 IAW SRM 53-11-10/ 51-42-06.Feb 8, 2011 · N163GJ · Cndair CL6002C10SDR V0XR413Y020811001Floorbeam · corrodedSTA 280 FLOORBEAM CORRODED. ACCOMPLISHED REPLACEMENT OF FLOORBEAM AT FS 280.00 IAW REO 670-53-11-351-A.Feb 8, 2011 · N163GJ · Cndair CL6002C10SDR IXXA11SMN044SFloorbeam · crackedDURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FLOORBEAM WEB CRACKED AT STA 960.000 LT BOTTOM LINE 56. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW EXTRUSION ANGLE AND FILLER. CLEANED TREATED, PRIMED AREA AND RFeb 7, 2011 · N821BX · Doug DC871FSDR IPXA11M64899Floorbeam · damagedINSPECTION TYPE:3C, DEFERED ITEM D-444065 FLOORBEAM AT STA 939 X=90 DAMAGE REPAIR. TRIMMED OUT DAMAGE ON STA 939 FLOORBEAM, FABRICATED REPAIR ANGLE AND FILLER AND INSTALLED REF STA,SA, EA 011-5310-01-A2888 AND EO MD11-5310-41562-A.Feb 7, 2011 · N287UP · Doug MD11FSDR MALA110032Floorbeam · damagedFLOORBEAM 280.0 HAS 2 RIVET HEADS DAMAGED AND CORRODED AT 9 LBL AND 9RBL MARKED. R & R 2 RIVETS IAW SRM 51-42-16 ALSO REMOVED MINOR SURFACE CORROSION AND RESTORED FINISH IAW 51-21-06.Feb 7, 2011 · N600LR · Cndair CL6002D24SDR ASOA201100237Floorbeam · crackedCABIN FLOOR SUPPORT STRUCTURE FS 280.00 AND LBL 9.0 CLIP IS CRACKED. REMOVED CRACKED FLOORBEAM IAW SRM 51-42-21. FABRICATED REPAIRE IAW REO 601R-53-11-638 REV A, STEP 4. INSTALLED REPAIR IAW REO 601R-53-11638 STEP 11.Feb 7, 2011 · N835AS · Cndair CL6002B19SDR USAA2011021090692Floorbeam · corrodedS2 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM UPPER CHORD AT FR75, S26L, Y450. REPAIRED FLOORBEAM UPPER CHORD AT FR75, S26L, Y450 IAW SRM 53-41-14.Feb 7, 2011 · N270AY · Airbus A330323
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