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 C77A201202180009Floorbeam · corrodedAFT CABIN RIGHT FLOORBEAM, AT FR 85 IS CORRODED BEYOND SRM LIMITS. R & R LT FLOORBEAM IAW SRM 51-41-02 AND 51-43-02 ON WO 452281-283 IAW EO E175-53MR094, WO 516804.Feb 14, 2012 · N619CZ · Emb ERJ170200LRSDR C77A201202180005Gusset · corrodedAFT CABIN RIGHT FLOORBEAM INBD GUSSET, AT FR 90 IS CORRODED BEYOND SRM LIMITS. R & R RT FLOORBEAM INBD GUSSET IAW SRM 51-41-02 AND 51-43-02 ON WO 452281-278 IAW EO E175-5300-045, WO 517415.Feb 14, 2012 · N619CZ · Emb ERJ170200LRSDR C77A201202180004Floor Splice · corrodedFWD CABIN FR 19, LEFT FLOORBEAM DOUBLER, IS CORRODED BEYOND SRM LIMITS. R & R LT FLOORBEAM DOUBLER IAW SRM 51-41-02 AND 51-43-02 ON WO 452281-268 IAW EO E175-5300-044, WO 517412.Feb 14, 2012 · N619CZ · Emb ERJ170200LRSDR FDEA201202140576Floorbeam · damagedDAMAGED HOLES FOUND IN FLOORBEAM AT BS 310, RBL 2.00 TO LBL 20.00. UNDER FLIGHT DECK DOOR KICK STRIP RETAINING INSERTS. INBD APPROX .005" DEEP, MID APPROX .017 DEEP, OTBD .022" DEEP. FLOORBEAM REPAIRED IAW EA F-5210-157298.Feb 14, 2012 · N918FD · Boeing 75723ASDR IPXA12671835Floorbeam · corrodedINSPECTION TYPE:C, FOUND MAIN CARGO DECK INTERIOR FLOORBEAM CORROED AT BS 1540, RBL 76. CORROSION: 1.7 INCH (LENGTH) X 0.6 INCH (WIDTH). REPAIRED IAW EO B767-5310-46116-A.Feb 13, 2012 · N313UP · Boeing 76734AFSDR IPXA12671834Floorbeam · corrodedINSPECTION TYPE:C, FOUND MAIN CARGO DECK INTERIOR FLOORBEAM CORROED AT BS 1540, RBL 63. REPAIRED IAW EO B767-5310-46118-A.Feb 13, 2012 · N313UP · Boeing 76734AFSDR IPXA12671833Floorbeam · corrodedINSPECTION TYPE:C, FOUND MAIN CARGO DECK INTERIOR FLOORBEAM CORROSION AT STA 1540, LBL 68. REPAIRED IAW EO B767-5310-46117-A.Feb 13, 2012 · N313UP · Boeing 76734AFSDR IPXA12671832Floorbeam · corrodedINSPECTION TYPE: C, FOUND MAIN CARGO DECK INTERIOR FLOORBEAM CORRODED AT BS 1263, RBL 78. CORROSION 1 INCH (LENGTH) X 0.48 INCH (WIDTH). REPAIRED IAW SRM 53-00-51.Feb 13, 2012 · N313UP · Boeing 76734AFSDR CHQA20120213061Floorbeam · corrodedDURING INSPECTION, THE MIDDLE BEAM ON CENTER FUSELAGE I FLOOR STRUCTURE WAS FOUND TO BE CORRODED. THE MIDDLE BEAM ON CENTER FUSELAGE I FLOOR STRUCTURE WAS REPLACED. THE NEW PART WAS INSTALLED IAW SRM 51-40-02.Feb 13, 2012 · N293SK · Emb EMB145LRSDR SWIA201229687Floorbeam · crackedC-CHECK, FS 280 FLOORBEAM IS CRACKED ON LEFT AND RIGHT SIDES. REPAIRED CRACKED FLOORBEAM.Feb 13, 2012 · N217AG · Cndair CL6002C10SDR USAA2012021500023Floorbeam · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR17 BETWEEN -Y1456 TO -Y1959. REPLACED FLOORBEAM AT FR17 BETWEEN -Y1456 TO -Y1959 IAW SRM 51-44-11 & 51-42-11.Feb 13, 2012 · N276AY · Airbus A330323SDR DALA1208793117Floorbeam · corrodedAFT CABIN BETWEEN FR 65 & 66 FLOORBEAM Y765 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, AFTER CORROSION REMOVAL. ORIG MAT. 0.157" DAMAGE DIM. L=1" W=1" D=.035".Feb 13, 2012 · N317NB · Airbus A319114SDR SWAA2012030902033Floorbeam · crackedLONGITUDINAL FLOORBEAM UPPER CHORD CRACKED AT BS 