N340NB

Service difficulty reports · 211

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 = 'N340NB' 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 DALA13043773140Lug · gougedFWD CARGO DOOR LOCK FITTING NR 2 AFT LUG GOUGED. BLENDED GOUGE IAW SRM 51-73-00. PERFORMED DVI IAW NTM 51-10-02-250-801. DAMAGE REMOVED AND FOUND TO BE IN LIMITS. TREATED AND PRIMED AREA IAW SRM 51-21-11. PAINTED AREA IAW SRM 51-75-12.Sep 7, 2013 · N340NB · Airbus A319114 · Cargo/Baggage DoorsSDR DALA13043763140Roller · gougedRIGHT AFT DOOR ROLLER STOP FITTING LOCATED ON MID FRAME 68 OTBD UPPER SURFACE HAS GOUGE. R & R ROLLER STOP FITTING IAW SRM 51-42-11. TOPCOATED FASTENERS IAW SRM 51-75-12 & DWG D53480122.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Main, StructureSDR DALA13043603140Floor Panel · damagedAFT CARGO BAY SLOPE PANEL 161FF HAS PREVIOUS REPAIR & DENTED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043593140Floor Panel · damagedAFT CARGO BAY SLOPE PANEL 151FE HAS MULTIPLE DENTS & CRACKED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043583140Floor Panel · damagedAFT CARGO BAY SLOPE PANEL 152UG HAS MULTIPLE DENTS & CRACKED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043573140Floor Panel · damagedAFT CARGO BAY SLOPE PANEL 151GE HAS CRACK AND DEBONDED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043563140Floor Panel · damagedAFT CARGO BAY SLOPE PANEL 162EF HAS 3 EA DENTS & DEBONDED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043553140Floor Panel · damagedAFT CARGO BAY FLOOR PANEL 151ZG HAS MULTIPLE DENTS, PUNCTURED, CRACKED & DEBONDED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043543140Floor Panel · damagedAFT CARGO BAY FLOOR PANEL 151CE HAS MULTIPLE DENTS AND EDGE CRACKED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043533140Floor Panel · damagedAFT CARGO BAY FLOOR PANEL 151PE HAS MULTIPLE DENTS AND EDGE CRACKED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043523140Floor Panel · damagedAFT CARGO BAY FLOOR PANEL 151VG HAS THREE PREVIOUS REPAIRS, MULTIPLE DENTS & DEBONDED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D25-40532.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043513140Floor Panel · damagedFWD CARGO BAY FLOOR PANEL 131AF HAS MULTIPLE DENTS, SIX PUNCTURES & ONE CRACK. FOUND OUT OF LIMITS IAW SRM 53-02-00, TABLE 105. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043503140Floor Panel · dentedFWD CARGO BAY SLOPE PANEL 131CF HAS MULTIPLE DENTS, CRACKED & DELAMINATED. FOUND OUT OF LIMITS IAW SRM 53-02 -00. FABRICATED NEW SLOPE PANEL IAW SRM 53-02-00, FIG 209.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043493140Floor Panel · dentedFWD CARGO BAY SLOPE PANEL 132EG HAS MULTIPLE DENTS AND DEBONDED. FOUND OUT OF LIMITS IAW SRM 53-02-00. FABRICATED NEW SLOPE PANEL IAW SRM 53-02-00, FIG 209.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043483140Floor Panel · dentedFWD CARGO BAY SLOPE PANEL 131DG HAS MULTIPLE DENTS, TWO PLACES OF CRACKED & DEBONDED. FOUND OUT OF LIMITS IAW SRM 53-02-00. FABRICATED NEW SLOPE PANEL 131DG IAW SRM 53-02-00, FIG 209.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043363140Floor Panel · debondedFWD CARGO BAY SLOPE PANEL 131EG HAS MULTIPLE DENTS AND DEBONDED. FOUND OUT OF LIMITS IAW SRM 53-02-00. FABRICATED NEW SLOPE PANEL IAW SRM 53-02-00 FIG 209.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043373140Blanking Plate · corrodedAFT UTILITY AREA AT R2 DOOR AFT CUT OUT AREA, BLANKING PLATE CORRODED. INSTALLED ON WC 2500-6602.Sep 6, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13043193140Stringer · corrodedAFT CARGO BAY BILGE AREA BETWEEN FRAMES 59-60, STRINGER 43L CORRODED.Sep 4, 2013 · N340NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA13043173140Floor Panel · puncturedCENTER CABIN FLOOR PANEL 252GF PUNCTURED "1.0 X 1.0" AND IS OUT OF LIMITS IAW SRM 53-02-00, FIG 102 SH 1. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D2540640 AND INSTALLED.Sep 4, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043163140Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241EF DELAMINATED OUT OF LIMITS IAW SRM53-02-00, FIG 102. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3D2540640.Sep 4, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13043153140Sill · corrodedAFT CARGO BAY DOOR SILL PLATE 152YG CORRODED. INSTALLED ON WC 2500-5919.Sep 3, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13043023140Sill · corrodedAFT RT PAX DOOR SILL BEAM, AT INBD FRAME 66 UPPER SURFACE FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 101. R & R SILL IAW SRM 51-42-11 & DWG D53480019.Sep 3, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13043013140Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FRAMES 66-68, Y-1292 UPPER SURFACE FLANGES & HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMIT IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW TRM 53-21-01.Aug 31, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13043003140Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FRAMES 65-66, Y1292 UPPER SURFACE FLANGE 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 TRM 53-21-01.Aug 31, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13042993140Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FRAMES 66-68 UPPER SURFACE FLANGE 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 TRM 53-21-01.Aug 31, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13042983140Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FRAME 68-69 UPPER FLANGE 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 TRM 53-21-01.Aug 31, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13042963140Fitting · corrodedAFT RT PAX DOOR FWD FR68 LOWER CUT-OUT CORNER FITTING HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. R & R CORNER FITTING, IAW SRM 51-42-11 & DWG D53480019.Aug 30, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13042953140Lug · chafedRT ELEVATOR, OTBD SERVO ACTUATOR FITTING, LOCKING LUG CHAFED. REMOVED DAMAGE IAW SRM 51-73-00. CHECKED LIMITS L=0.350" W=0.24" D=0.035" FOUND TO BE OUT OF LIMITS IAW SRM 55-26-00, FIG 104. R & R LOCKING LUG IAW SRM 55-26-47, FIG 201. FABRICATED LOCKING LUG Aug 30, 2013 · N340NB · Airbus A319114 · Elevator StructureSDR DALA13042943140Blanking Plate · corrodedAFT UTILITY AREA AT L2 DOOR AFT CUT-OUT AREA BLANKING PLATE CORRODED. INSTALLED NEW BLANKING PLATE ON WC 2500-6602.Aug 30, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13042933140Beam · corrodedAFT LT PAX DOOR SILL BEAM AT INBD FRAME 68 UPPER SURFACE HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. R & R DOOR SILL IAW SRM 51-42-11 & DWG D53480020.Aug 30, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13042923140Shear Plate · corrodedAFT UTILITY AREA LT SIDE S23L, BETWEEN FRAMES 69-70, SHEAR PLATE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO ESTABLISHED LIMITS IN SRM. R & R SHEAR PLATE IAW SRM 51-42-11 & DWG D53474180.Aug 30, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13042913140Shear Plate · corrodedAFT UTILITY AREA RT SIDE S23R BETWEEN FRAMES 69-70 SHEAR PLATE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO ESTABLISHED LIMITS IN SRM. R & R SHEAR PLATE IAW SRM 51-42-11 & DWG D53474180.Aug 30, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13042903140Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 241MF DELAMINATED AT UPPER SURFACE L=8.5 OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SHEET 1. CENTER CABIN FLOOR PANEL FABRICATED IAW SRM 53-02-00 FIG 209, DWG 3D25-40640.Aug 30, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042353140Floor Panel · damagedCENTER CABIN FLOOR PANEL 242KF UPPER SKIN DELAMINATED, OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 1. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Aug 29, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042343140Floor Panel · damagedMAIN CABIN FLOOR PANEL 221LF MULTIPLE DAMAGED INSERTS OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 1. MAIN CABIN FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Aug 29, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042333140Floor Panel · damagedMAIN CABIN FLOOR PANEL 261PF OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 1. MAIN CABIN FLOOR PANEL 261PF FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Aug 29, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042313140Floor Panel · damagedCENTER CABIN FLOOR PANEL 242LF DELAMINATED AT UPPER SURFACE OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH.1. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042303140Floor Panel · damagedCOCKPIT FLOOR PANEL 211GF OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 1 L=8.0, W=3.0. FABRICATED FLOOR PANEL 211GF IAW SRM 53-02-00, FIG. 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042293140Floor Panel · damagedMAIN CABIN FLOOR PANEL 221DF OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 1, L=9.2 X 5.0". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042283140Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 251RF DELAMINATED AT UPPER SURFACE OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042273140Floor Panel · damagedMAIN CABIN FLOOR PANEL 231WG OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 1, L=8.0, W=2.0. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042263140Floor Panel · damagedMAIN CARGO FLOOR PANEL 262HG OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 1 L=9.4 X 4.0". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042253140Floor Panel · damagedMAIN CABIN FLOOR PANEL 261HG, OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 1, L=8.3, W=2.0. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042243140Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 241LF DELAMINATED AT UPPER SURFACE OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH.1. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042233140Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 242GF UPPER SKIN DELAMINATED L=8.5, OUT LIMITS IAW SRM 53-02-00, FIG 102, SH 1. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042223140Floor Panel · damagedMAIN CABIN FLOOR PANEL 221PF OUT OF LIMITS IAW SRM 53-02-00, FIG 102, SH 1, L=8.0, W=3.0. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042213140Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 241JF UPPER SKIN DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102 SH 1. REMOVED AND REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13042203140Fitting · corrodedAFT LT PASSENGER/CREW DOOR LOWER AFT CUT-OUT CORNER FITTING HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. DIMENSIONS: L=1.0", W=0.800", D=0.015". NO ESTABLISHED LIMITS IN SRM. REMOVED DAMAGE CORNER FITTING AND INSTALLED ON NON-ROUTINE CARD.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Main, StructureSDR DALA13042193140Floor Support · corrodedFWD UTILITY AREA FLOOR SUPPORT BETWEEN FRAMES 12-16, Y-81 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW TRM 53-21-01.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13041983140Sill · corrodedR1 DOOR FRAME SILL CORRODED AT SCREW HOLES. REMOVED CORROSION IAW SRM 51-74-00. R & R SILL IAW SRM 51-42-11, DWG D53112198.Aug 28, 2013 · N340NB · Airbus A319114 · Fuselage Miscellaneous Structure
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