N341NB

Service difficulty reports · 213

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 = 'N341NB' 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 DALA13048683141Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT +Y1292 BETWEEN FRAMES 65-66 UPPER FLANGE & HARD POINT HOLES HAS CORROSION. BLENDED AREA IAW SRM 51-74-00 AND FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED & DRILLED NEW FLOOR SUPPORTSep 29, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048673141Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAMES 64 - 66 UPPER FLANGE HAS CORROSION. BLENDED AREAS IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED FLOOR SUPPORT IAW TRM 53-21-01.Sep 29, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048663141Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAMES 64 - 66 UPPER FLANGE HAS CORROSION. BLENDED AREAS IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Sep 29, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048653141Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292, BETWEEN FRAMES 66 - 68 UPPER FLANGE HAS CORROSION. BLENDED AREAS IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED & DRILLED NEW SUPPORT & NEW SPLICES IAW SRMSep 29, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048643141Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAMES 68 - 69 UPPER FLANGE HAS CORROSION. BLENDED AREAS IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED & DRILLED NEW FLOOR SUPPORT IAW SRM 51-44-11.Sep 29, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048753141Bearing · wornRIGHT WING INBD FLAP TRUNNION SPHERICAL BEARING HAS PLAY. REPLACED WITH NEW PEDULUM ASSY WITH NEW SPHERICAL BEARING ON RT WING INBD FLAP TRUNION IAW AMM 27-54-46-400-003-A. REMOVED AND INSTALLED NR 1 FLAP TRACK BEAM ASSY IAW AMM 57-51-33-400-001-A. REMOVED Sep 28, 2013 · N341NB · Airbus A319114 · Trailing Edge FlapsSDR DALA13048633141Sill · corrodedLEFT AFT PASSENGER DOOR SILL AT FRAME 68 GIRT BAR FITTING HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-13, FIG 1 (SHT 3) DETAIL II. R & R DOOR SILL IAW SRM 51-42-11 & DWG D53480020.Sep 28, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048623141Support Frame · corrodedAFT UTILITY AREA RT SIDE BETWEEN FRAMES 69 - 70 S23R FRAME SUPPORT ATTACHED TO SHEAR PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. R & R SUPPORT FRAME IAW SRM 51-42-11 & DWG D53474180.Sep 28, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048613141Sill · corrodedRT AFT PASSENGER DOOR SILL INBD FRAME 66 UPPER SURFACE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. R & R SILL IAW SRM 51-42-11 & SRM 51-44-11 AND DWG D53480019.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048603141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242BF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 2. FABRICATED NEW FLOOR PANEL 242BF IAW SRM 53-02-00 & DWG NW3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048593141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231CF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. MAIN CABIN FLOOR PANEL FABRICATED IAW SRM 53-02-00 AND DWG 3D25-40640. RETAINSep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048583141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251UF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. MAIN CABIN FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048573141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232XG DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 2. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048563141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231WG DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 2. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG NW3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048553141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221AF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00 & DWG NW3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048543141Floor Panel · delaminatedCOCKPIT FLOOR PANEL N211GF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00 FIG 102, SH 2. FABRICATED COCKPIT FLOOR PANEL 211GF IAW SRM 53-02-00, FIG 9 & DWG NW3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048533141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231ZG DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 2. FABRICATED NEW FLOOR PANEL 231ZG IAW SRM 53-02-00, FIG 9 & DWG NW3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048523141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 221DF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048513141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 232AH DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 2. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG NW3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048503141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231FF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 2. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG NW3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048493141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 252GF UPPER SURFACE DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-02-00, FIG 102 SH.2. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048483141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242CF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 2. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048473141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 231XG DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40640.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048463141Fitting · corrodedLEFT AFT PASSENGER DOOR LOWER CUT-OUT SHAPE SEAL AFT CORNER FITTING HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. REMOVED CORNER FITTING IAW SRM 51-42-11 & INSTALLED ON NR 3 30/260.Sep 27, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048303141Skin · gougedLWR FUSELAGE SKIN HAS GOUGE FROM PANEL FASTENER 1 IN. RT OF STR 44 AND 2 IN. AFT OF FR34. BLENDED AREA IAW SRM 51-73-00. FOUND TO BE WITHIN LIMITS IAW SRM 53-21-11, DIAGRAM 105, SHEET 1. TSep 26, 2013 · N341NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13048283141Fitting · corrodedRIGHT AFT PASSENGER DOOR CUTOUT AT FR 68 SHAPE SEAL AFT CORNER FITTING HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. L=1" W=.8" D=.015" NO ESTABLISHED LIMITS ON SRM. LOCATED AND DRILLED NEW CORNER FITTING, PN D5348004220 IAW SRM 51-44-11. TREATED AND PRIMSep 26, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048273141Shear Plate · corrodedAFT UTILITY AREA RT SIDE BETWEEN FRAMES 69-70, S23R, SHEAR PLATE CORRODED. R & R SHEAR PLATE IAW SRM 51-42-11 AND SRM 51-44-11 AND DWG D53474180.Sep 26, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048293141Skin · dentedDENT IN FUSELAGE SKIN, BETWEEN FRAMES 20-21, S25-26R. FOUND WITHIN LIMITS IAW SRM 53-11-11, DIAGRAM 102. PERFORMED DVI IAW SRM 53-11-11, DIA 102 NO ADDITIONAL DAMAGE FOUND. HFEC INTERNAL AND EXTERNAL AT DENT IAW NTM 51-10-08, NO CRACKS.