671.5, RBL 24.5. REPAIRED CHORD IAW EA.Feb 12, 2012 · N510SW · Boeing 7375H4SDR SWIA201229843Floorbeam · crackedFS 280.00 FLOORBEAM CRACKED. (C-CHECK) REPAIRED FS 280.00 FLOORBEAM CRACKED.Feb 12, 2012 · N753SK · Cndair CL6002C10SDR USAA2012022700010Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR68, Z-500, Y1162.5. REPLACED FLOORBEAM IAW SRM 51-72-11 & DRAWING D53472780.Feb 12, 2012 · N121UW · Airbus A320214SDR USAA2012022700008Floorbeam · corrodedC11 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR66, Z-500, Y1292. REPLACED FLOORBEAM AT FR66, Z-500, Y1292 IAW A320 SRM 51-72-11 & DRAWING D53472780.Feb 12, 2012 · N121UW · Airbus A320214SDR AALA20120220016Floorbeam · corrodedMAIN CABIN FLOORBEAM UPPER TEE SURFACE CORRODED AT BS 1640, LBL 6 TO RBL 17. INSTALLED NEW STRAP PER SRM`S 53-00-51, 51-20-01 AND 51-40-02.Feb 12, 2012 · N666A · Boeing 757223SDR USAA2012022100006Floorbeam · corrodedC11 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR20, Z-500, Y765. REPLACED FLOORBEAM IAW SRM 51-42-11, 51-75-12 & IPC 53-21-02.Feb 12, 2012 · N121UW · Airbus A320214SDR USAA2012022000036Floorbeam · corrodedC11 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69 & BETWEEN FR69 & FR70, Y160.5. REPLACED FLOORBEAM IAW SRM 51-42-11.Feb 12, 2012 · N121UW · Airbus A320214SDR USAA2012022000034Floorbeam · corrodedC11 CHECK, LEVEL 2 INTERGRANULAR & EXFOLIATION CORROSION ON FLOORBEAM AT FR20, Z-500, Y1292. REPLACED FLOORBEAM IAW SRM 53-42-11.Feb 12, 2012 · N121UW · Airbus A320214SDR USAA2012022000033Floorbeam · corrodedC11 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT FR16, Z-500, Y503.2. REPLACED FLOORBEAM IAW SRM 53-11-14 & 51-72-11.Feb 12, 2012 · N121UW · Airbus A320214SDR DALA1208803117Floorbeam · corrodedAFT CABIN, BETWEEN FR 66 & 68. FLOORBEAM Y765 CORRODED. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15. AFTER CORROSION REMOVAL, ORIG MAT. 0.157" DAMAGE DIM. L=2.6" W=.80" D=.035".Feb 12, 2012 · N317NB · Airbus A319114SDR FDEA201202120560Floorbeam · corrodedCABIN FLOORBEAM FOUND CORRODED AT STA 460 X= 48 TO X =53. REMOVED IAW SRM 51-31-01, REV 48 AND INSTALLED NEW FLOORBEAM IAW AMM 20-50-02, REV 70.2. NEW FLOORBEAM REPLACED IAW DWG ACA7364-1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114Feb 12, 2012 · N601FE · Doug MD11FSDR IPXA2B71994Floorbeam · corrodedINSPECTION TYPE:D, FWD CARGO COMPT STA 640, LBL 94 CEILING AREA FLOOR PANEL SUPPORT FOUND CORROSION CRACK. REPAIRED IAW RS R-53-25-37319 REV A & EO B747-5310-46204-A JUST BTW LBL83 TO LT MOST OTBD, ORIG MATL:BAC1505-101050-7075T6511 AND THICKNESS 0.196", CORRFeb 11, 2012 · N581UP · Boeing 7474R7FSDR UALA2012021300818Floorbeam · corrodedUPPER DECK FLOORBEAM STA 1020 LBL 6 UPPER T-CHORD CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED CORRODED SECTION OF T-CAP. SPLICED IN NEW SECTION PER SRM 53-10-07, FAA FORM 8100 -9, & ECRA 5310-05444. EVERY 3,000 CYCLES PERFORM DETAILED VISUAL INSP OF REPAIFeb 11, 2012 · N105UA · Boeing 747451SDR DALA1208280674Floorbeam · corrodedFLOORBEAM CORRODED