N336NB

Service difficulty reports · 224

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 = 'N336NB' 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 DALA13026773136Seat Track · corrodedFWD CABIN RT SIDE, BETWEEN FR 20-FR 21,Y-765 SEAT TRACK HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, FIG 101. R & R SEAT TRACK IAW SRM 51-42-11 AND TRM 53-21-01.Jun 1, 2013 · N336NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13026763136Stop Fitting · chafedLEFT AFT PASSENGER DOOR MID FRAME 68, ROLLER DOOR STOP FITTING UPPER SURFACE HAS CHAFED MARK. R & R DOOR STOP ROLLER FITTING AT FRME 68 OF LT AFT PAX DOOR IAW SRM 51-42-11 DUE NO SPECIFIED LIMITS L=1.5" W=3/8" D=0.030". TORQUE WRENCH USED TR9818. RETAIN FORMay 31, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13027573136Stringer · corrodedAFT CARGO BAY FR 62, S41R CORRODED. NO ALLOWABLE LIMITS ESTABLISHED IAW SRM 53-00-13, PG 101. ACCOMPLISHED REPAIR IAW SRM 53-00-13, FIG 201.May 30, 2013 · N336NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA13026253136Floor Panel · delaminatedFWD CABIN UTILITY FLOOR PANEL 222EF, DELAMINATED L=6.0" X W=1.75". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 29, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13026243136Beam · damagedRT AFT PASSENGER/CREW DOOR SILL BEAM AT FR 66 INBD UPPER SURFACE FLANGE REPAIR REQUIRES FOLLOW ON INSP IAW SRI. RT AFT PASSENGER/CREW DOOR SILL BEAM AT FR 66 INBD FLANGE REPAIR ACCOMPLISHED ON NR 260/55. FOLLOW-ON INSP REQUIRED AT 92731 FC AFTER REPAIR EMBODMay 28, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13026233136Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 231LF HAS SCRATCH AND DELAMINATED. L=18.0" X W=0.25". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 28, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13026223136Floor Panel · delaminatedFWD CABIN UTILITY FLOOR PANEL 221DF DELAMINATED L=6.0" X W=3.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 28, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13026213136Floor Panel · delaminatedFWD CABIN FLOOR PANEL 231KF IS DELAMINATED 3" X 4". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 28, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025833136Blanking Plate · crackedAFT CABIN L2 DOOR FWD BLANKING PLATE CRACKED. REPLACED BLANKING PLATE.May 24, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025823136Floor Panel · corrodedFWD CABIN FLOOR PANEL 221FF CORRODED. REPLACED FLOOR PANEL.May 24, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025813136Sill · corrodedLT AFT PASSENGER/CREW DOOR SILL BEAM AT FR68 GIRT BAR FITTING HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=.950" W=.800" D=.050" MAXIMUM HOLES OVERSIZED .787" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-13, DETAIL 2, FIG 1, SHT 3. R May 24, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025803136Floor Support · corrodedFWD CABIN LT SIDE, AT FR16 +Y765 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.059 W=1.029 D=.033 OUT OF LIMITS IAW SRM 53-11-15, FIG 101. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53112812.May 24, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025793136Fitting · corrodedL2 DOOR SILL FWD AND AFT CORNER FITTINGS CORRODED.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025783136Floor Support · corrodedAFT CABIN UTILITY AREA FLOORBEAM BETWEEN FR64-FR66, Y1292 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 CHECKED LIMITS L=2.0" W=1.0" D=0.050" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOORBEAM IAW TRM 53-21-01.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025773136Floor Support · corrodedAFT CABIN UTILITY AREA FLOORBEAM BETWEEN FR68-FR69 Y1292 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 CHECKED LIMITS L=1.50" W=1.20" D=0.30" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. FLOORBEAM IAW TRM 53-21-01. RETAIN FOR RECORDS.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025763136Floor Support · corrodedAFT CABIN UTILITY AREA FLOORBEAM BETWEEN FR66-FR68 Y1292 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOORBEAM IAW TRM 53-21-01.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025753136Nut Plate · corrodedRT FWD PASSENGER DOOR CUT OUT LOWER MID SHAPE SILL FITTING NUT PLATE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO ESTABLISHED LIMITS FOUND IN SRM. R & R MID SHAPE SILL IAW SRM 51-42-11 AND DWG D53112109.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025743136Floor Panel · corrodedFWD CABIN FLOOR PANEL 222FF HAS CORROSION AND DELAMINATED, REPLACED FLOOR PANEL AND INSTALLED.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025733136Fitting · corrodedL2 DOOR SILL FWD AND AFT CORNER FITTINGS CORRODED. REMOVED CORROSION ON LOWER CORNER FITTINGS AT FR66 & FR68 IAW SRM 51-74-00. NO ESTABLISHED LIMITS IN SRM. INSTALLED CORNER FITTINGS.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025723136Fitting · corrodedL2 DOOR SILL FWD AND AFT CORNER FITTINGS, CORRODED. REMOVED CORROSION ON LOWER CORNER FITTINGS AT FR66 & FR68 IAW SRM 51-74-00. NO ESTABLISHED LIMITS IN SRM. INSTALLED CORNER FITTINGS.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025713136Nut Plate · corrodedLEFT FWD PASSENGER/CREW DOOR CUT OUT LOWER MID SHAPE SILL FITTING NUT PLATE HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, NO ESTABLISHED LIMITS IN SRM. R & R MID SHAPE SILL FITTING IAW SRM 51-42-11 & DWG D53112109.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13025703136Floor Panel · delaminatedCENTER CABIN FLOOR PANEL 241EF DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025693136Floor Panel · crackedCENTER CABIN FLOOR PANEL 242LF CRACKED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025683136Floor Panel · damagedAFT CABIN UTILITY FLOOR PANEL 261BG HAS DAMAGE INSERT HOLE AND DEFORMED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025673136Floor Panel · delaminatedFWD CABIN FLOOR PANEL 232LF IS DELAMINATED DIM. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025663136Floor Panel · damagedFWD CABIN UTILITY FLOOR PANEL 221EF BOTTOM SURFACE HAS DAMAGED HONEYCOMB. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025653136Floor Panel · corrodedAFT CABIN UTILITY FLOOR PANEL 261PF HAS 4 EA CORRODED INSERTS AND DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025643136Floor Panel · debondedAFT CABIN UTILITY FLOOR PANEL 262BG DEBONDED AROUND INSERT HOLE. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025633136Floor Panel · damagedCENTER CABIN FLOOR PANEL 251FF CORNER EDGE HONEYCOMB DAMAGED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025623136Floor Panel · dentedFWD CARGO BAY FLOOR PANEL 131DG HAS MULTIPLE DENTS, CRACKS AND DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40632.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025073136Floor Panel · delaminatedAFT CABIN FLOOR PANEL 251LF IS DELAMINATED, DIM. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025063136Floor Panel · damagedFWD CARGO FLOOR PANEL 131EG HAS MULTIPLE DENTS, CRACKS AND DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40632.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025053136Floor Panel · damagedFWD CARGO FLOOR PANEL 132EG HAS MULTIPLE DENTS, DEEP SCRATCHES & DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40632.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025043136Floor Panel · damagedFWD CARGO FLOOR PANEL 132DG HAS MULTIPLE DENTS AND DELAMINATED. L=1.50" X W=1.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40632.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025033136Floor Panel · damagedFWD CARGO FLOOR PANEL 131BF HAS MULTIPLE DENTS & CRACKS. L=2.5" X W=0.75". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40632.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025023136Floor Panel · damagedFWD CARGO COMPT FLOOR PANEL 131CG HAS MULTIPLE DENTS AND CRACKS. L=2.0" W=0.50". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025013136Floor Panel · damagedAFT CABIN FLOOR PANEL 262EF HAS DAMAGED HOLE AND DELAMINATED 6" X 2". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13025003136Floor Panel · delaminatedAFT CABIN FLOOR PANEL 261EF DELAMINATED 8" X 6". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13024993136Floor Panel · delaminatedAFT CABIN FLOOR PANEL 261DF DELAMINATED 10" X 4". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40640.May 23, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13024983136Blanking Plate · corrodedR2 DOOR FWD BLANKING PLATE CORRODED 4 X 5". NO ESTABLISHED LIMITS. R & R BLANKING PLATE IAW SRM 51-42-11 TO BE INSTALLED ON WC 2500-6602.May 21, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13024973136Floor Panel · corrodedAFT CABIN FLOOR PANEL 262FF CORRODED AND TORN EDGE. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REPLACED FLOOR PANEL.May 21, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13024963136Floor Panel · corrodedAFT CABIN FLOOR PANEL 261FF HAS CORROSION AT SEVERAL AREAS. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REPLACED FLOOR PANEL.May 21, 2013 · N336NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13024953136Skin · dentedFWD FUSELAGE LT SIDE AT FR6 9" ABOVE S28L EXTERNAL SKIN DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11. CUT OUT SKIN. FABRICATED DOUBLER AND FILLER, IAW SRM 53-11-11, PAR 5.I, FIG 212. INSTALLED DOUBLER AND FILLER AND SEALED EDGES OF DOUBLER IAW SRM 53May 21, 2013 · N336NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13024553136Blanking Plate · corrodedR2 DOOR AFT BLANKING PLATE CORRODED 4" X 4" NO ESTABLISHED LIMITS. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DIMENSIONS L=4.0", W=4.0", D=0.006". NO ESTABLISHED LIMITS IN SRM 53-02-00. REPLACED AND TO BE INSTALLED ON WO 2500-6602.May 20, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13024313136Floor Support · corrodedFLOOR SUPPORT RT SIDE BETWEEN FR69-70, STRG 23R ATTACHED TO SHEAR PLATE UPPER AND LOWER SURFACE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS IN SRM. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53474180.May 20, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13024303136Floor Support · corrodedFLOOR SUPPORT LT SIDE BETWEEN FR69-70, STRG 23L ATTACHED TO SHEAR PLATE UPPER AND LOWER SURFACE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS IN SRM. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53474180.May 20, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13024293136Floor Support · corrodedFWD CABIN LT SIDE BETWEEN FR16 TO 18 +Y 1292, FLOOR SUPPORT HAS CORROSION. 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.May 20, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13024283136Floor Support · corrodedFWD CABIN LT SIDE, BETWEEN FR13 -16 +Y503, FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, FOUND OUT OF LIMITS IAW SRM 53-11-11, FIG 103. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND 51-44-11 AND TRM 53-21-01.May 19, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13024223136Floor Support · corrodedFWD CABIN LT SIDE, BETWEEN FR13 -16 +Y503, FLOOR SUPPORT HAS CORROSION.May 19, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13024213136Floor Support · corrodedAFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR66 -FR69, Y-765 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUNE OUT OF LIMITS IAW SRM 53-11-14. REMOVED DAMAGED FLOOR SUPPORT AND INSTALLED NEW IAW SRM 51-42-11 AND TRIM 53-21-01.May 19, 2013 · N336NB · Airbus A319114 · Fuselage Miscellaneous Structure
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