TCH.1C-27J-2-27JG
) (Cont'd)
NOTE
Remove protection caps from the electrical
connectors to be installed.
5.Connect the two electrical connectors (7CAA and
7CAB) (4 and 5) to the flap position transducer (7CA)
(6).
6.Remove a container with drained hydraulic fluid.
FOLLOW ON MAINTENANCE:
1.Close the access panel 532C (632C).
2.Remove maintenance platform (AGE NO. 00074).
3.Restore hydraulic power system (refer to manual
4.Connect electrical power to aircraft (refer to manual
5.When installation is complete perform the functional
test FLAPS FUNCTIONAL CHECK (refer to para
) and (refer to para
).
27-50-40
2-598