Aircraft empennage

An aircraft empennage, comprising:

• a rear fuselage section comprising a skin and a frame,
• a trimmable horizontal tail plane comprising a first and a second lateral torsion box, the first and the second lateral torsion box comprising a front spar and a rear spar,
• a front fitting and a rear fitting connected to the trimmable horizontal tail plane and to the fuselage section,
• an actuator configured to act on the front fitting for a rotation of the trimmable horizontal tail plane around a hinge axis passing through the rear fitting and orthogonal to a vertical longitudinal plane of symmetry of the fuselage section,
• wherein the front fitting comprises a first and a second front fitting units, the first front fitting unit being joined to the front spar of the first lateral torsion box and the second front fitting unit being joined to the front spar of the second lateral torsion box, and
• wherein the actuator comprises a first and a second actuator units, the first actuator unit being configured to act on the first front fitting unit and the second actuator unit being configured to act on the second front fitting unit,
• wherein the first and the second actuator units are located in front of the front spar and rearward of a most forward point of the trimmable horizontal tail plane on a longitudinal axis of the rear fuselage section,
• wherein the first front fitting unit and the second front fitting unit each comprise an elongated support bar located in a plane perpendicular to the front spar, the elongated support bars pointing towards lateral sides of the rear fuselage section.