The JAA
IR Instrumentation
test bank contains questions pertaining to
022-02-02 Autopilot
. The following list contains only a relatively small percentage of the pertinent
questions. Our software, which you are free to download now at no cost, will
generally contain a much more complete set of questions associated with this
test bank. This list is intended only to familiarize you in a general way with
the questions of the
Instrumentation
test bank.
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That said, while the following questions are intended
as a general familiarization tool, this list may not be up-to-date nor accurate.
We do not update this website as often as we update our software, which will
contain at any moment all questions that we have for a given test / topic. Therefore,
if you need to actually study for your test, instead of using the list below,
we strongly, strongly encourage you to download our GroundSchool
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written test prep software. Not only is it more complete and up-to-date, but is also considerably faster and more efficient as a study tool.
| Sample Questions
from the JAA IR
Instrumentation
Test Bank |
- Among the following functions of an autopilot, those related to the airplane stabilization are:1 pitch attitude holding2 horizontal wing holding3 displayed heading or inertial track holding4 indicated airspeed or Mach number holding5 yaw damping6 VOR axis holdingThe combination of correct statements is:
- The autopilot basic modes include, among other things, the following functions:1 pitch attitude hold2 pressure altitude hold3 horizontal wing hold4 heading holdThe combination of correct statements is:
- During a Category II automatic approach, the height information is supplied by the:
- The calibrated airspeed (CAS) or Mach holding mode is carried out by: 1 the autopilot pitch channel in the climb mode at a constant calibrated airspeed (CAS) or Mach number2 the autothrottles in the climb mode at a constant calibrated airspeed (CAS) or Mach number3 the autopilot pitch channel in the altitude or glide path holding mode4 the atothrottles in the altitude or glide path holding modeThe combination of correct statements is:
- A landing is performed automatically when the autopilot and auto-throttle ensure good performance from the final approach:
- Landing shall be considered as having been carried out automatically when the autopilot and the auto-throttle of an aircraft are disengaged by flight crew:
- The synchronization of the autopilot control channel system: 1 enables the prevention of jerks during disengagement2 enables the cancellation of rudder control signals3 enables the prevention of jerks during engagement4 functions in the heading, navigation, approach modesThe combination of correct statements is:
- The interception of a localizer beam by the autopilot takes place:
- The block diagram of an autopilot is shown in the annex. For each control channel (pitch, yaw, roll) the piloting law is the relationship between the deflection of the control surface commanded by the computer (BETA c) and the:
- In automatic landing mode, in cases of a failure of one of the two autopilots, the system is considered:
- An automatic landing system which can keep on operating without deterioration of its performances following the failure of one of the autopilots is called "FAIL...:
- If the auto-pilot is selected to VOR mode, what happens if the aircraft flies over the cone of confusion?
- In heading select the auto-pilot delivers roll commands to the controls to bank the aircraft:proportional to TAS, but not beyond a specified maximum.Set bank of 27 degrees.Set bank of 15 degrees.Proportional to the deviation from the selected heading
- During large control inputs from an automatic flight control system (AFCS), the control stick in the cockpit is moved to inform the pilot of the action. This is:
- The fundamental components of an autopilot control loop are:
- What does the auto-pilot pitch / rotate around?
- An autopilot suffers a failure which leaves the airplane trimmed and maintaining its original flight path although the autopilot is no longer engaged. The original status of the autopilot before the failure was:
- What are the auto-pilot minimum requirements in order to fly single pilot operations in IFR conditions or at night?
- Auto-land 'flare' is initiated at:
- What is the essential design feature of any closed loop control system?
- In autoland at 1000 feet A.G.L. with two autopilots engaged:
- If a rate gyro is used in an AFCS for the pitch channel its sensitive axis is aligned parallel to:
- Automatic flight systems may be capable of controlling the aircraft flight in:
- LOC ARMED' lights up on the Annunciator, this means:
- During an automatic landing, from a height of about 50 ft the:
The
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and may not be up to date! Download the software today to get
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Instrumentation
test bank, click here.
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