JASC 5321
Service difficulty reports · 49,350
Reports filed under 5321 · Fuselage Floor Panel, 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 = '5321' 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 = '5321' 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 FDEA202303310534Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1475/RBL38.5-40 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242LF(P/N:152W8452-20) AT STA1475/RBL38.5-40 CRACK.SIZE:L=1.6" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM 53-00SDR FDEA202303310533Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242PF(P/N:152W8652-6) AT STA1475/RBL27-29 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242PF (P/N:152W8652-6) AT STA1475/RBL27-29 CRACK.SIZE:L=1.8" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM 53-00-50-1SDR FDEA202303310532Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1430.5-1431/RBL45.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1430.5-1431/RBL45.5 CRACK.SIZE:L=1.4" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM SDR FDEA202303310531Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1391.25/LBL42.75-44.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241QF (P/N:152W8652-21) AT STA1391.25/LBL42.75-44.5 CRACK.SIZE:L=1.7" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PERSDR FDEA202303310530Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1415.5/LBL39-40 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1415.5/LBL39-40 CRACK.SIZE:L=1.5" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777 SRM 53-00-SDR FDEA202303310529Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1447.5/LBL43.5-44.25 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1447.5/LBL43.5-44.25 CRACK.SIZE:L=1.2" IN LOWER SURFACE HONEYCOMB CORE AREA.EVALUATED THE CRACK AS PER B777SDR SWAA2023041122273Floorboard · pulledDOT A24-10 CENTER CABIN FLOOR BOARD 241CF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 241CF AND FOUND DAMAGE TO UPPER SURFACE . FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 SDR SWAA2023041122275Floorboard · pulledDOT A24-6 CENTER CABIN FLOOR BOARD 242BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING PLIES LENGTH OF BOARD ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PSDR SWAA2023041122276Floorboard · pulledDOT A24-7 CENTER CABIN FLOOR BOARD 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 242AF AND FOUND DAMAGE TO UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PSDR SWAA2023041122277Floorboard · pulledDOT A24-8 CENTER CABIN FLOOR BOARD 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE ON UPPER SURFACE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1 PARA 1A. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A C E-F. VERIFIED MASDR SWAA2023041122278Floorboard · pulledDOT A24-9 CENTER CABIN FLOOR BOARD 231ZF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING PLIES LENGTH OF BOARD ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PSDR SWAA2023041122279Floorboard · pulledDOT A24-11 CENTER CABIN FLOOR BOARD 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING PLIES LENGTH OF BOARD ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND SDR SWAA2023041122284Floorboard · pulledDOT A24-18 CENTER CABIN FLOOR BOARD 231XF AFT O/B CORNER UPPER PLY PULLED AWAY FROM CORE.