EASA mod 11 questions

JAR 66 Module 11 Exam Exam Practice Exam Module 1 1 Aeroplane Aerodynamics, Aerodynamics, Structures and Systems This is exam number 1.

1. A lead-acid battery is considered to be fully charged when the a) SG reaches 1.180 b)cells begin to gas freely c) SG and voltage remain constant for specified period Answer:c Answer:c

. !he preferred preferred method of battery battery charging charging a "i-#ad "i-#ad battery battery is constant a) voltage b)current c) power Answer:b Answer:b

$. %ing spoilers& when used asymmetrically& asymmetric ally& are associated with a) elevators b)rudder c) ailerons Answer:c Answer:c

'. (n an an aircraft aircraft flying control system employing servo-tabs& theinstallation theinstallation of eternal ground loc*s to the main control surface a) is unnecessary since the system is irreversible and therefore the control surface cannot be displaced by the wind b)would not prevent movement of the control control column c) would also prevent movement of the control column Answer:b Answer:b

+. Air above ,ach 0. is a) compressible b)incompressible

c)

compressible only when above the speed of sound

Answer:a Answer:a

. Supersonic air passing through a divergent divergent duct causes the a) pressure to increase& velocity to increase b)pressure to decrease& decrease& velocity velocity to increase c) pressure to increase& velocity to decrease Answer:b Answer:b

. An aircraft flying below the tropopause descends at a constant !rue !rue Airspeed& its ,ach. "o. will a) increase b)decrease c) not change Answer:b Answer:b

8. Spongy bra*es are usually a result of a) air in the system b)internal lea*age lea*age c) eternal lea*age Answer:a Answer:a

/. ver inflated tyres may cause damage to the a) wheel hub b)wheel flange c) bra*e drum Answer:b Answer:b

10. lowout panels are fitted to to floors of pressurised pressurised aircraft aircraft to a) provide access for pressurising the aircraft b)relieve pressure if the maimum differential differential is eceeded eceeded c) provide venting should a differential pressure build up across the floor Answer:c Answer:c

This is exam number  .

1. (f an aircraft aircraft is yawing to the left& left& where would you position the trim tab on the rudder2 a) !o the left b)!o the right c) !o the centre Answer:a Answer:a

. (f an aircraft is flying flying with with a left wing low& low& where would you move move the left aileron trim tab2 a) 3p b)4own c) ,oving the aileron trim tab will not correct the situation Answer:a Answer:a

$. %hen a 5eading edge edge flap is fully etended& what is the slot in the wing for2 a) !o increase the lift b)!o re-energise the boundary layer c) !o allow the flap to retract into it when it retracts Answer:b Answer:b

'. A purpose of a cut-out cut-out in a hydraulic hydraulic system a) is to limit loss of fluid in the event of pipe fracture b)is to prevent creep creep in 6ac* operated operated services which which have several several selected positions c) is to relieve the pump of load when the operation of services is complete and the accumulator charged with fluid Answer:c Answer:c

+. 7ydraulic pressure can be restored by a) the use of a pressureheat echanger b)compressing the air air charge in in an accumulator accumulator

c)

compressing the fluid in a reservoir

Answer:b Answer:b

. Auto pilot servo bra*e is energised energised a) to actuate off b)at the same same time as the clutch c) to actuate on Answer:a Answer:a

. 7and held mi*es are not permissible on a) public transport aircraft b)public transport or aerial aerial wor* c) private aircraft only Answer:a Answer:a

8. !rac* !rac* altitude altitude in a radio radio altimeter altimeter system system begins at a) 10 000ft radio alt. b) +00ft radio alt. c) 1 000ft radio alt. Answer:b Answer:b

/. A fuel crossfeed crossfeed valve is usually usually in a) the open position b)the closed position position c) its last position Answer:b Answer:b

10. 9ull time yaw damper system detects a) only low fre:uencies b)all fre:uencies fre:uencies c) band pass fre:uencies Answer:c Answer:c

This is exam number !.

1. %hat is the radio altimeter trac* altitude2 a) +00ft b)+00ft c) 10000ft Answer:b Answer:b

. %hich category are hand mi*es considered essential2 a) 5ight aircraft b)Aerial wor* aircraft aircraft c) 7eavy passenger aircraft Answer:a Answer:a

$. ;mergency ;mergency fre:uency is a) 11.+ b)1$.+ c) 1+.+ Answer:a Answer:a

'. Sliding couplings in fuel systems are used on a) high pressure systems b)low pressure systems systems c) air or vapour systems Answer:c Answer:c

+. #argo and baggage baggage compartments compartments in which which a fire is completely confined come under a) #lass  b)#lass # c) #lass 4 Answer:c Answer:c

. %hen a current current transformer transformer is disconnected what should be done2 a) !erminals !erminals shorted b)
. %hat does the differential differential sensing sensing coil sense2 a) #urrent b)=o b)=olts c) >ower Answer:a Answer:a

8. 11.+ ,h? is what fre:uency2 a) =79 b)(5S c) =< Answer:a Answer:a

/. 11.1 ,h? is what fre:uency2 a) =< b)(5S c) =79 Answer:a Answer:a

10. %here does the G#3 gets its power2 a) >,G b)attery c)
This is exam number ".

1. Galley loads are wired in a) series b)parallel so load load shedding will lower lower current consumption consumption

c)

either series or parallel depending on the design

Answer:b Answer:b

. n a fibreglass aerial& what paint should be used2 a) #ellulose only b)"ot cellulose cellulose c) >olyurethane Answer:b Answer:b

$. A current limiter a) limits current flow to a load b)opens a circuit circuit after a timecurrent timecurrent condition has been been eceeded c) can be used as a radio suppressor Answer:b Answer:b

'. %hen a load load is is shed from a busbar the a) busbar voltage increases b)current consumption consumption from the bar decreases decreases c) busbar voltage decreases Answer:b Answer:b

+. (n unparalleled unparalleled A# generation systems the phase phase rotation rotation of one generator in relation to the others a) is unimportant b)must be synchronised synchronised prior to paralleling paralleling c) must be #A Answer:a Answer:a

. (n a multi-generator system& the generator generator which which ta*es ta*es more than its its reactive power share is protected by a) overcurrent and and under current protection protection circuits circuits b)over voltage and under voltage protection protection circuits c) over ecitation and under ecitation protection circuits Answer:b Answer:b

. Sharing of electrical electrical loads by paralleled paralleled 4# generators is controlled by a) e:ualising circuits which control the speed of the generators b)e:ualising circuits circuits which control the the field ecitation ecitation of the generators c) automatic load shedding Answer:b Answer:b

8. ;cessive commutator spar*ing can be caused by a) brushes positioned on ,"A b)wea* spring tension tension c) rotating field diode failure Answer:b Answer:b

/. efore chec*ing chec*ing the SG of a battery battery recently removed from an aircraft aircraft a) allow to stabilise for one hour b)ta*e the temperature temperature of the electrolyte electrolyte c) carry out a capacity test Answer:a Answer:a

10. %hen painting a neoprene coated radio antenna a) use cellulose paint b)use any paint c) do not use cellulose paint Answer:c Answer:c

This is exam number #.

1. n an A# eternal power power plug& the interloc* interloc* circuit is controlled controlled by pins a) A b)#4

c)

;9

Answer:c Answer:c

. ver voltage protection circuits are activated a) before the over voltage limit is eceeded b)dependent on the magnitude of the overvoltage overvoltage c) after a fied time delay Answer:b Answer:b

$. %ith %ith respect to flight spoilers they a) only operate on the ground b)only operate in flight flight c) can operate both on the ground and in flight Answer:c Answer:c

'. Aircraft Aircraft emergency emergency escape escape slides are are usually usually pressurised pressurised with a) oygen b)# c) helium Answer:b Answer:b

+. As an aircraft aircraft descends descends from cruising altitude altitude @$'&000ft)& @$'&000ft)& the cabin altitude must a) stay the same b)increase c) decrease Answer:c Answer:c

. A refrigerant is is used in which which of the following2 following2 a) Air cycle machine b)>neumatic pump pump c) =apour cycle Answer:c Answer:c

. %ith %ith aircraft lights - which of the following is true2

a) Starboard light red& port light green& tail light
8. An ;#A, system is is tested tested under the following following conditionsconditionsa) Aircraft Aircraft on the ground with one engine running b)Aircraft on the ground ground with par*ing bra*e seton c) Aircraft Aircraft in the air with both engines running Answer:b Answer:b

/. %ith %ith respect 4ifferential 4ifferential Aileron Aileron #ontrol& which of the following following is true2 a) !he up going Aileron moves through a smaller angle than the down going aileron b)!he up going and down down going ailerons both deflect deflect to the same same angle c) !he down going aileron aileron moves through a smaller angle than the up going aileron Answer:c Answer:c

10. 7ow many ais does the aircraft autopilot control2 a) !wo b)!hree c) 9our Answer:b Answer:b

This is exam number 6.

1. A diode connected across a coil will a) prevent bac* ;,9 and allow faster switching b)suppress arching when when relay is opening and closing c) prevent the coil being fitted the wrong way Answer:b Answer:b

. %hich fault does not trip the G#<2 a) 3nder fre:uency and under volts b)ver fre:uency and over volts c) ver fre:uency and under fre:uency Answer:c Answer:c

$. 4ifferential 4ifferential protection in a generating system a) detects voltage difference between source and load b)detects current current difference between between source and load c) uses the volts coil to trip the G#< Answer:b Answer:b

'. pen phase sensing on a current transformer a) is detected using all phases b)is detected using using any phase c) is detected on generator neutral circuit Answer:c Answer:c

+. ;mergency ;mergency floor lighting system is inoperative& then a) the aircraft is allowed to fly empty to a main base b)the aircraft is not allowed to fly fly until repaired c) the aircraft is allowed to fly in daylight conditions only Answer:a Answer:a

. A white light must be a) of five candela showing showing from starboard side side through an angle of 110 degrees in the hori?ontal plain b)of at least $ candela showing showing through an angle of 110 110 degrees from dead astern in the hori?ontal plain c) of at least $ candela showing through 0 degrees degrees from dead astern to each side in the hori?ontal plain Answer:c Answer:c

. (f battery battery is switched off in flight the a) battery is disconnected from bus

b)generator voltage falls to ?ero c) captainBs instruments will be powered from the standby bus Answer:a Answer:a

8. !o flash a generator field a) generator must be stationary b)rotate but not on line line c) on line and producing a voltage less than the flashing voltage Answer:a Answer:a

/. A hydraulic motor motor generatorBs voltage and and current is controlled controlled by a) the swash plate b)the constant speed speed drive c) the voltage regulator Answer:c Answer:c

10. !he ground interloc* pins are numbered a) A and  b)# and " c) ; and 9 Answer:c Answer:c

This is exam number $.

1. A nose down change change of trim @tuc* under) occurs occurs due to shoc* shoc* induced on a) tip stall on a straight wing aircraft b)tip stall on a delta wing aircraft aircraft c) root stall on a delta wing aircraft Answer:c Answer:c

. Cone $0 under the A!A system is a) vertical stabiliser

b)central fuselage fuselage c) hori?ontal stabiliser Answer:a Answer:a

$. %hen doing a bonding chec* chec* the maimum resistance between component and earth is a) 0.00+ohms b)1+0 ohms c) +0 milliohms Answer:c Answer:c

'. %hich instrument are most li*ely li*ely to damage damage if you have a rapid drop in pressure& when carrying out a pilot static lea* chec*2 a) Altimeter b)Air speed indicator indicator c) vertical speed indicator Answer:a Answer:a

+. !he aeroplane aeroplane fin is of symmetrical symmetrical aerofoil aerofoil section section and will therefore provide a side-load a) only when the rudder is moved b)if a suitable angle of attac* attac* develops due either either yaw or rudder movement c) only if a suitable angle of attac* attac* develops due to yaw Answer:b Answer:b

. An aircraft aircraft left wing is flying flying low. low. !he aileron aileron trimmer control to the left aileron trim tab in the coc*pit would be a) moved up causing causing the left left aileron to to move down b)moved up causing causing the left aileron to to move up c) moved down causing the left aileron to move down Answer:a Answer:a

. !he bearing used in a fibre pulley is

a) a roller bearing b)a plain bearing bearing c) a ball bearing Answer:c Answer:c

8. !he real time on a #,# is when a) eisting faults page is selected on the #43 b)ground test page is is selected on the the #43 c) fault history page is selected on the #43 Answer:a Answer:a

/. !he signal line between between the controller and discharge discharge valve is lea*ing. !his will cause a) the cabin pressure to decrease b)the cabin pressure pressure to increase c) it will not effect on cabin pressure Answer:b Answer:b

10. A spill valve opens a) to control the air from the cabin to outside b)to control the flow to the cabin c) to prevent an ecessive pressure difference Answer:b Answer:b

This is exam number %.

1. An aircraft aerofoil is eposed to supersonic flow. flow. !he boundary boundary layer a) is subsonic b)increases in depth depth c) is supersonic Answer:a Answer:a

. A bra*e debooster valve is provided provided for a) decreasing the pressure and slowly releasing the bra*es b)applying bra*e pressure pressure slowly and releasing releasing the the bra*es bra*es :uic*ly c) increasing the pressure and applying the bra*es rapidly Answer: Answer:

$. A symmetrical aerofoil is accelerating accelerating through through ,ach 1 with an angle of attac* of 0D. A shoc* wave will form for m a) on the upper surface only and move aft b)on the upper and lower lower surface and will will move aft until until the point of maimum camber c) on the upper and lower surface and will move aft Answer:c Answer:c

'. ne of the inputs in a #,# is autopilot controls. controls. !he !he data will be stored in a) volatile memory b)non-volatile memory memory c) erased only after end of sector Answer:b Answer:b

+. !he runway heading is a) E47 b)E4< c) E4, Answer:c Answer:c

. A spar web will ta*e loads in a) shear b)tension c) bending Answer:a Answer:a

. %hat *ind of seal are used on firewall firewall bul*heads2 bul*heads2 a) soft rubber

b)fire-proof grommets c) "one re:uired Answer:b Answer:b

8. A fuel cross-feed cross-feed valve is powered powered from a) A# busbar b)the battery c) 4# busbar Answer:c Answer:c

/. A fuel cross-feed cross-f eed valve is lubricated a) by the fuel b)by internal cooling cooling c) by air Answer:a Answer:a

10. A cabin altitude altitude is protected against against reaching reaching an altitude of 1$ 000ft by a) bellows in the outflow valve b)altitude sensor c) cabin over pressure relief valve Answer:b Answer:b

This is exam number &.

