N318NB

Service difficulty reports · 181

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 = 'N318NB' 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 DALA1204183118Blanking Plate · corrodedR2 DOOR AFT BLANKING PLATE CORRODED (PANEL RACK). REPLACED R2 DOOR AFT BLANKING PLATE IAW A319 SRM 51-72-00.Jan 21, 2012 · N318NB · Airbus A319114 · Service DoorsSDR DALA1203943118Floor Support · corrodedFLOOR SUPPORT BEAM -Y1292 FR68 CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 ORIG MAT .150. REWORK DIMENSIONS L=2" W=3" D=.075". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-15. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11.Jan 21, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1203863118Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BEAM +Y254 BETWEEN FR 16 AND FR 20 CORRODED IN SEVERAL AREAS. REMOVED CORROSION IAW A319 SRM 51-74-00. AFTER REWORK DIMENSION LENGTH 2.5" WIDTH 2.0" DEPTH .075" ORIGINAL MATERIAL THICKNESS .150". FOUND OUT OF LIMITS IAW A319 SRM Jan 21, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1203853118Floor Panel · corrodedAFT UTILITY FLOOR PANEL 261FF CORRODED (PANEL RACK). REPLACED PANEL 261FF STRINGER 490428 BFM.Jan 20, 2012 · N318NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1203843118Floor Support · corrodedFLOOR SUPPORT BEAM -Y1292 BET FR66 & FR68 CORRODED IN SEVERAL AREAS. REMOVED CORROSION IAW A319 SRM 51-74-00 ORIG MAT .087 REWORK DIMENSIONS L=1" W=1.9" D=.059". FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED FLOORBEAM SUPPORT IAW A31Jan 20, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1203833118Floor Support · corrodedFLOOR SUPPORT BEAM -Y1292 FR64 TO FR66 BOTH FWD AND AFT END CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 ORIG MAT .095" REWORK DIMENSIONS L=3.5" W=1.2" D=.070". FOUND TO BE OUT LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED FLOORBEAM SUPPORT IAW A3Jan 20, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202593118Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BEAM -Y1292 BETWEEN FR18 AND FR20 HAS CORROSION AT SEVERAL AREAS. BLENDED AREA IAW A319 SRM 51-74-00 L=1.80' W=1.70' D=.055' TOOL USED DEPTH GAUGE TR14402. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15 FIG 104. REMOVED AND REPLACEDJan 17, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202573118Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BEAM +Y765 AT FR16 AND FR20 HAS CORROSION. BLENDED AREA IAW A319 SRM 51-73-00 L=1.75 W=1.70 D=.047IN. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-15 FIG 102. REMOVED FLOOR SUPPORT +Y765 IAW A319 SRM 51-42-11. RECEIVED NEW FLOJan 17, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202563118Floor Support · corrodedFLOOR SUPPORT BEAM -Y318 AT FR66 FASTENER HOLE CORRODED. BLENDED CORROSION AREA IAW A319 SRM 51-74-00. ORIG MATERIAL .165' L=1.455' W=1.145 D=0.039' FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND INSTALLED NEW FLOOR SUPPORT BEAM FR65 TJan 17, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202473118Floor Support · corrodedFLOOR SUPPORT BEAM +Y512 AT FR68 HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00. CORRODED AREA MEASURE L=.450 W=.150 D=.040. OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED & REPLACED FLOOR SUPPORT IAW A319 SRM 51-42-11. RETAIN FOR RECORDS.Jan 16, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202463118Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BEAM +Y1292 FROM FR16 TO FR 20 HAS CORROSION. BLENDED AREA IAW A319 SRM 51-73-00. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-15 FIG 104. REMOVED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW A319 SRJan 16, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202043118Floor Support · corrodedFLOOR SUPPORT BEAM -Y1732 AT FR65 TO FR66 CORRODED. BLENDED AREA IAW A319 SRM 51-74-00 L=1.5" W=1.0" D=0.044". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11.Jan 16, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202033118Floor Support · corrodedFLOOR SUPPORT BEAM -Y765 BETWEEN FR64 AND FR65 IS CORRODED. BLENDED AREA IAW A319 SRM 51-74-00 L=1.2" W=1.0D=0.020" FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11.Jan 16, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202023118Floor Support · corrodedFLOOR SUPPORT BEAM -Y765 AT FR66 TO FR70 CORRODED. BLENDED AREA IAW A319 SRM 51-74-00 L=1.5" W=1.3" D=0.025. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11.Jan 16, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202013118Floor Support · corrodedFLOOR SUPPORT BEAM +Y765 AT FR66 AND FR68 IS CORRODED AT SEVERAL AREAS. BLENDED AREA IAW A319 SRM 51-74-00 L=2.20" W=1.30 D=0.095". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 101. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11.Jan 16, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1202003118Floor Support · corrodedFLOOR SUPPORT BEAM +Y765 AT FR66 IS CORRODED. BLENDED AREA IAW A319 SRM 51-74-00 L=4.0" W=1.3" D=0.065". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 101. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11.Jan 16, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1201993118Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT -Y189 FR21 HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00, AFT. REWORK DIMENSION L=3" W=1.3" D=.025" ORIG MAT. 0.068" FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 104. REMOVED OLD FLOOR SUPPORT IAW A319 SRM 51-42-1Jan 13, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1201983118Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT DUMMY BEAM +Y503 AT FR 16 IS CORRODED. REMOVE CORROSION PER SRM A319 51-74-00 ORIGINAL MATERIAL THICKNESS 0.159" AFTER REWORK DIMENSIONS L=1.5" W=1.5" D=0.065" FOUND TO BE OUT OF LIMITS PER SRM A319 53-11-14 FIG 103. REMOVED AND RJan 12, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1201633118Floor Support · corrodedFLOOR SUPPORT BEAM AT +Y 254 AFT OF FR66 AND 68. 4 EACH FASTENER HOLES ARE CORRODED. BLENDED AREA PER SRM 51-74-00, L=2.0" W=1.0" D=.045" ORIGINAL MAT .065" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14 FIG 102. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLEJan 10, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1201623118Floor Support · corrodedFLOOR SUPPORT BEAM AT +Y 254 AFT OF FR63 3 EA FASTENER HOLES ARE CORRODED. BLENDED AREA PER SRM 51-74-00 L=1.5" W=1.0" D=.055", FOUND TO BE OUT OF LIMITS PER SRM 53-00-14 FIG 102. ORIGINAL MATERIAL .080. REMOVED AND REPLACED BEAM P/N D534721962000 IAW SRM Jan 10, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1201653118Floor Support · corrodedFWD CABIN FLOOR SUPPORT WEB -Y1732 FR20 HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00 DIM L=2.745" W=2.735" D=.035". NO DAMAGED LIMITS FOUND IN SRM. REMOVED AND INSTALLED NEW FLOOR SUPPORT WEB -Y1732 FR20 P/N D531127840031 BATCH 0002144824 IAW A319 SRMJan 9, 2012 · N318NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1151473118Wire · brokenDURING NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT ROW 3 LEFT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE UNDER SEAT AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Sep 2, 2011 · N318NB · Airbus A319114 · Light System WiringSDR DALA1121973118Pin · looseDURING EMERGENCY LIGHT TEST FOUND SEAT ROW 5 INOPERATIVE. MAINTENANCE SECURED THE CONNECTOR PIN AND TESTS OK.Mar 24, 2011 · N318NB · Airbus A319114 · Light System WiringSDR DALA1121963118Wire Harness · brokenDURING EMERGENCY LIGHT TEST FOUND SEAT ROW 14 INOPERATIVE. MAINTENANCE FOUND A BROKEN HARNESS AND REPLACED IT. SYSTEM TESTS OK.Mar 24, 2011 · N318NB · Airbus A319114 · Light System WiringSDR DALA1113783118Wire Harness · brokenDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT 21L INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE HARNESS UNDER SEAT AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL.Feb 24, 2011 · N318NB · Airbus A319114 · Light System WiringSDR DALA1202723118Doubler · damagedWHILE WORKING ON APU STARTER, INSPECTION LIFTED THE LIFT TRUCK AND STRUCK THE AIRCRAFT, MAKING LESS THAN ONE INCH HOLE ON THE FUSELAGE OF THE AIRCRAFT AT LOCATION STA 32811 / FR 77 STRINGER 43R. REMOVED DOUBLER REPAIR IAW A319 SRM 51-42-11 AND SRM 53-00-11Jul 20, 2010 · N318NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA14003383118Hinge Fitting · damagedRIGHT MLG FORWARD HINGE FITTING. REPAIRED IAW ERA 478980-14AD.Jul 13, 2010 · N318NB · Airbus A319114 · Fuselage, Landing Gear Attach FittingsSDR DALA104723118Wire · brokenDURING A NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT ROW 7, 14, 20, AND 21 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND PERFORMED FUNCTIONAL CHECK. CHECK WAS NORMAL.Mar 2, 2010 · N318NB · Airbus A319114 · Light System WiringSDR DALA14003353118Hinge Fitting · corrodedLEFT MLG FWD HINGE FITTING CORRODED. REPAIRED IAW ERA 478979-14AD.Jan 14, 2010 · N318NB · Airbus A319114 · Fuselage, Landing Gear Attach FittingsSDR NWAA082533118Pump · leakingHYDRAULIC-G RSVR LO LVL, G ENG1 PUMP LOW PSI, GREEN HYDRAULIC QUANTITY ZERO, DETECTED STRONG SIMILAR ODOR DURING TAKEOFF ROLL THAT DISSIPATED DURING CLIMB. REPLACED NR 1 ENGINE DRIVEN PUMP, CHECKS OK. (A)Jun 5, 2008 · N318NB · Airbus A319114 · Hydraulic Pump (Electric/Engine), MainSDR 0100403118Smoke · detectedDURING TAXI TO THE GATE, SMOKE WITH A STRONG BURNING ODOR WAS REPORTED IN THE CABIN AFT OF THE WINGS. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES.Feb 5, 2001 · N318NB · Airbus A319114 · Air Distribution System
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