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Printed page label not indexed. PDF page 37.
door. Examination of the latch actuator of the aft cargo door on the left-hand side The irreversible actuator was taken off the door. The two bolts which attach the bracket on which it is mounted, were found sheared: the shearingOpen official document at PDF page 37French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page label not indexed. PDF page 43.
Restraining flange lock pin 7# terque tube stop “ latch hook a Overecentre achieved System irreversible Correct closure 38 Engegement of ©} lock pins impossiblé of actuator sheft Over~centre not achieve! System reversible Incorrect closure Fixecl points on the structureOpen official document at PDF page 43French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page 43. PDF page 48.
actuator withstood the compression force without displacement of its shaft, since it is irreversible. It therefore transmitted the force from the 4 latches to the two bolts (titanium 0.25 inch in diameter) which attach its fixed part to the doorOpen official document at PDF page 48French Commission of Inquiry final report: Turkish Airlines DC-10 TC-JAV, official UK-hosted English translation
Printed page 109. PDF page 111.
integrity and validate the needle positions. The mechanisms were demonstrated to be irreversible during certification tests, that is to say that leaning on the armrest did not modify the adjustments made with the knobs. 109 F-GZCP - 1st June 2009Open official document at PDF page 111Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447