N225NW

Service difficulty reports not matched to an aircraft · 27

They name N225NW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N225NW' AND registry_match IS NULL
  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 0601021225Power Supply · inoperativeEMERGENCY LIGHTS INOP ROW 30 BACK. REPLACED POWER SUPPLY. OPERATION CHECKS GOOD. May 15, 2006 · N225NW · Doug DC1030 · Emergency LightingSDR 0500641225Compressor · stalledDURING TAKEOFF ROLL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WITH EGT EXCEEDING RED LINE. TAKEOFF WAS ABORTED AT 110 KTS. THE ENGINE WILL BE REPLACED.Apr 29, 2005 · N225NW · Doug DC1030 · Turbine Engine Compressor SectionSDR 0401001225Fire Loop · malfunctionedON CLIMBOUT AT 31,000 FT, RECEIVED NR 2 ENGINE FIRE WARNING INDICATION. NR 2 ENGINE B-LOOP WAS PUT ON MEL. SHUT DOWN NR 2 ENGINE IAW COM PROCEDURE. DUMPED 90,000 LBS OF FUEL AND RETURNED TO NRT FOR AN UNEVENTFUL LANDING. WORK IN PROGRESS-SUPPLEMENTAL INFORMATJun 17, 2004 · N225NW · Doug DC1030 · Fire DetectionSDR 0301611225Generator · failedDURING CRUISE, NR 2 GENERATOR TRIPPED OFF AND THEN NR 1 CSD TEMPERATURE CLIMBED AND TRIPPED OFF. FLIGHT DUMPED 70,000 LBS OF FUEL AND RETURNED TO DTW. MAINTENANCE REPLACED THE NBR 1 GENERATOR AND SERVICED CSD AND REPLACED NR 2 GENERATOR CONTROL, GENERATOR, Aug 19, 2003 · N225NW · Doug DC1030 · AC Generation SystemSDR 0203401225Pump · inoperativePUMP WAS INSTALLED IN THE LOWER AUXILIARY FUEL TANK. IT WAS REMOVED AS PART OF EO 2815-01008 WHICH DEACTIVATES THE LOWER AUXILIARY FUEL TANK. PUMP FAILED THE STANDARD MEGGAR BENCH TEST. THE PUMP WAS DASSEMBLED AND FOUND TO HAVE CHAFING ON THE WIRING HARNESS.Oct 2, 2002 · N225NW · Doug DC1030 · Fuel Boost PumpSDR 0104671225GeneratorDURING CRUISE ENROUTE TO HNL, THE NBR 1 GENERATOR DROPPED OFF LINE. FLIGHT CREW FOLLOWED COM PROCEDURE AND DISCONNECTED CSD AND GENERATOR. FLIGHT CONTINUED TO HNL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NBR 1 GENERATOR FAILURE RESULTED IN STRUCTURAL Nov 28, 2001 · N225NW · Doug DC1030 · AC Generator-AlternatorSDR 0103151225Torque Link · disconnectedABORTED TAKEOFF AT 100 KNOTS DUE TO VIBRATION AND LOSS OF NOSE GEAR STEERING. FOUND NOSE LANDING GEAR TORQUE LINKS DISCONNECTED. AIRCRAFT WAS TOWED TO THE GATE. FOUND CEILING PANELS DOWN, CENTER OVERHEAD BIN DAMAGED, AND E/E SHELVING DAMAGED. AFTER INSPECTAug 30, 2001 · N225NW · Doug DC1030 · Nose/Tail Landing Gear Strut/AxleSDR 0003811225Unknown · odorAMS- SEVERAL PASSENGERS NOTED AN ELECTRICAL ODOR IN THE AREA OF SEATS 1AB BUT ODOR THEN DISSIPATED. AIRCRAFT CONTINUED TO AMS AND LANDED WITHOUT INCIDENT. REPLACED SEAT HARNESS 1A AND 1B, DISPLAY CABLES FOR 1A AND 1B, AND ALL LRUS. ALL COMPONENTS SENT TO RCOct 8, 2000 · N225NW · Doug DC1030 · Air Distribution SystemSDR 9810511225Power Supply · smokingDURING CRUISE, NOTICED SMOKE IN OVERHEAD CEILING BETWEEN FIRST GALLEY AND COAT CLOSET. ALSO, SMOKE COMING FROM EMERGENCY POWER SUPPLY. FLIGHT DIVERTED TO GEG AND LANDED WITHOUT INCIDENT. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK OK.Nov 24, 1998 · N225NW · Doug DC1030 · Emergency LightingSDR 9807591225Control · failedNR 1 GENERATOR OFF LIGHT ILLUMINATED AND NR 1 GENERATOR DROPPED OFF LINE. ON TAKEOFF ROLL, THE NR 1 GENERATOR OFF LIGHT ILLUMINATED AGAIN. RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 1 GENERATOR CONTROL, OPERATIONAL CHECK NORMAL.Apr 25, 1998 · N225NW · Doug DC1030 · AC Generation SystemSDR 9807471225Web · crackedDURING M CHECK, FOUND CRACK IN AFT WEB IN THE RIGHT WHEEL WELL. REPAIRED PER EA 12-156163.Mar 20, 1998 · N225NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 9805481225Frame · crackedDURING M-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME AT FS 459, RBL 62. REPAIRED PER EA 12-150786.Mar 18, 1998 · N225NW · Doug DC1030 · Fuselage Main, FrameSDR 9805471225Frame · crackedDURING M-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME AT FS 459 LBL 62. REPAIRED PER EA 12-150786.Mar 18, 1998 · N225NW · Doug DC1030 · Fuselage Main, FrameSDR 9805491225Frame · corrodedDURING M-CHECK, FOUND CORROSION ON FORWARD CARGO DOOR JAMB FRAME AT FS 895, STR 42R. REPAIRED PER EA 12-190781.Mar 16, 1998 · N225NW · Doug DC1030 · Fuselage Main, FrameSDR 9807371225Longeron · corrodedDURING M CHECK, FOUND CORRODED LONGERON IN THE NR 1 AC COMPARTMENT AT THE EXHAUST FS 568-587. REPAIRED PER EA 12-155546.Mar 11, 1998 · N225NW · Doug DC1030 · Fuselage Main, Longeron/StringerSDR 9804571225Skin · corrodedDURING M CHECK, FOUND CORROSION ON BELLY SKIN AT FS 1501-1531, LONGERON 48L-48R. REPAIRED PER EA 12-154586.Mar 3, 1998 · N225NW · Doug DC1030 · Fuselage Main, Plate/SkinSDR 9801931225Regulator Valve · failedON DEPARTURE, NR 1 PNEUMATIC TEMPERATURE LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. UNABLE TO DEPRESSURIZE DUCT. REDUCED THROTTLE AND BROUGHT TEMPERATURE DOWN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED PJan 31, 1998 · N225NW · Doug DC1030 · Pneumatic Distribution SystemSDR 9714131225Engine · failedWHILE CLIMBING THROUGH FL180, THE NR 2 ENGINE EGT AND FUEL FLOW SPIKED WITH AN ASSOCIATED VIBRATION. THE ENGINE STABILIZED ON ITS OWN. THIRTY MINUTES LATER THE EGT REACHED MAXIMUM AND THE VIBRATION RETURNED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED Jul 23, 1997 · N225NW · Doug DC1030 · Engine (Turbine/Turboprop)SDR 9618881225Seal · wornDURING CRUISE, CABIN PRESSURE FLUCTUATED AND UNABLE TO CONTROL NR 2 PNEUMATIC SYSTEM. FLIGHT RETURNED TO HNL. MAINTENANCE REPLACED THE CENTER E/E DOOR SEAL, REINSTALLED NR 1 AND NR 2 FAN BYPASS CHECK VALVE, AND LOCKED THE NR 2 PRSOV INTO THE CLOSED POSITION.Aug 29, 1996 · N225NW · Doug DC1030 · Electrical/Electronic Compartment DoorsSDR 9618331225Press Reg Valve · malfunctionedDURING CLIMB, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED AND WAS UNABLE TO CLOSE PRV PER COM. DUMPED 45,000 LBS OF FUEL AND RETURNED TO DTW. MAINTENANCE LOCKED THE NR 2 PRV IN THE CLOSED POSITION AND PLACED ON MEL.Aug 25, 1996 · N225NW · Doug DC1030 · Pressure Regulator/Outflow ValveSDR 9617161225Pneum Sys · malfunctionedDURING CRUISE, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED. FOLLOWED COM AND SHUT OFF THE PNEUMATIC SUPPLY. DUMPED 15,000 LBS OF FUEL AND RETURNED TO HNL. MAINTENANCE DEFERRED THE NR 2 PNEUMATIC SYSTEM AND REPAIRED THE NR 3 SYSTEM WHICH WAS ON MEL.Aug 9, 1996 · N225NW · Doug DC1030 · Pneumatic Indicating SystemSDR 9611781225Power Supply · inoperativeDURING LINE INSPECTION, FOUND THE EMERGENCY LIGHT AND STANDBY POWER CIRCUIT BREAKERS TRIPPED. MAINTENANCE REPLACED THE FORWARD BATTERY POWER SUPPLY.May 23, 1996 · N225NW · Doug DC1030 · Emergency LightingSDR 9611761225Battery Pack · dischargedDURING LINE INSPECTION, FOUND THE EMERGENCY LIGHT INOPERATIVE AT DOOR 1L AND 1R AND THE FIRST CLASS FLOOR LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND TIGHTENED WIRES.May 10, 1996 · N225NW · Doug DC1030 · Emergency LightingSDR 9607331225Indication Syst · malfunctionedDURING CRUISE, THE NR 1 PNEUMATIC TEMPERATURE WAS 220 DEGREES AND THE NR 3 PNEUMATIC TEMPERATURE LIGHT ILLUMINATED WITH NR 3 TEMPERATURE INDICATING 150 DEGREES. DUMPED 70,000 LBS OF FUEL AND RETURNED TO HNL. MAINTENANCE SECURED THE PRESSURE REGULATOR VALVE CMar 31, 1996 · N225NW · Doug DC1030 · Pneumatic Indicating SystemSDR 9601601225Skin · corrodedDURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1950 TO 1958, LONGERON 50L TO 52. REPAIRED SKIN (P/N AGA 7418-1) PER EA 12-104396.Jan 10, 1996 · N225NW · Doug DC1030 · Fuselage Main, Plate/SkinSDR 9600681225Fitting · corrodedDURING T-CHECK, FOUND CORROSION ON THE CENTER GEAR WELL STRINGER FITTINGS AT LBL 21, 14, 7, BL 0, AND RBL 21 FROM BS 1509 TO 1521. REPLACED STRINGER FITTINGS.Jan 8, 1996 · N225NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 9601551225Skin · corrodedDURING T-CHECK, FOUND CORROSION ON THE MOUNTING RINGS FOR ALL 4 RADIO ALTIMETER MOUNTING RINGS. REPAIRED RINGS (P/N AYB7022-1; AYB 7053-1, -501) PER EA 12-103877.Jan 3, 1996 · N225NW · Doug DC1030 · Fuselage Main, Plate/Skin
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