SELF-CHECK 2 : AVIONICS Tech. Manual (Ch. 10) Flashcards
Reference: Technical Manual (Chapter 10)
The standby instruments use the ____ pitot tube input.
A. Pilot’s
B. Copilot’s
C. Pilot’s and copilot’s
D. Center
B. Copilot’s
The standby instruments use their own static source, independent of the pilot’s and copilot’s static sources.
A. True
B. False
A. True
What resource is available to the pilot to quick learn the meaning of acronyms relating to the G200 FMS 6100 Flight Management System?
A. The Pilot Training Manual
B. The Collins FMS Taskbook
C. The Introduction chapter of the Collins FMS-6100 Operator’s Guide
D. Mygulfstream.com
C. The Introduction chapter of the Collins FMS-6100 Operator’s Guide
What does the G200 Flight Management Computer do?
A. Accepts data from multiple navigation sensors, uses it to estimate position, and provides navigation in the en route, terminal, and approach phases of flight.
B. Determines that the airplane is in terminal phase of flight when a destination airport is entered in the flight plan, and the airplane is 30 NM from that airport.
C. Determines that the airplane is in approach phase of flight when approach is activated and the airplane is 2 NM from the FAF.
D. All of the above
D. All of the above
During preflight, how does the pilot initialize the FMS position of the airplane?
A. FMS position is initialized on the POS INIT pages of the FMS.
B. FMS position is initialized using either RTU.
C. The pilot can begin the procedure by pressing the IDX menu key and selecting POS INIT from the available options.
D. Both A and C
D. Both A and C
Once SYNC mode is selected from the FMS CONTROL page of the FMS, only those flight plan changes made from the FMS designated as the MASTER will automatically be made to the other FMS.
A. True
B. False
B. False
The basic steps to create a flight plan in the FMS 6100 include which of the following:
A. Entering the origin, destination, and alternate airports.
B. Selecting a departure runway or a SID with a departure runway.
C. Entering a route from the departure to the arrival, and entering a STAR with or without a transition and approach
D. All of the Above
D. All of the Above
How can the pilot transform a waypoint to a flyover waypoint so that the FMS will steer the airplane over the waypoint before initiating a turn?
A. With the keypad, from the LEGS pages, add a slash-letter O suffix to the waypoint identifier.
B. With the keypad, from the FPLN pages, add a slash-letter O suffix to the waypoint identifier.
C. With the keypad, from the LEGS pages, add a @ symbol prefix to the waypoint identifi er.
D. With the keypad, from the LEGS pages, add a slash- zero suffi x to the waypoint identifier.
D. With the keypad, from the LEGS pages, add a slash- zero suffix to the waypoint identifier.
Where would the pilot find guidance on initializing the FMS 6100 PERFORMANCE calculation features?
A. The Airplane Flight Manual, Volumes 2 and 3, PERFORMANCE charts and tables.
B. Chapter 5 of the FMS 6100 Operator’s Guide
C. The Confi guration Deviation List
D. There is no guidance
B. Chapter 5 of the FMS 6100 Operator’s Guide
In what section of the Collins FMS 6100 Operator’s Guide will the pilot find detailed guidance on use of the DIR function key?
A. Chapter 18, PRINCIPLES OF VNAV
B. Chapter 12, DATABASE OPERATIONS
C. Chapter 6, DEPARTURE
D. Chapter 7, EN ROUTE
D. Chapter 7, ENROUTE
If while on the LEGS page the pilot changes the FROM waypoint (the second waypoint from the top, in green), then the LEG from that waypoint to the next can be established as the active leg, allowing the pilot to set a radar vector and heading leg to intercept a specifi ed flight plan leg, thereby arming the FMS to intercept the route and fl y the new course to the TO waypoint:
A. True
B. False
B. False
The Collins FMS 6100 is capable of navigating the airplane to:
A. Hold at a flight plan waypoint
B. Hold at a non-fl ight plan waypoint
C. Hold at present position
D. All of the above
D. All of the above.
“CME025/7” and TAGGS275.3T/15.5” are examples of what
A. PLACE BRG/PLACE BRG waypoints, described in Chapter 7 of the Collins FMS 6100 Operator’s Guide.
B. Coordinates for random waypoints in remote portions of the Pacific.
C. PLACE BRG/ DIST waypoints, described in Chapter 7 of the Collins FMS 6100 Operator’s Guide.
D. PLACE BRG/ DIST waypoints, described in Chapter 4 of the Collins FMS 6100 Operator’s Guide.
C. PLACE BRG/ DIST waypoints, described in Chapter 7 of the Collins FMS 6100 Operator’s Guide.
“L2,” “5L,” “R28,” and “17R” are examples of what?
