# Service difficulty reports: N220AU, cancelled Jan 25, 2017 A list on [N220AU, cancelled Jan 25, 2017](https://openairdocs.org/deregistered/N220AU-2017-01-25.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SRXR2015042900001](https://openairdocs.org/sdr/SRXR2015042900001.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > 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.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > 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.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Miscellaneous Structure > 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.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > 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.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Miscellaneous Structure > 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.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Miscellaneous Structure > CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT STA 1219 TO 1239. - [SDR SRXR20150429005](https://openairdocs.org/sdr/SRXR20150429005.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 884. - [SDR SRXR20150429004](https://openairdocs.org/sdr/SRXR20150429004.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 874. REF NRC A011633. - [SDR SRXR20150429003](https://openairdocs.org/sdr/SRXR20150429003.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 603 REF NRC A011632. - [SDR SRXR20150429002](https://openairdocs.org/sdr/SRXR20150429002.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT STA 522 - [SDR SRXR20150429001](https://openairdocs.org/sdr/SRXR20150429001.md): Skin · corroded · Apr 29, 2015 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > 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.md): Skin · corroded · Jan 17, 2011 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > 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 53-00-01 VOLUME I, FIGURE 1A REVISION 97 LIMITS. TRIMMED-OFF CORROSION AREA PER SRM 53-20-00 VOLUME I F - [SDR VGQY2011011700013](https://openairdocs.org/sdr/VGQY2011011700013.md): Skin · corroded · Jan 17, 2011 · N220AU · Doug DC1010 · Fuselage Main, Plate/Skin > 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 FOUND EXCEEDED SRM 53-00-01 VOLUME I, FIGURE 1A REVISION 97 LIMITS. TRIMMED-OFF CORROSION AREA PER - [SDR VGQY2011011500011](https://openairdocs.org/sdr/VGQY2011011500011.md): Structure · cracked · Jan 15, 2011 · N220AU · Doug DC1010 · Elevator Structure > 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 PER DC-10 SRM 55-10-00 FIGURE 7 VOLUME I REVISION 97. INSTALLED FABRICATED REPAIR DOUBLER AND FIL - [SDR VGQY2011011500012](https://openairdocs.org/sdr/VGQY2011011500012.md): Structure · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Nacelle/Pylon, Main Frame > 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.md): Spar Cap · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer, Spar/Rib > 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.md): Retainer · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer Miscellaneous Structure > LEFT LOWER VERTICAL STABILIZER, BELOW AIR INTAKE DUCT FOUND WITH CORROSION AFT OF PANEL 361BL. REMOVED AND DISCARDED CORRODED AJC7331-29 RETAINER. FABRICATED NEW RETAINER PER DWG AJC7331 REQUIREMENTS USING MATERIAL 7075-0-0.125". NEW RETAINER INSTALLED AS P - [SDR VGQY2011011500009](https://openairdocs.org/sdr/VGQY2011011500009.md): Spar Cap · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Wing Spar > 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.md): Spar · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Wing Spar > 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.md): Balance Weight · cracked · Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer Miscellaneous Structure > 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 55-00-01 FIGURE 3 VOLUME I REVISION 97. FABRICATED REPAIR DOUBLER AND FILLER AS PER SRM 55-00-01 - [SDR VGQY2011011500006](https://openairdocs.org/sdr/VGQY2011011500006.md): Spar Cap · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Wing Spar > 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.md): Spar Cap · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer, Spar/Rib > 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.md): Spar Cap · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer, Spar/Rib > 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.md): Support Bracket · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Wing Miscellaneous Structure > 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 LONG BEACH DWG ANB7135 REV A. NEW ANGLE INSTALLED AS PER DC-10 SRM 51-31-01 REVISION 97 VOLUME I - [SDR VGQY2011011500001](https://openairdocs.org/sdr/VGQY2011011500001.md): Skin · corroded · Jan 15, 2011 · N220AU · Doug DC1010 · Horizontal Stabilizer, Plate/Skin > 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.md): Spar Cap · corroded · Dec 1, 2010 · N220AU · Doug DC1010 · Horizontal Stabilizer, Spar/Rib > 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 DC10-5510-1134. - [SDR 2010F00248](https://openairdocs.org/sdr/2010F00248.md): Structure · corroded · Dec 1, 2010 · N220AU · Doug DC1010 · Horizontal Stabilizer Structure > (VGQY) RT HORIZ STABILIZER INTEGRAL LOWER CHORD AND STR NR1, STA XE 48.500 TO XE 67.333 FOUND WITH CORROSION. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N220AU' AND deregistration_id = 'N220AU-2017-01-25' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N220AU-2017-01-25/reports --- 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.