TCH.1C-27J-2-27JG
2-40.2
ELEVATORS TRAVEL CHECK (refer to figure
)
and (refer to figure
(Cont'd)
-right balance tab 20
°
±
1.3
°
downwards with
respect to right elevator fully travel upwards.
18.Return the Copilot control stick (4) to neutral position.
19.Remove templates (AGE NO. 00065) to the stabilizers
surface, in correspondence of the trim tab outer end.
20.Remove templates (AGE NO. 00038) to the elevators
surface, in the area between balance tab and trim tab.
21.Remove hydraulic power to the aircraft (refer to
).
22.Disconnect electrical power from aircraft (refer to
).
2-40.3
ELEVATORS BREAKOUT FORCE CHECK
(Without hydraulic) (refer to figure
1.Ensure that the hydraulic pressure in both systems
No.1 and No. 2 is nulled.
2.By means of dynamometer (AGE NO. 00034), apply a
load until the Pitot control stick (5) begins to move.
Check that the breakout force does not exceed 115 N.
3.Return the Pilot control stick (5) to neutral position.
4.Perform the same operations on the Copilot control
stick (4) and verify the same value.
27-30-00
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