JASC 5321

Service difficulty reports · 49,402

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.

SDR FDEA201109214003Floor Panel · crackedFLOOR PANEL 251BH HAS 1EA 10" CRACK. FABRICATED REPLACEMENT FLOOR PANEL 251 BH IAW DWG SRZ25-005, REV J. MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605RSDR FDEA201109214002Floor Panel · crackedFLOOR PANEL 232YG HAS 2 EA 9" CRACKS. FABRICATED FLOOR PANEL 232YG IAW DWG SRZ 25-005, REV J, MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605RSDR FDEA201109214001Floorboard · crackedFLOORBOARD HAS 2 EA 6" CRACKS ON BACKSIDE AND 1EA DELAMINATED CORNER FABRICATED REPLACEMENT FLOORBOARD 132MG IAW DWG SRZ-25-005, REV J MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605RSDR FDEA201109214000Floorboard · damagedFLOORBOARD HAS MULTIPLE PUNCTURES ON BACK SIDE AND DELAMINATED CORNER. FABRICATED REPLACEMENT FLOORBOARD 132KG IAW DWG SRZ-25-005 REV J IDENTIFIED. REPLACEMENT FLOORBOARD IAW GMM 7-0-1001. MAJOR REPAIR IAW GMM6-2-100.Sep 21, 2011 · N669FE · Airbus A300F4605RSDR FDEA201109213988Floorboard · crackedFLOORBOARD 242RG HAS 1EA 12" CRACK. FABRICATED REPLACEMENT FLOORBOARD 242 RG IAW DWG SRZ 25-005, REV J.Sep 21, 2011 · N669FE · Airbus A300F4605RSDR ASOA201101762Pressure Deck · corrodedCORROSION FOUND AT PRESSURE FLOOR FS 424-559 LBL 36, STR 17. REMOVED COSSOSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT INSP PROCEDURE UT-3 MIN. MATERIAL REMAINING IS .071" WITHIN ALLOWABLE LIMITS OF REO 601R-53-41-666.Sep 20, 2011 · N839AS · Cndair CL6002B19SDR FDEA201109203975Floor Panel · crackedFLOOR PANEL 251QH HAS 1EA 10" CRACK. FABRICATED REPLACEMENT FLOOR PANEL 251QH IAW DWG SRZ 25-005 REV J.Sep 20, 2011 · N669FE · Airbus A300F4605RSDR FDEA201109203974Floor Panel · crackedFLOOR PANEL 241DF HAS 2EA 10" CRACKS FABRICATED REPLACEMENT FLOOR PANEL 241DF IAW DWG SRZ 25-005, REV J.Sep 20, 2011 · N669FE · Airbus A300F4605RSDR FDEA201109203972Floor Panel · damagedBULK CGO COMPT 161JF EDGE AND UPPER SKIN GOT IMPACT DAMAGE. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM, IRM 9701 AND DWG 17 A532 79960.Sep 20, 2011 · N679FE · Airbus A300F4605RSDR ZZDA2011791Floor Panel · corrodedR1 DOOR LWR JAM CUTOUT SILL FWD AFT FLOOR SUPPORT PANELS, CORROSION. ACCOMPLISHED FLOOR SUPPORT PANELS REPLACEMENT PER B717 SRM 51-41-01 AND 53-00-00.Sep 19, 2011 · N996AT · Boeing 717200SDR UIEA2011092100517Floor Panel · corrodedDURING THE PRESENT C4-CHECK, CORROSION WAS REPORTED ON UPPER DECK LIFT CAR ASSY, PN 747-9202-14 LOWER FLOOR PANEL ASSY SHOWN IN FIG 1. CORROSION AFFECTED LOWER PANEL ASSY PN 747-9262-1 BOTH UPPER AND LOWER SURFACE SHEET SIDES AND AFT EDGES AS SHOWN IN FIG 2. Sep 19, 2011 · N464MC · Boeing 747446SDR FDEA201109193957Floor Panel · crackedFLOOR PANEL 252VF HAS 3EA. 9" CRACKS FABRICATED REPLACEMENT FLOOR PANEL 252VF IAW DWG 25-005, REV J.Sep 19, 2011 · N669FE · Airbus A300F4605RSDR FDEA201109193956Floor Panel · crackedFLOOR PANEL 252PH HAS 1EA 12" CRACK FABRICATED REPLACEMENT FLOOR PANEL 252PH IAW DWG 25-005, REV J.Sep 19, 2011 · N669FE · Airbus A300F4605RSDR FDEA201109193955Floor Panel · crackedFLOOR PANEL 252UH HAS 2EA 12" CRACKS FABRICATED REPLACEMENT FLOOR PANEL 252UH IAW DWG SRZ 25-005, REV J.Sep 19, 2011 · N669FE · Airbus A300F4605RSDR FDEA201109183951Floor Panel · damagedM/D COMP'T AFT REMOVED 242EK FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70614.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183950Floor Panel · damagedM/D COMP'T AFT REMOVED 242ZJ FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70609.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183949Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242QJ FLOOR PANEL INSP CHECK, FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG NR 15 B532 70600.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183948Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242GF FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 14 B532 70480.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183947Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242MF FLOOR PANEL INSPECTION CHECK FOUND UPPER SKIN ADN EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70337.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183946Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242RG FLOOR PANEL. INSPECTION CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70620.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183945Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242VG FLOOR PANEL, INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 16 B532 70260.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183944Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 241TH FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG NR 15 B532 70600.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183943Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 241AJ FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70609.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183942Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252UH FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70337.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183941Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252PH FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 16 B532 70260.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183940Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252BF FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 16 B532 70262.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183939Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 241GJ FLOOR PANEL AND INSP CHECK. FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70620.