ISOLATION PROCEDURES FOR CHECKING CONTROLS LOOSENESS
CHECK CLOSET, TRANSFER AND COCKPIT
There is no overall looseness check
of the cockpit controls. The controls
feel loose when there is no hydraulic
pressure applied. Each connecting
link must be checked.
Working from passageway, check ten connecting
links (52 thru 61) for loose swaged inserts (Tasks
11-7 and 11-7.1) and loose rod end (Task 11-9).
Remove pilots and copilots floor panels (Task
Working in cockpit, check six connecting links
(62 thru 67) and four links (68) for loose swaged
inserts (Tasks 11-7 and 11-7.1) and loose rod
end bearings (Tasks 11-9).
Remove left and right landing lights (Task 9-69).