1. 7ow is damage to to the nose cone of an aircraft prevented prevented during a lightning stri*e2 a) onded Strip b);arthing Strap c) Special paint Answer:a Answer:a

. (5S mar*er beacon lights are a) green& blue& amber

b)blue& amber& amber& white white c) blue& white& green Answer:b Answer:b

$. 111.1 111.1 ,7? is a) an (5S fre:uency b)a =< =< fre:uency c) a 79 fre:uency Answer:a Answer:a

'. An autopilot >9#3 servo bra*e is a) energised on b)energised b)energised off c) energised energised at the same time as the clutch Answer:b Answer:b

+. A fluorescent fluoresc ent tube contains a) orange coatings& rare gases and mercury vapour b)phosphor coatings& rare gases and mercury mercury vapour c) iodine coatings and rare gases Answer:b Answer:b

. 4istilled water should be added added to to a ni-cad battery a) when fully charged b)at any time time c) only in the battery wor*shop Answer:a Answer:a

. verflowing electrolyte in a ni-cad battery indicates a) ecessive charging current b)not enough charging charging current c) low electrolyte temperature Answer:a Answer:a

8. !he aviation distress fre:uency is

a) 1.+,7? b)11.+,7? c) 11.+*7C Answer:b Answer:b

/. A radar altimeter altimeter in trac* mode is effective effective to a) 000 ft b)100 ft c) +00 ft Answer:c Answer:c

10. 4uring a normal engine engine shutdown& shutdown& generator generator tripping is initiated initiated by a) undervoltage b)underfre:uency c) overcurrent Answer:a Answer:a

This is exam number 1'.

1. 11.1 ,7? is a) an (5S fre:uency b)a =< =< fre:uency c) an A49 fre:uency fre:uenc y Answer:b Answer:b

. %hat does a 4ecca 4ecca "avigation system operate on2 a) 5ow 9re:uency b)7igh 9re:uency c) =ery 7igh 9re:uency Answer:a Answer:a

$. %hat is is the minimum separation separation between between a seat bac* bac* cushion and another seat or fied structure2

a) ' inches b) inches c) 8 inches Answer:b Answer:b

'. (n an an autoland autoland aircraft fitted with a #,# a) all faults are recorded in =olatile memory b)all faults are recorded in "on-=o "on-=olatile memory c) only >rimary 9aults are recorded Answer:b Answer:b

+. Adhesive Adhesive onding is a) wetting F gripping b)wetting F Setting Setting c) spread F setting Answer:b Answer:b

. !ension !ension is the stress of a) twisting b)elongating or stretch stretch c) crush or compression Answer:b Answer:b

. %hat are are the minimum number number of fire bottles in a cabin cabin with 01- $00 people2 a) $ #9 b)' ,ethyl romide romide c) ' 9ire ;tinguishers Answer:c Answer:c

8. n an aircraft with with asymmetrical asymmetrical ailerons what happens happens to induced drag when ban*ing right2 a) 4rag on inside aileron goes up but not as much as the outer b)4rag on the outer outer aileron increases increases

c)

4rag on the outer aileron is less

Answer:c Answer:c

/. %hen the the primary stops fitted fitted to a control run have been been contacted contacted a) a clearance eists at the secondary stops b)the secondary stops stops will 6ust be in in contact c) the secondary stops have been over-ridden Answer:a Answer:a

10. ;cessive wear on both sides of the control cable cable pulley pulley groove is evidence of a) pulley misalignment b)cable misalignment misalignment c) ecessive cable tension Answer:a Answer:a


1. A universal protractor protractor used to measure measure degrees of aileron aileron travel should be ?eroed a) with the aileron in the neutral position b)with the aileron aileron in the down position position c) when the aircraft is in level flight attitude Answer: Answer:

. A flying control static friction chec* a) can only be carried out during flight b)will demonstrate demonstrate that a high force force is always necessary to operate operate non-powered controls. c) demonstrates the force the pilot re:uires to overcome system inertia and move the controls

$. Anoia is due to a) release of nitrogen bubbles in the blood b)lac* of oygen c) low air pressure on the body

'. !he basic basic system system of cabin pressurisation pressurisation is is to arrange a constant constant a) inlet and outlet b)outlet and vary the the inlet c) inlet and vary the outlet

+. !he purpose of the differential capsule in a pressure controller is to control a) the rate of pressurisation b)cabin differential differential pressure c) cabin air flow

. #ontrol of rate rate of change of cabin cabin pressure is a) more important in descent b)e:ually important important in ascent and descent descent c) more important in ascent . %ith %ith a pressurised aircraft aircraft at ma differential differential pressure pressure and a cabin pressure increase occurs& the differential capsule in the pressure controller will a) have a constant mass flow b)let all pressurising pressurising air to be spilled spilled over board c) let pressurisation to be be switched off until lea*s cause a drop in pressure

8. (f the cabin altitude increases above the normal maimum a) a warning light comes on in the coc*pit

b)compressor delivery delivery is automatically automatically boosted c) an inward relief valve opens

/. 9uel cross feed valves are lubricated by a) fuel b)special lubricant lubricant c) no lubrication needed

10. 9uel cross feed valves are operated by a) 8 v dc bus b)battery dc c) 11+ v ac A(S)ERS 1.  ! A * +

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This is exam number 1.

1. %hat is the colour of the band band on a hydraulic hydraulic seal2 seal2 a) white b)green c) yellow

. %hich of the the following has hyperbolic curve2 a) =< b)4,;

c)

5oran #

$. %hat would you use to neutralise nicad battery battery spillage2 spillage2 a) oric acid b)icarbonate of soda soda c) 4istilled water

'. A G>S satellite will come into view a) 0D above the hori?on with respect to the viewer b)1+D above the hori?on hori?on with respect to the viewer c) 10D above the hori?on with respect to the viewer

+. Apparent Apparent drift of a vertical gyro is a function function of a) sin latitude b)cos latitude c) tan latitude

. %hat is an aileron balance cable for2 a) !o allow the cable to be tensioned b)!o allow aircraft aircraft to fly hands off c) !o correct for wing heaviness . %ith %ith an increase in the ,ach number& number& the boundary boundary airflow a) remains constant b)decreases thic*ness thic*ness c) increases thic*ness

8. A comfortable cabin altitude rate of climb is a) +00ft per minute b)$00ft per minute

c)

100ft per minute

/.
10. A white steady light is re:uired a) of at least $ candelas& at the rear of the aircraft 0 degrees either side of dead astern b)of at least $ candelas& at the rear of the aircraft aircraft 110 110 degrees either either side of dead astern c) of at at least least $ lumens& at the the rear rear of the aircraft 110 degrees either side of dead astern A(S)ERS 1.  ! + * A

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This is exam number 1!.

1. efore operating generators in parallel& parallel& their voltages should be be matched to prevent a) overloading the generator drive and shearing of splines b)voltage spi*es of sufficient magnitude magnitude to trigger G#3 overvoltage circuits c) large circulating currents developing

. #onsumer loads are connected to a busbar a) in parallel so when loads are shed current is reduced b)in series so when when loads are shed shed current is reduced reduced c) in series so when loads are shed voltage is reduced

$. A current transformer transformer connected connected on the the neutral star point of a generator is for a) negative se:uence protection b)overload protection protection c) differential differential current protection

'. 4ifferential 4ifferential protection protection as applied applied to A# generation systems compares compares a) generator current to busbar current b)generator voltage to busbar voltage c) ambient pressure to cabin pressure

+. %hen a current transformer is disconnected a) a shorting lin* should be fitted b)a resistor should be installed c) no further precautions re:uired

. (n an A# generation system& the fre:uency fre:uency and phase rotation rotation a) must be synchronised prior prior to paralleling paralleling b)must be out of phase phase prior to paralleling paralleling c) is of no conse:uence after paralleling

. 4iodes are placed across a contactor to a) speed up operation by reducing bac* ;,9 b)prevent contact contact bounce

c)

ensure smooth contactor operation

8. >lacing the battery battery master master switch switch to off during during flight will a) isolate the battery from the main busbar b)disconnect all all power to the main main busbar c) shut down the A>3

/. !he purpose of the clutch in an an autothrottle autothrottle servo is a) to protect the servo motor in the event of inadvertent runaway b)to limit the range range of control movement movement c) to allow the pilot to override

10. %hilst operating paralleled paralleled A# constant fre:uency fre:uency generators& generators& it is important to maintaingenerator outputs at the same voltage a) to prevent a circulating current developing between two or more !<3s b)to prevent a circulating circulating current of considerable magnitude magnitude developing between two two or more generators c) to prevent #S4 shoc* loading A(S)ERS 1.  ! A A *

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This is exam number 1".

1. A voltage regulator regulator installed installed in series with with a generator generator field field

a) uses a current coil in parallel with generator output b)uses a voltage coil in series with with generator output c) uses a voltage coil in parallel with generator output

. #S4 warning lights on the flight flight dec* dec* normally normally indicate indicate a) high oil pressure& low oil temp b)low oil pressure& pressure& high oil temp c) low oil pressure& underfre:uency

$. !he output output fre:uency fre:uency of a hydraulically hydraulically driven driven standby generator is controlled by a) a hydraulicall hy draulically y actuated swash plate b)an (4G c) a #S4

'. An A# generator used with a #S4 a) does not need a voltage controller because voltage is *ept constant b)does not need a voltage controller controller because current is *ept constant c) needs a voltage controller to maintain voltage with increasing load

+. >ower to a G#3 is supplied a) initially by a field tic*lingB supply and then >,G output b)generator output only only c) battery bus or rectified generator output

. !rip signals for a G#< are a) underfre:uency and overcurrent b)differential b)differential protection and undervoltage undervoltage c) overfre:uency and undervoltage

. Abnormal Abnormal #S4 operation is monitored on the flight dec* by observing indications of a) high oil temp  low oil pressure b)7igh oil temp temp  low oil :uantity :uantity c) low oil :uantity  low oil temp

8. %ires %ires in hot temperature temperature areas areas should should be bound with with a) "ome b)!eflon b)!eflon c) >=#

/. A heat gun should be operated at a) 100 degrees above the specified b)100 degrees below the specified specified c) at the specified temperature

10. 7igh voltages voltages on a generator generator in a parallel parallel system system should be prevented because because a) it will damage the drive shaft b)it will cause cause high circulating circulating current in the bus  other generators c) it will trip the G#< A(S)ERS 1.  ! * + A

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This is exam number 1#.

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1. ver voltage condition trips the generator. generator. !he time time ta*en to trip the G#3 depends on a) closing of fuel and hydraulic valves b)amplitude of voltage voltage c) time delay circuit

. Speed of 7,G is controlled by a a) swash >late b)#S4 unit c) (4 unit

$. !rac* mode of
'. >ermanent ,agnet should have a) low retentivity& high coercivity b)high retentivity& retentivity& low coercivity coercivity c) low retentivity& retentivi ty& low coercivity

+. 7ow many many floor path lights lights can you fly with unserviceable2 unserviceable2 a) 1+H b)0H c) +H

. 7ow many aerials are there in a !#AS system2 a) $

b) c) 1

. %a %avelength velength of I band radar is a) $ cm b)+ cm c) 10 m

8. >recipitation static is caused by a) 79 radiation b)lightning stri*es c) s*in to air particle collisions

/. 79 aerials have wea* points designed at a) front end b)bac* end c) both ends

10. 7ow is a serrated rod ice ice detector detector bench tested2 a) y a motor load test b),otor test and gono-go gono-go gap measurement measurement c) Screwdriver tor:ue test A(S)ERS 1.  ! + A +

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1. %hat is reply fre:uency of an aircraft transponder2 a) 1000 ,7? b)10$0 ,7? c) 10/0 ,7?

. 7ow often do hand-held etinguishers have to be weighed a) Annually b)i-annually c) ;very + years

$. #A!  <=< <=< limit limi t is a) 10&000 ft b)100 ft c) 1000 ft

'. =ertical pro6ected separation between seat rows must be a) $ inches b)' inches c) + inches

+. 4issimilar ,etal 9usion onding is best for a) high strength and high stiffness b)high strength and toughness toughness c) high strength and ductility

. A 9uselage Station is a a) longitudinal point point on the the aircraft aircraft fuselage b)lateral point on aircraft fuse c) lateral point on aircraft wing

. >rior to aluminium alloy bonding& we use a) solvent etch b)al*aline etch etch c) acid etch

8. %hat will happen if if the aircraft battery becomes overheated2 a) !he hot battery bus will be disconnected from the battery b)!he battery charger charger will switch to tric*le tric*le charge mode mode c) !he power supply to the battery charger charger will will be interrupted

/. !he purpose of a slot in a wing is to a) act as venturi& venturi& accelerate accelerate the air and re-energise re-energise boundary layer b)speed up the airflow airflow and increase increase lift c) provide housing for the slat

10. !he purpose of primer is to a) help bonding of the topcoat b)provide shiny surface for the topcoat c) provide fleible surface for the top coat A(S)ERS 1.  ! * A +

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This is exam number 1$.

1. 5arge flap deployment a) causes increased spanwise flow towards tips on wing upper surface

b)causes increased increased spanwise flow flow towards tips on wing wing lower surface c) has no effect on spanwise flow

. At speeds greater greater than mach1 airflow airflow in the boundary layer is a) subsonic b)supersonic c) stationary

$. A machmeter wor*s a) above 10000ft b)always c) always ecept on the ground

'. %ith %ith the elevator trim trim wheel ad6usted fully fully aft. @nose up) range of movement of the elevator is restricted a) for JupJ travel movement b)for JdownJ travel movement movement c) would ma*e no difference to the movement

+. Acrylic Acrylic windows must be able to fle in situ because because they have a) larger coefficient coefficient of epansion than surrounding structure b)smaller coefficient coefficient of epansion than surrounding surrounding structure c) slight shrin*age due to age

. ;ngine wing wing firebottles firebottles should be charged charged with nitrogen nitrogen at 1+o# to a) 1+00psi b)1+0psi c) 00psi . %hen the temperature temperatu re increases in a lead acid battery& the SG will

a) increase b)decrease c) remain the same

8.
/. Angle of Attac* Attac* alarm alarm is sounding too close to stall.
10. %hen does auto trim trim operate operate at a lower speed2 a) %hen flaps down b)%hen gear down c) %hen flaps up A(S)ERS 1.  ! + A +

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This is exam number 1%.

