N360NB

Service difficulty reports · 179

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 = 'N360NB' 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 DALA13073183160Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 262FF SKIN DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. REPLACED FLOOR PANEL IAW SRM 51-72-11.Dec 27, 2013 · N360NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13073173160Floor Panel · damagedMAIN CABIN FLOOR PANEL 222FF HAS EDGE DAMAGE. REPLACED FLOOR PANEL IAW SRM 51-72-11.Dec 27, 2013 · N360NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13073163160Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT -Y254 BETWEEN FRAMES 16-20 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15, FIG. 107. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.Dec 27, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13072123160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y1292 BETWEEN FRAMES 64-66 HARD POINT HOLES AND UPPER 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 SRM 51-42-11 AND TRM 53-21-01.Dec 26, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13072113160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y1292 BETWEEN FRAMES 68-69 UPPER 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 SRM 51-42-11 AND TRM 53-21-01.Dec 26, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14003713160Skin · chafedL2 DOOR, UPPER FWD CORNER OF THE FUSELAGE DOOR FRAME, EXTERNAL SURFACE, CHAFED. BLENDED AREA IAW SRM 51-73-00. FOUND WITHIN LIMIT IAW SRM 53-41-11, FIG 106.Dec 24, 2013 · N360NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13072093160Beam · corrodedLEFT AFT PASSENGER DOOR SILL BEAM UPPER FLANGE AT AFT FRAME 66 INBD GIRT BAR FITTING HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, L=1.5", W=1", D=0.080", FOUND OUTPUT OF LIMIT IAW SRM 53-41-14, FIG 101. R & R DOOR SILL IAW SRM 51-42-11 AND DWG DDec 24, 2013 · N360NB · Airbus A319114 · Fuselage Main, StructureSDR DALA13071623160Seat Track · corrodedFORWARD CABIN SEAT TRACK -Y765 BETWEEN FRAMES 20-22 CROWN CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 101. R & R SEAT TRACK IAW SRM 51-42-11 & TRM 53-21-01.Dec 23, 2013 · N360NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13071613160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAMES 64- 66 UPPER FLANGE AND HARD POINT HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, PAR 3D. R & R FLOOR SUPPORT IAW TRM 53-21-00 & SRM 51-42-11 AND SRDec 22, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13071603160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAMES 68-69 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, P3.D. R & R FLOOR SUPPORT IAW TRM 53-21-00 & SRM 51-42-11 AND SRM 51-44-11.Dec 22, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13071593160Frame · corrodedUPON REMOVAL OF RT SIDE SHEAR PLATE BETWEEN FRAMES 69-70 FOUND SUPPORT FRAME CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE LIMITS ESTABLISH ON SRM. R & R SUPPORT FRAME IAW SRM 51-42-11 AND DWG D53474180.Dec 22, 2013 · N360NB · Airbus A319114 · Fuselage Main, FrameSDR DALA13071583160Shear Plate · corrodedAFT UTILITY AREA RT SIDE BETWEEN FRAMES 69-70, S23R SHEAR PLATE CORRODED. REMOVED CORROSION IAW SRM 51-74-00, CHECK LIMITS DIMENSION L=5.8", W=2.7", D=.039". NO ESTABLISH LIMITS FOUND IN SRM, R & R SHEAR PLATE IAW SRM 51-42-11 AND DWG D53474180.Dec 22, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13071573160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAMES 66-68 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 51-41-15 PAR. 3D. R & R FLOOR SUPPORT IAW TRM 53-21-00 & SRM 51-42-11 AND SRM 51-44-11.Dec 22, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13071563160Sill · corrodedLEFT AFT PASSENGER/CREW DOOR SILL BEAM AT FWD FR68 CORNER FITTING HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, CHECKED LIMITS DIMENSION L=1", W=.500", D=.039". NO LIMIT ESTABLISHED FOR SRM, LOCATED AND DRILLED NEW CORNERS FITTING IAW SRM 51-44-11. INSDec 22, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13071553160Floor Support · corrodedFWD UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAME 18 - 20 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15, FIG 104. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Dec 21, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13071543160Floor Support · corrodedFWD UTILITY AREA FLOOR SUPPORT, Y503.2 BETWEEN FRAMES 12-16 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-11-14, FIG 105. R & R FLOOR SUPPORT IAW TRM 53-21-01.Dec 21, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13071533160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y765 AT FR 68 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.Dec 20, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13071523160Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT Y254 BETWEEN FRAMES 16-20 UPPER FLANGE HAS SCRIBE LINE AND 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 & TRM 53-21-01.Dec 20, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13070753160Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM, Y1292 AT FRAME 68 UPPER INBD SPLICE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REMOVED AND INSTALLED SPLICE.Dec 19, 2013 · N360NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA13070743160Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM Y1292 AT FRAME 68 UPPER INBD SPLICE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REMOVED & INSTALLED.Dec 19, 2013 · N360NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA13070733160Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT, Y189 BETWEEN FRAMES 20-22, UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-17. REMOVED FLOOR SUPPORT IAW SRM 51-42-11 & INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11 ANDDec 19, 2013 · N360NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13070723160Lug · gougedRT WING SLAT 4 INBD UPPER LUG HAS GOUGED. REMOVED DAMAGED IAW SRM 51-73-00. CHECKED REMAINING LUG THICKNESS IS 0.510" FOUND TO BE WITHIN LIMITS IAW SRM 57-40-00, FIG. 111. HFEC IAW NTM 51-10-08. NO DEFECTS NOTED. FOLLOW-UP INSPECTION IAW SRI 57-40-00-1-004Dec 17, 2013 · N360NB · Airbus A319114 · Leading Edge DevicesSDR DALA13072803160Floor Panel · damagedMAIN CABIN FLOOR PANEL 251LGIS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3025-40640.Dec 12, 2013 · N360NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13063453160Wire · brokenEMERGENCY LIGHT AT 19ABC INOPERATIVE. REPAIRED BROKEN WIRE IAW ESPM 20-00. CHECKED OK.Nov 20, 2013 · N360NB · Airbus A319114 · Light System WiringSDR DALA1164433160Wire Harness · defectiveSEAT 8C ONE RED EMERGENCY PATH LIGHT INOP. REPLACED LIGHT HARNESS AND TESTS OK.Nov 22, 2011 · N360NB · Airbus A319114 · Light System WiringSDR DALA1135043160Light · failedDURING ROUTINE CHECK, FOUND THE RIGHT AFT SLIDE EMERGENCY LIGHT SYSTEM FAILED. MAINTENANCE REPLACED SLIDE RAFT EVAC AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.May 17, 2011 · N360NB · Airbus A319114 · Emergency LightingSDR DALA1135033160Power Supply · no testDURING A NON ROUTINE CHECK, FOUND THE EPSU AT 13 WL AFT FAILED SELF TEST. MAINTENANCE REPLACED EPSU AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.May 17, 2011 · N360NB · Airbus A319114 · Emergency LightingSDR DALA1134003160Power Supply · inoperativeDURING A NON ROUTINE CHECK, EPSU INDICATED FAULT AND SUBSEQUENT FAILURE OF SEVERAL EMERGENCY PATH LIGHT. MAINTENANCE REPLACED THE EPSU AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.May 14, 2011 · N360NB · Airbus A319114 · Emergency LightingSDR NWAA082523160Wire · damagedDURING LINE CHECK DISCOVERED ROW 1, 2, 5, 6 EMERGENCY EGRESS LIGHTS INOP. REPAIRED 2 WIRES BELOW SEAT 1 & 2 REPLACED EPSU (10WL), CHECKS NORMAL. (A)Jun 5, 2008 · N360NB · Airbus A319114 · Light System Wiring
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