# N229NW: 1972 Mcdonnell-Douglas DC-10-30, registration cancelled 2012-09-27 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 27, 2012 - 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: 46551 - Year built: 1972 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 5, 1995 - Certificate issued: April 27, 2006 - Last registry action: September 14, 2009 - Mode S code: A203B1 - Owner when cancelled: [Miami Leasing Inc](https://openairdocs.org/faa-owner/MIAMI%20LEASING%20INC) - Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale) - Owner type: Corporation - Owner's area on the map: 26.0870° N, 80.1530° W: Placed by OpenAirDocs at the center of ZIP code 33315, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N229NW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=229NW - Page: https://openairdocs.org/deregistered/N229NW-2012-09-27 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 0002981229](https://openairdocs.org/sdr/0002981229), Aug 18, 2000: PIN. INSTALLED. ON TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND NOSE LANDING GEAR PIN INSTALLED. REMOVED PIN AND RETU - [SDR 0000621229](https://openairdocs.org/sdr/0000621229), Feb 2, 2000: STIFFENER. CORRODED. DURING M-CHECK, SEVERAL STIFFENERS WERE FOUND TO BE CORRODED ON AT BS 2007 AFT PRESSURE BULKHEAD. REPAIRED PER EA 172806. - [SDR 0000641229](https://openairdocs.org/sdr/0000641229), Jan 19, 2000: BULKHEAD. CRACKED. DURING M-CHECK, FOUND CRACK AT BS 2122 LOWER BULKHEAD WEB. REPAIRED PER EA 12-172785. - [SDR 0000631229](https://openairdocs.org/sdr/0000631229), Jan 13, 2000: SKIN. CORRODED. DURING M-CHECK, FOUND CORROSION ON THE CORNER DOUBLERS AT LT AND RT SIDES OF CENTER WHEEL WELL GEAR CUTOUT AREA. REPAIRED PER EA 12-173105. - [SDR 0000591229](https://openairdocs.org/sdr/0000591229), Jan 11, 2000: FINGER DOUBLER. CORRODED. DURING M-CHECK, FOUND CORROSION ON FINGER DOUBLER AT BS 1126 L19L. REPAIRED PER EA 12-170440. - [SDR 0000601229](https://openairdocs.org/sdr/0000601229), Jan 10, 2000: RIB. CRACKED. DURING M-CHECK, FOUND CRACK ON LOWER SKIN PANEL STRINGER NUMBER 12 OF HORIZONTAL STATION XE407 AT STRINGER RIB CLIP. REPAIRED PER EA 12-173332. - [SDR 0000611229](https://openairdocs.org/sdr/0000611229), Jan 8, 2000: SKIN. CRACKED. DURING M-CHECK, FOUND CRACK ON FUSELAGE SKIN AT BS 589 ON LT AFT SIDE OF NOSE GEAR CUTOUT RADIUS. REPAIRD PER EA 12-173910. - [SDR 9900281229](https://openairdocs.org/sdr/9900281229), Jan 27, 1999: BATTERY. DISCHARGED. DURING LINE CHECK, FOUND EMERGENCY PATH LIGHTS OUT IN FORWARD AFT SECTION OF CABIN. REPLACED BATTERY SOURCE, OPERATIONAL CHECK OK. - [SDR 9807611229](https://openairdocs.org/sdr/9807611229), Apr 24, 1998: COMPUTER. FAILED. AFTER DEPARTING, THE NR 1 AUTO PILOT OR ATS WOULD NOT ENGAGE. NR 2 AUTO PILOT WOULD ENGAGE BUT WOULD NOT TRIM. FLIGHT RETURNED TO AMS AND LANDED WITHOUT INCIDEN - [SDR 9717951229](https://openairdocs.org/sdr/9717951229), Sep 22, 1997: WIRE. FAILED. DURING CLIMB, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED. FLIGHT RETURNED TO MSP. MAINTENANCE REPLACED WIRES FOR THE AFT UPPER MANIFOLD LOOP. - [SDR 9715331229](https://openairdocs.org/sdr/9715331229), Jul 30, 1997: SKIN. CORRODED. DURING H-CHECK, FOUND CORROSION ON SKIN AFT OF CENTER WHEEL WELL FS 1509 TO 1531, LONGERON 47L TO 47R. REPAIRED PER EA 12-150737. - [SDR 9707451229](https://openairdocs.org/sdr/9707451229), Apr 13, 1997: FAIL LIGHT. ILLUMINATED. DURING CRUISE, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED. AIRCRAFT RETURNED TO HNL. MAINTENANCE DEFERRED PER MEL 36-10A- AND MOVED LIVE ANIMAL TO FORWARD CARGO C - [SDR 9627021229](https://openairdocs.org/sdr/9627021229), Dec 24, 1996: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK, THE AFT EMERGENCY LIGHT POWER SUPPLY FAILED TEST. REPLACED AFT EMERGENCY LIGHT POWER SUPPLY (EMBS139-2) AND THE BATTERY (EMSE299). - [SDR 9617381229](https://openairdocs.org/sdr/9617381229), Aug 10, 1996: TRANSMITTER. FAILED. DURING TAKEOFF ROLL, THE WARNING HORN SOUNDED WITH 15 DEGREE FLAPS, 21 DEGREE TRIM, AND SPEED BRAKES FULL FORWARD. MAINTENANCE REPLACED THE LEFT OUTBOARD FLAP P - [SDR 9617031229](https://openairdocs.org/sdr/9617031229), Aug 5, 1996: FUEL FILTER. CLOGGED. DURING TAKEOFF ROLLOUT, THE NR 1 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECT - [SDR 9609101229](https://openairdocs.org/sdr/9609101229), Apr 17, 1996: ENGINE. FAILED. DURING TAXI TO RAMP, THE NR 3 ENGINE WAS SHUTDOWN DUE TO FUEL LEAKING OUT OF FRONT OF COMPRESSOR. REPLACED NR 3 ENGINE AFTER REPLACING THE FUEL/OIL EXCHANGER AN - [SDR 96ZZZM999](https://openairdocs.org/sdr/96ZZZM999), Apr 16, 1996: ATTACH FITTING. CORROSION. DURING CHECK, LEFT MLG FIXED SIDE BRACE ATTACH BOLT HOLE SHOWS EVIDENCE OF CORROSION IN TRAP FITTING. REPAIRED LEFT MLG FIXED SIDE BRACE ATTACH FITTING INBOARD - [SDR 96ZZZM1005](https://openairdocs.org/sdr/96ZZZM1005), Apr 16, 1996: ATTACH FITTING. CORROSION. DURING CHECK, TRAPEZOIDAL OUTBOARD FITTING SIDE BRACE ATTACH POINT BARREL NUT HOLE CORRODED RIGHT SIDE. REPAIRED OUTBOARD TRAPEZOIDAL SIDE BRACE ATTACH POINT BA - [SDR 96ZZZM1002](https://openairdocs.org/sdr/96ZZZM1002), Apr 16, 1996: ATTACH FITTING. CORROSION. DURING CHECK, RIGHT MLG SIDE (FIXED) ATTACH FITTING INBOARD BOLT BARREL NUT HOLE IS BLEEDING RUST. REPAIRED MLG SIDE BRACE ATTACH FITTING BARREL/NUT HOLE INBOAR - [SDR 96ZZZM1001](https://openairdocs.org/sdr/96ZZZM1001), Apr 16, 1996: TRAPEZOIDAL FTG. CORROSION. DURING CHECK, LEFT MLG FIXED SIDE BRACE ATTACH FITTING INBOARD ATTCH BOLT HOLE SHOW EVIDENCE OF CORROSION IN TRAP FITTING. REPAIRED BOLT HOLE ON LEFT MLG FIXED - [SDR 96ZZZM1000](https://openairdocs.org/sdr/96ZZZM1000), Apr 16, 1996: TRAPEZOIDAL FTG. CORROSION. DURING CHECK, RIGHT MLG FIXED SIDE BRACE ATTACH FITTING INBOARD ATTACH BOLT HOLE SHOWS EVIDENCE OF CORROSION IN TRAP FITTING. REMOVED CORROSION AND REPAIRED INB - [SDR 96ZZZM1003](https://openairdocs.org/sdr/96ZZZM1003), Mar 19, 1996: LONGERON. CRACKED. DURING CHECK, AFT BULK CARGO STRINGER 42R HAS 4 INCH CRACK AND 4 SQUARE INCHES OF INTERGRANULAR CORROSION ON INBOARD SIDE OF STRINGER 42R AT SPLICE FS 1877. REM - [SDR 96ZZZM1004](https://openairdocs.org/sdr/96ZZZM1004), Mar 11, 1996: LONGERON. CORROSION. DURING CHECK 53 SQUARE INCHES OF INTERGRANULAR CORROSION ON LONGERON 38 LEFT AFT FS 791-798 AND AT FS 807-824, LONGERON IS IN SKIN AND LONGERON INSTALLATION. RE - [SDR 96ZZZX920](https://openairdocs.org/sdr/96ZZZX920), Jan 9, 1996: PANEL. CRACKED. DURING L-CHECK, FOUND RIGHT MLG WHEELWELL OUTBOARD PANEL IN SCW 118, FS 1420, HAS A .50 INCH CRACK IN LEFT CORNER. FABRICATED DOUBLER, STOP DRILLED CRACK, SEALE ## Other aircraft with N229NW - [Registered now](https://openairdocs.org/aircraft/N229NW): DJI AGRAS T100, S/N 1872 --- 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.