1. A water separator is located

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a) downstream of turbine b)downstream of heat heat echanger c) upstream of the turbine

. A cargo bay must have signs stating a) no ha?ardous cargo b)ma dimensions dimensions c) ma loadings

$. %here is alpha angle used2 a) Accelerometer b)(
'. A fire that can be put out by a crewmember in a cargo bay is a a) class A b)class  c) class 4

+. Spoilersspeedbra*es Spoilersspeedbra*es deploy to a) 1+ deg b)$0 deg c) 0 deg

. 9uel systems that are interconnected interconnected must must have a) air spaces interconnected interconnected b)separate venting venting for each tan* c) no airspace . As fuel level increases& system capacitance

a) decreases b)increases c) no change

8. %hen refuelling a) the fuel no??le will automatically cut off the supply when the tan* is full b)it is important to to fill the epansion space space in the tan* tan* c) it is important not to fill the epansion space in the the tan*

/. %hich part of the wing wing of a swept-wing swept-wing aircraft aircraft stalls stalls first2 first2 a) !ip stalls first b)
10. #omposite material is bonded by a) copper wire b)special paint paint c) aluminium wire A(S)ERS 1.  ! A * *

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1. #argo nets are manufactured from a) hessian

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b)polypropylene c) nylon

. %ith %ith autopilot autopilot engaged engaged which control surface surface is inhibited2 a) ;levators b)Ailerons c) !7S

$. %hen flaps are lowered the the automatic automatic trim trim system will a) increase the angle of incidence of the !7S b)decrease the angle of incidence incidence of the !7S !7S c) angle of incidence remains the same

'. 4uring flight an aircraft aircraft is yawing to the right. !he aircraft aircraft would have a tendency to fly a) left wing low b)right wing low c)

nose up

+. (n autopilot the control column a) does not move b)moves in pitch c) moves in pitch and roll

. %here is the spinuprundown bra*e2 a) (nner gimbal b)uter gimbal c)
. n replacing a pre-indeed flu valve you would would a) carry out a chec* swing after fitment b)fit the serviceable serviceable pre indeed flu flu valve into the same position as the unserviceable pre-indeed flu valve was removed from c) align the Aircraft onto itKs itKs LAK:uotient LAK:uotient so that no error is induced

8. (n Airways Airways flying& flying& what is the barometric scale of the altimeter altimeter set to2 a) E9; b)E"7 c) 101$.+

/. Cone 4 #argo compartment windows a) are made from fire retardant >erspe b)must have blinds pulled down c) must be blan*ed off

10. A LhyperbolicK Lhyperb olicK system is a) (5S b)=< c) 5
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1. A fire ?one in in which a crew member member could enter enter to fight a fire is a) class A b)class  c) class ;

. %hen is LautothrottleK disengaged2 a) n selection of thrust reverse b)After thrust reverser reverser has deployed beyond beyond /0H so that !GA !GA can be selected in case of emergency c) n landing

$. n testing testing a generator it it is found to re:uire ad6usting& ad6usting& where where would would you ad6ust it2 a) (n the coc*pit on the flight engineers panel b)n the G#3 c) y means of a remote trimmer

'. !ubeless tyres are stored a) hori?ontally maimum of four high with smallest diameter tyre on top b)vertically c) at 1+ to 0 >.S.(.

+. #ontrol of hydraulically powered emergency emergency electrical electrical generator fre:uency is a) by angle of swash plate b)by (4G c) by #S3

. Aircraft Aircraft with autopilot and and auto trim& a pitch command command input will cause a) column to move and trim system to move b)column to move and and trim system not to to move c) column will not move and trim system will move . A!A 100 10 0 is a) upper fuse b)lower fuse c) left hand wing

8. n a wheel bogie unit& positive camber is a) top of wheels closer together b)bottom of wheels closer together c) front of wheels closer together

/. (n regard to the aircraft transponder& transponder& what is is the pulse fre:uency2 fre:uency2 a) Amount Amount of times interrogating signal is sent per second b)"umber of pulses per per signal c) Amount Amount of times reply signal is sent per second

10. %e %eight ight of an etinguisher etinguis her is stamped a) on base of body b)on head fitting c) on brac*et A(S)ERS 1.  ! A A *

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This is exam number 1 .

1. (n a #,# #,# system where would would you find a Lreal timeK timeK fault2 a) (n !est b)(n 9ault c) (n 9ault 7istory

. !oilet oilet flush motor is is protected protected from overheat by a) cooling fan on timer switch b)thermal protection protection c) water cooling

$. (n a capacitive fire detection system& if a) there is a brea* the system will wor* but not test satisfactory b)there is a short short to earth the system system will wor* but not test satisfactory c) there is a brea* the system will not wor*

'. 5ife 6ac*ets are inflated with cylinders of a) air b)# c) "itrogen

+. %hen using iopor microbial fuel growth treatment a) it is applied wet and flushed out b)it is applied dry and left c) it is added to the fuel and burnt

. ,icrobial growth is a) brown blac* slime b)red dots c) green sludge . =ibration =ibration monitoring monitori ng signals are sent a) direct to the gauge b)via a 1 wave wave rectifier to the the gauge c) via a signal conditioner to the gauge

8. !he vacuum vacuum system gauge reads reads + inches inches of mercury. mercury. !his is from a) ambient and minus b)?ero and minus c) ?ero and positive

/. Solid burning oygen units have a burn time time of a) 1+ min b)$0 min c) '+ min

10. A direct reading reading bordon gauge has a restriction restriction in the inlet& this is to a) prevent 94 ingestion b)dampen sudden pressure pressure changes c) allow for calibration A(S)ERS 1.  ! + + +

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This is exam number .

1. %indshield %indshield heating provides a) impact resistance enhancement b)increases strength strength to resist cabin pressure c) thermal epansion for a tighter fit

. #A!  <=< <=< limit limi t is a) 800m b)'00m c) 00m

$. %hen the the moisture separator is is purged purged in a pneumatic system& it dumps a) the whole system b)6ust the moisture trap c) the system between compressor and regulator valve

'. !he pneumatic system pump is a) rotor vane b)piston c) centrifugal

+. A badly corroded corroded and pitted bra*e bra*e dis* will a) wear bra*e pads too :uic*ly& and should be replaced b)be o*& and provide better grip

c)

produce a loss of fluid

. At what press press and temp is is anti ice fluid applied2 applied2 a) 0 deg deg # at 100psi b) deg 9 at 100psi 100psi c) 0 deg 9 at 10psi

. (n semi-monoco:ue semi-monoco:ue construction& compression loads are ta*en by a) stringers b)frames c) bul*heads

8. %ing %ing bending bending and shear loads loads are are ta*en ta*en by a) spar cap b)main spar c) s*in

/. !he dilutor demand regulator functions a) when the user breathes in b)all the time time c) only when the supply valve is opened by the user

10. A maintainer valve in in an hydraulic system system will will a) allow continued press to essential systems during times of reduced supply b)dampen pressure inputs inputs c) maintain a high pressure to all systems A(S)ERS 1.  !

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This is exam number !.

1. (n a pneumatic pneumatic system system the maintainer valve valve will will be fitted in supply lines to a) essential e:uipment b)non-essential e:uipment e:uipment c) all e:uipment

. A comfortable rate rate of cabin cabin altitude altitude climb climb for passengers passengers is a) +00ft per min b)$00 ft per min c) 100 ft per min

$. !he hot 6unction of thermocouple is a) in the instrument b)in the combustion combustion chamber c) aft of combustion chamber

'. %ith %ith a drop in ambient ambient temperature& temperature& an aircraft service service ceiling ceiling will a) lower b)rise c) not be affected

+. efore carrying out a ground pressure chec*& a) chec* all pitot and static lines are fitted

b)turn on all instruments instruments c) set altimeter to E"7

. !he bonding bonding lead to a remote aircraft aircraft component component must must be a) 0.+ in wide b)0.+ in wide and and  A% A%G c)  A%G

. !o measure moisture in an oygen oygen system system use a) a glass plate b)litmus paper c) a hygrometer using the dew point method

8. ,ost large transport aircraft s*ins are a) 0' b)0+ c) +0+

/. %here is the temperature overheat switch switch located located in a hydraulic pump2 a) (n the pressure line b)(n the suction line line c) (n the case drain

10. 7ow much oygen is in a tyre2 a) +H by volume b)1+H by volume c) +H by pressure A(S)ERS 1.  !

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This is exam number ".

1. A tyre specification specification $  10.+ 10.+ - 1'. %hat does the 10.+ refer refer to2 a) ead diameter b)Section %idth %idth c) verall diameter

. %hat happens if if a component has an internal hydraulic lea*2 a) (ncrease in pressure b)(ncrease in temperature temperature c) 9luid loss

$. %hat happens to hydraulic fluid when when it it is overheated2 a) (ncrease viscosity b)(ncrease acidity c) (ncrease al*alinity

'. %hen servicing servicing an oleo& fluid comes out of the air valve when the leg is depressurised2 a) !he leg is serviceable - the separator has bottomed b)5ea*ing airoil seals seals c) Separator plate stuc* open

+. %hen does auto trim trim operate operate at a lower speed2 a) %hen flaps down

b)%hen gear down c) %hen flaps up

. %hat force is an (-eam sub6ected to2 a) ending b)!ension b)!ension c) Shear . 7ow is the hydraulic pump depressurising depressurising solenoid actuated2 a) ;nergised pen b);nergised b);nergised #losed for fail-safe c) ;nergised ;nergised both open and closed depending on coc*pit selection

8. 7ow do you prevent hydraulic fluid frothing2 a) =ia tray b)=e b)=ent
/. %hen a ni-cad battery is fully charged a) the electrolyte level stays the same b)the electrolyte electrolyte level is higher higher level than normal normal c) the electrolyte level is lower than normal

10. 7ow many programs can a 9,# store2 a) ne current b)!wo. b)!wo. ne active active and one standby c) !wo. !wo. oth active A(S)ERS 1.  ! + + +

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This is exam number #.

1. ;>< and speed for autothrottle autothrottle is activated at a) cruise b)ta*e off c) approach

. 7ow does an (
$. %hat is the the arc arc of a landing landing light light is is a) 11 degrees b)1+ degrees c) 0 degrees

'. (n an autopilot what controls pitch mode2 a) Glideslope b)=< c) 5ocali?er

+. Glideslope controls autopilot in a) pitch b)yaw

c)

roll

. Static dischargers dischargers help eliminate radio interference interference by dissipating dissipating static electricity into the atmosphere at a) low current levels b)high voltage levels levels c) all voltage levels . ;lectrical load on aircraft is controlled by a) a G#3 b)a >#3 c) an (
8. %hen a rad. alt. alt. reaches reaches +00 ft what happens happens to the display2 display2 a) rad. alt. out of view b)rad. alt. flag in view c) error warning in view

/. A radome is protected protected from static electricity electricity buid-up by a) onding strips b)Special conductive conductive grease c) #onductive paint

10. An aspect ratio of 8 would mean a) span '& mean chord 8 b)mean chord '& span span 8 c) span s:uared '& chord 8 A(S)ERS 1.  ! + A A

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This is exam number 6 .

1. %hich of the following statements is correct& correct& in relation to >5( washers used in critical bolted 6oints2 a) >5( washers can be used more than once& providing they are used in critical bolted 6oints b)>5( washers can can be affected affected by thread or nut friction friction or by lubrication c) >5( washers can only be used with self loc*ing loc*ing nuts and the washers should be used once

. >recise points are located on an aircraft by by a system of a) frame stations& water lines and buttoc* lines b)frame stations& stations& vertical lines and and lateral lines lines c) longitudinal& vertical and lateral lines

$. %indscreen delamination delaminati on is a) windscreen peeling away from the airframe b)bubbling of the glass due due to overheat c) separation of the glass from the vinyl interlayer

'. %hat is the ideal storage temperature temperature for windscreen windscreen panels2 panels2 a) +0o9 to 0o9 b)$0o# to +0o# c) +0o# to 0o#

+. %hat is is the maimum temperature temperature of warm water water which which is used used to clean dirty aircraft acrylic panels2 a) 10'o9 b)'0o9 c) 1+o9

. >itot tubes are heated a) electrically b)by compressed bleed bleed air c) by *inetic heating

. Accumulators Accumulators as fitted fitted to aircraft aircraft hydraulic hydraulic systems a) provide additional fluid if lea*s occur b)are only ever used used in an emergency emergency c) store fluid under pressure

8. A S*ydrol hydraulic hydraulic fluid seal would be made of a) utyl rubber& ethylene propylene or !eflon b)natural rubber c) synthetic rubber

/. Synthetic hydraulic fluid sub6ected sub6ected to overheating is high high in a) acidity b)al*alinity c) viscosity

10. !he advantage of leading edge fluid de-icing is a) aerodynamic shape is not disturbed

b)more efficient efficient c) less of a fire ha?ard A(S)ERS 1.  ! * A *

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This is exam number $.

1. !he type type of fluid in an oleo oleo strut will depend depend upon a) type of fluid most readily available b)the type of seal seal material c) heat generated in operation of the system

. A restrictor restricto r valve a) may be used to slow down undercarriage etension b)restrict the etent etent of travel of the undercarriage c) speed up the flow in one direction

$. !he function function of the oil in a shoc* absorber absorber is to a) damp the rebound b)absorb the landing landing shoc* c) ensure the separator does not bottom

'. !he purpose of the flutter plate plate in a shoc* absorber is to a) separate the oil from the air b)restrict the compression compression of the air c) permit free flow of oil during compression and restriction of oil during etension

+. ygen cylinder test dates a) are painted in white on the cylinder b)may be stamped stamped on the nec* of the the cylinder c) are variable depending on discharge

. 9luorescent tubes are contain a) phosphates& rare gases gases and mercury b)oides& rare gases gases and mercury c) ionides& rare gases and mercury . A '1 step-up transformer receives 10=A# 10=A# in its primary and has 100 hms resistance in its secondary. %hat is the current drawn2 a) $ A b)1. A c) 0.$ A

8. %hat is -<"A -<" A=2 a) Ability Ability to store  waypoints b)(ndicates true airspeed airspeed c) (ndicates bearing and airspeed until net active waypoint

/. An Automatic Automatic 9light #ontrol System receives inputs from the following ground based transmitters a) 4,;& (5S& A49 b)=<& (5S c)
10. After After engine start using a "i#ad "i#ad battery& battery& the pilot observes observes on the battery charger charger indicator& indicator& an initial initial high current draw followed followed by a rapid decrease in current

a) there is a problem with the charging circuit and he must shut-down the engines b)the battery is faulty c) no cause for concern A(S)ERS 1.  ! * A +

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This is exam number %.