STA 338 RBL 23-RBL 44. REPAIRED PER B757 SRM 53-00-51 ON N/R 42955, THIS REPAIR IS RE-WRITTEN FROM ORIGINAL N/R 43191.Feb 11, 2012 · N674DL · Boeing 757232SDR AALA20120211TUL03Floorbeam · damagedHOLES ELONGATED IN FLOORBEAM RIGHT SIDE STATION 845 4 INCHES FROM OUTBOARD. INSTALLED CHANNEL DOUBLERS PER EA MD80-53-021678.Feb 11, 2012 · N110HM · Doug DC983SDR SWAA2012030201866Floorbeam · corrodedFLOORBEAM CAP CORRODED BS 986, BETWEEN TO BL 0 TO RBL 18. REMOVED AND REPLACED BEAM IAW REO AND EA.Feb 10, 2012 · N510SW · Boeing 7375H4SDR USAA2012022100011Floorbeam · corrodedC11 CHECK, LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR20+5 INCHES, -Y189.REPLACED FLOORBEAM IAW SRM 51-72-11 & EA 500531.Feb 9, 2012 · N750UW · Airbus A319112SDR USAA2012021700020Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM. REPLACED FLOORBEAM IAW SRM 51-72-11 & DRAWING D53472780.Feb 9, 2012 · N750UW · Airbus A319112SDR USAA2012021600020Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR66+13.5 INCHES, Y1227. REPLACED FLOORBEAM IAW SRM 51-72-11.Feb 9, 2012 · N750UW · Airbus A319112SDR USAA2012021600015Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 TO FR67, -Y318. REPAIRED FLOORBEAM BETWEEN FR65 TO FR67, -Y318 IAW A319 SRM 51-72-11 & AIRBUS DRAWINGS # D53472814.Feb 9, 2012 · N750UW · Airbus A319112SDR USAA2012021600001Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR66, Y1732. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR65 TO FR66, Y1732 IAW A319 SRM 51-72-11 & AIRBUS DRAWING # D53474250.Feb 9, 2012 · N750UW · Airbus A319112SDR USAA2012021500007Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEEN FR66+5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66+5 INCHES TO FR70, Y765 IAW A319 SRM 51-72-11, AIRBUS DRAWING # D53472780.Feb 9, 2012 · N750UW · Airbus A319112SDR USAA2012021500006Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEEN FR12 TO FR24, S23L, Y254. REPLACED FLOORBEAM BETWEEEN FR12 TO FR24, S23L, Y254 IAW A319 SRM 51-72-11, AIRBUS DRAWING # D53112816 & D53110920.Feb 9, 2012 · N750UW · Airbus A319112SDR USAA2012021500005Floorbeam · corrodedC11 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEEN FR12 TO FR24, Y1292. REPLACED FLOORBEAM BETWEEEN FR12 TO FR24, Y1292 IAW A319 SRM 51-72-11, AIRBUS DRAWING # D53110920, D53112812 & D53110984.Feb 9, 2012 · N750UW · Airbus A319112SDR AALA20120209AFW02Floorbeam · corrodedCABIN FLOORBEAM STATION 347 FROM LEFT BUTTLINE 37 TO RIGHT BUTTLINE 44 HAS CORROSION AND WEAR FROM NUT CLIPS. INSTALLED REPAIR STRAP PER EA B767-53-021477.Feb 9, 2012 · N388AA · Boeing 767323SDR USAA2012022400004Floorbeam · corrodedC3 CHECK - CORROSION ON FLOORBEAM T-CAP AT BS700, Y2218. REPAIRED FLOORBEAM T-CAP AT BS 700, Y2218 IAW B757 SRM 53-00-51-3R.Feb 8, 2012 · N201UU · Boeing 7572B7SDR DALA1206980139Floorbeam · corrodedFS 1197 + 132 LBL 22 FLOORBEAM UPPER CHORD IS CORRODED AND REPLACED PER B767-300 SRM 51-10-02 PG 2 PARA 9 AND DWG 146T1229 SH 1.Feb 8, 2012 · N139DL · Boeing 767332SDR IPXA12572152Floorbeam · corrodedINSPECTION