TCH.1C-27J-2-27JG
2-74.2
INSTALLATION. Proceed as follows:
(Cont'd)
G.Screw the flap slidingend assy on the flap cable
assy till previously noted position.
H.Screw the Flap Clevis to Flap Cable Assy till
previously noted posiiton.
I.Screw the flap clevis on the flap cable assy and
torque tighten to 53
÷
62 in lb between flap
slidingend assy and flap clevis.
J.Lock the safety wire using double twist method per
MS33540.
K.Place the washers and the nut in the Flap Clevis
connection.
L.Screw the bolt fixing the flap clevis to flap lever
assy and torque tighten to 50
÷
75 in lb.
FOLLOW ON MAINTENANCE:
1.Close the access panels 210E, 210F, 711A, 712A,
130B, 130C.
2.Install pilot seat (refer to manual
).
3.Restore hydraulic power system (refer to manual
4.Connect electrical power to aircraft (refer to manual
5.Perform the functional test:
A.FLAP CONTROL CABLE TENSION (refer to para
).
B.MEASUREMENT OF FLAP CONTROL FRICTION
FORCE (refer to para
27-50-45
2-595