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Arrangement adapted to connect a rocker arm device of compensation of the efforts of impulse generated by an aircraft engine to a structure of a display ru00ecgida stirrup of the motor device, compensation of the efforts of impulse generated by an aircraft engine, the stirrup of FA Ixau00e7u00e3o a engine, and,Process for mounting an aircraft engine in a structure of a hanger ru00ecgida display engine
Arrangement adapted to connect a rocker arm device of compensation of the efforts of impulse generated by an aircraft engine to a structure of a display ru00ecgida stirrup of the motor device, compensation of the efforts of impulse generated by an aircraft engine, the stirrup of FA Ixau00e7u00e3o a engine, and,Process for mounting an aircraft engine in a structure of a hanger ru00ecgida display engine
Arrangement adapted to connect a rocker arm device of compensation of the efforts of impulse generated by an aircraft engine to a structure of a display ru00ecgida stirrup of the motor device, compensation of the efforts of impulse generated by an aircraft engine, the stirrup of FA Ixau00e7u00e3o a engine, and,Process for mounting an aircraft engine in a structure of a hanger ru00ecgida display engine.The invention relates to an arrangement (33) adapted to connect to a rocker arm to a rigid structure of a hanger for display of aircraft engine, which comprises a system axis (32) mounted sliding in a first passage (38) of a hardware (34) so as to permit displacement of a Finally, according to the first longitudinal axis.In a first direction from a normal position is extracted to a fallback position in which he is hidden in the same hardware, and vice versa.In addition, the arrangement comprises a u00f3rgu00e1o extension axis (60) driven by the system (32) and capable of being moved parallel to the longitudinal axis in a second direction from a normal position back to a position in which he is supportive of the extracted system (32) and salient in re Lation to this last, and vice versa.
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