TCH.1C-27J-2-27JG
2-57.5 Q-FEEL OPERATING (AIR DATA NOT VALID)
(refer to figure
) (Cont'd)
8.By means of dynamometer (AGE NO. 00034), set the
control stick to 6 ° and 9 ° forward. Check that the
effort required is: 280 N and 400 N max.
9.Return the control stick to neutral position.
10.By means of dynamometer (AGE NO. 00034), set the
control stick to 6 ° and 9 ° backward. Check that the
effort required is: 310 N and 440 N max.
11.Move the AIR SPEED selector (14) to HIGH position
and verify that the ACAWS caution message
Q-FEEL/TLU MAN SEL is still displayed on CMDU
(16).
12.By means of dynamometer (AGE NO. 00034), set the
control stick to 6 ° and 9 ° forward. Check that the
effort required is: 370 N and 530 N max.
13.Return the control stick to neutral position.
14.By means of dynamometer (AGE NO. 00034), set the
control stick to 6 ° and 9 ° backward. Check that the
effort required is: 400 N and 580 N max.
15.Set the AIR SPEED selector (14) to AUTO position
and verify that the ACAWS caution message
Q-FEEL/TLU MAN SEL disappears on CMDU (16).
16.Restore the electrical power to ADC1 and ADC 2 and
verify the following conditions:
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).
17.Return the aircraft simulated airspeed to 0 Kts.
(Cont'd)
27-30-40
2-452