TCH.1C-27J-2-27JG
Consumable Material Required:
None
Safety Conditions:
Be aware of information contained in SAFETY
PRECAUTIONS (refer to para
maintenance.
PROCEDURE:
2-57.1 MANOEUVRE EFFORT AND Q-FEEL
FUNCTIONAL CHECK (refer to figure
) and (refer to figure
1.Install on the Pilot control stick the fixture (AGE NO.
00007).
2.Install on the Pilot control stick the inclinometer (AGE
NO. 00061).
3.Connect the dynamometer (AGE NO. 00034) to the
fixture (AGE NO. 00007).
4.Connect the air data test set plus (AGE NO. 00002)
related adaptor to the Pitot tubes and switch-on.
5.Power-up the Avionics to get availability of the
ACAWS and of the Air data system (DADS)
functionality by inserting the following circuit breakers
on RH Overhead Circuit Breaker Panel (230 VE) (4):
A.AIR DATA SYS ADC 1 (7FF) (5) in position H 9;
B.AIR DATA SYS ADC 2 (8FF) (6) in position H 10;
C.AIR DATA SYS SPTU 1 (9FF) (7) in position H 11;
D.AIR DATA SYS SPTU 2 (10FF) (8) in position H
12.
(Cont'd)
27-30-40
2-446