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TCH.1C-27J-2-27JG
2-73.2
INSTALLATION (refer to figure 
2-67
) (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
TCH.1C-27J-2-00GV
).
4.Connect electrical power to aircraft (refer to manual
TCH.1C-27J-2-00GV
).
5.When installation is complete perform the functional
test FLAPS FUNCTIONAL CHECK (refer to para 
2-65
), (refer to para 
2-78
) and (refer to para 
2-80
).
27-50-40
2-590