On a modern aircraft, the flight director modes are displayed on the:

In case of accidental closing of an aircraft"s left static pressure port (rain, birds), the altimeter:

Considering the maximum operational Mach number (MMO) and the maximum operational speed (VMO), the captain of a pressurized aircraft begins his descent from a high flight level. In order to meet his scheduled time of arrival, he decides to use the maximum ground speed at any time of the descent. He will be limited :

Mode "Localizer ARM" active on Flight Director means: line

If an aircraft is equipped with one altimeter which is compensated for position error and another altimeter which is not . and all other factors being equal...

Indication of Mach number is obtained from:

An Air Data Computer (ADC) :

In An Air Data Computer (ADC), aeroplane altitude is calculated from:

The hysteresis error of an altimeter varies substantially with the:

In a non-pressurized aircraft, if one or several static pressure ports are damaged, there is an ultimate emergency means for restoring a practically correct static pressure intake :

The essential components of a flight director are : 1- a computer 2- an automatic pilot 3- an autothrottle 4- command bars The combination of correct statements is :

Today"s airspeed indicators (calibrated to the Saint-Venant formula), indicate, in the absence of static (and instrumental) error :

The altimeter consists of one or several aneroid capsules located in a sealed casing. The pressures in the aneroid capsule (i) and casing (ii) are respectively :

Sound propagates through the air at a speed which only depends on :

The aim of the flight director is to provide information to the pilot:

(For this question use annex 022-9768A) An aircraft is under guidance mode following a VOR radial. From the ADI and HSI information represented in the enclosed annex, it is possible to deduce that the aircraft is :

(For this question use annex 022-9771A) The atmospheric pressure at FL 70 in a "standard + 10" atmosphere is:

All the anemometers are calibrated according to:

The velocity of sound at the sea level in a standard atmosphere is:

In a standard atmosphere and at the sea level, the calibrated airspeed (CAS) is :

The QNH is by definition the value of the:

A VMO-MMO warning device consists of an alarm connected to :

When flying from a sector of warm air into one of colder air, the altimeter will :

With a constant weight, irrespective of the airfield altitude, an aircraft always takes off at the same :

During a climb after take-off from a contaminated runway, if the total pressure probe of the airspeed indicator is blocked, the pilot finds that indicated airspeed :

The mach number is the:

The principle of the Mach indicator is based on the computation of the ratio :

The reading of a Mach indicator is independent of :

The calibrated airspeed (CAS) is obtained by applying to the indicated airspeed (IAS) :

The velocity maximum operating (V.M.O.) is a speed expressed in :

The limits of the white scale of an airspeed indicator are :

The limits of the green scale of an airspeed indicator are :

The limits of the yellow scale of an airspeed indicator are :

During a straight and uniform climb, the pilot maintains a constant calibrated airspeed (CAS) :

With a pitot probe blocked due to ice build up, the aircraft airspeed indicator will indicate in descent a :

At sea level, on a typical servo altimeter, the tolerance in feet from indicated must not exceed :

After an aircraft has passed through a volcanic cloud which has blocked the total pressure probe inlet of the airspeed indicator, the pilot begins a stabilized descent and finds that the indicated airspeed :

The static pressure error of the static vent on which the altimeter is connected varies substantially with the:

The pressure altitude is the altitude corresponding :

The response time of a vertical speed detector may be increased by adding a:

The density altitude is :

On board an aircraft the altitude is measured from the:

The altitude indicated on board an aircraft flying in an atmosphere where all the atmosphere layers below the aircraft are cold is :

The purpose of the vibrating device of an altimeter is to:

VLE is the maximum :

VLO is the maximum :

VNE is the maximum speed :

VNO is the maximum speed :

The vertical speed indicator of an aircraft flying at a true airspeed of 100 kt, in a descent with a slope of 3 degrees, indicates :

The advantages provided by an air data computer to indicate the altitude are : 1. Position/pressure error correction 2. Hysteresis error correction 3. Remote data transmission capability 4. Capability of operating as a conventional altimeter in the event of a failure The combination of correct statements is :

The altitude indicated on board an aircraft flying in an atmosphere where all atmosphere layers below the aircraft are warm is:

For a constant Calibrated Airspeed (CAS) and a level flight, a fall in ambient temperature will result in a:

When climbing at a constant Mach number below the tropopause, in ISA conditions, the Calibrated Airspeed (CAS) will:

If the static source to an airspeed indicator (ASI) becomes blocked during a descent the instrument will:

If the static source to an altimeter becomes blocked during a climb, the instrument will:

The primary factor which makes the servo- assisted altimeter more accurate than the simple pressure altimeter is the use of:

If the static source of an altimeter becomes blocked during a descent the instrument will:

A leak in the pitot total pressure line of a non- pressurized aircraft to an airspeed indicator would cause it to:

The pressure measured at the forward facing orifice of a pitot tube is the :

The airspeed indicator circuit consists of pressure sensors. The pitot tube directly supplies:

If the outside temperature at 35 000 feet is -40§C, the local speed of sound is :

The Head Up Display (HUD) is a device allowing the pilot, while still looking outside, to have:

Flight Director Information supplied by an FD computer is presented in the form of command bars on the following instrument:

The error in altimeter readings caused by the variation of the static pressure near the source is known as:

When descending through an isothermal layer at a constant Calibrated Airspeed (CAS), the True Airspeed (TAS) will:

Machmeter readings are subject to:

At a constant Mach number, the calibrated air speed (CAS) :

At a constant calibrated airspeed (CAS), the Mach number :

The Mach number is :

The use of the TCAS (Traffic Collision Avoidance System) for avoiding an aircraft in flight is now general. TCAS uses for its operation :

Different pressure sensors are used according to the intensity of the pressure measured (low, medium or high) Classify the following sensors by order of increasing pressure for which they are suitable : 1- bellows type 2- Bourdon tube type 3- aneroid capsule type

The airspeed indicator of a twin-engined aircraft comprises different sectors and color marks. The blue line corresponds to the :

The airspeed indicator of an aircraft is provided with a moving red and white hatched pointer. This pointer indicates the:

A pitot blockage of both the ram air input and the drain hole with the static port open causes the airspeed indicator to :

VFE is the maximum speed :

A pitot tube covered by ice which blocks the ram air inlet will affect the following instrument (s) :

Given : - Ts the static temperature (SAT) - Tt the total temperature (TAT) - Kr the recovery coefficient - M the Mach number The total temperature can be expressed approximately by the formula :

A manifold pressure gauge of a piston engine measures :

If a manifold pressure gauge consistently registers atmospheric pressure, the cause is probably.

The "Bourdon tube" is used to measure :

The probe used to measure the air intake pressure of a gas turbine engined powerplant is:

The pressure probe used to measure the pressure of a low pressure fuel pump is:

(For this question use annex 022-10217A) After having programmed your flight director, you see that the indications of your ADI (Attitude Director Indicator) are as represented in diagram N§1 of the appended annex. On this instrument, the command bars indicate that you must bank your airplane to the left and :

The command bars of a flight director are generally represented on an:

Alarms are standardised and follow a code of colours. Those requiring action but not immediately, are signalled by the colour:

An aeroplane is equipped with a Flight Director (with crosshair trend bars), heading 270§, in HDG mode (heading hold). A new heading, of 360§, is selected the vertical trend bar :

The altimeter is fed by :

The vertical speed indicator (VSI) by :

Among the following engine instruments, the one operating with an aneroid pressure diaphragm is the :

In a modern airplane equipped with an ECAM (Electronic centralized aircraft monitor), when a failure occurs in a circuit, the centralized flight management system: 1- releases an aural warning 2- lights up the appropriate push- buttons on the overhead panel 3- displays the relevant circuit on the system display 4- processes the failure automatically The combination regrouping all the correct statements is:

The flight director indicates the : distance.

The position of a Flight Director command bars:

When the altitude acquisition mode is engaged on a jet transport airplane equipped with autopilot (AP) and auto-throttle (ATS) systems the:

A "Bourdon Tube" is used in:

The operating principle of the vertical speed indicator (VSI) is based on the measurement of the rate of change of:

(For this question use annex 022-11232A) After having programmed your flight director, you see that the indications of your ADI (Attitude Director indicator) are as represented in diagram N§1 of the appended annex. On this instrument, the command bars indicate that you must :

For capturing and keeping a preselected magnetic heading, the flight director computer takes into account: 1- track deviation 2- rate of track closure 3- rate of change of track closure 4- wind velocity given by the inertial reference unit The combination regrouping all the correct statements is :