1. !opping !opping up a "i#ad battery in situ a) is not allowed b)is only allowed allowed in the shop c) is permitted

. %hat opposes buc*ling in a semi-monoco:ue structure2 a) 9rames b)Stringers c) ul*heads

$. !he visible visible angle angle of a white white tail tail navigation navigation light is a) 11 degrees b)110 degrees c) 1'0 degrees

'. %hat is the wavelength of # band radar2 a) $ cm b)1 m c)  cm

+. 0 system pressure has lea*ed away away after after charging. charging. %hat %hat is the most probable cause2 cause2 a) Supernumarator regular b)!emperature b)!emperature #ompensator #ompensator c) reathing
. ,ade up wheels should be stored a) vertical at 0$0 >S( charge b)hori?ontal no more than than ' high c) vertical at wor*ing pressure . 7igh pressure pneumatic source is a a) reciprocating pump b)centrifugal #ompressor #ompressor c) butterfly pump

8. 7igh pressure pneumatic pump is a a) spur gear b)butterfly pump c) reciprocating pump

/. efore an aircraft reaches critical mach a) the nose pitches up because the #> moves 9orward b)the nose pitches pitches down because the #> moves rear c) the aircraft buffets because the #> moves to the shoc* wave

10. A cantilever wing is a) top wing of a biplane b)normal airliner airliner wing c) sweep bac* wing

A(S)ERS 1.  ! A + *

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This is exam number &.

1. A horn balance on a control will a) increase degree of movement at high speed b)decrease degree degree of movement at at low speed c) decrease degree of movement at high speed

. !he suction suction gauge reads + inches of mercury. mercury. !his is a) above ambient pressure b)below ambient ambient pressure c) above ?ero pressure

$. (n normal flight if the the control column is pulled bac*& bac*& a servo tab fitted to the elevator will a) move up b)move down c) remain in line with the elevator

'. (n normal flight& if the control wheel is is moved to the left& then then the aileron on the right wing will a) increase the angle of attac* of the right hand wing b)decrease the angle of attac* attac* of the right hand wing wing c) *eep the angle of attac* of the right wing constant

+. n an aircraft fitted fitted with elevons in normal flight& if a column is

moved forward& the elevons will a) remain stationary b)both move up c) both move down

. ;tending a leading edge edge slat will have have what effect on the angle of attac* of a wing2 a) increase the angle angle of attac* b)decrease the angle of attac* attac* c) no effect on angle of attac*

. !o ensure ensure that a wing stalls stalls at the root first& stall stall wedges are a) installed on the wing leading edge at the wing tip b)installed on the wing leading edge edge at the wing wing root c) installed at the wing trailing edge at the wing root

8. n a standard day at which altitude will the speed of sound be the the greatest2 a) sea level b)10&000 ft c) 0&000 ft

/. %hich of the following following will will increase the #ritical #ritical ,ach "umber of an aerofoil2 a) using a thin airfoil and sweeping the wings bac* b)increasing the aspect aspect ratio of the wings c) decreasing the fineness ratio of the wings

10. As an aircraft aircraft accelerates accelerates through the transonic transonic region the centre centre

of pressure tends to a) move forward b)move rearward c) turn into a shoc* wave A(S)ERS 1.  ! A * +

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This is exam number !'.

1. %hich of the following following is an eample eample of a fail safe structure2 a) Spar b)Stringer c) 5ongeron

. 4amage tolerant design a) allows for certain damage to the structure to go un-repaired between scheduled maintenance b)allows for damage damage to structure by distributing distributing loads to other other structure c) is applied only to secondary structure

$. %hat is primary radar2 a) 5and based b)
'. 5ead acid acid battery battery after after numerous chec*s one cell cell has low reading. reading. a) (t is defective b)(t must be replaced replaced c) (t needs topping up

+. %hat is (5S mar*er beacon fre:uency2 a) +0,7? b)+,7? c) 100,7?

. !#AS is selected a) automatically b)by a switch& by pilot on selector selector panel c) not available in cruise . !he minimum minimum passenger passenger aisle aisle width width for an aircraft aircraft with with a seating capacity of 0 or more is a) 1+J b)'J c) dependant upon aircraft type

8. A short range passenger aircraft aircraft has complete electrical electrical failure. %hat time duration would the battery be epected to power essential e:uipment2 a) forever b)$0 minutes c) 0 minutes

/. An eternal power plug has two short pins& these are are used for

a) the interloc* circuit b)ground handling bus c) a guide for correct correct alignment of the plug in the soc*et

10. %hat are the primary colours colours for use in #
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This is exam number !1.

1. %ing %ing navigation navigation lights must be visible from which angle2 a) 110 degrees b)180 degrees c) 1+ degrees

. !he purpose of a synchronising bus bar is is a) to allow monitoring and trimming from the flight dec* b)to monitor total current current load c) to enable two propeller systems to be synchronised

$. !he manual =< input is for a) <,( b)course deviation deviation bar c) glideslope .

'. (n an aircraft where the autopilot is controlling controlling a turn turn a) 1 aileron is up& 1 aileron down for the duration of the turn b)both ailerons down for the duration of the turn turn c) 1 aileron up& 1 aileron aileron down to set the ban* angle and then ailerons bac* to neutral

+. (n the A!A 100 ?onal system the passenger entry door will have a designation of a) '00 b)00 c) 800

. %hich area of the aircraft aircraft is sub6ect to hoop stress2 a) %ings b)>ressure cabin c) #ontrol surfaces

. (n a monoco:ue structure& which component carries the ma6ority ma6ority of the loads2 a) 5ongerons b)Stringers c) S*in

8. %hich anti corrosive corrosive treatment is found on alloy alloy steels2 steels2 a) #admium plating b)Cinc plating c) "ic*el plating

/. %hat material can be chromated as a protection against corrosion2

a) Aluminium alloys b),agnesium alloys alloys c) 9errous alloys 10. %hen carrying carrying out a symmetry symmetry chec* on a large aircraft what what method method of measurement is normally used2 a) Steel tape and spring balance b)5ongitudinal alignment alignment method c) 5ateral alignment method A(S)ERS 1.  ! A A +

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This is exam number !.

1. 7ow are are passenger passenger door pressure loads loads transmitted transmitted to the fuselage fuselage structure2 a) y door stops b)y the pressure seal seal c) !hrough the latching mechanism

. >assenger cabin cabin windows windows are constructed with with two panes and a seal between them. them. 3nder normal flight flight conditions which pane@s) pane@s) ta*e the differential differential pressure loads2 a) oth b)(nner c) uter

$. 7ow are passenger seats secured to the the floor2 a) y the bac* legs while the front attachment provides anti rattle b)y the front legs while while the bac* attachment provides provides anti rattle. rattle. c) y both front and bac* legs

'. n a monospar wing& wing& what gives the the wing its profile contour2 a) !he position of the spars b),illed stringers c)
+. A normal hydraulic hydraul ic system will a) show pressure and source of hydraulics b)show fluid temperature temperature and :uantity :uantity c) illuminate a light in the coc*pit when the system is ready

. A fire detection detection ?one wiring wiring can pass through another fire ?one when a) the system and the etinguishing etinguishing system are the same same b)the system is the same but the etinguishant is different different c) the system is different but the etinguishant is the same . n touch down of aircraft a) the cabin pressure will be ?ero b)the outflow valve will be shut c) the outflow valve will be fully open

8. A galley trolley will be designed to a) not eceed the floor loading limits b)not eceed the the floor limits more than than $ times in one hour c) does not matter as the trolleys move

/. #oc*pit dome lighting is provided by the a) battery bus b)battery bus and ground services services bus c) ground services bus

10. %hen a fire test on a Systron 4onor fire detector detector system test is carried out a) a signal passes through the unbro*en centre conductor to produce the warning b)the signal passes passes through the centre centre and bac* through the outer to give warning c) it chec*s the integrity of the contacts A(S)ERS 1.  ! A * A

" *

# A

6 A

$ *

% A

& +

1' *

This is exam number !!.

1. A material commonly used for pressure bul*head bul*head sealing sealing is a) soft rubber b)aluminium c) >!9;

. !he velocity velocity of air from the cabin cabin ventilation ventilation system system should should not eceed a) 0 feet per second b)'0 feet per second second c) 10 feet per second

$. !o avoid moments moments bending the root of the wing& the aircraft will will be fitted with a) symmetrical flight control trim b)integrated fuel monitoring system c) automatic trim control for controlled turns and rudder movements

'. After After ,5G down down and securely loc*ed loc*ed a red light is illuminated illuminated in the flight dec*. dec*. !he possible causes causes are are a) shorted sensor b)out of ad6ustment sensor sensor c) wiring problem

+. A wingBs leading leading edge would have provisions and lin*ages for slats and a) slots b)leading edge flaps flaps c) trailing edge flaps

. A yaw damper gain could be fitted with a) increased sensitivity for increased speed b)decreases sensitivity sensitivity for decreased decreased speed c) decreases sensitivity for increased speed

. !o confirm the state of charge of a nicad battery a) sub6ect the battery to load and chec* the voltage b)measure the discharge discharge time time c) sub6ect the battery to load& load& chec* chec* voltage and chec* the SG SG of each cell

8. #irculating currents are associated with a) A# generators in parallel b)4# generators in parallel c) A# and 4# generators generator s in parallel

/. (n an aircraft system employing employing balance balance tabs& the the installation installation of

eternal ground loc*s between the control surface and the balance tabs a) is unnecessary since the system is irreversible b)would prevent the movement of the control column c) would not prevent the movement of the control column 10. Supersonic air air going through an incipient shoc* wave wave will will decrease decrease its speed and a) decrease temperature and increase density b)increase temperature temperature and decrease decrease density c) increase temperature and increase density A(S)ERS 1.  ! A * A

" +

# +

6 A

$ +

% A

& +

1' *

This is exam number !" .

1. Generator brush bedding a) should not be done on the aircraft b)should only be done if +0H of the width and 80H of the length length is already being done c) can be done on the aircraft

. %hen loading a cargo aircraft a) the manufacturer specifies the maimum floor loads b)the #ofG limits limits of the aircraft could could be eceeded under careful monitored circumstances circumstances c) the weight limits of the aircraft could be eceeded under careful monitored circumstances circumstances

$. %hat is is the amperage at the shunt of the the generator generator to the nearest amp2

a) 100 Amps b)10 Amps Amps c) 10+ Amps

'. !he two switches for pitch pitch trim are located located a) on the central column with the #aptain having priority over the 9irst fficer. b)on the central central column acting li*e li*e an BA"4B switch switch c) on the central column acting li*e an B
+. !he mach trim is initiated by a) the autopilot motor b)an electric electric motor c) a >#3 . %hen chec*ing for alignment alignment of a ,5G& chec* a) symmetry& trac*ing& camber b)symmetry& b)symmetry& splay& splay& trac*ing c) symmetry& twist& trac*ing

. (f the flaps are are sluggish sluggish or erratic erratic on final approach& the possible possible cause may be a) flap trac*s out of rigging b)flap motor internal internal lea*age c) bearing sei?ed 8. Alpha vane signal could be fed fed to NNNNNNNNNNNNNNNNN NNNNNNNNNNNNNNNN when close to stall. a) thrust levers b)fastslow switch switch c) flap position /. (f an   system is lea*ing& lea*ing& where would you most li*ely li*ely find the the cause2 a) !hermal itot tubes are heated by a) A# b)4# c) A# or 4# A(S)ERS 1.  ! A A +

" +

# A

6 A

$ +

!his is eam number $+.

1. Shear stress is described as a) compressing forces b)pulling forces c) slip away under the action of forces

% *

& +

1' *

. !he ground cable must be a) copper stranded 0.+ mm cross sectional area b)single strand copper copper wire 0.+ mm cross cross sectional area area c) single strand 18 A%G

$. %hat is the the colour colour of the middle mar*er beacon2 a) %hite b)lue c) Amber

'. n large large transport aircraft& aircraft& the windshield windshield wiper system is a) independent on each side with different power sources b)independent on each each side but with with the same power power source c) one system for both sides but with the same power source

+. %here on the aircraft 9S'+& <%S'+2 a) '+J from the nose of the aircraft and '+J from the centreline of the right wing b)'+J from the nose of the aircraft and '+J from the tip of the right wing c) '+J from the datum line of the aircraft and '+J from the centreline of the right wing

. %hen performing maintenance maintenance operations on an aircraft e:uipped e:uipped with with <=S, =S, system& and a :uic* release disconnect connection is disturbed a) a full test of the system should be carried out b)a full test of the system should be carried carried out only if the aircraft manufacturer recommends to do so c) the allowances for the system should be halved

. 9or aircraft certificated after 1// and with <=S,& <=S,& the maimum tolerance for the system would be a) F- 00 feet plus F- +0 feet for instrument error b)F- +00 feet for the system overall c) F- $00 feet plus F- +0 feet for instrument errors

8. A G>S system is formed from a) space& control& user b)satellites& b)satellites& processing unit& display display unit c) receiver& receiver& processing unit& interactive console

/. 9or aircraft with dual #,#s& when when only one #,# is available& it a) must be connected to the left side b)must be connected connected to the right side side c) can be connected to either side 10. !hese mar*ings are found on a tyre - $  10&'+ - <1'. %hat does the number $ mean2 a) (nner diameter b)uter diameter diameter c) width A(S)ERS 1.  ! * + *

" A

# *

6 +

$ A

% A

& A

This is exam number !6.

