N328NW

Service difficulty reports · 190

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 = 'N328NW' 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 DALA2014121606549Floor Support · corrodedAFTER REMOVAL CENTER FITTING WAS FOUND CORROSION ON LOWER SILL LOCATION BETWEEN FRAME 16 TO FRAME 20 AND AT LEVEL OF STRG 23 RT L=1", W=0.50" AND D= 0.002" APPROXIMATELY SSI 531189. REPLACED LOWER SILL LOCATION BETWEEN FRAME 16 TO FRAME 20 AND AT LEVEL OF STDec 15, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014121606548Seat Track · out of limitsSEAT TRACK -Y765, BETWEEN FRAMES 47-64 FOUND OUT THE LIMTS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG 53472000.Dec 15, 2014 · N328NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014121306526Floor Panel · crackedDURING INSPECTION, FOUND CRACK ON FLOOR PANEL 241HF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00, FIG 209 .Dec 12, 2014 · N328NW · Airbus A320211 · Fuselage Floor PanelSDR DALA2014121306525Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 42R BETWEEN FRAMES 33 - 34 IN FWD CARGO BAY . REPLACED THE STRINGER IAW SRM 51-72-11, DWG D53231375, AND D53230320.Dec 12, 2014 · N328NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA2014121306524Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING LOCATED AT LEVEL OF FRAME 16 AND S23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG 53112109.Dec 12, 2014 · N328NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014121306523Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 20 STRINGER 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53112109.Dec 12, 2014 · N328NW · Airbus A320211 · Fuselage Main, Attach FittingsSDR DALA2014121306522Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FRAMES 16 - 20, S23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53112109.Dec 12, 2014 · N328NW · Airbus A320212 · Fuselage Main, Attach FittingsSDR DALA2014121306521Floor Panel · delaminatedDURING INSPECTION, FOUND DELAMINATE FLOOR PANEL 222FF. REPLACED THE FLOOR PANEL IAW AMM 53-12-12.Dec 12, 2014 · N328NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2014121106506Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FRAMES 16 - 20 STRINGER 23L. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53112109.Dec 10, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014121106505Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Dec 10, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014121106504Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1292 BETWEEN FRAMES 64 - 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Dec 10, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014121006483Dummy Rail · corrodedDURING INSPECTION, FOUND CORROSION ON DUMMY RAIL Y503.2, FRAME 16. REPLACED THE DUMMY RAIL IAW SRM 51-72-11 AND DWG D53110984.Dec 9, 2014 · N328NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2014120706428Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1292. REPLACED THE FLOOR SUPPORT FRAMES 12 - 24 IAW SRM 51-75-11 AND DWG D53112812 AND D53110900.Dec 6, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014120706427Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1292 BETWEEN FRAMES 18 - 20. