1) Satellite transmits updates on every Report

2nd orbit

9th orbit

13th orbit

2) Galley and cabin lighting operate on Report

DC bus bar

AC bus bar

G N D services

3) Buffer amp on transmitter is located between Report

modulator and power amp

local oscillator and modulator

local oscillator and demodulator

4) Aircraft is North of V O R beacon on a course of 090 R M I pointer points to Report

0

090

180

5) What is power at pulse? Report

Peak power

Pulsed power

Average power

6) What frequency increases radar relative range? Report

High

Low

Radar relative range cannot be increased by frequency change

7) If radar pulse is reduced there is Report

increased relative range

reduced relative range

no effect

8) Adding 6 foot of cable to T X R X aerials on rad alt would give you Report

3 ft error

6 ft error

12 ft error

9) Maximum power on a wave guide is governed by the Report

widest width

narrowest width

number of joints and bends

10) A full operational autopilot system will ensure that Report

the automatic pilot will automatically disengage whenever any failure is detected

the automatic pilot will automatically cause the aircraft to overshoot if any failure is detected

the aircraft will continue its automatic landing in the event of a single failure

11) What is the 'Q' code for runway heading? Report

Q D H

Q D M

Q D R

12) During an automatic landing, the aircraft descent rate is sensed by Report

pitch rate gyros

radio altimeters

vertical accelerometers

13) The aircraft decrabbing signal, used during autoland, originates from Report

roll errors

localiser deviation errors

heading errors

14) An automatic throttle, engaged in the E P R mode, will control Report

the aircraft altitude to maintain constant engine input pressure

the engine throttles to maintain a constant acceleration rate

the engine throttles to maintain a constant engine power setting

15) Overshoot or go-around mode can be initiated Report

only when autopilot is engaged

after glideslope capture

at any time

16) The wheel height at which the approach path has been visually assessed as satisfactory to continue the approach to a landing is known as the Report

decision height

intercept height

alert height

17) The International Civil Aviation Organisation weather category 3A is Report

operation down to and along the surface of the runway without external reference

operation down to sixty meters and RVR of 800 meters

operation down to and along the surface of the runway with RVR of 200 meters

18) Runway visual range in (RVR) is obtained by Report

information obtained the local Meteorological Office

three sets of instruments at the side of the runway

one set of instruments the threshold of the runway

19) A category 3 B aircraft using fail operational automatic landing equipment which fail operational control and roll out guidance will have Report

a decision height of about 50 feet

no decision height

a decision height depending upon the RVR

20) The purpose of a yaw damper is to Report

assist the aerodynamic response

produce a co-ordinated turn

block the Dutch roll frequency

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