PROJECT ORBIS INTERNATIONAL
Also recorded as: ORBIS, PROJECT ORBIS INTERNATIONAL
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
No NTSB accidents or incidents linked to this operator.
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
15 reports on file.
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.
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.
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.
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.
LEFT HORIZONTAL STAB FRONT SPAR UPPER ANGLE STRAP AT STA XE 57 FOUND WITH CORROSION IN SEVERAL LOCATION. COMPLIED WITH EA DC10-5510-1140.
LT HORZ STAB FRONT SPAR LOWER ANGLE STRAP AT STA XE 57 FOUND WITH CORROSION IN SEVERAL LOCATION. COMPLIED WITH EA DC10-5510-1140.
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.
LT WING INNER REAR SPAR APPROX STA XORS 197 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1132.
LT WING INNER REAR SPAR APPROX STA XORS 264 FOUND EXTRUSION CORRODED. COMPLIED WITH EA DC10-5710-1131.
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.
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.
RT HORZ STAB FRONT SPAR INTERIOR LOWER SURFACE FOUND WITH CORROSION AT STA APPROX XE 44 - XE 67. COMPLIED WITH EN 1003-11.
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.
EVIDENCE OF CORROSION ON BOTH STREAKES ON NR 1 ENGINE COWLING EVALUATE CORROSION. COMPLIED WITH EA DC10-7110-1169.
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.
Linked aircraft
No aircraft currently linked.