1. %ith %ith reference to differential aileron control

1' +

a) drag increases on the inner wing b)drag decreases decreases on the outer wing c) drag increases on the outer wing

. 7S( provides information on a) =<& (5S& plan& attitude b)=<& plan& map& (5S& radar c) =<& (5S& map& radar& attitude

$. 5aser gyros are a) aligned to the aircraft structure b)aligned to the magnetic north c) aligned to the true north

'. 5aser gyros a) have rotational parts b)do not have rotational rotational parts c) have moveable parts

+. !he sensing element of the flu valve a) aligns itself to the new heading of the aircraft after it has stabilised b)aligns itself to the new heading heading as the aircraft aircraft turns c) remains in the same position attached to the aircraft structure

. As the cabin altitude reaches $0' metres metres a) the 0 mas*s deploy automatically and hang half way etended b)the 0 mas*s deploy deploy automatically automatically and the 94 crew crew must activate activate the system from the coc*pit c) the 0 mas*s deploy automatically and the 9A crew activates the

system from the emergency emergency panel

. >aint remover substances a) are damaging to some aircraft parts b)are not damaging damaging for aircraft parts c) should only be used once

8. 7ow is the radome protected from lightning stri*e2 a) 4iverter strips b)Special paint paint c) Special grease on the hinges

/. Galley e:uipment which does not need electrical electrical power is is called called a) minimum e:uipment b)controlled e:uipment e:uipment c) uncontrolled e:uipment 10. Galley trolleys must have placards indicating a) location& position& flight number b)maimum weight& weight& position& flight number number c) ,ust be stowed for ta*e-off& landing and turbulence. A(S)ERS 1.  ! A + A

" +

# *

6 A

$ A

% A

& *

1' *

This is exam number !$.

1. %hen inspecting 5avatory installations a) J"o Smo*ingJ sign should be fitted net to the ashtrays only b)the ashtray should should not be located located close to the toilet toilet paper holder c) the ashtray must be made of a thermoplastic material

. 5avatories must have in the disposal container a) waterglycol etinguisher with white ball mar*ings indicating when discharged b)9reon etinguisher with with white ball mar*ings indicating indicating when discharged discharged c) 9reon etinguisher with blac* ball mar*ings indicating when discharged

$. 9ire detection loop must be capable of a) detecting fireoverheat condition within + seconds and etinguishing such that after $0 seconds the condition is no longer present b)using master warning warning visual and aural signals signals c) using master warning visual signals only

'. >aralleling is used for a) A# and 4# electrical generators b)A# electrical generators generators only c) 4# electrical generators only

+. %hen testing emergency emergency slide bottles a) all three pins must be shorted together and grounded to the cartridge body b)one pin must be grounded grounded to the cartridge cartridge body at one time time c) any pin could be chec*ed by connecting directly to ground

. attery charging procedures procedur es can be found in A!A a) #hapter ' Section 1 b)#hapter ' Section Section $1 c) #hapter $1 Section 1 . (n a carbon pile regulator regulator the resistive resistive element is a) in series with the field and changes resistance with changing length

b)in series with the field and changes changes resistance resistance with surface area area contact c) in parallel with the field and changes resistance with changing length

8. (n fully 9ly 9ly y %ire %ire aircraft& aircraft& wing root bending moments are reduced by a) transfer of fuel from one wing tan* to another b)symmetrical application application of aileron aileron c) operation of elevator

/. A green  grey dot mar*ing on aircraft tyre casing represents represents a) breather points b)the light part of the the tyre c) military reference

10. (n detachable detachable flange flange type wheels& the flange flange is secured by a) bolts b)a loc* ring c) a retainer plate A(S)ERS 1.  ! + + +

" A

# A

6 +

$ +

% +

This is exam number !%.

1. ladder type fuel tan*s are secured by a) press type rivets b)contact adhesive adhesive c) bolts

& A

1' +

. 9use plugs in aircraft tyres are a) for overpressure protection b)for over temperature temperature protection c) to deflate the tyre before removal

$. A brea*er strip in an aircraft tyre is a) to provide strength b)to provide a wear wear indication c) to indicate the position for tyre levers

'. ygen cylinders are normally fitted with a) pressure and :uantity gauge b)oygen purity gauge c) temperature gauge

+. !o remove a rivet a) chisel off the rivet head& and remove the shan* with a metal punch b)4rill the head with a drill bit bit the same si?e si?e as the rivet shan*& chisel off the rivet head& and remove the shan* with a metal punch c) 4rill the head with a drill bit slightly smaller than the rivet shan*& chisel off the rivet head& and remove the shan* with a metal punch

. %hen acrylic acrylic and sheet metal metal is 6oined together& together& allowance should be made for a) epansion of the acrylic due to heat b)epansion of the metal metal due to heat heat c) galvanic corrosion of the metal

. ,ost aircraft s*ins are made of

a) 0' b)0+ c) 01

8. 4utch role is movement in a) yaw and roll b)pitch and roll c) yaw and pitch

/. A ?ero fuel test on a fuel :uantity :uantity indicating system is carried carried out by a) tan*s completely empty b)tan*s completely completely full c) tan*s empty with unusable fuel amount

10. A radio coupled approach is a) localiser first& followed by glideslope b)glideslope first& followed followed by localiser localiser c) in any order A(S)ERS 1.  ! A + A

" A

# +

6 A

$ A

% A

This is exam number !&.

1. Aileron Aileron signal signal is fed to rudder channel a) for turn coordination b)for yaw damping compensation compensation c) for turn command bac*-up

& *

1' A

. Maw damping rate changes with a) airspeed b)altitude c) flap position

$. After After a tan* bag has been replaced& replaced& a fuel flow test should be carried out at a) engine inlet b)tan* outlet c) tan* shut-off valve point

'. (n biologically biologically contaminated fuel& corrosion ta*es place a) below the fungal colonies b)the bottom  inches inches of the tan* c) the top of the tan*

+. (n a compass swing "orth error - degrees& South error -  degrees. degrees. !he coefficient of # is a) 0 degrees b)F degrees c) - degrees

. (f fluid lea*s along with with air whilst oleo charging& charging& this is a) caused by a lea*y seal b)normal c) due to ecessive charging pressure

. A demand regulator in in a portable oygen bottle bottle opens a) when 100H selected b)when breathing

c)

all the time

8. >ortable oygen bottles are fitted with a) a demand regulator b)an over temperature temperature indicator c) an overpressure indicator

/. American American made crew oygen cylinders are a) green in colour with a <7 thread b)green in colour with with a 57 thread thread c) blac* in colour with a <7 thread

10. !he rate of GS GS warning in G>%S a) changes with radio altitude b)changes with with barometric altitude altitude c) does not change A(S)ERS 1.  ! A A A

" A

# A

6 A

$ +

% A

& A

1' A

This is exam number "'.

1. (f you short the two prongs with the single single prong of a bonding tester together& what would the gauge read2 a) 0 b)full scale deflection deflection c) centre scale

. %hat is the the main main purpose purpose of a fri?e fri?e aileron2 aileron2 a) 7elp pilot overcome aerodynamic loads

b)(ncrease drag on the up going wing c) 4ecrease drag on the up going wing

$. %hat fre:uency are =< and (5S2 a) =79 b)379 c) 79

'. n an aircraft employing employing a heater system on the air conditioning conditioning system& after an overheat how is the heater reset2 a) n ground only by engineer b)After it cools the pilot resets c) After After cooling below $00 degrees # it auto resets

+. #onstant pressure pressure hydraulic hydraulic system uses what what to relieve pressure in system when no services are being used2 a) >ressure relief valve b)A#= c)
. (f the pneumatic pneumatic water water drain drain trap is is left open for a long time it will drain a) all the system b)between the compressor and the ><= ><= c) 6ust the moisture trap

. %hich connector has a left hand thread2 a)  b)" c) 9reon

8. %hen aligning an aircraft aircraft for a compass compass swing& swing& the maimum allowable error is a) 1 degrees b)$ degrees c) + degrees

/. %hat happens to to a hydraulically operated flight control control surface when pressure is removed2 removed2 a)
10. scillation and hunting hunting of flight control control surface are prevented prevented by a) !achogenerator b)9eedbac* from control control surface c) 9eedbac* from servo motor A(S)ERS 1.  ! A * A

" +

# +

6 +

$ A

% *

& *

1' A

This is exam number "1 .

1. Stic* sha*er sha*er activates activates at a speed which is is above the stalling stalling speed by a) 'H b)H c) 10.$1H

. !he pitot head is fitted on the aircraft. !he alignment of pitot pitot head is carried out with a) an inclinometer b)micrometer c) spirit level

$. A red dot  triangle mar* on aircraft tyres tyres means a) breather points b)the light part of the the tyre c) military reference

'. ,aimum battery temperature on charging charging before protection circuit starts is a) 1 degrees 9 b)1'' degrees 9 c) 1'' degrees #

+. (f an aircraft aircraft has no battery charger the battery battery is charged charged by a) constant voltage b)constant current c) constant current until a predetermined limit when it automatically automatically switches to constant voltage

. attery charging procedures procedur es can be found in A!A a) #hapter ' Section 1 b)#hapter ' Section Section $1 c) #hapter $1 Section 1 . (n a carbon pile regulator regulator the resistive resistive element is a) in series with the field and changes resistance with changing length

b)in series with the field and changes changes resistance resistance with surface area area contact c) in parallel with the field and changes resistance with changing length

8. !he output of a carbon carbon pile regulator with with no variation variation of loading is a) stationary b)fluctuating c) pulse width modulating

/. (n a transistor voltage regulator regulator the the voltage output is controlled by by a) transformers and transistors b)diodes and transformers transformers c) ?eners and transistors

10. >aralleled relay for 4# system system is energised energised and connected by a) voltage coil b)current coil c) voltage and current coil A(S)ERS 1.  ! + A +

" +

# A

6 +

$ +

% A

& *

1' *

This is exam number ".

1. (ncreasing the real load primarily a) decreases fre:uency b)decreases output output voltage c) increases output voltage and increases fre:uency

. (nductive reactive load causes a) no effect on tor:ue but produces etra heat dissipated b)increase in tor:ue tor:ue and increase in heat dissipated dissipated c) increase in tor:ue only

$. !he power power factor of an A# generator identifies identifies the proportion of a) apparent power from the generator that does wor* b)reactive power power from the generator generator that does wor* c) real power from the generator that does wor*

'. !he control control of hydraulically powered emergency emergency electrical electrical generator fre:uency is by a) angle of swash plate b)(4G c) restriction valve

+. 4ifferential 4ifferential protection protection in an A# system protects against a) A reverse current flowing from fro m the battery b)short circuits c) line-line& line-line-line& line-earth faults

. %hen resetting the #S4 #S4 on the ground& the engine engine should be a) stationary b)rotating at idle c) rotating at "sync . ne of the main purposes of a #S4 #S4 is to a) enable generators to be paralleled b)prevent engine overload overload c) maintain constant load on the generator

8. (n a undervolt undervolt condition condition in an A# generator system& system& the most li*ely li*ely conse:uence is a) activation of the time delay circuit b)de-activation b)de-activation of the field regulatory !
/. (f voltage and fre:uency fre:uency of the generator generator drop to ?ero in flight& flight& it would be an indication that the a) #S4 drives shaft had sheared b)phase se:uence se:uence detection circuit circuit has operated operated c) bus tie interloc* is inoperative

10. Assuming Assuming all systems are operating normally& normally& as aircraft aircraft electrical electrical load increases& generator output voltage will a) decrease and amperage output increases b)increases and amperage output increases increases c) remain constant and amperage output increases A(S)ERS 1.  ! A + *

" A

# +

6 A

$ A

% A

& A

1' *

This is exam number "!.

1. attery trays are a) metal for earthing purposes b)metal with >=# >=# coating and anti anti corrosive paint c) absorbent to soa* up electrolyte

. %hen installing multiple batteries on aircraft aircraft they are connected connected in a) parallel

b)series c) either parallel or series and switched between as an option

$. %hat is the small pin pin on the 4# ground power connector2 a) Ground or earth b)>ositive to battery battery relay c) >ositive to eternal power relay

'. n selection selection of ,5G ,5G down& the gear etends then begins to retract again. !he cause is a) a faulty selector valve b)a faulty actuator actuator c) gear lowered at too high an airspeed

+. A radio fre:uency fre:uency of 1 ,7? would be used for a) weather radar b)79 communications communications c) mar*er beacons

. A wing mounted stall warning vane a) moves up at impending stall b)moves down at impending impending stall c) gives a visual indication of impending stall . 4uring an autopilot controlled turn a) ailerons and rudder will move b)ailerons& rudder and elevators will will move c) ailerons& rudder and !7S will move

8. A Systron-4onner fire detection system uses

a) nitrogen gas b)helium gas c) oygen gas

/. A toilet is fitted fitted with with thermal thermal protection protection a) to protect against free?ing at altitude b)to protect against against the dangers of smo*e smo*e and fire in the event event of an overheat c) to protect against continuous flushing

10. n a full fly-by-wire system& a speedbra*e speedbra*e screw6ac* screw6ac* servomotor is is controlled by a) flight augmentation computer b)flight control computer computer c) flight management and guidance computer A(S)ERS 1.  ! + * *

" A

# +

6 A

$ +

% +

& +

1' +

This is exam number "".

1. (n a fly-by-wire aircraft what controls the roll spoilers2 spoilers2 a) 9light control computer b)9light augmentation augmentation computer c) 9light management computer

. (f aircraft aircraft has ability to transfer transfer fuel in flight& provision must must be made to a) shut off fuel before structural damage b)provide overflow facility facility to dump fuel c) stop engine from using tan* during transfer

$. (f an aircraft is aerodynamically aerodynamically stable a) # of > moves bac* b)aircraft becomes becomes too sensitive c) aircraft returns to trimmed attitude

'. %hat is the principle of  generator2 a) sodium chlorate and iron using a mechanical detonator producing  when mied with air b)sodium chlorate and and iron mied by an electronic electronic detonator detonator c) sodium chloride and iron mied by an electronic detonator

+. >rior to securing a leading leading edge de-icing boot you must a) remove all paint b)shave rivet to prevent prevent further abrasion c) paint the surface

. %here would you find information regarding galley e:uipment2 a) A%" // b)#A
. A large flap deployment deploy ment causes a) increased spanwise flow from root to tip on the wing lower surface b)reduced spanwise spanwise flow from root to tip tip on the wing upper surface surface c) no effect on spanwise flow

8. n a full fly-by-wire system& a speedbra*e speedbra*e screw6ac* screw6ac* servomotor is is controlled by a) flight augmentation computer b)flight control computer computer

c)

flight management and guidance computer

/. !he primary primary purpose of sealant sealant in use in pressurised aircraft is a) to seal the cabin b)to provide eternal eternal streamlining c) to prevent corrosion

10. %hat is the purpose of thermal protection protection on electric electric toilet toilet motor2 a) >revent toilet free?ing b)Stop motor running beyond 10 10 seconds if timer become become unserviceable unserviceable c) >revent motor overheating and become fire ha?ard A(S)ERS 1.  ! A A *

" +

# A

6 A

$ A

% +

& *

1' *

This is exam number "#.

