TCH.1C-27J-2-27JG
2-40.1
ELEVATORS FREE DEFLECTION CHECK (refer
to figure
(Cont'd)
NOTE
If the above travel values are not reached,
adjust properly the end stop screws (located
on the stabilizer) in order to satisfy the
requirements. If necessary, perform the wire
locking of the end stop screw.
2-40.2
ELEVATORS TRAVEL CHECK (refer to figure
)
and (refer to figure
1.Supply the hydraulic pressure to 3000 psi (210
Kg/cm
²
) and set the flowrate to 25 lt/min (6.6 gpm)
applied to the aircraft.
2.Connect the external electrical feeder (AGE NO.
00117) to the aircraft and switch-on.
3.On the Overhead Circuit Breaker Panel (271VE) (1),
ensure that following circuit breakers are closed:
FLIGHT CONTROL RUDDER TRIM CNTR (1CC)
position F 1 (2) and FLIGHT CONTROL Q FEEL
RTLU PWR (2CG) position F 10 (3) to feed the left
and right channels of the Electronic Control Unit.
4.Install on both stabilizers surface, in correspondence
of the trim tab outer end, the templates (AGE NO.
00065) for elevator travel check.
5.Install on both elevators surface, in the area between
balance tab and trim tab, the templates for balance
tab travel check (AGE NO. 00038).
(Cont'd)
27-30-00
2-320