# N223NW: 1975 Mcdonnell-Douglas DC-10-30, registration cancelled 2013-09-24 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 24, 2013 - 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: 46580 - Year built: 1975 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 16, 1992 - Certificate issued: September 5, 2008 - Last registry action: September 5, 2008 - Mode S code: A1ED67 - 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/N223NW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=223NW - Page: https://openairdocs.org/deregistered/N223NW-2013-09-24 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 (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0601941223](https://openairdocs.org/sdr/0601941223), Sep 3, 2006: ENCODER. ODOR. APPROX 2 HRS AFTER DEPARTURE NOTICEABLE ELECTRICAL TYPE ODOR COMING FROM SEAT 17A AND B. ELECTRICAL BOX UNDER SEAT 17A QUITE WARM. READING LIGHTS IN COACH WOULD - [SDR 0402061223](https://openairdocs.org/sdr/0402061223), Nov 23, 2004: ENGINE. FIRE. DURING NR 2 ENGINE START, GROUND CREW REPORTED A TAILPIPE FIRE. CFR WAS CALLED OUT AND SPRAYED FIRE EXTINGUISHING AGENT INTO THE TAILPIPE OF THE NR 2 ENGINE. TH - [SDR 0301291223](https://openairdocs.org/sdr/0301291223), Jul 13, 2003: SWITCH. MALFUNCTIONED. ZONE 'C' FLIGHT ATTENDANT CALL LIGHTS INTERMITTENTLY RING FROM VARIOUS ROWS AND SEATS. FORTY MINUTES PRIOR TO LANDING, FLIGHT ATTENDANT NOTED A BURNING RUBBER O - [SDR 0100491223](https://openairdocs.org/sdr/0100491223), Jan 9, 2001: DOOR FRAME. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE CENTER CARGO DOOR JAMB FRAME AT BS 1781 L41R AND 42R. REPAIRED PER EA 12-178406. - [SDR 0100501223](https://openairdocs.org/sdr/0100501223), Jan 4, 2001: SKIN. CORRODED. DURING H-CHECK, FOUND CORROSION ON THE RIGHT UPPER WING SKIN AT REAR SPAR BETWEEN XORS 770-775. REPAIRED PER EA 12-181626. - [SDR 0100471223](https://openairdocs.org/sdr/0100471223), Jan 4, 2001: FRAME. CRACKED. DURING H-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME AT BS 459 X58L AND X61L, CRACKS BEGIN AT EDGE OF FRAME AND TERMINATE AT LIGHTENING HOLES. REPAIRED PER - [SDR 0100511223](https://openairdocs.org/sdr/0100511223), Jan 3, 2001: FRAME. CRACKED. DURING H-CHECK, FOUND CRACK IN THE RT MAIN LANDING GEAR WHEEL WELL FRAME AT BS 1505. REPAIRED PER EA 12-181629. - [SDR 0004701223](https://openairdocs.org/sdr/0004701223), Dec 7, 2000: SKIN. CORRODED. DURING H-CHECK, FOUND CORROSION ON FUSELAGE SKIN BETWEEN BS 1509-1531, L48L-L48R. REPAIRED PER EA 12-152789. - [SDR 0002901223](https://openairdocs.org/sdr/0002901223), Aug 4, 2000: LIGHT. SHORTED. EN ROUTE TO AMS, FLIGHT ATTENDANT REPORTED READING LIGHTS IN AFT OF AIRCRAFT FLASHING ON AND OFF WITH NO CONTROL OVER THEM. ALSO, NOTED AN ELECTRICAL SMOKE SMEL - [SDR 0000471233](https://openairdocs.org/sdr/0000471233), Dec 6, 1999: CAP. CORRODED. DURING ''''H'''' CHECK, FOUND CORROSION ON PRESSURE BULKHEAD CAP AT BS 1521 BETWEEN LBL 31 AND RBL 31. REPAIRED PER EA12-172780. - [SDR 9902181223](https://openairdocs.org/sdr/9902181223), May 17, 1999: RIB. CRACKED. DURING L CHECK, FOUND CRACK IN RIGHT OUTBOARD FLAP CLOSURE RIB NEAR ROLLER ASSEMBLY REPAIRED PER EA 12-162794. - [SDR 9803581226](https://openairdocs.org/sdr/9803581226), Feb 28, 1998: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, FOUND ESCAPE PATH LIGHTING FAILS EMERGENCY LIGHT TEST. REPLACED C-SECTION POWER SUPPLY AND BATTERY, OPERATIONAL CHECK OK. - [SDR 9725051223](https://openairdocs.org/sdr/9725051223), Dec 23, 1997: JAMB. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON CENTER CARGO DOOR FORWARD DOOR JAMB FRAME 6 TO 10.5 INCHES FROM BOTTOM CORNER. REPAIRED PER EA 12-154210. - [SDR 9725281223](https://openairdocs.org/sdr/9725281223), Dec 20, 1997: RIB. CRACKED. DURING PERIODIC CHECK, FOUND A CRACK IN THE LEADING EDGE RIB 22 INCHES INBOARD OF NR 18 LEADING EDGE SLAT TRACK. REPAIRED PER EA 12-154205. - [SDR 9724771223](https://openairdocs.org/sdr/9724771223), Dec 20, 1997: FRAME. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON LOWER FORWARD CORNER OF DOOR FRAME AT FS 1708. REPAIRED PER EA 12-154222. - [SDR 9724761223](https://openairdocs.org/sdr/9724761223), Dec 19, 1997: FRAME. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION AROUND FASTENER ON FORWARD SIDE OF FS 1701 FRAME, LONGERON 43R. REPAIRED PER EA 12-154222. - [SDR 9725261223](https://openairdocs.org/sdr/9725261223), Dec 18, 1997: WEB. CRACKED. DURING PERIODIC CHECK, FOUND SEVERAL CRACKS IN THE NOSE WHEEL WELL RIGHT VERTICAL WEB FROM 24 TO 29 INCHES BELOW THE WHEEL WELL CEILING AT FS 478-486. REPAIRED - [SDR 9725271223](https://openairdocs.org/sdr/9725271223), Dec 17, 1997: LONGERON. CORRODED. DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 36R AT FS 753-758. REPAIRED PER EA 12-152785. - [SDR 9700041223](https://openairdocs.org/sdr/9700041223), Jan 5, 1997: STRUT SEALS. FAILED. DURING TAKEOFF, THE GEAR HANDLE WOULD NOT RAISE. FOLLOWED COM PROCEDURE AND RECYCLED THE GEAR BUT RECEIVED THE RED UNSAFE NOSE GEAR INDICATION. RETURNED TO MSP. - [SDR 9627591223](https://openairdocs.org/sdr/9627591223), Dec 19, 1996: DOUBLER. CORRODED. DURING MAINTENANCE INSPECTION, A CRACK WAS FOUND IN THE NR 1 PYLON UPPER SPAR DOUBLER AT STA YN=367. REMOVED DAMAGED AREA PER EA 12-120123 (P/N AUB7366-501). - [SDR 9621051223](https://openairdocs.org/sdr/9621051223), Oct 3, 1996: COMPRESSOR. STALLED. AFTER TAKEOFF AT 1,000 FEET, THE NR 3 ENGINE EXPERIENCED TWO COMPRESSOR STALLS. FLIGHT CREW SHUTDOWN NR 3 ENGINE, DUMPED FUEL AND PERFORMED AN UNEVENTFUL LANDIN - [SDR 9518651223](https://openairdocs.org/sdr/9518651223), Nov 13, 1995: SKIN. CORRODED. DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN BS 1197 TO 2005, LONGERONS 45L TO 46L AND 45R TO 46R. REPAIRED SKIN (P/N AJC 7164), PER EA 12-103213 AND -1 - [SDR 9518641223](https://openairdocs.org/sdr/9518641223), Nov 10, 1995: SKIN. CORRODED. DURING T-CHECK, FOUND CORROSION ON THE FUSELAGE SKIN INNER SURFACE FS 1524 BETWEEN LONGERON 50R TO 51R. REPAIRED SKIN (P/N AYB7065-2). - [SDR 9518631223](https://openairdocs.org/sdr/9518631223), Nov 10, 1995: SUPPORT. CORRODED. DURING T-CHECK, FOUND CORROSION ON THE FS 495 FLOOR SUPPORT BETWEEN RBL 25 TO 50. REPAIRED SUPPORT PER EA 12-104181. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19961003037909I](https://openairdocs.org/incident/19961003037909I), Oct 3, 1996: Doug DC1030 (N223NW), UK. Narrative: #3 engine failed after take-off. Dumped fuel and aircraft returned without incident. Root cause of engine failure still under investigation by klm. ## Other aircraft with N223NW - [Registered now](https://openairdocs.org/aircraft/N223NW): DJI AGRAS T100, S/N 0791 --- 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.