TCH.1C-27J-2-27JG
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para
maintenance.
PROCEDURE:
2-82.1 REMOVAL (refer to figure
) , (refer
to figure
) and (refer to figure
1.Check that the following circuit breakers are opened:
-FLIGHT CONTROL FLAP IND (3CA) (2) located
on Overhead Circuit Breakers Panel (271VE) (1) in
position F 14;
-FLAP ASYM (12CA) (5) and FLAP ASYM (1CA)
(7) located respectively on Rear Upper Circuit
Breakers Panel (452VE) (3) in position H 4 and on
Rear Center Circuit Breakers Panel (451VE) (6) in
position L 5;
-ELECTRICAL SYS DC BUS 2 CNTR (24PA)
located on Rear Upper Circuit Breakers Panel
(452VE) (3) in position H 17.
2.Remove the four screws (11) fixing the Flap Position
Indicator (8) to the control instrument panel (9).
3.Extract the Flap Position Indicator (8) from its location.
CAUTION
––––––––––––––––––––––––––––––––––
Install protection cup to the electrical
connector that you disconnect.
––––––––––––––––––––––––––––––––––
4.Disconnect electrical connector (10) from Flap
Position Indicator (8).
5.Remove Flap Position Indicator (8).
27-50-50
2-607