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13048253141Floor Panel · corrodedFORWARD UTILITY AREA FLOOR PANEL 222FF, CORRODED. REPLACED FLOOR PANEL IAW SRM 51-72-11.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13048243141Plate · corrodedAFT UTILITY AREA AT L2 DOOR FWD SIDE PLATE ASSY CORRODED. REPLACED PLATE ASSY IAW SRM 51-72-11.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13048233141Floor Panel · corrodedAFT UTILITY AREA FLOOR PANEL 262FF CORRODED. NO ALLOWABLE LIMIT ESTABLISH ON SRM. REPLACED FLOOR PANEL IAW SRM 51-72-11.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13047753141Fitting · corrodedFORWARD RT PASSENGER DOOR ENTRANCE LOWER FRAME CENTER SHAPE SEAL FITTING AROUND NUTPLATE HOLES HAS CORROSION. NO ESTABLISHED LIMIT ON SRM. R & R FITTING IAW SRM 51-42-11 & DWG D53112198.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13047743141Floor Panel · corrodedAFT UTILITY AREA FLOOR PANEL 261FF IS CORRODED. NO ALLOWABLE LIMIT ESTABLISH ON SRM. REPLACED FLOOR PANEL IAW SRM 51-72-11.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13047733141Sill · corrodedL1 FOOR ENTRY WAY, CENTER SHAPE SILL CORRODED AT SCREW HOLES. REMOVED CORROSION IAW SRM 51-73-00. NO ESTABLISHED LIMITS IAW SRM 53-00-15. R & R SILL IAW SRM 51-42-11 & DWG D53112198.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13047723141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251PF IS DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 9 AND DWG NW3D25-40640.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13047713141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251SF IS DELAMINATED OF LIMITS IAW SRM 53-02-00, FIG 102. MAIN CABIN FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 9 AND DWG NW3D25-40640.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13047703141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241BF IS DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. MAIN CABIN FLOOR PANEL FABRICATED IAW DWG 3D25-40640.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13047693141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241JF DELAMINATED ON UPPER SURFACE AND IS OUT OF LIMITS IAW SRM 53-02-00, FIG 102 SH2. MAIN CABIN FLOOR PANEL FABRICATED IAW DWG 3D25-40640.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13047683141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251NF DELAMINATED AND IS OUT OF LIMITS IAW SRM 53-02-00, FIG 102. MAIN CABIN FLOOR PANEL FABRICATED IAW SRM 53-02-00 AND DWG NW3D25-40640.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13047673141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 252GG DELAMINATED AND IS OUT OF LIMITS IAW SRM 53-02-00, FIG 102. MAIN CABIN FLOOR PANEL FABRICATED IAW SRM 53-02-00 AND DWG NW3D25-40640.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13047663141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 247MF UPPER SURFACE DELAMINATED & OUT OF LIMITS IAW SRM 53-02-00, FIG 102. MAIN CABIN FLOOR PANEL FABRICATED IAW SRM 53-02-00 AND DWG NW3D25-40640.303913.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13047653141Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 252MF DELAMINATED & OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00 AND DWG NW3D25-40640.Sep 25, 2013 · N341NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13046933141Shear Plate · corrodedAFT UTILITY AREA LT SIDE BETWEEN FRAMES 69 - 70, S23L SHEAR PLATE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM. R & R SHEAR PLATE, IAW DWG 53474180 & SRM 51-42-11.Sep 24, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13046783141Skin · dentedDENT IN FUSELAGE SKIN, BETWEEN FRAMES 9-10, 17 INCHES BELOW THE F/O PITOT TUBE. FOUND WITHIN LIMITS IAW SRM 53-11-11, DIAGRAM 102. PERFORMED DVI IAW SRM 53-11-11 DIA 102. NO ADDITIONAL DAMAGE FOUND. HFEC INTERNAL AND EXTERNAL SURFACE IAW NTM 51-10-08. NO Sep 23, 2013 · N341NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13046773141Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT Y1292, BETWEEN FRAMES 16-21, UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15, FIG 102. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Sep 23, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13046763141Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT, Y765 BETWEEN FRAMES 66-70, UPPER FLANGE CORRODED. 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 DWG D53472000.Sep 23, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13046753141Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y765 BETWEEN FRAMES 65 - 66, UPPER FLANGE CORRODED. 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 DWG D53472818.Sep 23, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13046743141Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y765, BETWEEN FRAMES 66-70, UPPER FLANGE AND HARD POINT HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, FIG 1, PAGE 3. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53472000.Sep 23, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13046733141Web · corrodedFWD CABIN RT SIDE STRINGER 23R BETWEEN FRAMES 20 - 21, UPPER SURFACE WEB HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. FOUND OUT OF LIMITS. R & R WEB IAW SRM 51-42-11 AND DWG D53112783.Sep 21, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13046723141Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT Y503.2 BETWEEN FRAMES 12 - 16, UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15, FIG 103. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Sep 20, 2013 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
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