TYPE: C, MAIN CARGO FLOORBEAM STA 1200, LBL 45 TO RBL 55 FLOORBEAM CORRODED ON UPPER FLANGE AT NUTPLATE HOLES. REMOVED CORROSION. ORIGINAL THICKNESS .270, MATERIAL REMOVED IS .025-.05, REMAINING THICKNESS .180-.205, OUT OF LIMITS IAW SRM 53- 00-5Feb 7, 2012 · N456UP · Boeing 75724APFSDR IPXA12572144Floorbeam · corrodedINSPECTION TYPE: C, MAIN CARGO BAY BS 1680, LBL 3 TO LBL 14, FLOORBEAM HAS CORROSION. REMOVED CORROSION, ORIGINAL THICKNESS IS .075 LOSS OF .005-.025 WITH .070- .050 REMAINING IS OUT OF LIMITS. REMOVED DAMAGE AND REPAIRED IAW EA 128249 EO B757-5310-46277-A.Feb 7, 2012 · N456UP · Boeing 75724APFSDR IPXA12572143Floorbeam · corrodedINSPECTION TYPE: C, MAIN CARGO BAY BS 1680, RBL 27 TO RBL 41, FLOORBEAM HAS CORROSION. REMOVED CORROSION ORIGINAL THICKNESS IS .075, LOSS OF .003- .030 WITH .072- .045. REMAINING IS OUT OF LIMITS, REMOVED DAMAGE AND REPAIRED IAW EA 128249. EO B757-5310-46277Feb 7, 2012 · N456UP · Boeing 75724APFSDR IPXA12572096Floorbeam · corrodedINSPECTION TYPE: C, MAIN CARGO FLOORBEAM, BS 1100, BL 0 TO RBL 45, CORRODED ON UPPER SURFACE AT NUTPLATE HOLES. REMOVED CORROSION ON FLOORBEAM, ORIGINAL MATERIAL .0196 LOSS OF .101 WITH .095. FOUND OUT OF LIMITS IAW SRM 53-00-51-1A1. REMOVED DAMAGE AND REPAIFeb 7, 2012 · N456UP · Boeing 75724APFSDR DALA1208240674Floorbeam · corrodedMAIN CABIN FLOORBEAM CORROSION OUT OF LIMITS AS DOCUMENTED ON N/R 42955. REPAIRED ON N/R 43191 PER B757 SRM 53-00-51.Feb 7, 2012 · N674DL · Boeing 757232SDR DALA1206940674Floorbeam · corrodedMAIN CABIN FLOORBEAM HAS CORROSION NUMEROUS SPOTS BS 365, RBL1 - RBL 64. CORROSION OUT OF LIMITS. REPAIRED PER B757 SRM 53-00-51, FIG 201, REPAIR 1.Feb 7, 2012 · N674DL · Boeing 757232SDR DALA1206611603Floorbeam · crackedFS 999 LONGITUDINAL FLOORBEAM CRACKED AND REPAIRED PER B767-300 SRM 53-00-51 REPAIR 3 FIG 201.Feb 7, 2012 · N1603 · Boeing 767332SDR AALA20120207TUL02Floorbeam · corrodedTOP OF CABIN FLOORBEAM HAS SMALL AREA OF CORROSION AROUND FASTENER. BLENDED OUT CORROSION AND INSTALLED REPAIR ANGLE PER AARD 53-00-00-7.Feb 7, 2012 · N931AN · Boeing 737823SDR ASOA201200425Floorbeam · corrodedREMOVED FLOORBEAM CAP ANGLE OTBD SIDE OF FLOORBOARD SUPPORT STRUCTURE OF FS 349.00. RBL 36. REINSTALLED FLOORBEAM STRUCTURE AT FS 349, RBL 36.0 IAW SRM 51-42-06 AND 51-42-21.Feb 6, 2012 · N972EV · Cndair CL6002B19SDR IPXA2572185Floorbeam · corrodedINSPECTION TYPE:C, MAIN CARGO BAY BS 1100, LBL 25 TO LBL 45 FLOORBEAM TEE CAP HAS CORROSION AROUND EVERY NUT PLATE HOLES. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .196 LOSS OF .056 WITH .140. REMAINING IS OUT OF SRM LIMITS REPAIRS IAW EA 120254 EO B757Feb 6, 2012 · N456UP · Boeing 75724APFSDR IPXA2572033Floorbeam · corrodedINSPECTION TYPE: C, MAIN CARGO BS 1055, BL 0 TO RBL 25 FLOOR SUPPORT INTERCOSTAL HAS CORROSION AROUND 4 EA NUT PLATE HOLES. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .050 MATERIAL LOSS OF .013 WITH .037 REMAINING IS OUT OF LIMITS IAW SRM 53-00-51-1A1. FFeb 6, 2012 · N456UP · Boeing 75724APF
Back to JASC 5315