TCH.1C-27J-2-27JG
2-5.2
PREPARATION (Cont'd)
NOTE
When the templates installation are required,
apply a light force on the template itself in
order to reduce or annull the possible offset
due to skin surface waveness.
3.On flap control panel, ensure that the flap control lever
is to UP position and the flap surfaces are retracted (0
position).
4.Fit on the inner and outer flaps surfaces the four
inclinometer (AGE NO. 00061) ( use biadhesive tape),
non in contact with their rivets. Switch on the
inclinometer and perform the proper calibration so that
the inclinometer assume their zero reference with the
flaps up position (related angle shall be set). Remove
the template.
5.Connect external AC power supply to aircraft (refer to
).
6.Close the following circuit breaker to feed the flap
system:
A.FLAP ASYM (1CA) (6) located on Rear Mid Circuit
Breaker Panel (451VE) (5) in position L 3 (refer to
figure
B.FLAP ASYM (12CA) (4) located on Rear Upper
Circuit Breaker Panel (452VE) (3) in position H 4
(refer to figure
) .
C.FLAP IND (3CA) (2) located on Overhead Circuit
Breaker Panel (271VE) (1) in position F 14 (refer to
figure
7.Power-up the avionic system in order to have the
availability the cockpit displays (ACAWS and FD
Maintenance Page).
8.Connect headset to the external socket of the
interphone system and switch on the system (refer to
manual
(Cont'd)
27-00-30
2-13