N362NB

Service difficulty reports · 152

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N362NB' AND registry_match = 'registration'
  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 DALA13032353162Floor Panel · damagedAFT CARGO FLOOR PANEL 151ZG HAS MULTIPLE DENTS & DELAMINATING. FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.Jun 27, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032343162Floor Panel · damagedFWD CARGO FLOOR PANEL 131AF HAS PREVIOUS REPAIRS, CRACKS & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.Jun 27, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032333162Floor Panel · damagedFWD CARGO FLOOR PANEL 131CG HAS PREVIOUS REPAIRS & MULTIPLE DENTS. FABRICATED NEW FLOOR PANEL IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.Jun 27, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032323162Floor Panel · damagedFWD CARGO SLOPE PANEL 131DG HAS PREVIOUS REPAIRS & MULTIPLE DENTS. FABRICATED NEW SLOPE PANEL IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.Jun 27, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032313162Floor Panel · dentedFWD CARGO SLOPE PANEL 131CF HAS PREVIOUS REPAIR & MULTIPLE DENTS. FABRICATED NEW SLOPE PANEL IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.Jun 27, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032303162Floor Panel · dentedFWD CARGO BAY SLOPE PANEL 132EG HAS MULTIPLE DENTS. FABRICATED NEW SLOPE PANEL IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.Jun 27, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032293162Floor Panel · damagedFWD CARGO BAY SLOPE PANEL 131EG HAS MULTIPLE DENTS & DELAMINATED. FABRICATED NEW SLOPE PANEL IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.Jun 27, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032183162Floor Panel · corrodedAFT UTILITY FLOOR PANEL 261FF CORRODED. NEW FLOOR PANEL INSTALLED.Jun 24, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032173162Blanking Plate · debondedAFT CABIN FWD R2 GIRT BAR FITTING BLANKING PLATE DISBONDED AND CORRODED. R & R R2 FWD BLANKING PLATE IAW SRM 51-42-11.Jun 23, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13032163162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231XG DELAMINATED. REMOVED AND INSTALLED FLOOR PANEL IAW MM 53-42-12, PB 401 AND SRM 51-42-12. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 22, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032153162Skin · damagedAFT RY FUSELAGE EXTERNAL SKIN BETWEEN FR 64-65 AND STR 16-18R HAS DEEP GOUGE MEASURED 1.3" X 1.1". PERFORM PRELIMINARY AND HIDDEN DAMAGE INSPECTION IAW RSQCM 6.3.3.1 AROUND THE VICINITY OF DAMAGED SKIN. BLENDED DAMAGED AREA IAW SRM 51-73-00 CHECKED LIMITS, FJun 21, 2013 · N362NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13032143162Floor Support · corrodedAFT UTILITY AREA FR 68 FLOOR SUPPORT -Y1292 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Jun 21, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13032133162Floor Support · corrodedAFT UTILITY AREA BETWEEN FR 64 AND 66 FLOOR SUPPORT STRUCTURE -Y129. 2 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Jun 21, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13032123162Floor Support · corrodedAFT UTILITY AREA BETWEEN FR 67 AND 68 FLOOR SUPPORT -Y129 2 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Jun 21, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13032113162Floor Support · corrodedAFT UTILITY AREA AT FR 66 FLOOR SUPPORT -Y1732 HAS CORROSION. BLENDED AREA ON FLOOR SUPPORT -IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. R & R FLOOR SUPPORT IAW SRM DWG 53470-150 AND SRM 51-42-11.Jun 21, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13032103162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231CF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 21, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032093162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232DF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 21, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032083162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222CF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 21, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13032073162Blanking Plate · corrodedR1 DOOR FWD BLANKING PLATE CORRODED 2.0" X 2.0". R1 DOOR FWD BLANKING PLATE REPLACED IAW SRM 51-72-00.Jun 21, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13032063162Blanking Plate · corrodedAFT CABIN FWD L2 GIRT BAR FITTING BLANKING PLATE PREVIOUS MISDRILLED SCREW HOLE AND CORRODED. L2 DOOR FWD BLANKING PLATE REPLACED IAW SRM 51-72-00.Jun 21, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13030813162Blanking Plate · corrodedAFT CABIN AFT L2 GIRT BAR FITTING BLANKING PLATE CORRODED 3" X 1". INSTALLED NEW BLANKING PLATE.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13030803162Floor Panel · corrodedAFT UTILITY FLOOR PANEL 262FF CORRODED 3" X 3". NEW FLOOR PANEL INSTALLED.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030793162Floor Panel · corrodedFWD UTILITY FLOOR PANEL 221FF CORRODED 3" X 3". PANEL INSTALLED.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030783162Floor Panel · delaminatedFWD UTILITY FLOOR PANEL 221PF DELAMINATED 4" X 4". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030773162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221DF DELAMINATED 12" X 8". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030763162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 222EF DELAMINATED 8" X 4". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030753162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231FF DELAMINATED 6" X 4". