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 DALA1036689864Floorbeam · chafedDURING M-CHECK, FOUND MAIN PASSENGER CABIN STA 237 BL 0- LBL 22 FLOORBEAM IS CHAFED, BLENDED CHAFE. REMAINING WAS OUT OF LIMITS IAW SRM 53-01, FIG 1, FABRICATED PARTS AND COMPLETED REPAIRS IAW SRM 53-05, FIG 20A AND SRM 51-30-5.Dec 23, 2010 · N773NC · Doug DC951SDR UALA2010122704704Floorbeam · corrodedCORROSION FOUND ON FLOORBEAM AT STA 1640. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION AND DETERMINED THAT MATERIAL LOSS IS BEYOND LIMITS. R & R FLOORBEAM TEE CAP AND SPLICE ANGLE IAW SRM.Dec 23, 2010 · N557UA · Boeing 757222SDR USAA2010122793251Floorbeam · crackedCLT - MAJOR REPAIR - Q1 CHECK - CRACKED FLOORBEAM AT BS 660, RBL 07. REPAIRED FLOORBEAM AT BS 660, RBL 07 IAW EA 102403.Dec 23, 2010 · N405US · Boeing 737401SDR FDEA201012234740Floorbeam · misrepairedPREVIOUSLY INSTALLED REPAIR LOCATED AT MAIN CABIN FLOORBEAM FRAME 25 FWD UPPER FLANGE BETWEEN SEAT TRACKS NR2 AND NR3 RT WAS DETERMINED TO NOT BE IAW SRM 53-10-15, FIG 206 (SHEET 4) PAGES 231-232, REPAIRED IAW SRM 53-10-15 (SHEET 4) PAGES 221-224 & 231-232.Dec 23, 2010 · N423FE · Airbus A310203SDR DALA1101939855Floorbeam · crackedMAIN PAX CABIN/GALLEYS; FLOORBEAM AT STA. 718 AND RBL 55" CRACKED AT FASTENER HOLE. REMOVED FLOORBEAM & SPLICE IAW SRM 51-30-2, 51-30-3 & 51-3 0-5. INSTALLED FLOOR BEAM & SPLICE IAW SRM 51-30-2, 51-30-3 & 51-30-5, FABRICATED NEW FLOORBEAM IAW DWG 9915527. Dec 22, 2010 · N764NC · Doug DC951SDR UHLA2010122200323Floorbeam · corrodedLEVEL 2 CORROSION RT LONGITUDINAL FLOORBEAM IN SEVERAL AREAS BETWEEN FR 12-18. REMOVED AND REPLACED SEAT TRACK BEAM FR12-14 IAW EMB 170 SRM 51-40-00.Dec 22, 2010 · N634RW · Emb ERJ170100SESDR ASOA201002007Floorbeam · corrodedFS 280.00 BEAM HAS CORROSION AT SCREW HOLES ALL ALONG BEAM. BEAM REMOVED & INSTALLED IAW REO 670-53-11-047.Dec 22, 2010 · N659CA · Cndair CL6002C10SDR V0XR413Y122210010Floorbeam · crackedTEE FITTING, STA 280, LBL 11.16 CRACKED. R & R BRACKET STA 280 IAW SRM 51-42-06, W/C 1052.Dec 22, 2010 · N156GJ · Cndair CL6002C10SDR V0XR413Y122210009Floorbeam · cracked(V0XR) T-FITTING, STA 280, RVL 11.16 CRACKED. R & R TEE FITTING, STA 280, RBL 11.16 IAW SRM 51-42-21. W/C 1051Dec 22, 2010 · N156GJ · Cndair CL6002C10SDR V0XR413Y122210008Floorbeam · corroded(V0XR) FLOOR SUPPORT, STA 280 BL 0 CORRODED.Dec 22, 2010 · N156GJ · Cndair CL6002C10SDR V0XR413Y122210002Crossbeam · corroded(V0XR) STA 280 CROSSBEAM CORRODED BEYOND LIMITS. R & R CROSSBEAM FS 280.00 IAW REO 670-53-11-047 W/C 1040Dec 22, 2010 · N156GJ · Cndair CL6002C10SDR A6WA201140073Floorbeam · corrodedFLOORBEAM IS CORRODED AROUND 7 SCREW HOLES UNDER CARGO PIT FLOORBOARD 281 LLF. R & R FLOORBEAM CAP AT LBL 27.0, BETWEEN FS 569 AND FS 610, WL 73.10 IAW REO 601R-53-61-3778.Dec 21, 2010 · N454AW · Cndair CL6002B19SDR SWAA107932Floorbeam · crackedDURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 705 TO BS 715, LBL 24.5. REPAIRED BEAM PER EO & EA.Dec 20, 2010 · N682SW · Boeing 7373Y0SDR SWAA107924Floorbeam · corrodedDURING SCHEDULED 26Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, BETWEEN RBL 0 TO RBL 45.5. REPAIRED BEAM PER