# Service difficulty reports: N224NW, cancelled Jul 7, 2017 A list on [N224NW, cancelled Jul 7, 2017](https://openairdocs.org/deregistered/N224NW-2017-07-07.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0600851224](https://openairdocs.org/sdr/0600851224.md): Motor · leaking · Apr 29, 2006 · N224NW · Doug DC1030 · Stabilizer Control System > CLIMBING OUT OF MSP NR 3 HYDRAULIC SYSTEM LOST TOTAL QUANTITY. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO MSP FOR UNEVENTFUL LANDING. FOUND HORIZONTAL STAB TRIM MOTOR LEAKING. REPLACED STAB TRIM MOTOR. OPERATION AND LEAK CHECKS GOOD. - [SDR 0501531224](https://openairdocs.org/sdr/0501531224.md): Smoke · detected · Oct 13, 2005 · N224NW · Doug DC1030 · Air Distribution System > DURING CRUISE SMELLED ELECTRICAL FUMES IN COCKPIT AND OBSERVED SMOKE AROUND FLOOR BEHIND F/O SEAT. FOLLOWED COM LIST TO "RECIRC FANS OFF" AND SMOKE DISSIPATED. DID NOT RE-OCCUR FOR REMAINDER OF FLIGHT WITH CIRC FANS OFF. FLIGHT CONTINUED TO MEM AND LANDED W - [SDR 0301981224](https://openairdocs.org/sdr/0301981224.md): Floorbeam · cracked · Oct 1, 2003 · N224NW · Doug DC1030 · Fuselage Main, Floor Beam > DURING M CHECK, FOUND CRACK ON FLOORBEAM AT BS 475 RBL 38. REPAIRED IAW EA 12-152773. - [SDR 9901411224](https://openairdocs.org/sdr/9901411224.md): Switch · failed · Apr 3, 1999 · N224NW · Doug DC1030 · Landing Gear Position and Warning > ON DEPARTURE FROM AMS, THE RIGHT MAIN LANDING GEAR DOOR LIGHT ILLUMINATED. FOLLOWED COM PROCEDURE. RECYCLED GEAR, LIGHT WENT OUT, ILLUMINATED, AND THEN WENT OUT AGAIN. LIGHT WAS ONLY VISIBLE ON FORWARD PANEL AND NOT ON SECOND OFFICER'S PANEL. REPLACED DOOR - [SDR 9900041224](https://openairdocs.org/sdr/9900041224.md): Outflow Valve · malfunctioned · Jan 4, 1999 · N224NW · Doug DC1030 · Pressure Regulator/Outflow Valve > DURING DESCENT INTO MSP, LOST CABN PRESSURE AT APPROXIMATELY 36,000 FEET AND MASKS DEPLOYED. CABIN PRESSURE WAS RESTORED MANUALLY, AT APPROXIMATELY 6,000 FEET, CABIN PRESSURE WAS LOST AGAIN. FLIGHT CONTINUED INTO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE - [SDR 9723741224](https://openairdocs.org/sdr/9723741224.md): Skin · corroded · Nov 12, 1997 · N224NW · Doug DC1030 · Fuselage Main, Plate/Skin > DURING M CHECK, FOUND CORROSION ON INTERNAL SKIN AT FS 1666 BETWEEN LONGERON 44R-45R. REPAIRED PER EA 12-153552. - [SDR 9723761224](https://openairdocs.org/sdr/9723761224.md): Blkhd T-Chord · corroded · Nov 11, 1997 · N224NW · Doug DC1030 · Fuselage Main, Bulkhead > DURING M CHECK, FOUND CORROSION T CHORD OF AFT PRESSURE BULKHEAD AT FS 2007, RBL 24. REPAIRED PER EA 12-152774. - [SDR 9723751224](https://openairdocs.org/sdr/9723751224.md): Frame · corroded · Nov 11, 1997 · N224NW · Doug DC1030 · Fuselage Main, Frame > DURING M CHECK, FOUND CORROSION ON CHORD AT FS 1681-1701 INBOARD OF LONGERON 43R. REPAIRED PER EA 12-1527776. - [SDR 9722861224](https://openairdocs.org/sdr/9722861224.md): Skin · corroded · Nov 11, 1997 · N224NW · Doug DC1030 · Fuselage Main, Plate/Skin > DURING M-CHECK, FOUND CORROSION ON BELLY SKIN BETWEEN FS 1505 TO 1530 AND LONGERONS 48L AND 48R. REPAIRED PER EA 12-150767. - [SDR 9723731224](https://openairdocs.org/sdr/9723731224.md): Frame · cracked · Nov 6, 1997 · N224NW · Doug DC1030 · Fuselage Main, Frame > DURING M CHECK, FOUND CRACK IN FRAME OF CENTER CARGO DOOR AFT SILL FS 1785, 40 INCHES ABOVE LOWER CUTOUT CORNER. ALODINED AND PRIMED PARTS. INSTALLED DOUBLER, FILLER, AND SHIMS WITH SEALANT PER EA 12-153545. - [SDR 9723721224](https://openairdocs.org/sdr/9723721224.md): Frame · corroded · Nov 6, 1997 · N224NW · Doug DC1030 · Fuselage Main, Frame > DURING M CHECK, FOUND CORROSION ON FORWARD CARGO DOOR CUTOUT FRAME AFT LOWER CORNER AT FS 1002. REPAIRED PER