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Worksheets200-242
Total questions: 43
Worksheet time: 11hrs 45mins
If an amber AP AIL MISTRIM CAS message appears, it may indicate a high Mach roll situation.
What are the pilot's actions?
Do nothing, the autopilot corrects itself
Disconnect the autopilot and slow down
Maintain attitude and airspeed while disconnecting the autopilot
Disconnect the autopilot and increase airspeed
Section 6
Special Requirements for IFR Operations
201. How is the selected MDA altitude is displayed on the PFD altitude tape?
Magenta bug and line
Blue MDA bug
White pointer
Only if FMS VNAV is active
What is the minimum altitude for autopilot operation during an ILS approach?
500 ft AGL
200 ft AGL
300 ft DH
200 ft above DH
Which of the following statements is correct?
An IS approach with the FMS:
Is authorized to a minimum altitude of 200 ft AGL
Is authorized to the published DH.
Is not authorized
Requires green data be selected on the slave display controller
How is descent below the selected baro altitude is indicated?
By a flashing of the WARN/CAUT annunciators
By an amber MIN in a white box displayed on the PFDs and the "Minimums" voice alert
By a flashing DH on the PFDs and the "Minimums" voice alert
By a flashing RA or BARO, as appropriate on the PFDs, and the "Minimums" voice alert
What should happen if an AHRS failure occurs during a coupled ILS approach? LR45/S6/5
The pilot should switch to the opposite AHRS on the reversion panel and continue the coupled
approach
The autopilot disconnects and a red AUTOPILOT message appears on EICAS
The autopilot is still available
The autopilot disconnects and a flashing red AP appears on the PFDs
How does the FPA indicate aircraft deceleration during a windshear encounter?
The FPA acceleration symbol (>) moves below the flightpath symbol
The FPA acceleration symbol (>) moves above the flightpath symbol
The FPA acceleration symbol (>) moves further left of the flightpath symbol
The FPA acceleration symbol (>) moves right of the flightpath symbol
Which of the following statements is correct?
Nuisance alerting by CAS messages during takeoff and landing:
Should be anticipated and prioritized with other aircraft duties
Is prevented by the CAS takeoff and landing inhibit mode
Is activated by pushing the WARN/CAUT annunciator until the lights extinguish prior to takeoff or
landing
Is inhibited except for engine fire and cabin smoke
Which of the following statements is correct?
Actuating the GO-AROUND button on the left thrust lever results in:
ROL and PIT annunciations with 9° pitchup/wings level attitude by the flight director on the PFDs
ROL and GA annunciations with 9° pitchup/wings level attitude by the flight director on the PFDs
HDG and GA annunciations with wings level/pitchup attitude commensurate with flap setting by
the flight director on the PFDs
HDG and GA annunciations with pitchup/bank attitude dependent on TCS selection by the flight
director on the PFDs
What approach category is the Learjet 40/45 aircraft?
C
Heavy Transport
Light Commercial
B
Below what altitude must the autopilot be disengaged?
100 ft in VFR conditions
200 ft AGL
300 ft on VOR or NDB approaches
400 ft on ILS approaches
What happens when reaching the decision altitude set on the minimums alerter?
Aural "C note" tone is heard
Aural alert "Terrain. Terrain" is heard
Amber MINS message is displayed on the PFD
Pin in the seat pokes you in the back
Which of the following statements is correct?
Pressing the GO-AROUND button on the left thrust lever:
Sets the autopilot to GO-AROUND mode
Disengages the autopilot
Disengages the flight director
Automatically moves the thrust levers to T/O power
The flight director always automatically commands level-off at the selected altitude (ASEL) except under what conditions?
Above FL 350
There are no exceptions; it always commands a level off
Below 500 ft AGL
On an approach glideslope (GS or VNV)
What is required to arm the flight director for an ILS approach?
Press the APP button on the flight guidance panel
Press the APP and GS buttons on the flight guidance panel
Press the APP and GS buttons on the flight guidance panel
Nothing; the flight director automatically arms
What does an amber ILS warning on the PFD indicate?
It is normal
Indicates a comparator warning
Indicates the glideslope is inoperative, the approach may be continued
Means the flight director is not coupled to the approach
To what Category minima is the Learjet 40/45 is authorized to conduct approaches to?
Category I and Il minimums
Category I minimums
Category Ill minimums only
Category IV minimums
Special Requirements for Glass Cockpit Aircraft
How is the crew advised that both PFDs are displaying data from the same source?
Nav source annunciations left of the HSI display are shown in green
Bearing pointers park at 3 o'clock position
Nav source/display indications left of the HSI display are shown in yellow
The scenario is automatically prevented by the IC-600 computers
When is the amber ATT annunciation displayed?
Both ADC1 and ADC2 failed
Both AHRS1 and AHRS2 failed
Both IC/SG1 and IC/SG2 failed
Differences in pitch and roll data exceeded comparator limits
The amber annunciation SG2 appears when?
Pilot and copilot selected the same attitude information source
Pilot and copilot selected the same air data information source
This annunciation is present for normal operations
IC/SG NORM knob has been rotated to the number 2 position
What would failure of one (1) symbol generator Would result in?
