STEMME S6-RT, Руководство по эксплуатации самолета

Страница: 176 / 236

7 5 Revision:
Date of Issue: 18. November 2011 Date of Rev.: . .
! " # ! 1111111111111111111111111111111111
The control forces are transmitted to the flight controls with control rods or
control cables. Control brackets – made of rust proof coated steel – are
laminated into each flight control. The bearings are prepared for easy movement
at all times.
The connections of the three control elements integrated into each wing
(aileron, flap and airbrake) to the control rods are located in the midsection of
the fuselage. These connections are disconnectable. Additional connections of
the flight controls between the inner wing and the outer wing are designed as
secured quick connectors (non automatic).
!
Design: CFC Sandwich, 2 part Aileron across the span of the outer
wing.
Mounting: Inner aileron: 9 joints and 1 control connector each
Outer aileron: 7 joints and 1 control connector each
Axial fixations near the control connectors
Operation: Operated with control rods
Aileron differential realized by parted ailerons. Outer ailerons
deflect more than inner ailerons. Flap deflection is also
overlayed.
Movement by sideways deflection of control stick.
! 2
Design: CFC Sandwich
Mounting: 3 joints on each elevator side, 1 centralized automatic control
connector
Operation: Operated with control rods (which are located in the front
section, midsection and rear section of the fuselage).
Removable horizontal stabilizer mounted by screwing the self
securing connection bolt.
Movement by push and pull on control stick
The electric trim is moved with a toggle switch on the control stick.