# Service difficulty reports: N211NW, cancelled Apr 4, 2017 A list on [N211NW, cancelled Apr 4, 2017](https://openairdocs.org/deregistered/N211NW-2017-04-04.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0400981221](https://openairdocs.org/sdr/0400981221.md): Fire Detector · malfunctioned · Jun 8, 2004 · N211NW · Doug DC1030 · Smoke Detection > DURING 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 - [SDR 0200911211](https://openairdocs.org/sdr/0200911211.md): Stringer · cracked · Feb 24, 2002 · N211NW · Doug DC1030 · Horizontal Stabilizer Structure > During "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. - [SDR 0101551211](https://openairdocs.org/sdr/0101551211.md): Gearbox · leaking · Apr 28, 2001 · N211NW · Doug DC1030 · Turbine Engine Accessory Drive > DURING 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 R - [SDR 0003821211](https://openairdocs.org/sdr/0003821211.md): Control Box · overheated · Oct 7, 2000 · N211NW · Doug DC1030 · Entertainment System > EN 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 OBSTRUCTI - [SDR 9703491211](https://openairdocs.org/sdr/9703491211.md): Casting · cracked · Feb 6, 1997 · N211NW · Doug DC1030 · Wing, Control Surface Attach Fittings > DURING TRANSITION CHECK, FOUND CRACK IN THE LEFT INBOARD FLAP INBOARD TRACK ATTACH CASTING. REPAIRED PER EA 12-121503. - [SDR 9703011211](https://openairdocs.org/sdr/9703011211.md): Skin · cracked · Feb 3, 1997 · N211NW · Doug DC1030 · Wing, Plate/Skin > DURING TRANSITION CHECK, FOUND CRACK AT FORWARD INBOARD CORNER OF CUTOUT SKIN DOOR FUELING PANEL 519CB. REPAIRED PER EA 12-121471. - [SDR 9702271211](https://openairdocs.org/sdr/9702271211.md): Fitting · corroded · Feb 1, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9702241211](https://openairdocs.org/sdr/9702241211.md): Fitting · corrosion · Feb 1, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9702231211](https://openairdocs.org/sdr/9702231211.md): Fitting · corroded · Feb 1, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9702281211](https://openairdocs.org/sdr/9702281211.md): Fitting · corroded · Jan 31, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9702261211](https://openairdocs.org/sdr/9702261211.md): Fitting · corroded · Jan 31, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9702251211](https://openairdocs.org/sdr/9702251211.md): Fitting · corroded · Jan 31, 1997 · N211NW · Doug DC1030 · Fuselage Miscellaneous Structure > DURING 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. - [SDR 9623431211](https://openairdocs.org/sdr/9623431211.md): Computer · failed · Nov 5, 1996 · N211NW · Doug DC1030 · Stall Warning System > DURING 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. - [SDR 9615501211](https://openairdocs.org/sdr/9615501211.md): Compressor · stalled · Jul 17, 1996 · N211NW · Doug DC1030 · Turbine Engine Compressor Section > AFTER 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 THE - [SDR 9611771211](https://openairdocs.org/sdr/9611771211.md): Power Supply · inoperative · May 27, 1996 · N211NW · Doug DC1030 · Emergency Lighting > DURING LINE INSPECTION, ZONE B, FOUND FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND RETURNED TO SERVICE. - [SDR 9611751211](https://openairdocs.org/sdr/9611751211.md): Battery · discharged · May 3, 1996 · N211NW · Doug DC1030 · Emergency Lighting > DURING LINE INSPECTION, FOUND THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE MID-CABIN BATTERY. - [SDR 9600531211](https://openairdocs.org/sdr/9600531211.md): Apu · failed · Jan 11, 1996 · N211NW · Doug DC1030 · Airborne Auxiliary Power Unit (APU) System > DURING 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 REPLACE - [SDR 9520761211](https://openairdocs.org/sdr/9520761211.md): Door Frame · corroded · Nov 23, 1995 · N211NW · Doug DC1030 · Fuselage Miscellaneous Structure > DURING 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. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N211NW-2017-04-04/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.