# N236NW: 1974 Mcdonnell-Douglas DC-10-30, registration cancelled 2007-11-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 28, 2007
- Status when cancelled: Valid registration
- 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: 46934
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 7, 1998
- Certificate issued: November 2, 2006
- Last registry action: November 2, 2006
- Mode S code: A2200B
- Owner when cancelled: [Omni Air International Inc](https://openairdocs.org/faa-owner/OMNI%20AIR%20INTERNATIONAL%20INC)
- Location: [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa)
- Owner type: Corporation
- Owner's area on the map: 36.1993° N, 95.9089° W: Placed by OpenAirDocs at the center of ZIP code 74115, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N236NW
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=236NW
- Page: https://openairdocs.org/deregistered/N236NW-2007-11-28

From the FAA registry file of November 12, 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 (8)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 0600751236](https://openairdocs.org/sdr/0600751236), Apr 20, 2006: FLOORBEAM. CORRODED. DURING LINE CHECK DISCOVERED CORROSION ON FORWARD CARGO DOOR SCUFF PLATE. THE CORROSION HAS PUSHED UP THE FUSELAGE SKIN AND IT APPEARS THERE ARE CRACKS AND CORR
- [SDR 0600601236](https://openairdocs.org/sdr/0600601236), Mar 24, 2006: SMOKE DETECTOR. FALSE INDICATION. EN ROUTE TO MSP FROM AMS, AFT CARGO FIRE WARNING ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND DIVERTED TO KEF FOR AN UNEVENTFUL LANDING. VISUAL INSPECTION OF AF
- [SDR 0501491236](https://openairdocs.org/sdr/0501491236), Sep 22, 2005: POWER SUPPLY. INOPERATIVE. DURING LINE CHECK MAINTENANCE FOUND LT AND RT EMERGENCY LIGHTS INOP ROWS 10 TO 20 ZONE B. REPLACED POWER SUPPLY AND OPERATION CHECKS GOOD. 
- [SDR 0501041236](https://openairdocs.org/sdr/0501041236), Jul 17, 2005: CONTROLLER. MALFUNCTIONED. EN ROUTE FROM FCO TO DTW CREW NOTICED FUEL CONSUMPTION MUCH HIGHER THAN FLIGHT PLAN PREDICTION. APPROX 2000 LBS/HR. FLIGHT DIVERTED TO AMS AND LANDED WITHOUT IN
- [SDR 0500051236](https://openairdocs.org/sdr/0500051236), Jan 12, 2005: ENGINE. FAILED. WHILE AT CRUISE, THE CREW REPORTED THE NR 3 ENGINE FAILED WITH NO INDICATION OF OIL PRESSURE OR N2 SPEED. THE CREW SECURED THE ENGINE PER COM AND CONTINUED TO A
- [SDR 0300691236](https://openairdocs.org/sdr/0300691236), Apr 2, 2003: RESERVOIR. DISCHARGED. DURING SLIDE SHOP TEST FOUND RESERVOIR COMPLETELY DEFLATED. FIRING LANYARD WAS INTACT. CAUSE OF CYLINDER DEFLATION COULD NOT BE DUPLICATED. INSTALLED OVERHAULED
- [SDR 0002411236](https://openairdocs.org/sdr/0002411236), Jul 9, 2000: PUMP. FAILED. DURING CRUISE, NR 2 HYDRAULIC PRESSURE BEGAN TO FLUCTUATE AND EVENTUALLY DROPPED TO ZERO. FLIGHT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 2 ENGINE HYDRAUILC
- [SDR 9802411236](https://openairdocs.org/sdr/9802411236), Feb 6, 1998: FITTING. CORRODED. DURING M CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON END FITTING FOR LONGERON 45L, FS 1811. REPLACED END FITTING PER SRM 51-33-01, VOL 1.

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