N301NB

Service difficulty reports · 169

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 = 'N301NB' 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 DALA1021113101Floorboard · dentedFT CARGO COMPARTMENT FLOORBOARD 151CE HAS DENTS. FABRICATED NEW PANEL ON STAM TRAVELER T10/848916. 3D25-40532.Sep 2, 2010 · N301NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1021103101Floor Panel · dentedFWD CARGO FLOOR PANEL NR 131AF HAVE MULTIPLE DENTS. FABRICATED NEW PANEL ON STAM TRAVELER T10/848915 IAW DWG 3D25-40532.Sep 2, 2010 · N301NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1021093101Floor Panel · dentedAFT CARGO COMPARTMENT FLOOR PANEL NR 161NF HAS SEVERAL DENTS. RII: N FABRICATED NEW PANEL ON STAM TRAVELER T10/848970 IAW DWG 3D25-40532.Sep 2, 2010 · N301NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1020963101Frame · corrodedFWD CARGO COMP FR, BETWEEN S-42R & S-43R, HAS CORROSION ON FRAME ANGLE & RIVETS. RII: N, REMOVED 2EA FASTENERS FROM FR 28ST42R & 43R IAW SRM 51-42-11, REMOVED FRAME ANGLE AT FR27, STR 42R, STR43R IAW SRM 51-42-11, FABRICATED NEW CLEAT, LOCATED AND DRILLED ANGAug 31, 2010 · N301NB · Airbus A319114 · Fuselage Main, FrameSDR DALA1020943101Seat Track · corrodedAFT CABIN UTILITY AREA FR66 SEAT TRACK Y+1292 HAS CORROSION. CHECKED LIMITS AT BLENDED OUT AREA, DIMENSIONS L=1.740" W=1.360" D=0.070" ORIG MAT THICKNESS 0.157 FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. LOCATED & DRILLED IAW SRM 51-44-11. INSTALLED SEATAug 30, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020933101Floor Support · corrodedAFT CABIN UTILITY AREA BETWEEN FR68 & FR69 FLOOR SUPPORT Y+1292 HAS CORROSION. CHECKED LIMITS AT BLENDED OUT AREA, DIMENSIONS L=1.500" W=1.300" D=0.075" ORIG MAT THICKNESS 0.157" FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15 FIG 1. LOCATED AND DRILLED FLOOR SUPPOAug 30, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1020923101Floor Support · corrodedAFT CABIN UTILITY AREA BETWEEN FR66 & FR68 FLOOR SUPPORT Y+1292 HAS CORROSION. CHECKED LIMITS AT BLENDED OUT AREA, DIMENSIONS L=2.100" W=1.100" D=0.055" ORIG MAT THICKNESS 0.157 FOUND TO BE OUT OF LIMITS IAW SRM TRM 53-41-15 FIG 1. REMOVED, LOCATED, AND DRILLEAug 30, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1020953102Seat Track · corrodedFWD CABIN FLOOR DUMMY RAIL RT Y-189 CORRODED AT FR20. RII N: BLENDED CORROSION ON DUMMY RAIL RT Y-189 ATFR20 DIM. L=2.0"W=1.5" D=.030" FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. INSTALLED NEW RAIL IAW SRM 51-42-11. PAINTED FASTENERS IAW SRM 51-75-12.Aug 29, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020913101Seat Track · corrodedFWD CABIN, FR16 TO FR20, SEAT TRACK -Y254 CORRODED AT 2 AREAS. BLENDED OUT CORROSION AREA IAW SRM 51-74-00 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15. REMOVED DAMAGED SEAT TRACK & BRACKETS (12) IAW SRM 51-42-11. LOCATED, DRILLED, AND INSTALLED NEW BEAM, BRAAug 29, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020893101Floor Support · corrodedAFT CABIN UTILITY AREA BETWEEN FR 66 & FR 70 FLOOR SUPPORT Y-765 HAS CORROSION. BLENDED OUT CORRODED AREA IAW SRM 51-74-00 DIMENSION L=1.900" W=1.020" D=.065" MAX ALLOWEDD=.027 ORIGINAL MATL.THICKNESS .157 FOUND TO BE OUT OF LIMITS IAW SRM TRM 53-41-15 FIG I. Aug 28, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1020883101Seat Track · corrodedFWD CABIN, FR20 DUMMY RAIL AT -Y189 CORRODED THRU T-CHORD OF SEAT TRACK. REMOVED DUMMY RAIL AT FR20 Y-189 IAW SRM 51-42-11 REMOVED CORROSION IAW SRM 51-74-00 BLENDED THE AREA L=2" W=1.5" D=.015 FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15 INSTALLED NEW FWD CABINAug 28, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1020453101Floor Support · corrodedDURING M-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS +Y765 BETWEEN FR 66 & FR 69. REPAIRED IAW SRM 51-42-11, 51-44-11.Aug 25, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1020443101Seat Track · corrodedDURING M-CHECK, FOUND CORROSION ON SEAT TRACK AT BS +Y765 BETWEEN FR 65 & FR 66. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.Aug 25, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1019913101Seat Track · corrodedDURING M-CHECK, FOUND CORROSION ON SEAT TRACK MOUNT HOLE AT +Y765 FR16. REPAIRED IAW SRM 51-42-11.Aug 21, 2010 · N301NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1017893101Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND L/R OVERWING EMERGENCY LIGHTS INOPERATIVE. MX REPLACED EPSU AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Jul 31, 2010 · N301NB · Airbus A319114 · Emergency LightingSDR NWAA093493101Controller · malfunctionedCABIN ALTITUDE HAD SLOW CONTINUOUS CLIMB, REACHING 9820FT AT FL290. BEGAN IMMEDIATE DESCENT TO 10000FT. MASKS DID NOT DROP. RETURNED TO DTW, LANDING EVENTFULLY. REPLACED CPC NR 1, AND STRUCTURAL LEAKAGE CHECK ACCOMPLISHED (SECURED PACK CONDENSOR BELLOWS, AOct 6, 2009 · N301NB · Airbus A319114 · Cabin Pressure ControllerSDR NWAA09923101Line · leakingON FINAL APPROACH, GREEN HYD RSVR LO LVL INDICATED ON ECAM, PERFORMED COM. ACFT LANDED UNEVENTFULLY, AND WAS TOWED TO GATE. REPLACED HYD LINE FOR RT MLG DOOR BYPASS VALVE (D3237005104000). LANDING GEAR DOORS TEST AND LEAK TEST OK. (K)Mar 24, 2009 · N301NB · Airbus A319114 · Hydraulic System, MainSDR NWAA072543101Power Supply · malfunctionedDURING OVERNIGHT LINE CHECK OF EMERGENCY ESCAPE LIGHT SYSTEM, EPSU INT LOAD AFT L FAULT MESSAGE DISPLAYED. REPLACED AFT 13WL EMERGENCY LIGHT POWER SUPPLY UNIT, CHECKS OK.Jul 21, 2007 · N301NB · Airbus A319114 · Emergency LightingSDR 0601253101Fan · malfunctionedVENT BLOWER FAULT, SMOKE IN COCKPIT, MAINTENANCE CONTROL NOTIFIED, DIVERTED TO BZN WITH UNEVENTFUL LANDING. REMOVED AND REPLACED AVIONICS EXTRACT FAN.   Jun 16, 2006 · N301NB · Airbus A319114 · Air Distribution Fan
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