# N220AU: 1971 Mcdonnell Douglas DC-10-10, registration cancelled 2017-01-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 25, 2017 - Status when cancelled: Second renewal notice - Airframe: [Mcdonnell Douglas DC-10-10](https://openairdocs.org/model/mcdonnell-douglas-dc-10-10) (registry code 3022110) - Engine: [GE CF6-6 series](https://openairdocs.org/engine/ge-cf6-6-series) (registry code 30020) - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 46501 - Year built: 1971 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 16, 1991 - Certificate issued: February 2, 1995 - Last registry action: January 8, 2014 - Mode S code: A1E114 - Owner when cancelled: [Project Orbis International Inc](https://openairdocs.org/faa-owner/PROJECT%20ORBIS%20INTERNATIONAL%20INC) - Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York) - Owner type: Corporation - Owner's area on the map: 40.7553° N, 73.9927° W: Placed by OpenAirDocs at the center of ZIP code 10018, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N220AU - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=220AU - Page: https://openairdocs.org/deregistered/N220AU-2017-01-25 From the FAA registry file of October 31, 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-10-10: https://openairdocs.org/model/mcdonnell-douglas-dc-10-10.md ## Service difficulty reports (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR SRXR2015042900001](https://openairdocs.org/sdr/SRXR2015042900001), Apr 29, 2015: SKIN. CORRODED. CORROSION MAIN CABIN LH SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE INSTALLATION AT BS 1119 TO 1139. - [SDR SRXR20150429010](https://openairdocs.org/sdr/SRXR20150429010), Apr 29, 2015: SKIN. CORRODED. CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE SEAL INSTALLATION BETWEEN BS 1099 TO 1119. - [SDR SRXR20150429009](https://openairdocs.org/sdr/SRXR20150429009), Apr 29, 2015: SKIN. CORRODED. CORROSION ON MAIN CABIN RT SIDE WINDOW BELT DOUBLER FROM IMPROPER WINDOW PANE SEAL INSTALLATION AT BS 1681 TO 1701. - [SDR SRXR20150429008](https://openairdocs.org/sdr/SRXR20150429008), Apr 29, 2015: SKIN. CORRODED. CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE INSTALLATION AT BS 1521 - 1561. - [SDR SRXR20150429007](https://openairdocs.org/sdr/SRXR20150429007), Apr 29, 2015: SKIN. CORRODED. CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE INSTALLATION AT STA 1521 TO 1541. - [SDR SRXR20150429006](https://openairdocs.org/sdr/SRXR20150429006), Apr 29, 2015: SKIN. CORRODED. CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT STA 1219 TO 1239. - [SDR SRXR20150429005](https://openairdocs.org/sdr/SRXR20150429005), Apr 29, 2015: SKIN. CORRODED. CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 884 . - [SDR SRXR20150429004](https://openairdocs.org/sdr/SRXR20150429004), Apr 29, 2015: SKIN. CORRODED. CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 874. REF NRC A011633. - [SDR SRXR20150429003](https://openairdocs.org/sdr/SRXR20150429003), Apr 29, 2015: SKIN. CORRODED. CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 603 REF NRC A011632. - [SDR SRXR20150429002](https://openairdocs.org/sdr/SRXR20150429002), Apr 29, 2015: SKIN. CORRODED. CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT STA 522 - [SDR SRXR20150429001](https://openairdocs.org/sdr/SRXR20150429001), Apr 29, 2015: SKIN. CORRODED. CORROSION FOUND ON LH CABIN WINDOW BELT DOUBLERS AT STA 1139 AND 1179 DUE TO IMPROPER WINDOW SEAL INSTALLATION REF NRC#A011277 - [SDR VGQY2011011700014](https://openairdocs.org/sdr/VGQY2011011700014), Jan 17, 2011: SKIN. CORRODED. SKIN CORROSION FOUND ON FRAME STA 1921 LT SIDE - BETWEEN LONGERON 45L-48L. REMOVED CORROSION PER SRM 51-21-01 VOLUME II REVISION 97 AND FOUND EXCEEDED SRM 53-00 - [SDR VGQY2011011700013](https://openairdocs.org/sdr/VGQY2011011700013), Jan 