A. Pilot entries programming the FMS to fly offset parallel courses, which entries are made on the ACT/MOD FPLN page as fully described in Chapter 7 of the Collins FMS 6100 Operator’s Guide.
B. Shorthand abbreviations for wind velocity.
C. SELCAL identifiers.
D. Passenger seat station numbers for manual weight and balance calculations.
A. Pilot entries programming the FMS to fl y offset parallel courses, which entries are made on the ACT/MOD FPLN page as fully described in Chapter 7 of the Collins FMS 6100 Operator’s Guide.
To learn how to select/change STARs and Approaches in the FMS 6100, the pilot can refer to:
A. Collins FMS 6100 Operator’s Guide Chapter 9
B. Collins FMS 6100 Operator’s Guide Chapter 13
C. Collins Pro Line 4 Pilot’s Guide, Chapter 3
D. Collins FMS 6100 Operator’s Guide Chapter 8
D. Collins FMS 6100 Operator’s Guide Chapter 8
To use FMS navigation to fly a localizer-based missed approach, the pilot should:
Select go-around (TOGA).
Set power, pitch, and confi guration.
Make sure AUTO sequence is selected on the ACT LEGS page of the FMS.
Make sure the first waypoint of the missed approach is the TO waypoint.
Set FMS as the NAV SOURCE.
A. True
B. False
A. True
To fly an FMS decent path to a down-track waypoint, the pilot’s first step in programming the FMS 6100 is
A. Pushing the IDX function key and selecting VERTICAL DIRECT-TO from available options.
B. Keying the mike and asking for lower.
C. Pushing the DIR function key to display the ACT DIRECT-TO page, as described in the Collins FMS 6100 Operator’s Guide Chapter 10.
D. Using ARINC 429 to communicate with the flight management computer.
C.Pushing the DIR function key to display the ACT DIRECT-TO page, as described in the Collins FMS 6100 Operator’s Guide Chapter 10.
Small square boxes on the data lines of the CDU (Control Display Unit) represent what?
A. Places for the input of optional data.
B. Prompts for the input of required data.
C. Either A or B, depending upon whether the airplane is equipped with Collins or Universal FMS.
D. Neither A nor B.
B. Prompts for the input of required data
What resource is available to the pilot for quickly learning the meaning of any acronym relating to the G200 ProLine 4 Avionics System?
A. The Pilot Training Manual
B. The Collins FMS Taskbook
C. The Avionics Glossary of the Collins Pro Line 4 Pilot’s Guide
D. Mygulfstream.com
C. The Avionics Glossary of the Collins Pro Line 4 Pilot’s Guide
The Display Control Panel (DCP) is used
A. To select the lateral navigation parameter/ source and the MFD display format.
B. To select the vertical navigation parameter/source.
C. To use the elapsed time function.
D. Both A and C.
D. Both A and C
The Air Data Reference Panel (ARP) is used
A. To step through VSPEED references, using the SEL button.
B. To adjust the value of the VSPEED reference, using the SPEED knob.
C. Generally to provide the pilot input into the Air Data Computers (ADC).
D. All of the above.
D. All of the above
Using the Reversionary Switching Panel (RSP), the pilot can deselect which of the following onside subsystems and transfer to their cross-side counterparts:
A. Attitude Heading System
B. Air Data Computer
C. Display Control Panel
D. All of the above
D. All of the above
The airspeed trend vector above (acceleration) or below (deceleration) the airspeed digital readout indicates what the airspeed will be in ________ seconds at present rate of acceleration/deceleration.
A. 5 seconds
B. 15 seconds
C. 10 seconds
D. 20 seconds
C. 10 seconds
Which of the following is not true of the DRIFT INDEX:
A. It is a magenta circle to the right of the airspeed scale.
B. It is displayed 3 seconds after takeoff and is removed with weight on wheels.
C. It can be used as a substitute for actual stall warning system.
D. It indicates 1.25 VSTALL.
C. It can be used as a substitute for actual stall warning system
