# N211NW: 1974 Mcdonnell-Douglas DC-10-30, registration cancelled 2017-04-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 4, 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: 46868 - Year built: 1974 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 30, 1991 - Certificate issued: May 19, 2006 - Last registry action: September 14, 2009 - Mode S code: A1BE7A - Owner when cancelled: [Picl Aviation IV LLC](https://openairdocs.org/faa-owner/PICL%20AVIATION%20IV%20LLC) - Location: [Miami, FL](https://openairdocs.org/faa-place/FL/Miami) - Owner type: Corporation - Owner's area on the map: 25.7795° N, 80.2996° W: Placed by OpenAirDocs at the center of ZIP code 33126, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N211NW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=211NW - Page: https://openairdocs.org/deregistered/N211NW-2017-04-04 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 (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 0400981221](https://openairdocs.org/sdr/0400981221), Jun 8, 2004: FIRE DETECTOR. MALFUNCTIONED. DURING CRUISE, THE FORWARD CARGO COMPARTMENT NR 2 AND NR 4 SMOKE DETECTOR LIGHTS AND FORWARD CARGO FIRE LIGHT ILLUMINATED. FOLLOWED COM PROCEDURE AND PROCEEDED - [SDR 0200911211](https://openairdocs.org/sdr/0200911211), Feb 24, 2002: STRINGER. CRACKED. During "H" check found cracks on LH horizontal stabilizer outboard aft skin panel integral stringers, #1-7.5 inch crack at stations XE 77.100 and stringer #4-6. - [SDR 0101551211](https://openairdocs.org/sdr/0101551211), Apr 28, 2001: GEARBOX. LEAKING. DURING CRUISE, THE NR 3 ENGINE OIL QUANTITY DECREASED TO ZERO AND OIL PRESSURE DROPPED INTO THE RED WITH THE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED. THE ENG - [SDR 0003821211](https://openairdocs.org/sdr/0003821211), Oct 7, 2000: CONTROL BOX. OVERHEATED. EN ROUTE TO DTW, PASSENGER AT SEAT 30F REPORTED SEAT FRAME HOT AND UNUSUAL SMELL. FOUND MUX CONNECTOR BOX COVER OPEN. RESEATED CONNECTORS AND CLOSED COVER. HEAT - [SDR 9703491211](https://openairdocs.org/sdr/9703491211), Feb 6, 1997: CASTING. CRACKED. DURING TRANSITION CHECK, FOUND CRACK IN THE LEFT INBOARD FLAP INBOARD TRACK ATTACH CASTING. REPAIRED PER EA 12-121503. - [SDR 9703011211](https://openairdocs.org/sdr/9703011211), Feb 3, 1997: SKIN. CRACKED. DURING TRANSITION CHECK, FOUND CRACK AT FORWARD INBOARD CORNER OF CUTOUT SKIN DOOR FUELING PANEL 519CB. REPAIRED PER EA 12-121471. - [SDR 9702271211](https://openairdocs.org/sdr/9702271211), Feb 1, 1997: FITTING. CORRODED. DURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT LBL 27 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01. - [SDR 9702241211](https://openairdocs.org/sdr/9702241211), Feb 1, 1997: FITTING. CORROSION. DURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT RBL 18 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01. - [SDR 9702231211](https://openairdocs.org/sdr/9702231211), Feb 1, 1997: FITTING. CORRODED. DURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT LBL 7 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01. - [SDR 9702281211](https://openairdocs.org/sdr/9702281211), Jan 31, 1997: FITTING. CORRODED. DURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT LBL 21 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01. - [SDR 9702261211](https://openairdocs.org/sdr/9702261211), Jan 31, 1997: FITTING. CORRODED. DURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT RBL 15 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01. - [SDR 9702251211](https://openairdocs.org/sdr/9702251211), Jan 31, 1997: FITTING. CORRODED. DURING TRANSITION CHECK, FOUND CORROSION ON FITTING IN CENTER LANDING GEAR WHEEL WELL AT BL 0 BETWEEN FS 1501 TO 1521. REPLACED FITTING PER SRM 51-33-01. - [SDR 9623431211](https://openairdocs.org/sdr/9623431211), Nov 5, 1996: COMPUTER. FAILED. DURING TAKEOFF, THE STALL WARNING STICK SHAKER ACTIVATED. FLIGHT DUMPED 41,000 POUNDS OF FUEL AND RETURNED TO HNL. MAINTENANCE REPLACED THE AT/SC COMPUTER AND T - [SDR 9615501211](https://openairdocs.org/sdr/9615501211), Jul 17, 1996: COMPRESSOR. STALLED. AFTER TAKEOFF AND DURING CLIMB, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AT 6,000 FEET. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, SHUT DOWN THE ENGINE, DUM - [SDR 9611771211](https://openairdocs.org/sdr/9611771211), May 27, 1996: POWER SUPPLY. INOPERATIVE. DURING LINE INSPECTION, ZONE B, FOUND FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND RETURNED TO SERVICE. - [SDR 9611751211](https://openairdocs.org/sdr/9611751211), May 3, 1996: BATTERY. DISCHARGED. DURING LINE INSPECTION, FOUND THE EMERGENCY LIGHTS WOULD NOT TEST. MAINTENANCE REPLACED THE MID-CABIN BATTERY. - [SDR 9600531211](https://openairdocs.org/sdr/9600531211), Jan 11, 1996: APU. FAILED. DURING CLIMB, A STRONG OIL SMELL WAS PRESENT THROUGH OUT THE AIRCRAFT. FLIGHT CREW FOLLOWED SMOKE REMOVAL PROCEDURES, BUT ODOR COULD NOT BE ISOLATED. FLIGHT RET - [SDR 9520761211](https://openairdocs.org/sdr/9520761211), Nov 23, 1995: DOOR FRAME. CORRODED. DURING LINE CHECK, FOUND CORROSION ON THE CENTER CARGO DOOR JAMB LOWER FORWARD FRAME, FS 1708 AT LONGERON 41R. REPAIRED FRAME (P/N AFA 3873-3) PER EA 12-99308. ## FAA accident and incident reports (2) 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 20000625032189I](https://openairdocs.org/incident/20000625032189I), Jun 25, 2000: Doug DC1030 (N211NW), Newark, NJ, Minor damage. (-23)Northwest airlines DC-10 Boeing pushed back for repositioning off of gate B-52 struck a Continental airlines DC-10 parked at gate B-51. Investigation… - [Incident 20000124000959I](https://openairdocs.org/incident/20000124000959I), Jan 24, 2000: Doug DC1030 (N211NW), Newark, NJ, 1 fatal. (-23) Upon landing mechanic [privacy data omitted] was performing a security check of the aircraft when he noticed a small bag in the forward part of the right… ## Other aircraft with N211NW - [Registered now](https://openairdocs.org/aircraft/N211NW): Bell 205A-1, S/N 30177, built 1975 --- 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.