<[01] EVALUATED AND FOUND DAMAGE ON UPPER SURFACE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1 PARA 1A. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A C E-F. VERIFIEDSDR SWAA2023041122285Floorboard · delaminatedDOT A24-20 CENTER CABIN FLOOR BOARD 241AF AFT LEFT EDGE COMPOSITE DELAMINATED.<[01] WORK ACCOMPLISHED ON W.O.#TTG8Q00K5U6C;[02] VERIFIED STEP 1SDR DALA2023040302519Baffle · cracked(LOG 2695400) DURING INSPECTION FOUND FWD CARGO COMPARTMENT L/H FLOOR BAFFLE BETWEEN STA 500 AND 500A CRACKED. REMOVED DAMAGED BAFFLE FROM FWD CARGO L/H SIDE BETWEEN STA 500 AND 500A AND REPLACED FOR A NEW PART PER B737 S.R.M 51-40-02-0G AND DWG# 143A7505.SDR DALA2023040302518Baffle · damaged(LOG 2695396) DURING INSPECTION FOUND FWD CARGO COMPARTMENT L/H FLOOR BAFFLE BETWEEN STA 500C AND 500D DAMAGED. REMOVED DAMAGED BAFFLE FROM FWD CARGO L/H BETWEEN STA 500C TO 500D AND REPLACED FOR A NEW PART PER B737 S.R.M 51-40-02-0G AND DWG# 143A7505.SDR DALA2023033102492Unknown · unknownSHIP 658 CORROSION ON WEB FROM STA. 760 TO 780, ABOVE S-22L AT FWD CARGO COMPARTMENT. CORRECTIVE ACITON: SUMMARY OF NRC 00340: WEB WAS FABRICATED AND REPLACE PER DWG 143N5335 REV.A, B-757-200 SRM. (2696218)SDR FDEA202303300524Floor Panel · crackedREWORK:MAIN DECK CARGO FLOOR PANEL P/N:152W8750-2 FOUND CRACKED AT STA2020 BL0. EVALUATED MAIN DECK CARGO FLOOR.P/N:152W8750-2 AT STA 2020 BL0 AS.PER B777 SRM 53-00- 50-1A. ALLOWABLE DAMAGE 1, REV.43.1 FOUND UPPER TEAR L X W=2.1" X 0.5", OUT OF ALLOWABLE LISDR DALA2023040302516Unknown · unknown(LOG 2694251) DURING INSPECTION FOUND FWD CARGO R/H Z-CHANNEL HAS EVIDENCE OF CORROSION FROM STA 500 - STA 500L STR 25. REMOVED AND REPLACED FWD CARGO R/H ZEE CHANNEL STA 500 TO STA 500L IAW B737 SRM 51-40-02, SRM 53-30-53-01, SRM 53-00-53-2R PROCEDURE 5, B737SDR DALA2023040302515Web · damaged(LOG 2694207) DURING INSPECTION FOUND FWD CARGO DOOR THRESHOLD WED DAMAGED STA 440-STA 480+10. REMOVED DAMAGED THRESHOLD WEB FROM FWD CARGO STA 440-480+10 PER B737 S.R.M 51-40-02-0G AND INSTALLED A NEW WEB PER B737 S.R.M 51-40-02-0G AND DWG# 143A8330 REV-A.SDR DALA2023033002439Unknown · unknown(LOG 2694270) DURING INSPECTION FOUND CORROSION ON SHIELD AFT OF FWD CARGO DOOR R/H SIDE STA 480+10 - STA 500A. REMOVED SHIELD AT STA 480+10 - STA 500A IAW B737 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW SHIELD IAW B737 SRM 51-40-05-0G-0 AND INSTALLED NEW SHIESDR DALA2023033002438Channel · corroded(LOG 2694190) DURING INSPECTION FOUND R/H Z CHANNEL AT STA 867 - 947 HAS MULTIPLE SPOTS OF CORROSION AT RBL 22 WL 158. REMOVED AND REPLACED ZEE CHANNEL STA 867-947 RBL22 WL158 IAW B737 SRM 51-40-02, SRM 51-40-05 AND BOEING DWG#147A7500.SDR DALA2023033002437Shield · corroded(LOG 2694164) DURING INSPECTION FOUND CORROSION ON FWD SHIELD AT STA 767 - 787 R/H RBL 22 WL 158 IN AFT CARGO. REMOVED AND REPLACED WITH NEW SHIELD STA 767-787 RH RBL 22 IN AFT CARGO IAW B737 SRM 51-40-02-0G DRAWING # 146A0081 REV A.SDR 2A6R2023032966802Floor Panel · delaminatedDENT, DELAMINATION, AND CRACK DAMAGE WAS DISCOVERED ON THE AFT CABIN FLOOR LOWER SKIN PANEL (PN: L533M1416234) ALL ALONG THE AFT LOWER EDGE WITH THE CRACK DAMAGE MEASURING APPROXIMATELY 1.5” AND THE DENT AND DELAMINATION APPROXIMATELY 36.0” X 1.5”. A DETAILEDSDR 2A6R2023032966801Floor Panel · delaminatedDURING 1000 HOUR INSPECTION, FOUND