TCH.1C-27J-2-27JG
2-57.5 Q-FEEL OPERATING (AIR DATA NOT VALID)
(refer to figure
) (Cont'd)
18.Move the AIR SPEED selector (14) to AUTO position
and verify that the ACAWS caution message
Q-FEEL/TLU MAN SEL disappears on CMDU (16).
19.Restore the electrical power to the ADC 1 and ADC 2
and verify that:
A.the MAN indication (15), on FCS2 Control Panel
(13), extinguishes;
B.the ACAWS caution message Q-FEEL/TLU AD
FAIL disappears on CMDU (16) (also the
messages ADC 1 / 2 extinguish);
C.the FD message Q-FEEL/TLU AD FAIL remains
displayed until the clearing of CMDU (16) is
performed via SAMU (17);
D.set the aircraft simulated airspeed to 0 Kts.
Table 2-8. Effort requirements - Control Stick (high
speed)
CONTROL STICK FORWARD EFFORT ALLOWED (REF.
ONLY)
EFFORT MEASURED
+6°
335 ÷ 400
+9°
505 ÷ 585
CONTROL STICK
BACKWARD
EFFORT ALLOWED (REF.
ONLY)
EFFORT MEASURED
-6°
345 ÷ 420
-9°
535 ÷ 615
2-57.6 CHECK OF RETURN TO NEUTRAL POSITION
-CONTROL STICK - AUTO CONDITION
1.Supply the hydraulic systems No. 1 and No. 2 to 3000
psi (210 kg/cm ² ).
2.Install the inclinometer (AGE NO. 00061).
(Cont'd)
27-30-40
2-453