Red X's on all four display units
Blank RMU displays
Red X's on two display units
Red X's on one display unit
Which of the following statements is correct?
Attitude and heading reference data is:
Supplied by the respective vertical gyro and flux gate assemblies
Reset by cycling the HEADING button on the AHRS panel
Supplied from the respective AHRS
Is a function of the ADC
What is failure of DU3 indicated by?
DU3 FAIL CAS message
Blank (dark) display
Automatic display reversion to DU4
DU OVHT CAS message
Which of the following statements is correct?
A red AT FAIL and HDG FAIL annunciation on a PFD indicates the respective
IC-600 failed
Air data computer failed (loss of true airspeed)
Data acquisition unit failed
AHRS failed
Which of the following statements is correct?
The DU3 knob on the copilot display panel:
Is used to dim DU3 and DU4
Swaps EICAS and PFD displays between DU2 and DU3
Controls power to DU3 (turns it on-off)
Display of DU3 as either MFD or PFD
Which of the following statements is correct?
If display unit (DU«2 fails, the EICAS page:
May be displayed on DU 1
May be displayed on the number one FMS CDU
May be displayed on DU 3
Is lost; it can only be displayed on DU 2
Where are the brightness controls for the display units located?
In the NAV LIGHTS switch
On the flight guidance panel located on the glareshield
On the pilot/copilot lighting panels located on the lower instrument panel
On the display control panels located on the glareshield
Which of the following statements is correct?
The flight director command bars follow navigation commands:
From the number one FMS CDU
Always from the pilot side PFD display
From the copilot (not the master side) display
From the master side PFD display
What does the magenta-colored bar on the airspeed indicator show?
Low speed awareness cue showing stall speed
VMO/Mo showing the speed limit
Airspeed trend vector showing acceleration or deceleration
There is no magenta-colored bar on the airspeed indicator
Where are the controls for the bearing pointers on the HSI located?
On the lower part of DU 1 or DU 2
On the center pedestal FMS control display unit
On the glareshield display control panels
On the pilot or copilot side panels
In addition to controlling the radios, what can the RMs can also show?
Engine and airspeed displays
Backup engine and navigation displays
Backup navigation and EGPWS displays
EGPWS and TCAS displays
What would loss of the left integrated computer (IC 600 #1) be indicated by?
An amber CAS message L IAC FAIL
Blank display units on the copilot side (DU 3 and DU 4)
Red X on both RMU displays
DU 1 and DU 2 displaying a large red X
Which of the following statements is correct?
If the AHRS reversion knob is selected to the 2 position:
Airspeed and heading indicators on the copilot side is blank
Automatic headset radio system only receives from the left side
Attitude and heading indications on both sides are from AHRS #1
Attitude and heading indications on both sides are from AHRS #2
Section 8
Flight Management System
In addition to initial position date and time, what other important information is presented on the
initialization (INIT) page?
FMS software version
Navigation database expiration date
Crossfill options for dual FMS installations
FMS software version, NAV database expiration date, crossfill options for dual FMS installations
Which of the following statements is correct?
A list search for airways uses a reference waypoint. this reference waypoint is the:
Waypoint following the current cursor location
Present aircraft position
Waypoint preceding the current cursor location
Departure airport
FMS data is displayed on the PFD via control which of the following?
DISPLAY button on the FMS NAV page
NAV button on the flight guidance panel
NAV button on the respective display control panel
MS button on the respective display control panel
Which of the following statements is correct?
FMS navigation data is shown differently than VOR/LOC navigation data by:
Position- FMS data is shown on the left PFD and VOR/LOC data on the right
Color-VOR/LOC data is magenta
Label-FMS data is clearly labeled FMS in the lateral and vertical mode fields of the PFD
Color-FMS data is normally white in a dual FMS installation
What should happen when using the DTO function?
A window opens showing the flight plan waypoints with the current FROM waypoint at the top of
the display list
A window opens showing all flight plan waypoints starting at waypoint number 1
A window opens showing a list of nearby VORs and pilot waypoints
The desired TO waypoint may be selected by pressing the adjacent line select keys
MS is coupled to the autopilot by which of the following?
Pushing the FMS button on the flight guidance panel
Pushing the NAV button on the display control panel
Selecting AP on the flight guidance panel
Selecting FMS on the display control panel and NAV on the flight guidance panel
The UNS-1E FMS is approved for which of the following instrument approaches?
ILS. VOR-DME, BC, and GPS
VOR, RNAV, VOR-DME, BC, NDB, and GPS
ILS, VOR, GPS, and RNAV
LDA-BC, GPS, VOR-DME, VOR, NDB
PFD1 normally displays FMS1 while PFD2 normally displays FMS2. The indications may be
selected by pressing which of the following?
NAV button on the flight guidance controller
FMS button on the respective display panel
NAV button on the respective display panel
DU2 and DU3 knobs between PFD1 and PFD2
Which of the following items are not on the FMS initialization (INIT) page?
Initial position
UTC time
Date
FROM - TO information
To load a departure procedure from the data base into the flight plan, what must the pilot do?
From the performance page, just type in the title of the departure procedure
From the flight plan page, push the FPL button and choose SID
From the flight plan page, push the MENU button and choose DEPART
Cannot be done; pilot must type in all departure waypoints