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53110900.Dec 6, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014120606426Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB LOCATED BETWEEN FRAMES 69 - 70 . REPLACED THE WEB IAW SRM 51-72-11 AND DWG D534 70100.Dec 6, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014120606425Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT, Y765 BETWEEN FRAMES 66+5 TO 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.Dec 5, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014120606424Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT, Y765 BETWEEN FRAMES 64 AND 66+5. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Dec 5, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014120606423Floor Support · corrodedDURING INSPECTION, FOUND CORROSION AROUND OF RIVET ON FLOOR SUPPORT -Y81. REPLACED THE FLOOR SUPPORT LOCATED BETWEEN FRAMES 12 TO 16 IAW SRM 51-72-11 AND DWG D53112828, D53110984.Dec 5, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014120406387Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765 BETWEEN FRAMES 66+5" - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Dec 3, 2014 · N328NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA14014523228Light · damagedDURING NON-ROUTINE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT DAMAGED AND INOPERATIVE AT LOCATION 25C. REINSTALLED LIGHT ASSY INTO SEAT BASE. OPS CHECKED GOOD.Mar 1, 2014 · N328NW · Airbus A320211 · Emergency LightingSDR DALA14008203228Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND SEATS 9-12, EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED RT EPSU 12WV AND FUNCTIONAL CHECKED NORMAL.Feb 7, 2014 · N328NW · Airbus A320211 · Emergency LightingSDR DALA14006673228Wire · brokenDURING INSPECTION, FOUND EMERGENCY EXIT FWD LIGHT ROW 1 ABC HAS BROKEN WIRE. MAINTENANCE REPAIRED WIRE AND FUNCTIONAL CHECKED NORMAL.Feb 1, 2014 · N328NW · Airbus A320211 · Light System WiringSDR DALA13049713228Battery Pack · inoperativeDURING EMERGENCY SYS TEST MESSAGE BATTERY, EMERGENCY LIGHT. REPLACED EMERGENCY LIGHT BATTERY AT EMERGENCY EXIT LT SIDE. OPS CK GOOD. OK FOR SVC.Oct 6, 2013 · N328NW · Airbus A320212 · Emergency LightingSDR DALA12011633228Connector · looseCABIN SEAT ROW 19C EMERGENCY LIGHT INOPERATIVE. SECURED LOOSE CONNECTOR. OPS CHECK GOOD. OK FOR SERVICE.Oct 29, 2012 · N328NW · Airbus A320211 · Light System WiringSDR DALA1113033228Hinge Fitting · crackedRT MLG FWD DOOR HINGE FITTING, FUSELAGE SIDE FORWARD HALF IS CRACKED AT LOWER TIE STRAP FASTENER. REMOVED AND REPLACED FITTING IAW SRM 51-42-11. REAMED BUSHING HOLES ON FITTING TO DIA.940 INCH ON STAM TRAVELER NR T11/871400 PER DWG D53370622. INSTALLED BUSHFeb 22, 2011 · N328NW · Airbus A320211 · Fuselage, Door HingeSDR DALA1112753228Floor Panel · delaminatedAFT PIT FLOOR PANEL 151DF IS DELAMINATED ON A 10 INCH BY 10 INCH AREA. REMOVED FLOOR PANEL NR 151DF IAW AMM 53-42-14-000-001. FABRICATED NEW PANEL AS PER TRAVELER T11/870852. INSTALLED PANEL 151DF IAW SRM 51-42-21. PANEL FABRICATED PER DWG 3D25-37498.Feb 21, 2011 · N328NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1112223228Floor Panel · delaminatedAFT CARGO FLOOR PANEL 151GF IS DELAMINATED ON A 30 INCH BY 30 INCH AREA. REMOVED FLOOR PANEL 151GF IAW AMM 53-42-14-000-001. FABRICATED NEW PANEL IAW NWD 3D25- 37498. INSTALLED PANEL 151GF IAW AMM 53-22-14-400-001.Feb 19, 2011 · N328NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1111763228Floor Panel · puncturedFWD CARGO COMPARTMENT FLOOR PANEL 131AF HAS A PUNCTURE AND DELAMINATION. REMOVED PANEL 131AF IAW AMM 53-22-14-000-001. FABRICATED NEW FLOOR PANEL 131AF ON STAM TRAVELER T11/870830 IAW DWG 3D25-37498. INSTALLED PANEL IAW AMM 53-22-14-400-001.Feb 