17, 2011: SKIN. CORRODED. SURFACE CORROSION FOUND AT FRAME STA 1701 - LONGERONS L 46 & L 47. REMOVED CORROSION AT STA 1701 LONGERON 46L TO 47L PER SRM 51-21-01 VOLUME II REVISION 97 AND - [SDR VGQY2011011500011](https://openairdocs.org/sdr/VGQY2011011500011), Jan 15, 2011: STRUCTURE. CRACKED. RT HORZ STAB I/B ELEVATOR LOWER O/B FWD EDGE FOUND CRACKED. TRIMMED OUT CRACKED AREA ON RT HORIZONTAL STABILIZER INBOARD ELEVATOR LOWER OUTBOARD FORWARD EDGE AS - [SDR VGQY2011011500012](https://openairdocs.org/sdr/VGQY2011011500012), Jan 15, 2011: STRUCTURE. CORRODED. EVIDENCE OF CORROSION ON BOTH STREAKES ON NR 1 ENGINE COWLING EVALUATE CORROSION. COMPLIED WITH EA DC10-7110-1169. - [SDR VGQY2011011500010](https://openairdocs.org/sdr/VGQY2011011500010), Jan 15, 2011: SPAR CAP. CORRODED. RT HORZ STAB FRONT SPAR INTERIOR LOWER SURFACE FOUND WITH CORROSION AT STA APPROX XE 44 - XE 67. COMPLIED WITH EN 1003-11. - [SDR VGQY2011011500008](https://openairdocs.org/sdr/VGQY2011011500008), Jan 15, 2011: RETAINER. CORRODED. LEFT LOWER VERTICAL STABILIZER, BELOW AIR INTAKE DUCT FOUND WITH CORROSION AFT OF PANEL 361BL. REMOVED AND DISCARDED CORRODED AJC7331-29 RETAINER. FABRICATED NE - [SDR VGQY2011011500009](https://openairdocs.org/sdr/VGQY2011011500009), Jan 15, 2011: SPAR CAP. CORRODED. RT MAIN LANDING GEAR WHEEL WELL - FOUND CORROSION AT OUTER WING REAR SPAR CAP, UPPER SIDE-BOTTOM SURFACE - STA XORS 118.200. COMPLIED WITH EA DC10-5730-1133. - [SDR VGQY2011011500007](https://openairdocs.org/sdr/VGQY2011011500007), Jan 15, 2011: SPAR. CORRODED. LT WING INNER REAR SPAR APPROX STA XORS 264 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1131. - [SDR VGQY2011011500005](https://openairdocs.org/sdr/VGQY2011011500005), Jan 15, 2011: BALANCE WEIGHT. CRACKED. LT HORZ STAB O/B ELEVATOR BALANCE WEIGHT AFT EDGE FOUND WITH ONE (1) INCH CRACKED. TRIMMED OUT DAMAGED AREA ON LT HORIZONTAL STABILIZER FAIRING AS PER DC-10 SRM - [SDR VGQY2011011500006](https://openairdocs.org/sdr/VGQY2011011500006), Jan 15, 2011: SPAR CAP. CORRODED. LT WING INNER REAR SPAR APPROX STA XORS 197 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1132. - [SDR VGQY2011011500004](https://openairdocs.org/sdr/VGQY2011011500004), Jan 15, 2011: SPAR CAP. CORRODED. LT HORZ STAB FRONT SPAR LOWER ANGLE STRAP AT STA XE 57 FOUND WITH CORROSION IN SEVERAL LOCATION. COMPLIED WITH EA DC10-5510-1140. - [SDR VGQY2011011500003](https://openairdocs.org/sdr/VGQY2011011500003), Jan 15, 2011: SPAR CAP. CORRODED. LEFT HORIZONTAL STAB FRONT SPAR UPPER ANGLE STRAP AT STA XE 57 FOUND WITH CORROSION IN SEVERAL LOCATION. COMPLIED WITH EA DC10-5510-1140. - [SDR VGQY2011011500002](https://openairdocs.org/sdr/VGQY2011011500002), Jan 15, 2011: SUPPORT BRACKET. CORRODED. UPPER LT WING-TO-FUSELAGE AREA FS 1119 - FOUND 1 EA SUPPORT BRACKET WITH CORROSION. REMOVED AND DISCARDED CORRODED ANB7135-5 ANGLE. FABRICATED NEW ANGLE PER DWG - [SDR VGQY2011011500001](https://openairdocs.org/sdr/VGQY2011011500001), Jan 15, 2011: SKIN. CORRODED. LT HORIZONTAL STAB LEADING EDGE MOST I/B SECTION FOUND INTERNAL STRUCTURE LOWER AND UPPER SURFACE WITH CORROSION. COMPLIED WITH EN 1318-10 AND EA DC10-5510-1130 - [SDR VGQY2012120100132](https://openairdocs.org/sdr/VGQY2012120100132), Dec 1, 2010: SPAR CAP. CORRODED. RIGHT HORIZONTAL STABILIZER INTEGRAL LOWER CHORD AND STRINGER NR 1, STA XE 48.500 TO XE 67.333 FOUND WITH EXFOLIATION CORROSION. COMPLIED WITH ORBIS EA DC10-551 - [SDR 2010F00248](https://openairdocs.org/sdr/2010F00248), Dec 1, 2010: STRUCTURE. CORRODED. (VGQY) RT HORIZ STABILIZER INTEGRAL LOWER CHORD AND STR NR1, STA XE 48.500 TO XE 67.333 FOUND WITH CORROSION. ## Other aircraft with N220AU - [Registered now](https://openairdocs.org/aircraft/N220AU): Piper PA-44-180, S/N 4496617, built 2025 --- 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.