N353NW

Service difficulty reports · 183

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 = 'N353NW' 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 DALA2015052103390Shear Tie · corrodedCORROSION ON CLEAT LOCATED FRAME 29 BETWEEN STR 43L TO STR 44 IN FWD CARGO COMPARTMENT, L=0.080", W=0.030", D=0.002". MEASURES APPROXIMATELY SSI 532180. REPLACED CLEAT LOCATED FRAME 29 BETWEEN STR 43L TO STR 44 IN FWD CARGO. COMPARTMENT IAW SRM 51-72-11.May 20, 2015 · N353NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015052103389Shear Tie · corrodedCORROSION ON CLEAT LOCATION FR 30 BETWEEN STR 43L TO STR 44 IN FWD CARGO COMPARTMENT L=0.080", W=0.046", D=0.002". MEASURES APPROX SSI 532180. REPLACED CLEAT LOCATED FR 30 BETWEEN STR 43L TO STR 44 IN FWD CC IAW SRM 51-72-11 AND DWG D53231712.May 20, 2015 · N353NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015052003387Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y512 BETWEEN FRAME 68 TO FRAME 69 AT AFT GALLEY AREA L=0.280", W=0.250", D=0.003". SSI 534147. REPLACED FLOORBEAM +Y512 BETWEEN FRAME 68 TO FRAME 69 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53474250, D53May 19, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015052003386Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y512, BETWEEN FRAME 65 TO FRAME 66 AT AFT GALLEY AREA L=0.395", W=0.350", D=0.003", SSI 534147. REPLACED FLOORBEAM +Y512 LOC. BETWEEN. FRAME 64 TO FRAME 67+10" AFT PAX CABIN IAW SRM 51-72-11 AND DWG D534728May 19, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015052003385Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM Y-464.8 BETWEEN FRAME 66 TO FRAME 67 AT AFT GALLEY AREA, L=0.245", W=0.225", D=0.003". SSI 534147. REPLACED FLOORBEAM -Y464.8 AND FASTENERS LOCATED BETWEEN FRAME 64 TO FRAME 67 IAW SRM 51-72-11 AND DWG. D53May 19, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015052003384Support Angle · corrodedDURING INSPECTION, FOUND CORROSION ON SUPPORT ANGLE LOCATION FRAME 30+13" BETWEEN STR 41R IN FWD CARGO COMPARTMENT, L=0.090", W=0.050", D=0.002". MEASURES APPROXIMATELY SSI 532180. REPLACED SUPPORT ANGLE LOCATED FRAME 30 + 13" BETWEEN STR 41R IN FWD CARMay 19, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015052003383Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM, Y503.2 AT LEVEL OF FR 16 AT FWD GALLEY AREAL=8", W=4", D=0.004". SSI 531189. REPLACED FLOORBEAM Y503.2 AT LEVEL OF FRAME 16 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53112825.May 19, 2015 · N353NW · Airbus A320211 · Fuselage Main, Floor BeamSDR DALA2015051903331Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y765 AT FWD GALLEY AREA FROM FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D531-12812 AND D531-10920.May 18, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051903330Fitting · corrodedCORROSION ON CORNER FITTING FRAME 16 AT FWD GALLEY AREA AND STRINGER 23R. REPLACED CORNER FITTING IAW SRM 51-72-11 AND DWG D53112225.May 18, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051903329Fitting · corrodedCORROSION ON CORNER FITTING FRAME 16 AT FWD GALLEY AREA TO STRINGER 23L. REPLACED CORNER FITTING LOCATED ON FRAME 16 AT FWD GALLEY AREA TO STR 23L SRM 51-72-11 AND DWG D53112225.May 18, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051903328Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y81 FRAMES 12 - 16. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11 AND DWG D53112829.May 18, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051803311Floor Support · corrodedCORROSION ON FLOORBEAM -Y160, BETWEEN FRAME 68 TO FRAME 69 AT AFT GALLEY AREA, L=0.260" W=0.256", D=0.003"; REPLACED FLOORBEAM -Y160, LOCATED BETWEEN FRAME 68 TO FRAME 70 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472800; MEASURES OF CORROSION ARE L=1.269May 17, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051703304Fitting · corrodedCORROSION ON CORNER FITTING FRAME 66 ON STRINGER 23L. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480505.May 16, 2015 · N353NW · Airbus A320212 · Fuselage Main, Attach FittingsSDR DALA2015051703303Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y254 FRAME 16. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IAW SRM 51-72-11 AND DWGS NR D53112816; D53110920 AND D53110984.May 16, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051503300Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y765, FRAME 16. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 & 24 IAW SRM 51-72-11, DWG D53112812, DWG D53110920 AND DWG D53110984.May 14, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051303216Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1292 AT LEVEL FRAME 16. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.May 12, 2015 · N353NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014082204679Battery Pack · inoperativeEPSU EXT LOAD AFT LEFT INOPERATIVE. REMOVED & INSTALLED EPSU BATTERY AT 11WL IAW AMM 33-51-38. OPS CHECKED GOOD. OK FOR SERVICE.Aug 19, 2014 · N353NW · Airbus A320212 · Emergency LightingSDR DALA1503213253None · noneREFUEL APERTURE/WING ELEC BOND INSPECT, IDENTIFIED AS MAJOR IAW AA 5724-01007.May 14, 2013 · N353NW · Airbus A320212 · Standard Practices/StructuresSDR DALA12012503253Wire · brokenDURING NON ROUTINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT 3A-B INOPERATIVE. MX REPAIRED BROKEN WIRE AT SEAT 3A-B AND FUNCTIONAL CHECK WAS NORMAL.Nov 10, 2012 · N353NW · Airbus A320212 · Light System WiringSDR DALA12008273253Light · disconnectedDURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT SEAT 20 INOPERATIVE. MX RECONNECTED AND FUNCTIONAL TEST WAS NORMAL.Sep 22, 2012 · N353NW · Airbus A320212 · Light System WiringSDR DALA1137603253Skin · corrodedAFT FUSELAGE BETWEEN FR 69 & FR 70 SKIN AROUND LAVATORY VACUUM OUTLET CORRODED. REMOVED CORR IAW SRM 51-74-00. REMAINING MAT OUT OF LIMITS IAW SRM 53-41-11. CUTOUT DAMAGED AREA IAW SRM 53-41-11 HFEC IAW NTM 51-10-08 NO CRACKS NOTED. FABBED DOUBLER & 2 EA FMay 26, 2011 · N353NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1503203253Skin · debondedRUDDER SIDE SHELL DISBONDED. INSP/REPAIR, IDENTIFIED AS MAJOR IAW AA 5540-01011.May 25, 2011 · N353NW · Airbus A320212 · Rudder, Plate/SkinSDR DALA1136483253Floor Panel · damagedFWD PIT FLOOR PANEL 131EF HAS EDGE DAMAGE AND IS WORN IN SEVERAL AREAS 12 INCHES BY 12 INCHES AREA. REMOVED PANEL 131EF IAW AMM 53-22-14-000-001. FABRICATED FLOOR PANEL 131EF ON STAM TRAVELLER T11/883644. INSTALLED FLOOR PANEL 131EF IAW AMM 53-221-14 PB401.May 25, 2011 · N353NW · Airbus A320212 · Fuselage Floor PanelSDR DALA1136473253Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 151DF IS DAMAGED. REMOVED AFT CARGO FLOOR PANEL 151DF IAW AMM 53-42-14-000-001. FABRICATED FLOOR PANEL 151DF ON STAM TRAVELER T11/883661 IAW DWG 3D25-37705. INSTALLED FLOOR PANEL 151DF IAW AMM 53-42-14-400-001.May 25, 2011 · N353NW · Airbus A320212 · Fuselage Floor PanelSDR DALA1136683253Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL 151AF IS DELAMINATED. REMOVED AND REPLACED AFT CARGO FLOOR PANEL 151AF IAW AMM 53-42-14-000-001.May 24, 2011 · N353NW · Airbus A320212 · Fuselage Floor PanelSDR DALA1119903253Wire · brokenDURING EMERGENCY LIGHT TEST FOUND PATH LIGHT FWD OF LEFT LAV DOOR INOP. REPAIRED BROKEN WIRES IN LAVATORY WALL AND TESTS OK.Mar 6, 2011 · N353NW · Airbus A320212 · Light System WiringSDR NWAA083983253Power Supply · inoperativeFOUND SEVERAL PAIRS OF SEAT ROW EMERGENCY EGRESS LIGHTING INOPERATIVE DURING LINE CHECK. REPLACED EPSU, CHECKED GOOD. (S)Aug 21, 2008 · N353NW · Airbus A320212 · Emergency LightingSDR NWAA083123253Power Supply · malfunctionedEMERGENCY EGRESS LIGHTING EPSU FAULTS "INT LOAD AFT L" AND "EXT LOAD AFT L". REPLACED EPSU 13WL, CHECKS GOOD. (S)Jul 12, 2008 · N353NW · Airbus A320212 · Emergency LightingSDR NWAA082753253Epsu · inoperativeEMERGENCY ESCAPE LIGHTING EPSU 13WL INOP. REPLACED EPSU 13WL, CHECKS OK. (A)Jun 15, 2008 · N353NW · Airbus A320212 · Emergency LightingSDR NWAA082063253Battery Pack · inoperativeON EMERGENCY LIGHT CHECK HAD "L" AFT EPSU MESSAGE ON FAP. REPLACED AFT BATTERY PACK.May 9, 2008 · N353NW · Airbus A320212 · Emergency LightingSDR 0002943253Controller · malfunctionedDURING APPROACH AT 1500 FEET AGL AND FULLY CONFIGURED FOR LANDING, THE FIRST OFFICER DISCONNECTED THE AUTOPILOT AND AIRCRAFT ROLLED 30 - 40 FEET RIGHT. FIRST OFFICER PUT IN FULL LEFT CONTROL STICK WITH SMALL AMOUNT OF RUDDER AND AIRCRAFT ROLLED BACK 20 - 30 FJul 13, 2000 · N353NW · Airbus A320212 · Aileron Control SystemSDR 0002513253Computer · malfunctionedDURING APPROACH AT 1500 FEET AGL, WINDS CALM, NO TURBULENCE, AND FULLY CONFIGURED FOR LANDING, THE FIRST OFFICER DISCONNECTED THE AUTOPILOT AND THE AIRCRAFT ROLLED 30 TO 40 FEET TO THE RIGHT. FIRST OFFICER PUT IN FULL LEFT CONTROL STICK WITH A SMALL AMOUNT OFJul 13, 2000 · N353NW · Airbus A320212 · Landing and Taxi AidsSDR 9900083253Fitting · leakingDURING DESCENT, RECEIVED HYD 'B' RSVR LOW LVL AND HYD 'B' ELEC PUMP LOW PR MESSAGES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED LEAKING HYDRAULIC LINE FITTING AND SERVICED SYSTEM. OPERATIONAL CHECK OK.Jan 11, 1999 · N353NW · Airbus A320212 · Hydraulic System, Main
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