N326NB

Service difficulty reports · 240

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 = 'N326NB' 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 DALA12008593126Panel · damagedAFT CARGO SLOPE PANEL 152XG DAMAGED 2.5"X 2.0". SLOPE PANEL FABRICATED NEW IAW DWG 3025-40532.Sep 24, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008583126Blanking Plate · brokenR2 DOOR, AFT BLANKING PLATE IS BROKEN. NR 250-4. R2 DOOR, AFT BLANKING PLATE REPLACED IAW SRM 51-72-00.Sep 20, 2012 · N326NB · Airbus A319114 · Service DoorsSDR DALA12008573126Floor Panel · delaminatedAFT CABIN FLOOR PANEL 261PF BOTTOM SKIN IS DELAMINATED, 3" X 2" AREA. FLOOR PANEL FABRICATED NEW IAW DWG 3D25-40640.Sep 19, 2012 · N326NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12008563126Floor Panel · delaminatedFORWARD CABIN FLOOR PANEL 222EF DELAMINATED "2 X 2". FLOOR PANEL FABRICATED NEW IAW DWG 3D25-40640.Sep 19, 2012 · N326NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12008553126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR 64-66 Y-765 UPPER FLANGE AND HARD POINT HOLES CORRODED. BLENDED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15, FIG 2. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT Sep 19, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008543126Floor Panel · corrodedMAIN CABIN FLOOR PANEL 222FF CORRODED "3 X 4". INSTALLED NEW FLOOR PANELSep 18, 2012 · N326NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12008533126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR68 TO FR69 Y-1292 UPPER FLANGE CORRODED. BLENDED FLOOR SUPPORT IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-14. R & R FLOOR SUPPORT IAW SRM 51-42-11. CHECKED DIMENSIONS: L=1.5" W=1.0" D=0.080".ORIGINAL MATERISep 18, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008523126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR 66 TO 68 Y-1292 UPPER FLANGE CORRODED. BLENDED FLOOR SUPPORT IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 51-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11. CHECKED DIMENSIONS: L=1.0" W=1.0" D=0.060". ORIGINAL MATESep 18, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008513126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR 64 TO 66 Y-1292 UPPER FLANGE AND HARD POINT HAS CORROSION. BLENDED AREA IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW TRM 51-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11. CHECKED DIMENSIONS: L=1.5" W=1.0" D=0.040 ORIGINSep 18, 2012 · N326NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12008443126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR65 TO FR67 Y-475 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. R & R FLOOR SUPPORT IAW SRM 51-42-11.Sep 16, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008433126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR65 TO FR66 Y-1732 UPPER FLANGE HOLE HAS CORROSION. R & R FLOOR SUPPORT IAW SRM 51-42-11.Sep 16, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008213126Seat Track · corrodedFORWARD CABIN SEAT TRACK BTW FR 20 TO FR 23 UPPER CROWN Y-765 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15. REMOVED FLOOR SUPPORT AND REPLACED IAW SRM 51-42-11.Sep 16, 2012 · N326NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12008143126Shear Plate · crackedAFT CABIN LT SIDE BTW FR 68 THROUGH 69 STR 23L, SHEAR PLATE CRACKED. REMOVED CRACKED SHEAR PLATE IAW SRM 51-42-11. INSTALLED NEW SHEAR PLATE IAW SRM 51-42-11.Sep 16, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12009223126Fitting · gougedNR 1 PYLON MATING FACE OF FWD PYLON PYRAMID FITTING LOWER SURFACE AFT CENTER HOLES HAS GOUGE. BLENDED DAMAGE AREA IAW SRM 51-73-00, DIMENSION AFT HOLE D1= .020" D2=.046" S1=0.0004 MID HOLE D1=.035" D2=.046"S1=0.0008. FOUND TO BE WITHIN LIMITS IAW SRM 54-51-1Sep 15, 2012 · N326NB · Airbus A319114 · Nacelle/Pylon, Attach FittingsSDR DALA12008883126Seat Track · corrodedFORWARD CABIN FLOOR SEAT TRACK BETWEEN FR18 TO FR20 Y-1292 UPPER FLANGE AND SEAT TRACK CROWN HAS CORROSION. R & R FLOORBEAM AT FR12 TO FR24 -Y1292 IAW SRM 51-42-11. BLENDED AREA AT FR20 L=.280" W=.084" D=.070". FOUND TO BE OUT OF LIMITS IAW TRM 53-00-15.Sep 15, 2012 · N326NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA12008423126Floor Panel · corrodedAFT CABIN FLOOR PANEL 261FF IS CORRODED, INSTALLED NEW FLOOR PANEL.Sep 15, 2012 · N326NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12008413126Floor Panel · corrodedAFT CARGO FLOOR PANEL 152BE CORRODED. INSTALLED NEW FLOOR PANEL.Sep 15, 2012 · N326NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12008203126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR66 TO FR68 Y-765 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED DAMAGED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11.Sep 15, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008133126Floor Panel · corrodedMAIN CABIN FLOOR PANEL 221FF CORRODED 3" X 4". INSTALLED FLOOR PANEL.Sep 15, 2012 · N326NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12008123126Floor Panel · corrodedAFT CABIN FLOOR PANEL 262FF IS CORRODED, 4" X 4" AREA. INSTALLED FLOOR PANEL.Sep 15, 2012 · N326NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12008193126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 64 TO FR 66 Y765 HARD POINT HOLES HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15, FIG 2. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW SRSep 14, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008113126Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BETWEEN FR 16 TO FR 20 HAS CORROSION. BLENDED AREAS ON FLOOR SUPPORT 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.Sep 14, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008073126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR 67 TO FR 70 Y765 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.Sep 14, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008183126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT, BETWEEN FR 68-69 Y1292 UPPER FLANGE HAS CORROSION. BLENDED AREA 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.Sep 13, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008173126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BTW FR 66 TO FR 68 Y1292 UPPER FLANGE HAS CORROSION. BLENDED AREA 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.Sep 13, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008163126Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT BETWEEN FR 64 TO FR 66 Y1292, CORRODED. BLENDED AREA 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.Sep 13, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008063126Sill · corrodedRIGHT AFT PAX DOOR SILL AT FR68 UPPER FLANGE HAS CORROSION. BLENDED CORRODED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. CUT OUT DAMAGED IAW SRM 53-41-14 FIG 201. FABRICATED FILLER AND FABRICATED ANGLE IAW SRM 53-41-14 FIG 201. Sep 12, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12008053126Floorbeam · corrodedFORWARD UTILITY AREA FLOORBEAM AT FR 16 Y503.2 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 103. R & R FLOORBEAM IAW TRM 53-21-01.Sep 12, 2012 · N326NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA12008043126Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT BETWEEN FR 16 TO FR 20 Y254 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 103. R & R FLOOR SUPPORT IAW SRM 51-42-11.Sep 12, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12009253126Skin · dentedRIGHT SIDE UPPER AFT FUSELAGE EXTERNAL SKIN FWD OF FR 61 AND LOWER OF S23R HAS DENT. MEASUREMENT DAMAGE A=1.0" B=.850" D=.022" T=.063" FOUND TO BE WITHIN LIMITS IAW SRM 53-41-11, DIAGRAM 104. PERFORMED DVI ON DENTED AREA, NO CRACK NOTED. HFEC IAW NTM 51-10Sep 11, 2012 · N326NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA12007093126Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT, BTW FR 20 TO FR 21 Y-189 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.Sep 10, 2012 · N326NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA12006033126Connector · disconnectedROW 20 WHITE EMERGENCY AISLE LIGHT INOPERATIVE. RECONNECTED CONNECTOR. OPS CHECKED GOOD.Aug 26, 2012 · N326NB · Airbus A319114 · Light System WiringSDR DALA12006023126Wire · brokenROW 6 EMERGENCY AISLE LIGHT INOPERATIVE. FOUND BROKEN WIRE. REPAIRED, OPS CHECKED GOOD. OK FOR SERVICE.Aug 26, 2012 · N326NB · Airbus A319114 · Light System WiringSDR DALA1150843126Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT TEST DISPLAYING "EMER SYS ATA 33-51-38 EPSU COMM EMER L". MAINTENANCE REPLACED POWER SUPPLY UNIT AT LEFT OVERWING EXIT AND FUNCTIONAL CHECK WAS NORMAL.Aug 31, 2011 · N326NB · Airbus A319114 · Emergency LightingSDR DALA1142503126Light · damagedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT 4C DAMAGED. MAINTENANCE REPLACED LIGHT MODULE AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jul 3, 2011 · N326NB · Airbus A319114 · Emergency LightingSDR DALA1137783126Battery Pack · dischargedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT L FAILED EPSU TEST. MAINTENANCE REPLACED BATTERY PACK AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jun 5, 2011 · N326NB · Airbus A319114 · Emergency LightingSDR DALA1130013126Fitting · corrodedRT MLG RIB 5 FWD LUG BORE AND FACES CORRODED BEYOND LIMITS PER SRM AND AD 2008-08-04. REWORKED PER PRI 492062-14. ACCOMPLISH ERA 492062-14 SECTION II INSPECTION EVERY 2000 CYCLES AFTER SECTION I AND 500 CYCLE INTERVALS THEREAFTER. ACCOMPLISH SECTION III AT Apr 28, 2011 · N326NB · Airbus A319114 · Wing, Landing Gear Attach FittingsSDR DALA107753126Wire · damagedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 20 INOPERATIVE. MX REPAIRED WIRE AT CONNECTOR UNDER SEAT AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Apr 13, 2010 · N326NB · Airbus A319114 · Light System WiringSDR DALA105563126Window · crackedON CLIMBOUT, CAPT`S AFT FIXED WINDOW CRACKED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. A SAFE AND UNEVENTFUL LANDING WAS ACCOMPLISHED. MX REPLACED CAPTAIN’S AFT FIXED WINDOW IAW AMM 56-11-12. ACFT HAS RETURNED TO SERVICE.Mar 14, 2010 · N326NB · Airbus A319114 · Flight Compartment WindowsSDR 0601243126Battery Pack · faultedEPSU BATTERY RIGHT FAULT ANNUNCIATED ON CIDS PANEL. REPLACED EMERGENCY LIGHTS BATTERY PACK.   Jun 11, 2006 · N326NB · Airbus A319114 · Emergency Lighting
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