17, 2011 · N328NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1111743228Floor Panel · puncturedFWD CARGO COMPARTMENT, FLOOR PANEL 131EF HAS PUNCTURES AND EDGE DELAMINATIONS. REMOVED PANEL 131EF IAW AMM 53-22-14-000-001. FABRICATED ON STAM TRAVELER T11/870851 IAW D25-37498. INSTALLED PANEL 131EF IAW AMM 53-22-14-400-001.Feb 17, 2011 · N328NW · Airbus A320211 · Fuselage Floor PanelSDR DALA1035333228Stringer · corrodedDURING LINE CHECK FOUND STR 31 AT FR 65 AND FR 66 RT HAS CORROSION JUST BELOW OUTFLOW VALVE. REMOVED DAMAGED SECTION OF STR REMOVED ENTIRE STR DRILLED UP NEW STRINGER. INSTALLED ENTIRE STR 31RT. COMPLIED WITH RII REQUIREMENTS FOR THE INSTALLATION AND SECURITY Dec 10, 2010 · N328NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR DALA100113228Wire · looseDURING A NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT ROW 6 AND 10 INOPERATIVE. REPAIRED AND SECURED WIRING AT BOTH LOCATION AND OPERATIONAL.Jan 1, 2010 · N328NW · Airbus A320211 · Light System WiringSDR NWAA072653228Power Supply · failedDURING EMERGENCY ESCAPE LIGHTING CHECK, FORWARD POWER SUPPLY UNIT FAILED. REPLACED FORWARD EPSU 10WL, CHECKS OK.Jul 29, 2007 · N328NW · Airbus A320211 · Emergency LightingSDR 0501783228Power Supply · inoperativeEMERGENCY EXIT LIGHTS IN REAR GALLEY INOP. REMOVED AND REPLACED POWER SUPPLY 13WL AND BATTERY. OPS CHECKS GOOD.Dec 16, 2005 · N328NW · Airbus A320211 · Emergency LightingSDR 9810833228Actuator · leakingDURING DESCENT, RECEIVED HYD G RSVR LO LVL MESSAGE. CREW SHUT OFF GREEN HYDRAULIC PUMP, PTU, GRAVITY EXTEND LANDING GEAR, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING LEFT YAW DAMPER ACTUATOR.Dec 8, 1998 · N328NW · Airbus A320211 · Autopilot SystemSDR 9718033228Hyd Lines · leakingDURING CLIMBOUT AFTER LANDING GEAR RETRACTION, THE YELLOW HYDRAULIC SYSTEM FLUID QUANTITY DECREASED TO ZERO. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE YELLOW HYDRAULIC SYSTEM GROUND SERVICED MANIFOLD (3146GM). LEAK AND OSep 23, 1997 · N328NW · Airbus A320211 · Hydraulic System, AuxiliarySDR 9716183228Battery · dischargedDURING LINE MAINTENANCE, THE EMERGENCY LIGHTS FAULTED DURING TEST. REPLACED BATTERIES IN AFT LEFT EPSU. OPERATIONAL CHECK OK.Aug 26, 1997 · N328NW · Airbus A320211 · Emergency LightingSDR 9706593228Wire · brokenDURING LINE MAINTENANCE, THE EMERGENCY PATH LIGHTS, AT ROWS 23 AND 24, WERE INOPERATIVE. REPAIRED BROKEN WIRE AT SEAT TRACK COVER. OPERATIONAL CHECK OK.Mar 28, 1997 · N328NW · Airbus A320211 · Light System WiringSDR 9614573228Battery Pack · dischargedDURING LINE MAINTENANCE, THE LEFT AND RIGHT AFT DOORS EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED BATTERY PACK, OPERATIONAL CHECK OK.Jun 26, 1996 · N328NW · Airbus A320211 · Emergency LightingSDR 9507433228Valve · malfunctionedDURING CLIMBOUT FROM SEA, RECEIVED VENT SKIN VALVE FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND THEN RECEIVED VENT BLOWER FAULT MESSAGE. UNABLE TO PRESSURIZE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SEA AND LANDED May 5, 1995 · N328NW · Airbus A320211 · Cabin Cooling SystemSDR 9507433204Vent Valve · malfunctionedDURING CLIMBOUT FROM SEA, RECEIVED VENT SKIN VALVE FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND THEN RECEIVED VENT BLOWER FAULT MESSAGE. UNABLE TO PRESSURIZE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SEA AND LANDED May 5, 1995 · N328NW · Airbus A320211 · Cabin Cooling System
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