1. 7ow is
. 7ow can fire etinguisher etinguisher be identified identified as being used2 a) %eighed b)#hec* the tell-tale tell-tale wire c) #hec* the pressure

$. %hat eternal warning is is there for an A>3 fire2 a)
'. %hich of the following is >erspe >erspe resistant to2 a) *erosene b),;O c) acetone

+. %hat pressure are oygen oygen cylinders cylinders usually usually pressurised to2 a) 1800 >S( b)$000 >S( c) $00 >S(

. 4itching control is used to a) achieve rapid depressurisation b)maintain cabin cabin pressure at sea level c) close the outflow valves

. 7ow often are life 6ac*ets inspected2 a) (n accordance with the A,, b)(n accordance with with the manufacturers manufacturers specification specification c) ;very 1 months

8. %hat *ind of gyro is is a rate gyro2 a) 4isplacement b)!ied b)!ied down c) Space

/. ;ngine fire bottle pressure switches are operated by a) A#

b)4# c) A# or 4#

10. 7ydraulic systems normally operate at a) $000 >S( b)$00 >S( c) 1800 >S( A(S)ERS 1.  ! A A *

" A

# A

6 *

$ +

% +

& +

1' A

This is exam number "6.

1. %hen flushing hydraulic systems a) flush with same hydraulic oil b)flush with any hydraulic hydraulic oil c) flush with methylated spirit

. %hen replenishing a hydraulic system a) use the samecorrect hydraulic fluid b)use any hydraulic fluid made by the same manufacturer manufacturer c) use any hydraulic fluid

$. %hen replacing a fleible pipe a) use two spanners to stop pipe from twisting b)do a bonding chec* chec* c) tighten only hand tight

'. 7ow is an aircraft battery rated2 a) Ampere hours b)%at b)%atts ts c) Poules

+. ,ass balance weights are used for a) counteract flutter on control surfaces b)balance tabs tabs c) balance trailing edge of flying control surfaces

. %hen pressurising the aircraft on the ground for test purposes& internal doors& cupboards etc. must be a) all closed b)all open c) removed

. 9ire tests on aircraft aircraft internal internal furnishings must must be carried out a) every two years b)only when e:uipment e:uipment items fail random tests c) every five years

8. >ortable fire etinguishers are operated by a) brea*ing tell taletamperproof seal then operated by handle b)one single operation operation until fire etinguisher etinguisher is empty c) turn upside down and s:uee?e buttontrigger

/. 3pper and lower strobe lights are coloured a) green b)red c) white

10. %hen fitting a tyre the red dot should be positioned a) ad6acent to the charging valve

b)opposite the charging charging valve c) on the other side of the the wheel wheel opposite to the charging valve A(S)ERS 1.  ! A A A

" A

# A

6 +

$ +

% A

& +

1' A

This is exam number "$.

1. #omposite bra*e units a) have less weight than normal bra*e units but fade away at high temperatures b)have less weight weight than normal bra*e bra*e units and have increased efficiency efficiency at high temperatures c) weigh the same as normal bra*e units and fade away at high temperatures

. #argo bay lights on a modern aircraft aircraft are supplied by a) the battery bus b)4# handling bus c) A# handling bus

$. A radio altimeter system can be self tested a) on the ground only b)in the air only c) both

'. A modern aircraft #,# uses a) magnetic fault indicator b)#
+. Ailerons Ailerons control the aircraft in the a) longitudinal ais b)lateral ais c) directional ais

. ygen storage cylinders& once charged should be a) turned on and safety wireloc*ed b)turned off c) turned on by crew

. (n a fuel system with interconnected interconnected vents a) the epansion space must be 10H of the tan* capacity b)the epansion space space must be H of the tan* capacity capacity c) an epansion space is not re:uired

8. (n a pressurised pressurised aircraft aircraft cabin window& window& the differential differential pressure pressure can be ta*en by a) the inner pane only b)the scratch scratch panel c) both panes

/. n an aircraft travelling travelling at speeds greater greater than ,ach 1 the boundary layer is a) thic*er than if the aircraft were travelling slower than ,ach 1 b)stationary c) supersonic

10. At speeds above above ,ach 1 shoc*waves shoc*waves will form above and below the wing a) at the leading edge

b)at the trailing trailing edge c) at both the leading edge and the trailing edge A(S)ERS 1.  ! + * *

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This is exam number "%.

1. A cantilever wing is a) a swept bac* wing b)the upper wing of a biplane c) a wing without any eternal struts or bracing

. >rior to conducting a ground pressurisation test& it is necessary to a) disconnect the emergency pressure relief valve b)set E9; c) resetdisable the pressure controller

$. n a Bhot rodB type type of ice detector& detector& it is switched switched on a) all the time b)when in the air air c) when selected by the crew

'. (ce formation on wings is due to a) suspended ice crystals melting on contact with the wing and instantly re-free?ing b)ice crystals crystals forming layers on contact contact with the wing wing c) supercooled water changing state on contact with the wing

+. %hen installing a B7i-loc*B bolt& it it is is necessary necessary to

a) lubricate the shan* and threads b)lubricate the collar c) simply fit the bolt as they are prelubricated

. !he web web of an ( beam ta*es mainly mainly which which type of load a) shear b)tension c) bending

. A condition after after which a permanent permanent deformation deformation of a material is caused& is *nown as a) bending b)shear c) strain

8. Sealant or levelling levelling compound is installed installed during structure repair a) according to S instructions b)according to separate separate manufacturerBs manufacturerBs documentations such such as A# c) according to A,, and S<, chapter +1

/. >!= type entertainment entertainment e:uipment a) is not the part of maintenance schedule b)has no capacity capacity for digital information information processing and transmitting transmitting c) is installed with seat electronic unit and multipleing techni:ues

10. #onstruction such as horn balance balance and inset hinge balance installed on control surface assembly a) is meant to trim #G of control surfaces b)serves as JservoJ JservoJ system of balance c) has same effect of the balance tab

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This is exam number "&.

1. !he purpose of the vinyl interlayer interlayer in window construction is a) to increase static strength b)to improve on brittle brittle behaviour c) to enable inclusion of heater film

. Semi-monoco:ue construction a) offers good damage resistance b)is used only for the fuselage c) utili?es the safe-life design concept

$. (n typical vapour cycle system& the subcooler a) is a heat echanger to superheat the vapour b)cools the vapour further further to prevent slugging c) delivers etra cooling effect when the aircraft is on ground

'. !he apparent wander for directional gyros is a) compensated by applying a constant tor:ue b)maimum at the the pole c) dependant on longitude

+. Active Active load control involves a) varying lift force to control vertical movement of the aircraft b)limiting the deflection deflection of control surface surface with airspeed airspeed c) (ntervention Q monitoring the human pilot

. !he mid-spar is found in large large aircraft to a) support fitting the engine mount Q landing gear mount b)assist the main main spar with operational operational loads c) provide redundant design

. 7ow do you remove remove air from hydraulic fluid2 a) =ent to atmosphere b)!ray b)!ray c)

>ass through a restriction

8. A thermal compensator compensato r is used in a) an hydraulic system b)an oygen system c) a fuel system

/. An aircraft lands in autoland. After touch down and thrust reversers are deployed what happens to autothrottle2 a) Automatically switches off b)Stays armed for go around in an emergency emergency c) Advances throttles throttle s

10. 7ow many many fire etinguishers are re:uired re:uired on an aircraft aircraft with with +01 passengers2 a) + b) c) 

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This is exam number #'.

1. >ilotBs instinctive cut-out buttons are positioned a) on right side of control wheel b)on side of control wheel wheel furthest from throttles throttles c) on left side of control wheel

. Active Active load control uses a) elevator and stab b)elevator and aileron aileron c) aileron and spoiler

$. !he 4irectional Gyro is is chec*ed chec*ed every 1+ minutes minutes for a) toppling b)drift c) erection

'. A pressure control control relay relay in a hydraulic hydraulic pump pump is a) energised to the run position b)de-energised b)de-energised to start the pump pump c) used to prevent anything happening until there is hydraulic pressure

+. A coc*pit chec* chec* on the engine firewire system is a a) calibration chec* b)continuity chec* c) function chec*

. %hen a vibrating rod ice detector detector has de-iced& the warning warning lamp on the flight dec* a) goes out immediately immediately b)goes out after one more cycle c) goes out after a set period of time

. 4e-misting of passenger windows is provided by a) an electrical heating element b)air from the cabin cabin c) sealed window

8. (5S and =< operate in which range a) 379 b)79 c) =79

/. An anti-balance anti-balan ce tab is used a) for trimming the aircraft b)to relieve stic* stic* loads c) to give more feel to the controls

10. !he fin helps to give a) directional stability about the longitudinal ais b)directional stability stability about the normal normal ais c) longitudinal stability about the normal ais

A(S)ERS

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This is exam number #1.

1. A reduction in field strength of a 4# shunt motor driving a constant load will result in a) reduced tor:ue and increased speed b)increased tor:ue and reduced speed speed c) increased tor:ue and speed

. %hen charging an oygen oygen bottle with gaseous gaseous oygen& the oygen oygen is a) passed into the bottle as :uic*ly as possible to *eep the temperature down b)passed into the bottle slowly to *eep *eep the temperature temperature at approimately approimately ambient c) passed into the bottle at any rate as this does not affect temperature

$. !he purpose of the autopilot servo-motor tor:ue setting setting is to to a) damp the system oscillation b)protect the servo motor c) prevent control surface runaway

'.
+. Structural members are designed to carry a) side loads b)end loads c) side and end loads

. ,ost radio aerials are a) bonded b)not bonded c) insulated from the fuselage

. A bonded waffle doubler& as well as acting as a s*in strengthener also acts as a a) shear tie b)6ury strut c) tear stopper

8. %here are the left handed handed threads threads found in an oygen system2 system2 a) #harging connection b)Shut-off valve c) 5ine valve

/. A restrictor restricto r valve can be used a) to increase the speed of the undercarriage etension b)to reduce the speed of the undercarriage undercarriage etension c) to increase the speed of undercarriage retraction

10. Standby #ompass ad6usting magnets @9linders ars)& when do they they eert the most amount of influence2 a) %hen parallel to each other b)%hen '+ degrees degrees apart

c)

%hen /0 degrees apart

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This is exam number #.

1. (n a fully fully 9ly y %ire %ire Aircraft& Aircraft& ground spoilers spoilers are deployed automatically automatically when the aircraft is on ground and a) thrust reversers are deployed b)bra*es are deployed deployed c) weight on ground switch is activated

. (n fully 9ly y %ire %ire aircraft& aircraft& rudder trim is nulled by a) electric flight control unit b)9light Augmentation Augmentation #omputers c) 9light Guidance and ,anagement #omputer

$. 9,# secondary flightplan is selected a) on the ground by the pilot b)by calendar date date monthly c) in the air by the pilot

'. n a high pressure pneumatic system& if the drain plug for oil oil and water is left open for long periods of time& the system would a) lose all pressure b)lose pneumatic pneumatic pressure partially partially c) lose pressure from the compressor side only

+. %hat are the faying surfaces of a repair2 a) ;dges of repair metal b),aterial under repair repair c) ,iddle of repair

. %hy is a 6oggle 6oint used2 a) So countersun* rivets do not need to be used b)Smooth contour of surface surface c) Added strength

. %ith %ith engine static ;>< gauge reads 6ust above 1. a) !his is O b)!ransmitter b)!ransmitter is unserviceable unserviceable c) Gauge re:uires re-calibration

8. Aileron Aileron input is fed into the yaw damper damper system system to a) prevent nose pitching down b)prevent adverse yaw in a turn c) prevent nose pitching up

/. >ortable  diluter demand valve wor*s when a) 100H selected b)less than +00psi in in bottle c) user breathes in

10. %hen the fire handle is operated it a) cuts off fuel and hydraulics. Generator remains on line to provide electrical electrical power

b)cuts off field field current& hydraulics and and fuel and operates operates fire etinguishers c) operates fire etinguisher only A(S)ERS 1.  ! A + *

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This is exam number #!.

1. #oefficient A is ad6usted a) 0 degrees b)$0 degrees c) on any heading

. %ith %ith an aircraft which has has more than one compass system system a) both are ad6usted on each heading b)master ad6usted& ad6usted& slave ad6usted& ad6usted& each having a corrected compass compass card c) master and slave ad6usted& correction card for master only

$. G>%S operating operating in mode 1 and  when close to ground will give a) amber warning b)red caption and aural Jwhoop whoop pull pull upJ c) red caption and aural Jpull up undercarriage& flaps& throttleJ

'. 4# electrical electrical cable cable must must be positioned positioned how far away away from a compass2 a) So as to give no more than  degrees deflection of compass b)0 inches c) ' inches

+. !he components of an (5S are a) a locali?er and a glide slope b)a locali?er& locali?er& a glide slope and the mar*er beacons c) a locali?er and the mar*er beacons

. (n (5S& the glideslope provides a) lateral steering b)vertical steering steering c) distance chec*s

. (f the /0 7? tone predominates in in a locali?er receiver& receiver& the deviation indicator will show a) the flag b)fly right c) fly left

8. Autopilot will operate after a) 1000 ft b)+0 ft c) +00 ft

/. %hich pitot probe provides info to the captains instruments2 a) 3pper b)5ower c) oth

10. n the A,4& what does amber indicate2 a) %arning b)>resent status status

c)

#autionary info

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This is exam number #" .

