# Service difficulty reports: Mcdonnell Douglas DC-10-10

A list on [Mcdonnell Douglas DC-10-10](https://openairdocs.org/model/mcdonnell-douglas-dc-10-10.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 77 · 3,826 reports

- [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 2013FA0000705](https://openairdocs.org/sdr/2013FA0000705.md): Engine · seized · Aug 15, 2013 · N450AX · Doug DC1010 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE HAD SUDDEN SEIZURE, NO FIRE INDICATION, PRECEDED BY LOAD BANG, PERFORMED EMERGENCY PROCEDURES.
- [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.
- [SDR 2010FA0000040](https://openairdocs.org/sdr/2010FA0000040.md): Valve · separated · Jan 15, 2010 · N910SF · Doug DC1010 · Hydraulic System, Main
  > THIS IS TO REPORT A LOSS OF NR 2 HYD SYS "PRESSURE AND QUANTITY" PRIOR TO TAKE-OFF, ACFT RETURNED TO GATE. INVESTIGATION FOUND VALVE ASY (M1-164) FOR THE 2-1 NON-REVERSIBLE MOTOR PUMP TO BE AT FAULT. REF IPC 29-12-59, FIG 1, PG 9, ITEM 340, PN 148995-1, SN 3
- [SDR FDEA200809123854](https://openairdocs.org/sdr/FDEA200809123854.md): Skin · cracked · Sep 12, 2008 · N10060 · Doug DC1010 · Wing, Plate/Skin
  > LT WING L/E FOUND CRACK ON LOWER EXT SKIN L/E. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.
- [SDR 08FDEA03854](https://openairdocs.org/sdr/08FDEA03854.md): Skin · cracked · Sep 12, 2008 · N10060 · Doug DC1010 · Wing, Plate/Skin
  > LT WING L/E FOUND CRACK ON LOWER EXT SKIN L/E.
- [SDR 08FDEA03636](https://openairdocs.org/sdr/08FDEA03636.md): Seat Track · corroded · Aug 29, 2008 · N40061 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK AT STA 1923 X=-57, Z=-19. REPAIR IAW SRM 53-70-00 VOL 1 FIG 13 SHEET 1-2.
- [SDR ARWA20080803](https://openairdocs.org/sdr/ARWA20080803.md): Windshield · shorted · Aug 29, 2008 · N68041 · Doug DC1010 · Windshield/Door Rain/Ice Removal
  > FIRST OFFICER`S WINDSHIELD STARTED ARCING, POWER REMOVED. OUTER PANEL CRACKED, CHECK LIST COMPLETED. REMOVED AND REPLACED FIRST OFFICER`S WINDSHIELD PANEL IAW DC-10 MM 56-11-00, OPERATIONAL CHECK NORMAL. REMOVED AND REPLACED RT WINDOW HEAT CONTROLLER IAW MM
- [SDR 08FDEA03381](https://openairdocs.org/sdr/08FDEA03381.md): Access Panel · cracked · Aug 12, 2008 · N10060 · Doug DC1010 · Nacelle/Pylon, Main Frame
  > AFTER REMOVAL ACCESS PANELS OF PYLON NR 3 WITH OAN J/C 0600B430-1JR FOUND CRACK ON HORIZ WEB UPPER. REPAIRED CRACK IAW SRM 54-00-01 FIG 2B SHT 2 VOL I.
- [SDR FDEA200808083319](https://openairdocs.org/sdr/FDEA200808083319.md): Frame · corroded · Aug 8, 2008 · N10060 · Doug DC1010 · Fuselage Main, Frame
  > AIR CONDITIONING COMPT PACK NR 1, FOUND EXFOLIATION CORROSION ON CAP ANGLE AND CLIP. REPAIRED AREA IAW SRM 53-00-01 FIG 8 SHT 1, 3, 4 VOL I.
- [SDR 08FDEA03319](https://openairdocs.org/sdr/08FDEA03319.md): Angle · corroded · Aug 8, 2008 · N10060 · Doug DC1010 · APU Cowling/Containment
  > AIR CONDITIONING COMPT PACK NR 1, FOUND EXFOLIATION CORROSION ON CAP ANGLE AND CLIP.
- [SDR 08FDEA03255](https://openairdocs.org/sdr/08FDEA03255.md): Skin · worn · Aug 5, 2008 · N10060 · Doug DC1010 · Wing, Plate/Skin
  > RT WING L/E DROOPED FOUND DEEP WEAR ON EXT SKIN. REPAIRED AREA IAW SRM 57-10-00 VOL I FIG 39.
- [SDR 08FDEA03101](https://openairdocs.org/sdr/08FDEA03101.md): Skin · cracked · Jul 28, 2008 · N40061 · Doug DC1010 · Horizontal Stabilizer, Plate/Skin
  > DURING INSP OF HORIZ STAB UPPER AND LOWER CONSTANT SECTION SKIN PLANK FLANGE, FOUND 4 PANEL WITH CRACK IN FLYABLE LIMIT, P/N 7208-1, P/N 7207-1, P/N 7205-1, P/N 7204-1, SEE ATTACHED INSPECTION FINDING FORM. REPAIRED AREA IAW EA NR 8-5510-120477.