DAMAGE TO THE CABIN FLOOR IN THE FORM OF DENTS AND DELAMINATION APPROXIMATELY 2.5” X 5.0” AT APPROXIMATELY FUSELAGE STATION 3,400 MM. A DETAILED DESCRIPTION OF THE DAMAGE AND APPROVED REPAIR PROCEDURES ARE PROVIDED IN AIRBUSSDR CALA2023032900922Unknown · corrodedPASSENGER CABIN FLOOR STRUCTURE R/H CREASE BEAM INNER CHORD IS CORRODED (2 PLACES) AT STA. 847. CREATED LOG PAGE TO CREATE AN ESFR WORK ACCOMPLISHED ON ECRA 5311-02957. SEE BAM LOG PAGE 001236817.SDR CALA2023032900921Structure · corrodedPASSENGER CABIN FLOOR STRUCTURE L/H CREASE BEAM INNER CHORD IS CORRODED AT STA 867 CREATED LOG PAGE TO CREATE AN ESFR WORK ACCOMPLISHED ON ECRA 5311-02958. SEE BAM LOG PAGE 001236817. SHOULD READ BAM LOG PAGE 001236815.SDR SWIA2023050100017Unknown · crackedRH FLOOR BEAM FS484.00 RBL 27 CLIP IS CRACKED (INBD CLIP) (C-CHECK RO 4/26/2023) REMOVED AND REPLACED FLOOR BEAM CLIP AT FS 484.0, RBL 27. REF. REO 601R-53-41-059 REV. -C DATED 2020-03-11. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRSDR SWIA2023050100016Unknown · crackedLEFT SIDE. FLOOR BEAM OUTBOARD CLIP AT FS 484.0 IS CRACKED. (C-CHECK RO 4/26/2023) REMOVED AND REPLACED LEFT SIDE FLOOR BEAM OUTBOARD CLIP AT FS484.0. REF. REO 601R-53-41-059 REV. -C DATED 2020-03-11.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL60SDR DALA2023033002436Unknown · unknown(LOG 2692655) DURING INSPECTION FOUND CORROSION FLOOR BEAM LOCATED BS947.5 AND RBL49 AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON FLOOR BEAM 947.5 BETWEEN RBL 50 AND LBL 50 ALL STEPS IS DOCUMENTS ON ORNRC 88/200 RII INSPECTION COMPLETE . JOB COMPLETE ASSOSDR DALA2023033002435Unknown · unknown(LOG 2692641) DURING INSPECTION FOUND CORROSION FLOOR BEAM LOCATED BS947.5 AT LEVEL LBL24.5 AT PASSENGER CABIN. PERFORMED REPAIR INSTRUCTIONS OF CORROSION DAMAGE ON THE UPPER CHORD OF THE FLOOR BEAM AT AT 947.5 AS PER ER/A 605919-14 REV.ORIGINAL.SDR DALA2023033002447Unknown · unknownSHIP 665 CORROSION ON FLOOR SUPPORTS (3EAS) BTW STA 660 TO STA 640 LBL 2,11 AND 15 AT FWD CARGO COMPARTMENT. CORRECTIVE ACITON: SUMMARY OF NRC 00245. FLOOR SUPPORTS (3EAS) BTW STA 660 TO STA 640 LBL 2,11 AND 15 AT FWD CARGO COMPARTMENT. WERE REPLACED PER B757-SDR DALA2023033002445Unknown · unknownSHIP 665 CORROSION ON LH SIDEPLATE STA.600 TO 640.AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00272: LH SIDE PLATE ON STA. 590 TO STA. 640 AT FWD CARGO COMPARTMENT WAS REPLACED PER B757- 200 SRM. (2692821)SDR DALA2023033002443Unknown · unknownSHIP 6706 CORROSION FLOOR STRUCTURE LOWER SILL BTW. STA.1380 TO STA.1440 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00049: LOWER SILL BTW. STA .1380 TO STA.1440 AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B757-200 SRM AND DWG 146N5391 REV.USDR DALA2023032902400Unknown · unknownSHIP 3352 CORROSION FLOOR BEAM -Y953 LOCATED FR33 TO FR38 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y953 LOCATED BTW FR33 TO FR38 IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2692842)SDR DALA2023032902399Unknown · unknownSHIP 3352 CORROSION FLOOR STRUCTURE Y450 LOCATED FR34 TO FR37 PLUS 10IN IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK Y450 LOC. FR34 TO FR37 IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2692757)SDR DALA2023032902398Unknown · unknownSHIP 3352 CORROSION FLOOR STRUCTURE LOCATED -Y2462 BTW