1. %hich instrument shows 4ecision 7eight2 a) 7S( b)A4( c) ;#A,

. %here does the the 7S( 7S( receive receive G"4 speed info from2 from2 a) ;(#AS b)>itot static probes probes c) ("S

$. %hat will will happen if the ,aster 4im and test switch is is switched switched to the on position2 a) All lights will illuminate b)4ome lights will will illuminate c)
'. %hat is the radio alt trac* altitude2 a) +00 ft b)10000 ft c) +00 ft

+. A radio coupled autopilot in pitch pitch uses uses a) =< b)glideslope c) A49

. ;>< and thrust modes in autothrottle are the only modes modes that can can be selected in a) ta*e off b)cruise c) approach

. (nertial nav unit uses pin programming for a) aircraft type b)location c) magnetic orientation

8. 7ow can can it be verified verified if 9,# update update is correct2 a) data plate on 9,# b)(!; c) 9,# via #43

/. %hat are the  short short prongs for on an A# plug2 a) 3sing A# current to pull on interloc* circuit b)>revent arcing during plug connection  disconnection c) 7elp plug location  fit

10. A vibration contact contact voltage voltage regulator consists of a shunt winding and a a) voltage regulating coil in parallel b)voltage regulating regulating coil in series c) current regulation coil in series A(S)ERS 1.  ! + * *

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This is exam number ##.

1. A de-icer boot is completely completely bonded to the leading edge edge to a) >revent electrical static build up b)Smoother airflow over over leading edge c) ,ore efficient efficient de-icer cycles

. !he wea* lin* on a wire wire aerial is at at a) the front b)the middle c) the rear

$. G>%S will show a fault fault if the following following fails a) ressure altimeter altimeter c) Air speed indicator

'. %hat is the contamination monitor for in a Systron 4onner 4onner fire detection system2

a) (ntegrity comparitor b)4irty contacts contacts c) =olts drop dro p

+. A double headed headed oygen oygen pressure regulator is is used for a) etra supply in case of emergency b)additional flightcrew flightcrew c) changes in altitude

. >itch trimming in autopilot is initiated by a) # of G ,ovement b)continued pitch input input c) pitch of aircraft in cruise

. Pet engines are usually mounted by a) welded steel tubing b)forged mounts and and bolted to aircraft aircraft forged structure structure c) aluminium castings

8. (n a coc*pit window heater system the autotransformer autotransformer a) steps up output for severe weather conditions b)supplies A# >ower >ower for heating c) supplies 4# power for heating

/. A high speed speed aircraft aircraft with ,A#7 warning will a) warn when ,crit is reached b)warn when ,ach ,ach 1 has been eceeded eceeded c) warn when coming to limits of upper envelope

10. A constant delivery pump has its output varied with with a) servo pressure b)regulators c) gears A(S)ERS 1.  ! A * A

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This is exam number #6 .

1. %hen power is switched switched off the gimbal bra*e a) stops outer gimbal b)restricts outer gimbal gimbal c) restricts inner gimbal

. (n an air conditoning conditoning system system heat is added added to air by a) restricting compressor inlet b)restricting compressor compressor outlet c) restricting duct outlets

$. !wo !wo compressors compresso rs driven by separate engines use a) "<=s to prevent compressors driving each other b)><= b)><=s c) (nterconnected to share loads

'. 9uel tan*s interconnected interconnected must have a) vents to allow overfueling b)tan* where fuel fuel is fed from both tan*s to engine inlet c) protection against overfill for tan*s and fuel system

+. (
. A#,S a) provides A!A tech log reference for all faults b)provides source of fault fault c) supplies #,# with source of fault

. After After successful successful ditching& ditching& use of life rafts must must be a) displayed clearly on leaflet in pouch in front of seat b)shown how to be deployed by air stewardesses stewardesses c) clear instructions given with ease of use on raft

8. Secondary bonding is usually with a) stranded copper 0.+ inch b)single strand 0.+ inch inch c) 18 A%G

/. %hat is the the purpose purpose of diode in in a power G#<2 a) !o prevent bac*flow of current in the ;,9 coil b)!o speed up the operation operation c) !o allow flow in the event of failure of the relay

10. ;ddy currents are a) caused by resistance of the coil b)circulating currents currents c) caused by heating effect of the coil A(S)ERS

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This is exam number #$.

1. 4ifferential 4ifferential aileron control will a) cause a nose down moment b)cause a nose up moment c) prevent yawing in con6unction with rudder input

. 7ow many many fire etinguishers are re:uired re:uired on an aircraft aircraft having having '01 +00 people2 a) + b) c) 8

$. !oilets !oilets must have a smo*e detection a) light in the coc*pit b)aural and visual visual warning in the main main cabin c) connected to a pump to pump the smo*e out

'. %hen an undercarriage is lowered& lowered& it tends to creep bac* up. !he fault could be a) a lea*y selector valve b)a stuc* relief relief valve c) the emergency emergency system

+. ;scape route lighting must not have more than a) 10H obscured b)1+H obscured

c)

0H obscured

. 9ireproofing of cabin material should be done a) every  years b)when a sample sample fails c) every + years

. 7ow many many emergency emergency lights are allowed to be inoperative2 a) "one b)10H c) +H

8. !he angle of a runway turnoff light is a) '0o b)+0o c) 0o

/. !he small pins in the power power connector plug are are a) positive b)negative c) neutral

10. #abin fluorescent lighting circuits are supplied with a) 11+ = A# b)8 = A# c) 8 = 4# A(S)ERS 1.  ! * + A

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This is exam number #%.

1. n a fly-by-wire aircraft& what controls stabili?er trim2 a) S;# b);5A# and S;# c) ;5A#

. %hen an an overvolt is present on an ac ac generator generator system the tripping tripping circuit a) trips at a set level b)trips after a time time delay c) trips after a time delay inversely proportional to overvolt amplitude

$. (n an A# distribution system the purpose of the synchronising bus-bar bus-bar is to a) provide interconnection between the generator load busbars b)supply essential essential services c) provide a means of monitoring the load

'. %hen a 9A4;# 9A4;# system loses air data input it goes to a) soft reversion b)hard reversion c) mechanical reversion

+. =ibrating =ibrating contact voltage regulator sensing coil is a) across the generator output b)in series with the field windings c) in parallel with the field windings

. A current transformer transformer connected connected across the neutral neutral of a $ phase generator is for a) differential protection b)phase se:uence se:uence monitoring c) load monitoring

. Cener diodes are for a) voltage stabilisation stabilisation b)voltage regulation regulation c) rectification

8. Generator output indications are a) O% b)O% Q O=A O=A< c) O=A Q O%

/. A 9light 4ata
10. n an ;A4( the command bars show a) re:uired flight path compared with hori?on b)re:uired flight path compared compared to planned planned flight path c) re:uired flight path compared with aircraft position A(S)ERS 1.  ! + * A

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1. !he airdata computer inputs to a) mach meter& standby altimeter& AS( b)cabin rate sensors& sensors& machmeters& machmeters& AS(& AS(& altimeter altimeter c) altimeter& 9,#& secondary radar

. (f the runway picture picture in the ;A4( ;A4( moves moves down during an (5S approach the aircraft must a) up b)down c) nowhere - this is normal on an (5S approach

$. 5oad shedding allows a) more current to the busbar b)less current to the busbar c) more voltage to the busbar

'. 7ow may the output output of a transistorised transistorised voltage regulator be described2 a) Slightly variable 4# b)>ulse width modulated modulated 4# c) =ariable A#

+. (n the event event of complete complete A# A# generator failure failure in an A# split bus-bar generation system& how is power maintained to the essential A# A# bus-bar2 a) y power fed from static inverter only b)y power fed from a hot battery bus-bar only only c) y power fed from a battery supplied static inverter

. %hich components within a generator control unit unit connects connects the output of the field power supply to the generator eciter2 a) Generator control relay b)Generator line contactor c) Generator power pilot relay

. (n what units are static inverters rated2 a) *% b)*=A b)*=A c) *=A<

8. %hat modulation modulation is used for the beams beams of a localiser in in an (5S2 a) 1+0 7? right of runway centre line& line& /0 7? left of runway centre centre line b)1+0 7? left of runway runway centre line& line& /0 7? right of runway runway centre line c) /0 7? below the glide path& 1+0 7? above the glide path

/. %hat deviation deviation is indicated by by  dots in a =< system2 system2 a) .+o b)10o c) o

10. (n an automatic flight control control system system when may yaw damper be applied2 a) 4uring automatic control only b)4uring manual control control only c) 4uring either manual or automatic control A(S)ERS 1.  ! + + +

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This is exam number 6'.

1. (n what fre:uency range range does the automatic automatic direction direction finding @A49) system operate2 a) 108.00 - 11./+ 11./+ ,7? b)10+ - 11+0 11+0 O7? c) 1/0 - 1+/ O7?

. (n a generator system& a stability winding is used used a) in series with the field to prevent oscillations b)to prevent voltage voltage overshoot c) to control output current

$. n engine engine shut shut down down what what prevents prevents G#< G#< being being tripped2 tripped2 a) undervolt b)underfre:uency c) under current

'. 7ow is real and reactive load sharing achieved in an A# parallel generator system2 a)
+. 7ow are passenger reading lights normally tested2

a) ;ach one is switched on individually at passenger panel b)y using a <;A4 <;A4 5(G7! !;S! switch switch at any passenger passenger panel c) y using using a <;A4 5(G7! !;S! switch on the cabin attendant panel

. (n what position should the selector selector switch switch be for a standby and emergency emergency lighting system during flight2 a) 99 b)Armed c) "

. 7ow does an aircraft aircraft distinguish its own own 4istance 4istance ,easuring ;:uipment reply from those for other aircraft2 a) y using an alternate fre:uency b)y modulation of an audio tone c) y changing at random the time delay between the pulse pairs of the interrogation signal

8. from where where is bearing information received for display display on the digital-distance radio-magnetic indicator @44<,() a) 9rom =< and A49 systems b)9rom =< =< only c) 9rom A49 only

/. 7ow may may the basic principle of the radio altimeter altimeter be described2 described2 a) As As a comparison of radio altitude against a barometric altitude referenced to (SA sea level @101$.+mb) b)As a measure measure of the time between between a <9 pulse pulse transmission and the reception of its echo from the ground directly below the aircraft c) As a series of radio radio pulses to the the ground their fre:uency depending on the epansion or contraction of an evacuated capsule and the deflection of an ; and ( bar transducer

10. %hich fre:uency is is used to achieve achieve line line of sight radio radio communication2 a) =79 and 379 b)79 c) =79 A(S)ERS 1.  ! * + +

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1. %hy is is an aerial tuning unit used in a high fre:uency @79) @79) communication communication system2 a) !o etend or retract the aerial and so vary its physical length b)!o select the transmissionrecep transmissionreception tion fre:uency in the 79 79 band c) !o electrically electrically lengthen or shorten the aerial for optimum matching of impedance

. %hat would be the purpose of an input from an inertial inertial reference reference system being connected to a weather radar2 a) !o provide stabilisation stabilisation for the radar antenna b)!o place the weather weather radar target target in a?imuth a?imuth and distance distance for the display c) !o ensure that there is no radar radar transmission with aircraft on ground

$. %hich systems provide envelope envelope modulation information for a Ground >roimity %arning System @G>%S) a) 9lapsundercarriage b)Autothrottle

c)

'. (n a compass system& what senses the the hori?ontal hori?ontal component component of the earths magnetic field and where is it normally fitted2 a) 4irectional gyro mounted on the roll ais of the aircraft b)9lu detectors detectors fitted in the wing tips c) A precession device mounted on the yaw ais of the aircraft

+. !he !ime !ime and 4%" b)(t operates in the the same manner manner as (5S but utilises utilises higher fre:uencies c) (t operates in con6unction with 4,; at lower fre:uencies than (5S

. ther than when there is a fault in an aircraft aircraft battery or its charging charging system& when is the charger charger switched off automatically2 a) %hen there is a failure of one alternator in a split-bus bar system b)%hen the battery battery is used for ecessively ecessively high discharge discharge currents such such as in starting c) %hen the alternators are fully loaded . !he 9,S nav data base is updated a) after a  or # chec* has been completed b)every 8 days c) daily

8. An <,( has inputs from =< and a) no other sources b)a a?imuth gyro

c)

a remote compass input

/. !he trimmer trimmer resister resister in a carbon carbon pile volts regulator regulator is a) in series with the generator field b)in parallel with with the generator volts volts coil c) in series with the generator volts coil

10. %hen a field relay relay trips the generator generator off line it can be reset a) on the ground only b)by cycling the generator switch c) after the fault has been cleared A(S)ERS 1.  ! * A A

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This is exam number 6.

1. An overvoltage condition trips trips the generator& generator& the time time ta*en to trip is dependant upon a) amplitude of voltage b)time delay circuit circuit c) closing fuel and hyd valves etc

. (n a paralleled paralleled A# generator system both A phases must be in synch and a) #A must e:ual A# b)phase rotation does not matter c) #A must e:ual #A

$. %hen loads are shed from a busbar busbar automatically automatically a) bus bar voltage rises b)bus bar current rises rises c) bus bar current decreases

'. (n a modern 7S(& the displays are a) course and direction b)course and attitude attitude c) direction and attitude

+. (n an an (
. (n an ("S system the acceleromete accelerometerr is a mass a) suspended between two springs in a tube b)a mass suspended suspended in free air c) a remotely mounted mass on the airframe

. (n a modern modern aircraft the A#A
8. %hat controls output from generator a) >#3 b)G#3 c) ;5#3

/. !he term JempennageJ incorporates a) elevators& stabiliser& stabiliser& rudder b)elevators& stabiliser& stabiliser& ailerons c) rudder& ailerons& spoilers

10. %hich of the following are primary control surfaces2 a) ;levators& roll spoilers& tabs b);levators& ailerons& ailerons& rudder c)
A(S)ERS 1.  ! A * *

" A

# A

6 A

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This is exam number 6!.

