# N224NW: 1975 Mcdonnell-Douglas DC-10-30, registration cancelled 2017-07-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 7, 2017 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Mcdonnell-Douglas DC-10-30](https://openairdocs.org/model/mcdonnell-douglas-dc-10-30) (registry code 3023501) - Engine: [GE CF6-50 series](https://openairdocs.org/engine/ge-cf6-50-series) (registry code 30018) - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 46581 - Year built: 1975 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 3, 1991 - Certificate issued: September 5, 2008 - Last registry action: September 5, 2008 - Mode S code: A1F11E - Owner when cancelled: [World Airways Inc](https://openairdocs.org/faa-owner/WORLD%20AIRWAYS%20INC) - Location: [Peachtree City, GA](https://openairdocs.org/faa-place/GA/Peachtree%20City) - Owner type: Corporation - Owner's area on the map: 33.3939° N, 84.5693° W: Placed by OpenAirDocs at the center of ZIP code 30269, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N224NW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=224NW - Page: https://openairdocs.org/deregistered/N224NW-2017-07-07 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell-Douglas DC-10-30: https://openairdocs.org/model/mcdonnell-douglas-dc-10-30.md ## Service difficulty reports (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0600851224](https://openairdocs.org/sdr/0600851224), Apr 29, 2006: MOTOR. LEAKING. CLIMBING OUT OF MSP NR 3 HYDRAULIC SYSTEM LOST TOTAL QUANTITY. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO MSP FOR UNEVENTFUL LANDING. FOUND HO - [SDR 0501531224](https://openairdocs.org/sdr/0501531224), Oct 13, 2005: SMOKE. DETECTED. 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. - [SDR 0301981224](https://openairdocs.org/sdr/0301981224), Oct 1, 2003: FLOORBEAM. CRACKED. DURING M CHECK, FOUND CRACK ON FLOORBEAM AT BS 475 RBL 38. REPAIRED IAW EA 12-152773. - [SDR 9901411224](https://openairdocs.org/sdr/9901411224), Apr 3, 1999: SWITCH. FAILED. 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 - [SDR 9900041224](https://openairdocs.org/sdr/9900041224), Jan 4, 1999: OUTFLOW VALVE. MALFUNCTIONED. 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, - [SDR 9723741224](https://openairdocs.org/sdr/9723741224), Nov 12, 1997: SKIN. CORRODED. 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), Nov 11, 1997: BLKHD T-CHORD. CORRODED. 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), Nov 11, 1997: FRAME. CORRODED. 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), Nov 11, 1997: SKIN. CORRODED. 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), Nov 6, 1997: FRAME. CRACKED. 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, F - [SDR 9723721224](https://openairdocs.org/sdr/9723721224), Nov 6, 1997: FRAME. CORRODED. 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), Nov 6, 1997: LONGERON. CORRODED. 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), Nov 4, 1997: RIB. CRACKED. 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), Oct 31, 1997: FITTING. CORRODED. 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) - [SDR 9721441224](https://openairdocs.org/sdr/9721441224), Oct 24, 1997: SUPPORT. CRACKED. 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), Jul 1, 1997: HYDRAULIC PUMP. FAILED. 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), Jun 26, 1997: TR UNIT. MALFUNCTIONED. 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. AIRCRAF - [SDR 9711431224](https://openairdocs.org/sdr/9711431224), Jun 13, 1997: TR UNIT. MALFUNCTIONED. 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 - [SDR 9614781224](https://openairdocs.org/sdr/9614781224), Jun 24, 1996: SKIN. CORRODED. 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), Jul 1, 1995: CONNECTOR. CROSSED. 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 PLU - [SDR 9511561224](https://openairdocs.org/sdr/9511561224), Jun 30, 1995: SKIN. CORRODED. 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), Jun 30, 1995: SKIN. CRACKED. 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 DOUBLE ## Other aircraft with N224NW - [Registered now](https://openairdocs.org/aircraft/N224NW): DJI AGRAS T100, S/N 0810 --- 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.