EA 12-150766. - [SDR 9721451224](https://openairdocs.org/sdr/9721451224.md): Longeron · corroded · Nov 6, 1997 · N224NW · Doug DC1030 · Fuselage Main, Longeron/Stringer > DURING M-CHECK, FOUND CORROSION ON BOTH SIDES OF LONGERON 52 FORWARD OF FS 1114. REPAIRED PER EA 12-153640. - [SDR 9721281224](https://openairdocs.org/sdr/9721281224.md): Rib · cracked · Nov 4, 1997 · N224NW · Doug DC1030 · Wing, Rib/Bulkhead > DURING M-CHECK, FOUND CRACK IN RIGHT WING LEADING EDGE RIB AT WS 1089. REPAIRED PER EA 12-152580. - [SDR 9720481224](https://openairdocs.org/sdr/9720481224.md): Fitting · corroded · Oct 31, 1997 · N224NW · Doug DC1030 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CORROSION ON LONGERON END FITTINGS ON THE CENTER GEAR WHEEL WELL AFT SHELF FROM LBL 20 TO RBL 20. REPLACED 6 END FITTINGS (P/N AYB7063-1) AND 1 END FITTING (P/N AYB7063-501) PER SRM 51-00-00, VOL I. - [SDR 9721441224](https://openairdocs.org/sdr/9721441224.md): Support · cracked · Oct 24, 1997 · N224NW · Doug DC1030 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CRACK IN UPPER FLANGE AT FS 475 FLOOR SUPPORT RAIL. REPAIRED PER EA 12-152773. - [SDR 9713111224](https://openairdocs.org/sdr/9713111224.md): Hydraulic Pump · failed · Jul 1, 1997 · N224NW · Doug DC1030 · Hydraulic Pump (Electric/Engine), Main > DURING CRUISE, LOST NR 3 SYSTEM HYDRAULIC FLUID. FLIGHT DUMPED 60,000 LBS OF FUEL AND RETURNED TO HNL. MAINTENANCE REPLACED THE LEFT ENGINE HYDRAULIC PUMP. - [SDR 9712551224](https://openairdocs.org/sdr/9712551224.md): Tr Unit · malfunctioned · Jun 26, 1997 · N224NW · Doug DC1030 · Engine Thrust Reverser > AFTER LANDING, THE NR 3 ENGINE WOULD NOT COME OUT OF REVERSE THRUST. THE ENGINE WAS SHUT DOWN. MAINTENANCE OPERATED NR 3 REVERSER AND FOUND NO PROBLEMS. AIRCRAFT RETURNED TO SERVICE. - [SDR 9711431224](https://openairdocs.org/sdr/9711431224.md): Tr Unit · malfunctioned · Jun 13, 1997 · N224NW · Doug DC1030 · Engine Thrust Reverser > AFTER LANDING, THE NR 3 ENGINE THRUST REVERSER DID NOT COME OUT OF REVERSE THRUST. THE ENGINE WAS SHUT DOWN AFTER CLEARING THE RUNWAY. MAINTENANCE LOCKED OUT NR 3 THRUST REVERSER PER MEL 78-1A. EXACT PART CAUSING PROBLEM TO BE DETERMINED. - [SDR 9614781224](https://openairdocs.org/sdr/9614781224.md): Skin · corroded · Jun 24, 1996 · N224NW · Doug DC1030 · Fuselage Main, Plate/Skin > DURING L-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN DOUBLER AT FS 1146 BETWEEN LONGERONS 51L TO 52L. REPAIRED SKIN (P/N AAA7058-1) PER EA 12-105442. - [SDR 9510231224](https://openairdocs.org/sdr/9510231224.md): Connector · crossed · Jul 1, 1995 · N224NW · Doug DC1030 · Pneumatic Distribution System > DURING CRUISE, THE NR 1 PNEUMATIC SUPPLY VALVE STUCK OPEN. DUMPED 6000 LBS OF FUEL AND RETURNED TO SEA. AIRCRAFT WAS INSPECTED AND SYSTEM WAS MEL'ED. CANNON PLUGS R5-8012 AND R5-8026 WERE REPOSITIONED. OPERATIONAL CHECK OK. - [SDR 9511561224](https://openairdocs.org/sdr/9511561224.md): Skin · corroded · Jun 30, 1995 · N224NW · Doug DC1030 · Fuselage Main, Plate/Skin > DURING LINE CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 808 - 824, LONGERONS 37L - 38L. REPAIRED SKIN AND LONGERON 38L PER EA 12-99010. - [SDR 9510581224](https://openairdocs.org/sdr/9510581224.md): Skin · cracked · Jun 30, 1995 · N224NW · Doug DC1030 · Wing, Plate/Skin > DURING L-CHECK, FOUND A CRACK, CORROSION, AND RIVETS PULLING THROUGH THE RIGHT WING OUTBOARD ISLAND PANEL (LOWER TRAILING EDGE) STA XC 948. REPAIRED SKIN DOUBLER AND T-ANGLE PER EA 12-98578. ## 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 = 'N224NW' AND deregistration_id = 'N224NW-2017-07-07' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N224NW-2017-07-07/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.