1. 9lutter can be prevented by a) mass balance b)trim tabs c) balance panels

. =ents holes are found on a) tubeless tyres b)tubed tyres c) spilt wheel tyres

$. %hich of the following can be used used on the ground2

a) !urbo bra*e b)!urbo b)!urbo compressor c) !urbo fan

'. >ressure refuelling is carried out at a) 1+ >S( b)0 >S( c) '0 >S(

+. %hat is important important about the air entering a dry air pump2 a) must be filtered b)must be pressure controlled controlled c) must be temperature controlled

. %hat test is carried carried out to ensure serviceability of a s:uib2 a) ottles are fired b)Safety ohmmeter ohmmeter is used to chec* chec* voltage c) A continuity continui ty chec*

. #ross feed valves permit fuel transfer from a) tan* to tan* b)left tan* to right tan* c) any tan* to any engine

8. %hat is fitted fitted to the fuel 6ettison pipe to prevent vaporisation2 a) anti corona device b)no??le c) corona device

/. Specific Gravity Gravity in a lead acid battery battery should give an indication of a) charge b)electrolyte level level c) electrolyte temperature

10. (f an an aircraft aircraft suddenly drops pressure at 1'000ft a) mas*s drop automatically automatically b)attendant must must drop mas*s c) passenger must get mas* from overhead stowage A(S)ERS 1.  ! A A *

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This is exam number 6".

1. 4uring normal engine shut down the generator a) brea*er is tripped b)brea*er and control relay tripped c) control relay tripped only

. At what temperature temperature does a yellow fuse plug melt at2 at2 a) 1+0 deg # b)00 deg # c) +0 deg #

$. Above the critical mach number& the drag coefficient a) increases b)decreases c) remains the same

'. (n a #,# warning signals are generated by a) %arning computer b)#,# c) 9,#

+. 4issimilar metal fusion bonding is best for a) high strength high ductility b)high strength high toughness toughness c) low strength high toughness

. (n a fully fully fly by wire system& system& if the the elevator elevator loses all electrical electrical power a) servos move to neutral and loc* b)servos remain stationary stationary and provide damping damping c) servos loc* at last position

. A variable angled pump starts at a) maimum stro*e b)minimum stro*e c) half way position

8. At what height does the rising runway runway appear appear a) +00ft b)$00ft c) 00ft

/. An 7 on the ;7S( indicates a) 4,; hold

b)=< hold c) (5S approach

10. %hat happens to the capacitance capacitance in a fuel contents contents gauge as fuel is used a) increase b)decrease c) 4epends on altitude A(S)ERS 1.  ! A + A

" A

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This is exam number 6#.

1. %hat are the main areas of the autopilot2 a) ;rror& correction& follow up& demand b);rror& correction & demand& demand& resolved c) ;rror& correction& follow up& command

. =79 fre:uency is a) 108 - 11 ,7? b)108 - 1$ ,7? c) 108 - 118 ,h?

$. !he call call system system for the captain captain will will have the audio audio a) two tone chime b)horn c) hi tone chime

'. #hannel $ on a #=< records a) first officer b)captain c) flightdec*

+. 4,; wor*s on the fre:uency of a) =79 b)379 c) 79

. A radial is referenced a) from a beacon b)to a =< =< c) on a compass

. A49 wor*s by using a) loop aerial b)sense aerial c) both loop and sense aerial

8. !he ideal conditions for paint paint spraying spraying an aircraft are a) 0o# to $0o# and humidity below 0H b)1+o# to +o# and humidity humidity below +H c) 1+o# to +o# and humidity above 0H

/. %hen an an aircraft is put into storage for medium  long periods& periods& the fuel tan*s should be a) empty b)full

c)

some fuel left in to prevent sealant from deterioratingdrying out

10. !he generator warning light will come on when a) voltage too high b)voltage above battery battery voltage c) voltage below battery voltage A(S)ERS 1.  ! * + A

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1. #ompared to air air driven gyros& the electric electric gyro runs a) faster b)slower c) same speed

. 7ot fluids in an aircraft galley galley must have closed closed container container lids at temperatures above a) '+ degrees # b)++ degrees # c) + degrees #

$. %indshield rain repellent is applied a) before rain and spread on window surface by wipers b)when rain is on windows and spread spread by wipers c) when in heavy rain so vision is unobscured

'. (n a gas gas firewire firewire system& what causes causes the firewire caption caption to come on

when heat is applied2 a) #apacitance increase b)#ontinuity c) >ressure

+. (n an auto trim trim system& system& for the trim trim system to operate operate a) autopilot must be engaged b)autopilot need not be engaged c) operation of the trim controls is re:uired

. 9luid viscosity a) increases with an increase in temperature b)decreases with with an increase increase in temperature c) decreases with a decrease in temperature

. A chec* flow valve valve in a hydraulic hydraulic system prevents a) pump cavitation b)reverse flow c) overpressure

8. A pneumatic indicator ta*es its indications from a) compressor inlet b)compressor outlet c) reservoir

/. %hat is apparent drift2 a) earths rotation b)errors when aircraft aircraft ban*ing c) gyro pivot friction

10. (ntegral fuel booster pumps a) re:uire no cooling b)re:uire ram air cooling cooling c) the fuel does cooling A(S)ERS 1.  ! A A +

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This is exam number 6$.

1. !oilet !oilet fire detection can be found in a) #AA(>s b)A%" b)A%" 80 c) A%" 8$

. !he outside casing of a firewire has a) 8vdc potential above ground b)11+vdc potential above ground c) same potential as ground

$. !he cam plate in a nose undercarriage undercarriage is for a) the shimmy damper b)alignment for nose wheel wheel steering on nose undercarriage undercarriage etension c) align for nose wheel on nose undercarriage retraction

'. An aircraft airspeed indicator has a) pitot to the capsule b)static to the capsule c) pitot to the capsule and static to the out side side of the capsule

+. %hat is tyre creep related to2 a) !yre moving around the wheel b)7ori?ontal movement movement of the tyre c) =ertical movement of the tyre

. %a %ater ter 5ines @%5s) are measured points on a a) hori?ontal line b)vertical line c) wing line

. !he four main structural structural items items ma*ing ma*ing up a hori?ontal hori?ontal stabiliser stabiliser are a) spar& rib& stringers& s*in panels b)spar& rib& longerons& s*in panels panels c) spar& rib& bul*heads& s*in panels

8. !he main undercarriage is attached to a) front main spar b)rear main spar spar c) aircraft structure

/. (n an auto pilot pilot coordinated coordinated turn& when the turn angle is reached2 reached2 a) both ailerons are down b)one is up one is down c) the ailerons are faired

10. A flat planer radar dish a) is used for <9 transmissions only

b)is a parabolic dish c) is a series of wave guides with slots cut in them

A(S)ERS 1.  ! * * *

" *

# A

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This is exam number 6%.

1. Above +00 ft the rad alt a) pointer goes to ?ero to show system is being monitored b)pointer is hidden behind behind a mas* with with off flag out of view view c) continues to indicate but with a warning flag

. %hen replacing a current transformer a) it can only be fitted one way round b)it can be fitted fitted any way round c) voltagecurrent selection must be made prior to fitting

$. 7ow is the net database on the the 9,# activated2 activated2 a) ,anually& on the ground b)Automatically b)Automatically by due date c) ,anually in the air

'. !he economy coil on a relay a) ma*es it cheaper to ma*e b)reduces current re:uired to hold closed closed c) reduces current re:uired to close

+. !he emergency emergency lighting system must be designed so that after after any single transverse vertical separation of the fuselage during crash landing the maimum amount of emergency lighting that fails is a) 10H b)1+H c) +H

. %hat is the the function function of the generator generator control relay2 relay2 a) #ontrol output voltage b)ring the generator generator online c) #onnect the generator to the busbar

. 7ow is automatic AoA protection provided2 a) Autothrottle Autothrottle applying more power b)9astSlow indication indication c)
8. %hat is the the output output angle angle of a landing landing light2 light2 a) 11 degrees b)1+ degrees c) 0 degrees

/. %hat sort of etch solution is used on Aluminium Aluminium alloys alloys a) Al*aline ;tch b)Acid ;tch c) Solvent ;tch

10. %hat are the types of true true bonded bonded 6oints2 a) cemented and specific b)mechanical b)mechanical and specific

c)

mechanical and cemented

A(S)ERS 1.  ! + A +

" +

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$ A

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This is exam number 6&.

1. %here would you find find information information on life-raft deployment2 a) #abin safety onboard card b)#abin operations manual manual c) PA
. %hat G>%S mode gives gives a J%hoop %hoop& >ull-upJ >ull-upJ command command a) ,ode  b),ode $ c) ,ode 

$. 7ow does a mach meter wor*2 a) true airspeed  indicated airspeed b)true airspeed and and true speed of sound c) indicated airspeed  temperature

'. A machmeter wor*s a) always b)always ecept ecept on the ground c) above 10000 ft

+. n a standard day at which altitude will the speed of sound be the the

highest2 a) Sea 5evel b)+&000 ft c) 10&000 ft

. !he purpose of the autopilot servo-motor tor:ue setting setting is to to a) prevent control surface runaway b)dampen oscillations oscillations c) provide autopilot

. !he current consumed by a 4# starter motor will a) increase as the engine speed increases b)decrease as the engine speed speed increases c) remain constant

8. !he various parts of the aircraft aircraft airframe are maintained maintained at the same same potential by 2 a) earthing b)static wic*s c) bonding

/. %hy is a 6oggle 6oint used2 a) !o provide a flush fit b)!o add strength c) !o provide a smooth contour to surface

10. Air conditioning systems a) (ncrease the temperature of air b)increase and decrease the temperature of air c) decrease the temperature of air

A(S)ERS 1.  ! + A *

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This is exam number $'.

1. 7ow do oygen cylinders show over pressure2 a) Green rupturing disc b)Audible warning warning c)
. Slats a) *eep the boundary layer from separating for longer b)increase the overall surface area area and lift effect effect of wing c) act as an air bra*e

$. BA:uaplaningB can be reduced by2 a) anti-s*id b)lowering slats c) increased flaring

'. An air cycle machine turbine a) drives compressor to pressurise aircraft b)drives compressor to increase increase temperature temperature c) drives compressor to decrease temperature

+. n passenger aircraft of  or more more ?ones a) seat bac*s fold forward at over wing emergency eits b)there should be at at least one eit eit per ?one c) emergency emergency eits are to be clearly signed

. (n a pressurised cabin there is a gauge gauge that that shows shows a) cabin differential pressure b)cabin pressure altitude altitude c) aircraft altitude

. 4ue to to the change of lift forces resulting resulting from the etension etension of flaps in flight a) nose should be raised increasing AoA b)nose should remain remain in same pos maintaining maintaining same AoA c) nose should be lowered reducing AoA

8. 9light spoilers a) can be used with differential ailerons to reduce adverse yaw in a turn b)can be deployed deployed on the down going wing wing in a turn to increase increase lift on that wing c) can be used to decrease lift to allow controlled decent without reduction of airspeed

/. (f the aircraft is flying nose heavy heavy which which direction direction would your move the elevator trim tab2 a) 4own to move elevator up b)3p to move elevator elevator up c) 3p to move elevator down

10. %hen changing a pitot static instrument with :uic* :uic* release release couplings couplings a) a lea* chec* is not re:uired b)a lea* chec* chec* is always re:uired

c)

a lea* chec* is only re:uired if stated by manufacturer

A(S)ERS 1.  ! A A A

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6 A

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This is exam number $1.

1. !he cross sectional area of a secondary secondary conductor must be not less than a) 18 S%G for a single wire b) S%G  0.+J c)  S%G  0.+J

. A neutralising agent for sulphuric acid is a) bora powder b)citric acid c) distilled water

$. (n a split bus power distribution system a) generators are paralleled on connection to the tie bus b)each generator generator supplies its own bus and distribution system in normal operation c) power is split between 11+= A# and 8= 4#

'. %ing tip vortices are strongest stronges t when a) flying high speed straight and level flight b)flying slowly at high angles of attac* attac* c) flying into a headwind

+. Air eiting the compressor compressor side of an A#, a) will have increased pressure and temperature b)will have decreased decreased pressure and temperature c) no change in temperature or pressure as it is a centrifugal compressor

. !he purpose of a scavenge system within a fuel system system is a) to ensure that all available fuel can be used b)to ensure that any any water in the the fuel is constantly constantly dispersed thus reducing microbiological contamination c) to ensure that all unused fuel is returned to the tan*s efficiently . >neumatic rain removal systems a) use engine bleed air at high velocity to remove water droplets from windscreen b)use a pneumatic pneumatic motor to drive windscreen windscreen wipers c) are not permitted on large transport aircraft

8. A transponder that is compatible compatible for use with with a !#AS !#AS system would be a) ,ode A b),ode # c) ,ode S

/. G>S a) uses ' satellites e:ually spaced around  orbits b)uses 18 satellites satellites e:ually spaced spaced around  orbits c) uses 1 satellites e:ually spaced around  orbits

10. %hen both both side is not easily reached reached which which type of fastener fastener would you use2 a) 7i loc* bolt b)>op rivet c) lind rivet A(S)ERS 1.  ! A A +

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6 +

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This is exam number $.

1. %here would you find find information information on life-raft deployment2 a) #abin safety onboard card b)#abin operations manual manual c) PA
. %hat G>%S mode gives gives a J%hoop %hoop& >ull-upJ >ull-upJ command2 command2 a) ,ode  b),ode $ c) ,ode 

$. Aerodynamic balance a) will cause #> to move forward of hinge and cause overbalance b)will cause #> to move towards the the trailing edge and cause instability instability c) will reduce aerodynamic loading

'.
+. !he (
~~. %hat manoeuvre does !#AS (( advise the pilot pilot to ma*e a) !A b)~~
. %hat are are the shapes of traffic shown on a !#AS !#AS display display 2 a) %hite diamonds& red s:uares and amber circles b)%hite s:uares& red diamonds and amber amber circles c) %hite circles& red diamonds and amber s:uares

8. !he laser ring gyro a) does not have gimbal b)does not have gimbal gimbal and rotating parts parts c) has a stabili?ed platform

/. A single failure of fly fly by wire a) has no effect on the aircraftBs operation b)will limit the flight profile c) will reduce the operational height and speed

10. 9ly-by-wire load alleviation function in turbulent weather conditions will result in a) ailerons moving symmetrically upward

b)ailerons and spoiler spoiler moving symmetrically symmetrically upward c) spoiler moving symmetrically upward

A(S)ERS 1.  ! + A *

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This is exam number $!.

1. !he flu detector element a) changes it position after the aircraft heading is changed b)gives heading with with respect to magnetic magnetic north c) changes heading with the heading of the aircraft A(S)ERS 1.  ! +

. a) b) c)

$. a) b) c)

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c)

+. a) b) c)

. a) b) c)

. a) b) c)

8. a) b) c)

/. a) b) c)

10. a)

b) c) b

EASA mod 11 questions

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