Q and A Learjet 60 (Flight Controls)

Question 0

Spoilerons are activated with _________.

Answer 0

Flaps at greater than 25 degrees

Question 1

There are ____ static wicks, ____ may be missing for dispatch.

Answer 1

19

14

Question 2

Rudder Boost is activated _________. (3)

Answer 2

1- Avionics Master and RB sw ON
2- Flaps greater than 8 degrees
3- 50 lbs pedal pressure applied

Question 3

All trim systems disengaged by _______.

Answer 3

Depressing the MSW

Question 4

Pri Pitch Trim motor is used by ___________. (2)

Answer 4

Primary pitch
and
Mach Trim

Question 5

Sec Pitch Trim motor is used by ______. (2)

Answer 5

Sec pitch
and
Autopilot

Question 6

Mach Trim engages when _________. (2)

Answer 6

speed over 0.695
and
Autopilot is disengaged

Question 7

Speed of the Pri Pitch Trim motor is based on _________.

Answer 7

Stab Position

Question 8

Pri Pitch Trim high speed is approx. _____ faster than low speed.

Answer 8

4

Question 9

Trim clicker will sound _______. (2)

Answer 9

TRIM USE Greater than 1 sec and Flaps are greater than ) degrees

Question 10

Mach Trim produces ___________.

Answer 10

Artificial control pressures ________.

Question 11

Flaps bias signals are produce at ______. (3)

Answer 11

3

13

25

Question 12

Flap position indicator is powered by _____ fails to ______.

Answer 12

28 VDC

0

Question 13

Symmetry of flap extension assured by _________.

Answer 13

Interconnect cable

Question 14

Flaps ______ selected and _____ actuated.

Answer 14

(28 VDC) Electrically

Hydraulically

Question 15

Spoilers operation _____ selected and _______ actuated.

Answer 15

28 VDC (airborne) and 115 VAC

Hydraulically

Question 16

Main Hyd Syst failure, spoilers _________.

Answer 16

Blow CLOSE and are Inop

Question 17

Max Spoiler extension in spoileron mode is approx _____ degrees.

Answer 17

15

Question 18

The YD can be manually disengaged by ___________. (2)

Answer 18

Depressing MSW

Depressing the YD button

Question 19

Yellow YD annunciator on PFD flashed for ________ when (man - auto) disengaged.

Answer 19

10 sec. then steady

Question 20

Yellow YD annunciator on PFD canceled by ______.

Answer 20

MSW

Question 21

STALL WARNING system becomes operational ________.

Answer 21

7 secs after airborne

Question 22

The stick shaker is actuated when the AOA indicators _____.

Answer 22

IN YELLOW range (10% above stall)