FR33 TO FR35 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y2462, LOC BTW FR26 TO FR37.4 IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2692742)SDR DALA2023032902397Unknown · unknownSHIP 3352 CORROSION FLOOR BEAM -Y450 LOCATED FR32 TO FR33 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM SECTION -Y450 LOCATED BETWEEN FR25 TO FR37 IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2692735)SDR DALA2023032902396Unknown · unknownSHIP 3352 CORROSION FLOOR STRUCTURE LOC. -Y1959 BTW FR33 TO FR37 PLUS 10IN. IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1959 LOC. - BTW FR33 TO FR37 IN PASSENGER CABIN. RII INSPECTION COMPLETE. (2692726)SDR SWAA2023042621298Floor Panel · brokenFWD CABIN FLOOR BOARD PANEL 221BF O/B AFT TANG IS BROKEN.<FOUND BROKEN TANG TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-0I-1 PARA 4B.REMOVED DAMAGED TANG AT O/B AFT CORNER AND CLEANED AREA IAW SRM 53-00-50-2R-6 PARA 3C-E. FABRICATED CORE PLUG FROM BMSDR SWAA2023041821236Floor Panel · delaminatedPANEL 193AR HAS A DELAMINATION ON THE OUTER SKIN AT 6' FWD OF AFT EDGE (MARKED)<[01] IDENTIFIED PART AND MATERIAL IAW SRM 53-40-70-0I-1 FIGURES 1-2; TABLE 2; ITEM [18].<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4.B (6).<BR>SDR SWAA2023041721247Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL #221FF LARGE AREA TOP SKIN FIBERGLASS PEELING OFF<[01] REPLACED MAIN CABIN FLOOR PANEL #221FF REF. B737-700 AMM 53-21-00-400-801. THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00HHHPE;[02] VERIFIED STEP 1SDR AALA202303281542Floorboard · damagedAIRCRAFT WAS NOT GROUNDED: FLOOR IN AISLE AROUND ROW 20 SOFT AND MAKES NOISE WHEN STEPPED ON. REPAIRED PER AARD.SDR DALA2023032902406Unknown · unknown(LOG 2689317) DURING INSPECTION FOUND CORROSION SUPPORT ZEE LOCATED BTW STA 500A TO STA 500L AT LEVEL STR 26R AT FWD CARGO COMPARTMENT. PERFORMED REPAIR INSTRUCTION CORROSION SUPPORT ZEE LOCATED BTW STA 500A TO STA 500L AT LEVEL STR 26R AT FWD CARGO COMPARTMENSDR DALA2023032802380Unknown · unknownSHIP 658 IN REF NRC #00317: CORROSION ON LH SIDE PLATE (UPPER AND LWR SURFACE) FROM STA. 720 TO 765 AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00721: LH SIDE PLATE (UPPER AND LWR SURFACE) FROM STA. 720 TO 765 AT FWD CARGO COMPARTMENT WAS REPAISDR DALA2023032802378Unknown · unknownSHIP 658 SECONDARY NRC: CORROSION OUT OF LIMITS ON FLOOR STRINGERS RBL 2 BSTA. 550 AT FWD CARGO. IN REF NRC 00369. CORRECTIVE ACTION: SUMMARY OF NRC 00740: FLOOR STRINGER RBL 2 BSTA. 550 AT FWD CARGO WAS REPLACED PER B757-200 SRM. (2688247)SDR DALA2023032702346Unknown · unknownSHIP 3352 CORROSION FLOOR BEAM +Y953 LOCATED BTW FR33 TO FR37.1 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK Y953 AND FASTENERS LOC. BTW FR26/28 TO FR37.4 MID PASSENGERS CABIN. (2689566)SDR DALA2023032702345Unknown · unknownSHIP 3352 CORROSION FLOOR STRUCTURE LOCATED -Y1456 BTW FR36 TO FR37 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK SECTION -Y1456 LOC. FR28 TO FR37 IN PASSENGER CABIN. (2688371)SDR CALA2023032700886Unknown · corrodedPASSENGER CABIN FLOOR STRUCTURE R/H CREASE BEAM INNER CHORD IS CORRODED (2 PLACES) AT STA. 847.SDR CALA2023032700885Unknown · corrodedPASSENGER CABIN FLOOR STRUCTURE L/H CREASE BEAM INNER CHORD IS CORRODED AT STA 867
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