SRM.Dec 20, 2010 · N682SW · Boeing 7373Y0SDR DALA1036149855Floorbeam · crackedDURING M-CHECK FOUND MAIN CABIN STA 775, RBL-54 FLOORBEAM IS CRACKED. REMOVED CRACKED FLOORBEAM SECTION STA 775, RBL 16-RBL 60 IAW SRM 51-30-2 AND 51-30-5. LOCATED AND DRILLED NEW FLOORBEAM SECTION IAW SRM 51-10-4. INSTALLED NEW FLOORBEAM SECTION IAW SRM 51-3Dec 20, 2010 · N764NC · Doug DC951SDR FDEA201012204720Floorbeam · corrodedCABIN FLOORBEAM AT STN 363.23 HAS SURFACE CORROSION AROUND SCREW HOLES AT RBL2 TO RBL 12. CORROSION REPAIR CARRIED OUT IAW EA F-5310-142383, (BS 365.25) FLOOR BEAM CORROSION REPAIR AT RBL 2 TO RBL 14.) REPAIR IS CLASSIFIED AS MAJOR.Dec 20, 2010 · N946FD · Boeing 757236SDR SWAA108010Floorbeam · crackedDURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 709 TO BS 716, BBL .07. REPAIRED BEAM PER EO & EA.Dec 19, 2010 · N682SW · Boeing 7373Y0SDR SWAA108007Floorbeam · crackedDURING SCHEDULED 26Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 706 TO BS 714, BBL .07. REPAIRED BEAM PER EO & EA.Dec 19, 2010 · N682SW · Boeing 7373Y0SDR ASAA1178779Floorbeam · corrodedMAIN CABIN FLOORBEAM CORRODED BS 986.5 LBL 30. REPAIRED FLOORBEAM IAW B737 700 SRM 53 00 51 REPAIR 1 FIG 203.Dec 18, 2010 · N617AS · Boeing 737790SDR USAA2011011390209Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 + 18 INCHES TO FR69 +3 INCHES, -Y1165. REPLACED FLOORBEAM BETWEEN FR67 + 18 INCHES TO FR69 +3 INCHES, -Y1165 IAW A319 SRM 51-72-11.Dec 18, 2010 · N805AW · Airbus A319132SDR USAA2011011390208Floorbeam · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 + 18 INCHES, -Y1162. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR67 + 18 INCHES, -Y1162 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472000.Dec 18, 2010 · N805AW · Airbus A319132SDR CALA2010122000624Floorbeam · gougedSUPPORT TASK FLOORBEAM LOWER LEG HAS GOUGES FROM CEILING PANEL SCREWS AT STA 560, BL 0 - RBL 24, 4 EA, REMOVED & AMP; REPAIRED FLOORBEAM LOWER LEG GOUGES IAW SRM 53-00-51, PAGES 201 TO 204.Dec 18, 2010 · N75854 · Boeing 757324SDR DALA1035949864Floorbeam · chafedDURING M-CHECK FOUND MAIN PASSENGER CABIN STA 237 BETWEEN BL 0-LBL 22 FLOOR SUPPORT CHAFED. BLENDED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01-1. REMOVED FLOOR SUPPORT IAW SRM 51-30-05. FABRICATED AND DRILLED HOLES IAW SRM 51-10-4 AND DWG 5914617. INSDec 18, 2010 · N773NC · Doug DC951SDR DALA1506089220Floorbeam · corrodedFORWARD CARGO BAY FLOOR SUPPORT AT BS 218, LONGERON 28L TO 28R LEVEL 1 CORROSION. REPLACED IAW SRM 51-30-02, VOL II, PAGE 11, PN 9936719-169. NR 19838.Dec 17, 2010 · N920DN · Doug MD9030SDR SWAA107941Floorbeam · corrodedDURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 787+18, RBL 17. REPAIRED FLOOR TRACK PER SWA EA.Dec 17, 2010 · N498WN · Boeing 7377H4SDR USAA2010122093185Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR20, -Y189. REPLACED FLOORBEAM AT FR20, -Y189 IAW A319 SRM 53-11-14.Dec 17, 2010 · N712US · Airbus A319112SDR USAA2010122093184Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOOR BEAM BETWEEN FR20 TO FR24, -Y189. REPLACED FLOORBEAM BETWEEN FR20 TO FR24, -Y189 IAW A319 SRM 53-11-14 & 51-72-11.Dec 17, 2010 · N712US · Airbus A319112SDR USAA2010121793157Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR20, -Y180. REPLACED FLOORBEAM AT FR20, -Y180 IAW A319 SRM 53-41-00.Dec 17, 2010 · N712US · Airbus A319112SDR F3LA2010122000567Splice · corrodedC-CHECK: NON ROUTINE N0438; LT FLOORBEAM, Y1292 SPLICE COUPLING AT FRAME 66L HAS 2 INCHES OF CORROSION. CORROSION IS OUT OF LIMITS. REPLACED SPLICE COUPLING AT FRAME 66L IAW SRM 53-72-11, PARA 6.Dec 17, 2010 · N945FR · Airbus A319112SDR F3LA2010122000565Floorbeam · corrodedC-CHECK: NON ROUTINE N0436; LT FLOORBEAM, Y1292 AT FRAME 68L HAS A 2 SQ. INCHES OF CORROSION ON THE UPPER AND LOWER SIDERS. CORROSION IS OUT OF LIMITS. REPLACED FLOORBEAM, Y1292 BETWEEN FRAMES 68LT AND 69LT IAW SRM 51-72-11, PARA 6.Dec 17, 2010 · N945FR · Airbus A319112SDR DALA1036025519Floorbeam · corrodedDURING M-CHECK FOUND FWD CABIN FLOORBEAM, STN 365 PREVIOUS REPAIR FROM LBL 15 TO RBL 64 CORRODED AT SEVERAL LOCATIONS AS MARKED. BLENDED AREA ON FLOORBEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101. FABRICATED NEW UPPER CHORD TREATED AND PRIMED NDec 17, 2010 · N519US · Boeing 757251SDR DALA1036015519Floorbeam · corrodedDURING M-CHECK FOUND FWD CABIN FLOORBEAM PREVIOUS REPAIR FROM LBL 64 TO RBL 38 CORRODED AT 7 LOCATIONS AS MARKED AT BS 377.7. REMOVED CORROSION AREA BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, ORIG MATERIAL .125 MAX ALLOWABLE 10 PERCENT. REMOVED (2 EA) Dec 17, 2010 · N519US · Boeing 757251SDR FDEA201012174713Floorbeam · corrodedBULK CARGO UNDER FLOOR FR 69 LATERAL FLOOR SUPPORT ANGLE HAS CORROSION AT 17 TO 19 INCH RT OF A/C CENTER LINE (ABOUT 8 SQ. INCH) REMOVED SUPPORT BEAM, FR 69 BULK CARGO FLOOR IAW SRM 51-72-10 PAR NR 2 , LOCATED AND DRILLED UP NEW BEAM IAW SRM 51-72-10 , INSTALDec 17, 2010 · N423FE · Airbus A310203SDR SWIA201025337Floorbeam · corrodedFS 280.0 FLOORBEAM IS CORRODED AND CRACKED. (C-CHECK) REPLACE PER SRM.Dec 16, 2010 · N607SK · Cndair CL6002C10SDR SWAA107935Floorbeam · corrodedDURING SCHEDULED 24Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 10 TO RBL 10. REPAIRED BEAM PER ER AND SWA EA.Dec 16, 2010 · N327SW · Boeing 7373H4SDR SWAA107903Floorbeam · crackedDURING SCHEDULED 24Y CHECK, FOUND LONGITUDINAL FLOORBEAM CRACKED AT BS 664, RBL 24.8. REPAIRED BEAM PER ER AND EA.Dec 16, 2010 · N327SW · Boeing 7373H4SDR USAA2010121793153Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT FR16, -Y1292. REPLACED FLOORBEAM AT FR16, -Y1292 IAW A319 SRM 51-72-11 & 51-42-11.Dec 16, 2010 · N712US · Airbus A319112SDR FDEA201012164702Floorbeam · corrodedSTN 780, RBL 38 TO RBL 40 FOUND CORROSION ON FLOORBEAM. CORRODED FLOORBEAM AT STN 780, RBL 38 TO RBL 40. R & R IAW SRM 51-40-02, REV 101. REPAIR IS CLASSIFIED AS MINOR.Dec 16, 2010 · N946FD · Boeing 757236SDR USAA2010121793118Floorbeam · crackedSAL - S5 - MAJOR REPAIR - CRACK ON FLOORBEAM BETWEEN FR46 TO FR47, -Y254. REPAIRED FLOORBEAM BETWEEN FR46 TO FR47, -Y254 IAW EA 133198.Dec 16, 2010 · N628AW · Airbus A320231SDR SIMA201035101Floorbeam · corrodedDURING MAINTENACE BASE VISIT FOUND THE LEFT CABIN FLOORBEAM AT FRAME 57 TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED DOUBLER IAW EO EM-53MR-1712. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 16, 2010 · N852AE · Emb EMB135KLSDR DALA1035869864Floorbeam · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN STA 200, RBL 44 - 55 FLOOR PANEL SUPPORT HAS CORROSION. REMOVED CORROSION ON FLOOR SUPPORT STA 200, RBL 40-55 IAW SRM 53-01, FIG 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-01, FIG 1. REMOVED FLOOR SUPPORT IAW SRM 51-30-Dec 16, 2010 · N773NC · Doug DC951SDR DALA1035849864Floorbeam · corrodedDURING M-CHECK FOUND MAIN PASSENGER CABIN STA 196, LBL 44-55 FLOOR SUPPORT PANEL HAS CORROSION. REMOVED FLOOR SUPPORT IAW SRM 51-30-5. FABRICATED AND PICKED UP HOLES IAW SRM 51-10-2 & 51-10-4. INSTALLED FLOOR SUPPORT IAW SRM 51-30-5.Dec 16, 2010 · N773NC · Doug DC951SDR DALA1135489220Floorbeam · corrodedAFT COMPARTMENT CARGO SURFACE CORRSION ON FLOORBOARD SUPPORT STA 1212 LGN 28L-28R. REMOVED CORROSION ON FLOOR SUPPORT ORIG THICKNESS .063 AFTER BLENDING .50 REMAINS .013 MAT LOSS OUT OF LIMITS PER SRM 53-00-01 PG 9. REPLACED FLOOR SUPPORT.Dec 15, 2010 · N920DN · Doug MD9030SDR USAA2011012190314Floorbeam · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON FLOORBEAM BETWEEN FR56 TO FR57, S44. REPLACED FLOORBEAM BETWEEN FR56 TO FR57, S44 IAW A320 SRM 51-72-11 & AIRBUS DRAWING 53470001.Dec 15, 2010 · N624AW · Airbus A320231SDR USAA2010121793156Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FR16, -Y81. REPLACED FLOORBEAM AT FR16, -Y81 IAW A319 SRM 51-72-11.Dec 15, 2010 · N712US · Airbus A319112SDR USAA2010121793152Floorbeam · corrodedPIT - C11 - MAJOR REPAIR - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM BETWEEN FR16 TO FR20, Y254. REPLACED FLOORBEAM BETWEEN FR16 TO FR20, Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53110900.Dec 15, 2010 · N712US · Airbus A319112SDR CALA2010121600621Floorbeam · crackedSUPPORT TASK; A/B/B LOWER STRAP CRACKED AT BOTTOM OF FLOORBEAM 1380 RBL 50 (LOOK FWD OF DOOR CUTOUT UPPER FLOORBEAM MARKED). REPAIRED DAMAGED AREA AT STA 1380 RBL 50 BELOW CABIN FLOOR REF ECRA 5360-01155, ALL STEPS OF ECRA HAVE BEEN COMPLIED WITH.Dec 15, 2010 · N78866 · Boeing 75733NSDR FDEA201012154693Floorbeam · corrodedSTA 1681, FLOORBEAM UPPER CAP LOWER SIDE IS CORRODED AROUND FLOOR PANEL HOLES. REMOVED DAMAGE IAW SRM. CORROSION DETERMINED TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 6, P 103; ORIGINAL MATERIAL .156", REMAINING - 090", LOSS - .066". FABRICATEDec 15, 2010 · N473AC · Boeing 757200SDR FDEA201012154691Floorbeam · corrodedFLOORBEAM UPPER CHORD AT STA 345 HAS SEVERAL CORROSIONS BETWEEN BL 0 TO LBL 45. REMOVED CORROSION IAW SRM 51-10-02. AREA OUT OF LIMITS IAW SRM 53-00-57, FIG 101, DETAIL III. ORIG MATT .125 AFTER REWORK .087 EXCEEDS MAX OF 10 PERCENT, REMOVED DAMAGED UPPER Dec 15, 2010 · N997FD · Boeing 757200SDR FDEA201012154689Floorbeam · gougedFLOORBEAM UPPER CHORD STIFFENER AT STA 365 BETWEEN BL 0 AND RBL 60 HAS GOUGES AND CORROSION. REMOVED DAMAGE IAW SRM 53-00-51, FIG 101, DETAIL 3; ORIGINAL MATERIAL -.090", AFTER REWORK -.038", LOSS - .012", MORE THAN 10 PERCENT ALLOWABLE, OUT OF LIMITS IAW SRDec 15, 2010 · N473AC · Boeing 757200
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