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030743162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232FF DELAMINATED 5" X 4". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030733162Floor Panel · puncturedMAIN CABIN FLOOR PANEL 231MF PUNCTURED 1.5" X 1.5". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030723162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231LF DELAMINATED 4" X 4". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030713162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241FF DELAMINATED 5" X 5". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030703162Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251JF DELAMINATED 3" X 3". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030693162Floor Panel · delaminatedAFT UTILITY FLOOR PANEL 262EF DELAMINATED 7" X 4" LONG. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DRWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030683162Floor Panel · delaminatedAFT UTILITY FLOOR PANEL 261DF DELAMINATED 6" X 5" LONG. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030673162Floor Panel · delaminatedAFT UTILITY FLOOR PANEL 261NF DELAMINATED 5" X 5". FABRICATED FLOOR PANEL IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030663162Floor Panel · delaminatedAFT UTILITY FLOOR PANEL 262AB DELAMINATED 4" X 4". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030653162Floor Panel · corrodedAFT UTILITY FLOOR PANEL 261PF HAS CORRODED INSERTS 1" X 1". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640. TO BE INSTALLED ON WC 2500-6602.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13030643162Floorbeam · corrodedAFT UTILITY AREA AT FR 68, FLOORBEAM Y1292 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R AFT UTILITY AREA FLOORBEAM Y1292 IAW SRM 51-42-11 AND DWG D53474180.Jun 20, 2013 · N362NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA13030633162Floor Support · corrodedAFT UTILITY AREA, PREVIOUS REPAIR, BET FR64 AND FR66, FLOOR SUPPORT Y1292 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. ORIGINAL THICKNESS 0.087", L=0.80", W=0.70", D=0.030", FOUND TO BE OUT OF LIMIT IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW TRM 53-21-01.Jun 19, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13030293162Skin · dentedFWD FUSELAGE EXTERNAL SKIN SURFACE HAS DENT BETWEEN FR 11 TO 12, S23-24L. PERFORMED DETAILED VISUAL INSP, NO CRACKS NOTED. ACCOMPLISHED INTERNAL AND EXTERNAL HFEC INSPECTION IAW NTM 51-10-08 PT 6, NO DEFECTS. NO REPAIR ACTION REQUIRED IAW SRM 53-11-11, DIA Jun 18, 2013 · N362NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13030253162Seat Track · corrodedFWD CABIN FRAME 20-22,-Y1292 SEAT TRACK CROWN HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105, R & R FLOOR SUPPORT IAW SRM 51-42-11 AND DG D53111008.Jun 18, 2013 · N362NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13030243162Floor Support · corrodedFWD UTILITY AREA FRAME 16-20 FLOOR SUPPORT +Y 1292 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-11-15, FIG 105. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53111008.Jun 18, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13030233162Floor Support · corrodedFWD UTILITY AREA FRAME 16-18 FLOOR SUPPORT Y254 HAS CORROSION (2 PLACES). REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53111008.Jun 18, 2013 · N362NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13030283162Skin · dentedFWD FUSELAGE EXTERNAL SKIN SURFACE HAS DENT 1.5" AFT OF FR 21, BETWEEN S22-23L. PERFORMED DETAILED VISUAL INSPECTION, NO CRACKS NOTED. ACCOMPLISHED INTERNAL AND EXTERNAL HFEC INSPECTION IAW NTM 51-10-08, PT 6, NO DEFECTS. NO REPAIR ACTION REQUIRED IAW SRM 53Jun 17, 2013 · N362NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13030273162Skin · dentedFWD FUSELAGE EXTERNAL SKIN SURFACE HAS DENT 5" AFT OF FR 20, BTW S24-25L. PERFORMED DETAILED VISUAL INSPECTION, NO CRACKS NOTED. ACCOMPLISHED INTERNAL AND EXTERNAL HFEC INSP IAW NTM 51-10-08, PT 6, NO DEFECTS. NO REPAIR ACTION REQUIRED IAW SRM 53-11-11, DIA Jun 17, 2013 · N362NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13030263162Skin · dentedFWD FUSELAGE EXTERNAL SKIN SURFACE HAS TWO DENTS BETWEEN FR 10 TO 11, BETWEEN S23-24L. PERFORMED DETAILED VISUAL INSP, NO CRACKS NOTED. ACCOMPLISHED INTERNAL AND EXTERNAL HFEC INSPECTION IAW NTM 51-10-08, PT 6, NO DEFECTS. NO REPAIR ACTION REQUIRED IAW SRM Jun 17, 2013 · N362NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13030043162Seat Track · corrodedFWD CABIN FRAME 20-24 -Y765, SEAT TRACK CROWN HAS CORROSION. REMOVED CORROSION, CHECKED LIMITS; L=1.0" W=.04" D=.030" NO MINIMUM ALLOWABLE BECAUSE CORROSION IS ON THE CROWN IAW SRM 51-74-00. REMOVED AND INSTALLED NEW BEAM IAW SRM 51-42-11, SRM 51-44-11, TRM Jun 17, 2013 · N362NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13011283162Battery Pack · failedDURING SERVICE CHECK, ESPU FWD LT AND ESPU RT FAILED BATTERY TEST. REPLACED BATTERYS IAW AMM 33-51. OPS NORMAL.Mar 9, 2013 · N362NB · Airbus A319114 · Emergency LightingSDR DALA1108233162Connector · not seatedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT FORWARD LEFT FAILED EPSU EXIT LOAD TEST. MAINTENANCE RESEATED CONNECTOR UNDER FORWARD LEFT SLIDE COVER. FUNCTIONAL TEST WAS NORMAL AND A/C RELEASED FOR SERVICE. (2011-00079)Feb 3, 2011 · N362NB · Airbus A319114 · Light System WiringSDR NWAA082733162Cable · brokenRT OVERWING EMERGENCY EXIT ESCAPE SLIDE ACTUATING CABLE FOUND BROKEN. REPLACED RT OVERWING SLIDE EXIT DOOR FLEXIBLE CABLE ASSEMBLY, CHECKED GOOD. (A)Jun 14, 2008 · N362NB · Airbus A319114 · Escape Slide
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