N211NW, cancelled Apr 4, 2017

Service difficulty reports · 18

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 = 'N211NW' AND deregistration_id = 'N211NW-2017-04-04'
  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 0400981221Fire Detector · malfunctionedDURING CRUISE, THE FORWARD CARGO COMPARTMENT NR 2 AND NR 4 SMOKE DETECTOR LIGHTS AND FORWARD CARGO FIRE LIGHT ILLUMINATED. FOLLOWED COM PROCEDURE AND PROCEEDED TO NEAREST AIRPORT (BIL) FOR AN UNEVENTFUL LANDING. BOTH FIRE BOTTLES RELEASED. REPLACED NR 2, 3 Jun 8, 2004 · N211NW · Doug DC1030 · Smoke DetectionSDR 0200911211Stringer · crackedDuring "H" check found cracks on LH horizontal stabilizer outboard aft skin panel integral stringers, #1-7.5 inch crack at stations XE 77.100 and stringer #4-6.25 inch crack at station EX 77.100. Repaired per EA 12-162218.Feb 24, 2002 · N211NW · Doug DC1030 · Horizontal Stabilizer StructureSDR 0101551211Gearbox · leakingDURING CRUISE, THE NR 3 ENGINE OIL QUANTITY DECREASED TO ZERO AND OIL PRESSURE DROPPED INTO THE RED WITH THE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO MNL. THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE RApr 28, 2001 · N211NW · Doug DC1030 · Turbine Engine Accessory DriveSDR 0003821211Control Box · overheatedEN ROUTE TO DTW, PASSENGER AT SEAT 30F REPORTED SEAT FRAME HOT AND UNUSUAL SMELL. FOUND MUX CONNECTOR BOX COVER OPEN. RESEATED CONNECTORS AND CLOSED COVER. HEAT AND SMELL DISSIPATED. AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. CLEARED OBSTRUCTIOct 7, 2000 · N211NW · Doug DC1030 · Entertainment SystemSDR 9703491211Casting · crackedDURING TRANSITION CHECK, FOUND CRACK IN THE LEFT INBOARD FLAP INBOARD TRACK ATTACH CASTING. REPAIRED PER EA 12-121503.Feb 6, 1997 · N211NW · Doug DC1030 · Wing, Control Surface Attach FittingsSDR 9703011211Skin · crackedDURING TRANSITION CHECK, FOUND CRACK AT FORWARD INBOARD CORNER OF CUTOUT SKIN DOOR FUELING PANEL 519CB. REPAIRED PER EA 12-121471.Feb 3, 1997 · N211NW · Doug DC1030 · Wing, Plate/SkinSDR 9702271211Fitting · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT LBL 27 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01.Feb 1, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 9702241211Fitting · corrosionDURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT RBL 18 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01.Feb 1, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 9702231211Fitting · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT LBL 7 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01.Feb 1, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 9702281211Fitting · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT LBL 21 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01.Jan 31, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 9702261211Fitting · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT RBL 15 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01.Jan 31, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 9702251211Fitting · corrodedDURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT BL 0 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01.Jan 31, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 9623431211Computer · failedDURING TAKEOFF, THE STALL WARNING STICK SHAKER ACTIVATED. FLIGHT DUMPED 41,000 POUNDS OF FUEL AND RETURNED TO HNL. MAINTENANCE REPLACED THE AT/SC COMPUTER AND THE NR 2 AOA SENSOR.Nov 5, 1996 · N211NW · Doug DC1030 · Stall Warning SystemSDR 9615501211Compressor · stalledAFTER TAKEOFF AND DURING CLIMB, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AT 6,000 FEET. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, SHUT DOWN THE ENGINE, DUMPED 12,000 LBS OF FUEL AND RETURNED TO SEA WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION OF THEJul 17, 1996 · N211NW · Doug DC1030 · Turbine Engine Compressor SectionSDR 9611771211Power Supply · inoperativeDURING LINE INSPECTION, ZONE B, FOUND FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND RETURNED TO SERVICE.May 27, 1996 · N211NW · Doug DC1030 · Emergency LightingSDR 9611751211Battery · dischargedDURING LINE INSPECTION, FOUND THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE MID-CABIN BATTERY.May 3, 1996 · N211NW · Doug DC1030 · Emergency LightingSDR 9600531211Apu · failedDURING CLIMB, A STRONG OIL SMELL WAS PRESENT THROUGH OUT THE AIRCRAFT. FLIGHT CREW FOLLOWED SMOKE REMOVAL PROCEDURES, BUT ODOR COULD NOT BE ISOLATED. FLIGHT RETURNED TO DEPARTURE AIRPORT LANDING WITHOUT FURTHER INCIDENT. GROUND PERSONNEL REMOVED AND REPLACEJan 11, 1996 · N211NW · Doug DC1030 · Airborne Auxiliary Power Unit (APU) SystemSDR 9520761211Door Frame · corrodedDURING LINE CHECK, FOUND CORROSION ON THE CENTER CARGO DOOR JAMB LOWER FORWARD FRAME, FS 1708 AT LONGERON 41R. REPAIRED FRAME (P/N AFA 3873-3) PER EA 12-99308.Nov 23, 1995 · N211NW · Doug DC1030 · Fuselage Miscellaneous Structure
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