Flight Controls
T-45A UJPT, E2-C2, ADV, & IUT Eng-11
(1) Failure of either actuator will not
affect remaining actuator
(2) Failure of either hydraulic system
will not affect operation
b.
Stick-to-aileron ratio changer
increases aileron deflection and
reduces maximum lateral stick
displacement when landing gear down
(1) Maximum aileron deflection up
and down is 12.5 degrees gear up
and 15.5 degrees gear down
(2) Maximum aileron trim deflection:
6 degrees up or down (with
landing gear extended, authority
increases to +/- 9 degrees)
(3) Rate of trim change is
approximately 2 degrees per
second
c.
Simultaneous operation of both trim
switches in opposite directions
disables the trim motor
?
and stabilators?
ANSWER: Elevators are attached to a fixed stabilizer
and move up or down to control pitch (as on the T-34/
T-2). A stabilator is one piece and the entire unit
rotates to control pitch.
Page 11-7
(8-03) Original