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183938Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242SF FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70618.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183937Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251PH FLOOR PANEL AND INSP CHECK. FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70276.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183936Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252VF FLOOR PANEL AND INSP CHECK, FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70339.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183935Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252WH FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG NR 17 B532 70278.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183934Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251BH FLOOR PANEL AND INSP CHECK, FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70287.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183933Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251VF FLOOR PANEL AND INSPECTION CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70339.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183932Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251YG FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG NR 17 B532 70281.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183931Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251WH FLOOR PANEL AND INSPECTED. FOUND UPPER SKIN AND EDGE AREA HAS IMPACT DAMAGE. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW FLOOR PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70278.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109183930Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251UH FLOOR PANEL AND INSPECTED, FOUND UPPER SKIN AND EDGE AREA HAS IMPACT DAMAGE. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW FLOOR PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70337.Sep 18, 2011 · N679FE · Airbus A300F4605RSDR USAA2011100600033Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232YF BETWEEN FR32 TO FR35, -Y1292. REPLACED FLOOR PANEL 232YF IAW A320 SRM 53-02-00 FIGURE 209.Sep 17, 2011 · N659AW · Airbus A320232SDR USAA2011100600032Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 252NF BETWEEN FR54 TO FR58, -Y1292. REPLACED FLOOR PANEL 252NF IAW A320 SRM 53-02-00 FIGURE 209.Sep 17, 2011 · N659AW · Airbus A320232SDR USAA2011100600031Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 252EF BETWEEN FR47 TO FR51, -Y1292. REPLACED FLOOR PANEL 252EF IAW A320 SRM 53-02-00 FIGURE 209.Sep 17, 2011 · N659AW · Airbus A320232SDR USAA2011100600030Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 251AF BETWEEN FR47 TO FR51, BETWEEN Y=0 TO -Y765. REPLACED FLOOR PANEL 251AF IAW A320 SRM 53-02-00 FIGURE 209.Sep 17, 2011 · N659AW · Airbus A320232SDR USAA2011100600021Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232UF BETWEEN FR28 TO FR32, -Y1292. REPLACED FLOOR PANEL 232UF IAW A320 SRM 53-02-00 FIG 209.Sep 17, 2011 · N659AW · Airbus A320232SDR USAA2011100300031Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR24 TO FR28, -Y254. REPLACED FLOOR PANEL BETWEEN FR24 TO FR28, -Y254 IAW A320 SRM 53-02-00 FIGURE 209.Sep 17, 2011 · N659AW · Airbus A320232SDR USAA2011092700004Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 232FF BETWEEN FR20 TO FR24, BETWEEN -Y1732 TO -Y1292. REPLACED FLOOR PANEL 232FF BETWEEN FR20 TO FR24, BETWEEN -Y1732 TO -Y1292 IAW A320 SRM 53-12-00, IRM 9701 REV G.Sep 17, 2011 · N112US · Airbus A320214SDR FDEA201109173922Floor Panel · damagedM/D COMP'T AFT REMOVED 242BF FLOOR PANEL INSPECTION CHECK FOUND UPPER SKIN AND EDGE AREA IMPACT DAMAGED. THE DAMAGED AREA IS OVER THE ALLOWABLE DAMAGE LIMITS . FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, IRM 9701 AND DWG B532 70478. THE REPAIR CLASSIFSep 17, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109173921Floor Panel · damagedM/D COMP'T AFT REMOVED 241QH FLOOR PANEL AND INSPECTION CHECK FOUND UPPER SKIN AND EDGE AREA RECEIVED IMPACT DAMAGED. THE DAMAGED AREA IS NOT WITHIN ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, IRM 9701 AND DG 15 B532 70 618. Sep 17, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109173920Floor Panel · damagedM/D COMP'T AFT REMOVED 231AH FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA IMPACT DAMAGED. THE DAMAGED AREA IS NOT WITHIN THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, IRM 9701, AND DWG 14 B532 70476. THE REPAIR ESep 17, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109173919Floor Panel · damagedM/D COMP'T AFT REMOVED 242UJ FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, IRM 9701, AND DWG 15 B532 70604. THE REPAIR EVALUSep 17, 2011 · N679FE · Airbus A300F4605RSDR FDEA201109173918Floor Panel · damagedM/D COMPARTMENT AFT REMOVED 232YG FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA IMPACT DAMAGED. THE DAMAGED AREA IS NOT WITHIN THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, AND DWG 14 B532 70506. THE REPAIR CLASSIFISep 17, 2011 · N679FE · Airbus A300F4605RSDR USAA2011100600035Floor Panel · delaminated2S CHECK - DELAMINATION ON FLOOR PANEL 252GF BETWEEN FR51 TO FR54, -Y254. REPLACED FLOOR PANEL 252GF IAW A320 SRM 53-02-00.Sep 16, 2011 · N659AW · Airbus A320232SDR IPXA20110916001JFloor Panel · damagedMAIN DECK FLOOR PANEL NR12 AT BS 460, RBL 50 IS DAMAGED. R & R FLOOR PANEL REF NR 475585Sep 16, 2011 · N413UP · Boeing 75724APF
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