- [SDR FDEA200807233028](https://openairdocs.org/sdr/FDEA200807233028.md): Seat Track · corroded · Jul 23, 2008 · N10060 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION AFTER REMOVAL FLOOR PANEL WITH OAN J/C 0600C180-1JR FOUND SEVERE CORROSION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 SHT 1-4 VOL I.
- [SDR 08FDEA03028](https://openairdocs.org/sdr/08FDEA03028.md): Seat Track · corroded · Jul 23, 2008 · N10060 · Doug DC1010 · Fuselage, Seat/Cargo Attach Fittings
  > DURING INSPECTION AFTER REMOVAL FLOOR PANEL WITH OAN J/C 0600C180-1JR FOUND SEVERE CORROSION ON SEAT TRACK.
- [SDR 08FDEA03025](https://openairdocs.org/sdr/08FDEA03025.md): Fitting · cracked · Jul 23, 2008 · N40061 · Doug DC1010 · Trailing Edge Flaps
  > RT WING OUTBD FLAP CRACK ON FITTING. REPAIRED AREA IAW EA 8-5750-120139.
- [SDR ARWA20080701](https://openairdocs.org/sdr/ARWA20080701.md): B-Nut · loose · Jul 17, 2008 · N68041 · Doug DC1010 · Rudder Control System
  > NR 1 HYDRAULIC SYSTEM LOSS PRESSURE AND QUANTITY ZERO. RUDDER STAND-BY POWER OFF, IGHT ON. REPAIRED LINE AND FOUND LOOSE B-NUT AT LT HORIZONTAL STABILIZER TRIM MOTOR. TIGHTENED B-NUT IAW DEIO M/M 20-10-0. PERFORMED OPERATIONAL CHECK, FOUND NORMAL IAW DEIO
- [SDR 08FDEA02957](https://openairdocs.org/sdr/08FDEA02957.md): Skin · cracked · Jul 17, 2008 · N40061 · Doug DC1010 · Wing, Plate/Skin
  > LT WING OUTBD FLAP CRACK ON LOWER SKIN. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I.
- [SDR 08FDEA02836](https://openairdocs.org/sdr/08FDEA02836.md): Web · cracked · Jul 12, 2008 · N40061 · Doug DC1010 · Nacelle/Pylon Miscellaneous Structure
  > AFTER REMOVAL ACCESS PANEL ON PYLON NR 3 WITH OAN J/C 0600B430-1JR FOUND HORIZ WEB WITH CRACKS. REPAIRED CRACKS IAW SRM 54-00-01 FIG 2B SHT 2 & FIG 13 SHT 6 VOL I.
- [SDR 08FDEA02704](https://openairdocs.org/sdr/08FDEA02704.md): Bracket · cracked · Jul 4, 2008 · N40061 · Doug DC1010 · Wing, Attach Fittings
  > PERFORMED INSP AFTER REMOVAL PANEL RT WING WITH OAN J/C MD10-2780620-1JR FOUND NR 3 CRACKS ON BRACKETS, RT WING DROOPED LEADING EDGE INTERNAL SIDE. REPAIRED AREA IAW SRM 57-00-01 FIG 10 SHT 1 VOL I.
- [SDR 08FDEA02632](https://openairdocs.org/sdr/08FDEA02632.md): Skin · cracked · Jul 2, 2008 · N40061 · Doug DC1010 · Wing, Plate/Skin
  > LT WING L/E CHORD FIXED PANEL FOUND CRACK. REPAIRED WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL I.
- [SDR FDEA200806302577](https://openairdocs.org/sdr/FDEA200806302577.md): Skin · corroded · Jun 30, 2008 · N10060 · Doug DC1010 · Spoilers
  > RT WING T/E MODERATE CORROSION ON LOWER SKIN SPOILER NR 2. NO ACTION TAKEN SPOILER WILL BE REPLACED WITH NRC N01190.
- [SDR FDEA200806302576](https://openairdocs.org/sdr/FDEA200806302576.md): Longeron · corroded · Jun 30, 2008 · N10060 · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT TUNNEL AREA FOUND CORROSION WITH EXFOLIATION. REPAIRED AREA IAW SRM 53-00-01 FIG 9 VOL I.
- [SDR 08FDEA02577](https://openairdocs.org/sdr/08FDEA02577.md): Skin · corroded · Jun 30, 2008 · N10060 · Doug DC1010 · Spoilers
  > RT WING T/E MODERATE CORROSION ON LOWER SKIN SPOILER NR 2.
- [SDR 08FDEA02576](https://openairdocs.org/sdr/08FDEA02576.md): Longeron · corroded · Jun 30, 2008 · N10060 · Doug DC1010 · Fuselage Main, Longeron/Stringer
  > FWD CARGO COMPT TUNNEL AREA FOUND CORROSION WITH EXFOLIATION.

Next page: https://openairdocs.org/model/mcdonnell-douglas-dc-10-10/reports.md?page=2

## 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 aircraft_model_key = 'DC1010'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/mcdonnell-douglas-dc-10-10/reports

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