N220AU
Registered owner: RUNAMUCK LLC, LA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
27 reports on file, 2010-12-01 – 2015-04-29.
Part: SKIN — CORRODED (BS 1521-1561) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE INSTALLATION AT BS 1521 - 1561.
Part: SKIN — CORRODED (BS 874) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 874. REF NRC A011633.
Part: SKIN — CORRODED (BS 603) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 603 REF NRC A011632.
Part: SKIN — CORRODED (BS 1521-1541) · airframe 37,228 hrs · 10,753 cycles
CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE INSTALLATION AT STA 1521 TO 1541.
Part: SKIN — CORRODED (BS 1119-1139) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION MAIN CABIN LH SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE INSTALLATION AT BS 1119 TO 1139.
Part: SKIN — CORRODED (BS 1099-1119) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER DUE TO IMPROPER WINDOW PANE SEAL INSTALLATION BETWEEN BS 1099 TO 1119.
Part: SKIN — CORRODED (BS 1219-1239) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT STA 1219 TO 1239.
Part: SKIN — CORRODED (BS 522) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT STA 522
Part: SKIN — CORRODED (BS 884) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION ON MAIN CABIN LT SIDE WINDOW BELT DOUBLER AT BS 884 .
Part: SKIN — CORRODED (BS 1681-1701) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION ON MAIN CABIN RT SIDE WINDOW BELT DOUBLER FROM IMPROPER WINDOW PANE SEAL INSTALLATION AT BS 1681 TO 1701.
Part: SKIN — CORRODED (BS 1139-1179) · corrosion level 2 · airframe 37,228 hrs · 10,753 cycles
CORROSION FOUND ON LH CABIN WINDOW BELT DOUBLERS AT STA 1139 AND 1179 DUE TO IMPROPER WINDOW SEAL INSTALLATION REF NRC#A011277
Earlier reports · 2010–2011 · 16 reports
2011
Part: SKIN — CORRODED (BS 1921 L45-48L) · airframe 36,916 hrs · 10,657 cycles
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 FIGURE 6 REVISION 97. FABRICATED INNER EXTERNAL DOUBLER AND OUTER EXTERNAL DOUBLER PER SRM 53-20-00 FIGURE 6 VOLUME I REVISION 97. FABRICATED FINGER DOUBLER PER SRM 53-20-00 FIGURE 6 VOLUME I REVISION 97. INSTALLED INNER EXTERNAL DOUBLER, OUTER EXTERNAL DOUBLER, FINGER DOUBLER AND FILLERS AT STA 1921 PER SRM 51-31-01 VOLUME II REVISION 97.
Part: SKIN — CORRODED (BS 1701 L46-47L) · airframe 36,916 hrs · 10,657 cycles
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 SRM 53-20-00 VOLUME I FIGURE 6 REVISION 97. FABRICATED INNER EXTERNAL DOUBLER AND OUTER EXTERNAL DOUBLER PER SRM 53-20-00 FIGURE 6 VOLUME I REVISION 97. FABRICATED FINGER DOUBLER AS FIGURE 6 PER SRM 53-20-00 VOLUME I REVISION 97. INSTALLED INNER EXTERNAL DOUBLER, OUTER EXTERNAL DOUBLER, FINGER DOUBLER AND FILLERS AT STA 1921 AS PER SRM 51-31-01 VOLUME II REVISION 97.
Part: SPAR CAP — CORRODED (WING) · airframe 36,916 hrs · 10,657 cycles
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.
Part: SKIN — CORRODED (ZONE 300) · airframe 36,916 hrs · 10,657 cycles
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.
Part: STRUCTURE — CORRODED (NR 1 NACELLE) · airframe 36,916 hrs · 10,657 cycles
EVIDENCE OF CORROSION ON BOTH STREAKES ON NR 1 ENGINE COWLING EVALUATE CORROSION. COMPLIED WITH EA DC10-7110-1169.
Part: SPAR — CORRODED (ZONE 300) · airframe 36,916 hrs · 10,657 cycles
LT WING INNER REAR SPAR APPROX STA XORS 264 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1131.
Part: STRUCTURE — CRACKED (RT ELEVATOR) · airframe 36,916 hrs · 10,657 cycles
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 FILLER AS PER DC-10 SRM 55-00-01 FIGURE 7 VOLUME I (UPPER AND LOWER SURFACE ELEVATOR SKIN REPAIR) REVISION 97.
Part: SPAR CAP — CORRODED (ZONE 300) · airframe 36,916 hrs · 10,657 cycles
LT WING INNER REAR SPAR APPROX STA XORS 197 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1132.
Part: SPAR CAP — CORRODED (ZONE 300) · airframe 36,916 hrs · 10,657 cycles
RT HORZ STAB FRONT SPAR INTERIOR LOWER SURFACE FOUND WITH CORROSION AT STA APPROX XE 44 - XE 67. COMPLIED WITH EN 1003-11.
Part: SPAR CAP — CORRODED (ZONE 300) · airframe 36,916 hrs · 10,657 cycles
LT HORZ STAB FRONT SPAR LOWER ANGLE STRAP AT STA XE 57 FOUND WITH CORROSION IN SEVERAL LOCATION. COMPLIED WITH EA DC10-5510-1140.
Part: SUPPORT BRACKET — CORRODED (ZONE 500) · airframe 36,916 hrs · 10,657 cycles
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 II.
Part: SPAR CAP — CORRODED (ZONE 300) · airframe 36,916 hrs · 10,657 cycles
LEFT HORIZONTAL STAB FRONT SPAR UPPER ANGLE STRAP AT STA XE 57 FOUND WITH CORROSION IN SEVERAL LOCATION. COMPLIED WITH EA DC10-5510-1140.
Part: RETAINER — CORRODED (ZONE 300) · airframe 36,916 hrs · 10,657 cycles
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 PER DC-10 SRM 51-31-01 REVISION 97 VOLUME II.
Part: BALANCE WEIGHT — CRACKED (ZONE 300) · airframe 36,916 hrs · 10,657 cycles
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 FIGURE 3 VOLUME I REVISION 97 USING MATERIAL 7075T6-0.050". INSTALLED REPAIR DOUBLER AND FILLER AS PER SRM 55-00-01 FIGURE 3 VOLUME I REVISION 97.
2010
Part: SPAR CAP — CORRODED (ZONE 300) · corrosion level 2 · airframe 36,916 hrs · 10,657 cycles
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.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 36,916 hrs · 10,657 cycles
(VGQY) RT HORIZ STABILIZER INTEGRAL LOWER CHORD AND STR NR1, STA XE 48.500 TO XE 67.333 FOUND WITH CORROSION.