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Questions for INDIGO INSTRUMENTS (1117-1427)

Answer the following questions

1.

In the Southern hemisphere, during deceleration following a landing in a Westerly direction, the magnetic compass will indicate

2.

The diagram on annex 022-648A shows three gyro assemblies: A, B and C. Among these gyros,-one is a roll gyro (noted 1)-one is a pitch gyro (noted 2)-one is a yaw gyro (noted 3)The correct matching of gyros and assemblies is

3.

Among the errors of a magnetic compass, are errors

4.

In a steep turn, the northerly turning error on a magnetic compass on the northern hemisphere is

5.

When an aircraft, operating in the VOR coupled mode, approaches the ""cone of confusion"" over a VOR station, the roll channel of the autopilot

6.

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

7.

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

8.

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

9.

In automatic landing mode, in case of failure of one of the two autopilots, the system is considered

10.

The purpose of the altitude alert system is to generate a visual and aural warning to the pilot when the

11.

The Primary Flight Display (PFD) displays information dedicated to

12.

A laser gyro consists of

13.

The operating frequency range of a low altitude radio altimeter is

14.

An autopilot capable of holding at least altitude and heading mode is compulsory

15.

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

16.

The stall warning system receives information about the :1- airplane angle of attack2- airplane speed3- airplane bank angle4- airplane configuration5- load factor on the airplaneThe combination regrouping all the correct statements is

17.

The stick shaker calculator receives the following informations :1- mass of the airplane2- angle of attack3- wing flap deflection4- position of the landing gear5- total air temperature6- pressure altitudeThe combination regrouping all the correct statements is

18.

When using the autopilot, the function of the pitch channel automatic trim is to:1- cancel the hinge moment of the elevator2- ease as much as possible the load of the servo-actuator 3- restore to the pilot a correctly trimmed airplane during the autopilot disengagement The combination regrouping all the correct statements is

19.

In a turn at constant rate, the turn indicator reading is

20.

In the event of a conflict, the TCAS (Traffic Collision Avoidance System) will give information such as

21.

In the Southern hemisphere, during deceleration following a landing in an Easterly direction, the magnetic compass will indicate

22.

If the GPWS (Ground Proximity Warning System) activates, and alerts the pilot with an aural warning ""DON'T SINK"" (twice times), it is because

23.

Heading information given by a gyro platform, is given by a gyro at

24.

A landing will be considered to be performed in the AUTOMATIC mode when:1- the autopilot maintains the airplane on the ILS beam until the decision height is reached then is disengaged automatically.2- the autothrottle maintains a constant speed until the decision height is reached then is disengaged automatically.3- the autopilot maintains the airplane on the ILS beam until the flare.4- the autothrottle decreases the thrust when the height is approximately 30 ft.5- the flare and the ground roll are performed automatically.The combination regrouping all the correct statements is

25.

A ""resolution advisory"" (RA) is represented on the display system of the TCAS 2 (Traffic Collision Avoidance System) by a

26.

Magnetic compass swinging is carried out to reduce as much as possible

27.

An ""intruding traffic advisory"" is represented on the display system of the TCAS 2 (Traffic Collision Avoidance System) by displaying

28.

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

29.

When the intruding aircraft is equipped with a serviceable mode C transponder, the TCAS II (Traffic Collision Avoidance System) generates a

30.

The purpose of compass swinging is to determine the deviation of a magnetic compass

31.

The ""Bourdon tube"" is used to measure

32.

On the ground, during a left turn, the turn indicator indicates

33.

The mach number is the

34.

A rate integrating gyro is a detecting element used in1. An inertial attitude unit2. An automatic pilot3. A stabilizing servo system4. An inertial navigation system5. A rate-of-turn indicatorThe combination of correct statements is

35.

When only one autopilot is used for climbing, cruising and approach, the system is considered

36.

An airborne instrument, equipped with a gyro with 2 degrees of freedom and a horizontal spin axis is

37.

The engagement of an autopilot is not possible when:1- there is a fault in the electrical power supply2- the controlled-turn knob is not set to centre-off3- there is a synchronization fault in the pitch channel4- there is a fault in the attitude reference unitThe combination regrouping all the correct statements is

38.

The low-altitude radio altimeters used in precision approaches:1 operate in the 1540-1660 MHz range.2 are of the pulsed type.3 are of the frequency modulation type.4 have an operating range of 0 to 5000 ft.5 have a precision of +/- 2 feet between 0 and 500 ft.The combination of the correct statements is

39.

The Engine Pressure Ratio (EPR) is computed by

40.

The purpose of a compass swing is to attempt to coincide the indications of

41.

The oncoming stall of a large transport airplane appears in the form of

42.

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

43.

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

44.

The quadrantal deviation of the magnetic compass is due to the action of

45.

All the last generation aircraft use flight control systems. The Flight Management System (FMS) is the most advanced system , it can be defined as a

46.

The fields affecting a magnetic compass originate from:1. magnetic masses2. ferrous metal masses3. non ferrous metal masses4. electrical currentsThe combination of correct statements is

47.

The voice recorder records on four different channels the following information:1- aural warnings2- radio communications3- conversations between the crew members through the cockpit interphone4- announcements to the passengersThe combination regrouping all the correct statements is

48.

Except for airplanes under 5,7 t airworthiness certificate of which is subsequent to 31 march 1998, a flight data recording system must be able to store the recorded data for a minimum of the last

49.

The operation of the GPWS (Ground Proximity Warning System) is governed by laws taking the aircraft height into account as well as :1- the descent rate2- the climb rate3- the aircraft configuration4- the selected engine rpmThe combination of correct statements is

50.

Compared with a conventional gyro, a laser gyro