Q and A Learjet 60 (Flight Controls) Flashcards
Spoilerons are activated with _________.
Flaps at greater than 25 degrees
There are ____ static wicks, ____ may be missing for dispatch.
19
14
Rudder Boost is activated _________. (3)
1- Avionics Master and RB sw ON
2- Flaps greater than 8 degrees
3- 50 lbs pedal pressure applied
All trim systems disengaged by _______.
Depressing the MSW
Pri Pitch Trim motor is used by ___________. (2)
Primary pitch
and
Mach Trim
Sec Pitch Trim motor is used by ______. (2)
Sec pitch
and
Autopilot
Mach Trim engages when _________. (2)
speed over 0.695
and
Autopilot is disengaged
Speed of the Pri Pitch Trim motor is based on _________.
Stab Position
Pri Pitch Trim high speed is approx. _____ faster than low speed.
4
Trim clicker will sound _______. (2)
TRIM USE Greater than 1 sec and Flaps are greater than ) degrees
Mach Trim produces ___________.
Artificial control pressures ________.
Flaps bias signals are produce at ______. (3)
3
13
25
Flap position indicator is powered by _____ fails to ______.
28 VDC
0
Symmetry of flap extension assured by _________.
Interconnect cable
Flaps ______ selected and _____ actuated.
(28 VDC) Electrically
Hydraulically
Spoilers operation _____ selected and _______ actuated.
28 VDC (airborne) and 115 VAC
Hydraulically
Main Hyd Syst failure, spoilers _________.
Blow CLOSE and are Inop
Max Spoiler extension in spoileron mode is approx _____ degrees.
15
The YD can be manually disengaged by ___________. (2)
Depressing MSW
Depressing the YD button
Yellow YD annunciator on PFD flashed for ________ when (man - auto) disengaged.
10 sec. then steady
Yellow YD annunciator on PFD canceled by ______.
MSW
STALL WARNING system becomes operational ________.
7 secs after airborne
The stick shaker is actuated when the AOA indicators _____.
IN YELLOW range (10% above stall)
