Avery Test III

50問 • 1年前

問題一覧

A turboJET aircrafts L/D max speed is at Y. At what speed do you need to fly to achieve maximum range?

TCAS 2 "TA Only" mode is selected by the flight crew. Which statement is correct regarding the advising of threat levels to the crew ?

RAs will not be displayed aurally or visually

In a steady climb at a constant IAS, the distribution of forces is best described as?

Life is less than weight, thrust is greater than drag

Which factor has the least affect in an aircraft which suffers an engine failure after takeoff?

Ground affect

Compared to minimum drag speed in the clean configuration, flight with the undercarriage extended would see the total drag curve?

Move up and left

On conventional flight controls rubber seals were attached to the leading edge of the primary flight controls - this was used to?

Prevent ice build up that could lock the control

An aircraft flies above its mach trim speed. The mach trim system shall ?

Deflect the leading edge of the horizontal tail plane downwards

To be "speed stable" in a holding pattern the selected airspeed would need to be ?

Faster than the speed for minimum fuel flow

In the B767 FMS/autopilot system a 'fail operational' ILS approach involves the reliable operation of how many autopilots?

Three

An advantage of a 'centrifugal' compressor compared to an 'axial flow' compressor is?

It is more robust

If a gas turbine engine was fuelled with Avgas instead of Avtur the affect on the range is to?

Reduce it because Avgas has a lower specific gravity

In a B767 an airspeed over-speed is announced in the cockpit by which aural ?

A siren

In the en route cruise zone of a flight sector the most appropriate EHSI display mode is?

Map mode

Current TAS can be found where on a B767 FMS/EFIS presentation

The CDU progress page

Which of the EHSI display modes listed below can NOT display weather radar returns ?

Plan mode

In a typical pressurisation system, other than setting the barometric value what else must be set prior to departure?

Desired cabin altitude and rate of pressure increase

On large aircraft over pressure protection to pneumatic user systems is provided by?

A pressure reduction valve

Which wing attributes are best to delay separation ?

Turbulent with least skin friction

Vmcg speed is highest if the CoG ?

Is at the rearward end of the loading envelope

B767 'thrust' indication in cruise at FMC altitude is?

SPD

In the B767 thrust setting/means by which speed is maintained when in a 'flight level change' descent mode are primarily?

Flight idle/pitch variations

The CDU line select keys can?

Copy a line to/from the scratch pad

GPWS warnings are inhibited for what kind of TCAS threat level?

None

The hot battery bus is powered?

Only by the aircraft battery

Which is NOT an element of anti skid ?

Pneumatic reserve braking

In a trust management system the most significant factor for takeoff is?

Inlet temperature

In the B767 FMS, after takeoff the minimum height for engagement of VNAV is ?

400ft

In the B767 FMS during an autopilot controlled climb in VNAV, selecting a lower than current altitude in the autopilot MCP altitude window would see the aircraft?

Continue the climb to the VNAV cruise level

With respect to a shockwave on a conventional wing section, which answer best describes the characteristics of the airflow ahead and behind the shockwave ?

Supersonic ahead of the shockwave, subsonic behind, with no change in airflow direction

The captains EADI horizon is not showing, the FOs EADI is showing horizon information. The likely cause is?

The left IRS has not entered NAV mode

The TCAS 2 symbology in ascending order of threat is?

Open white diamond/ solid white diamond/ solid yellow circle / solid red square`

The CDU "Unable Next Altitude" message appears while on climb in VNAV. To achieve the FMS programmed level?

The pilot should manually select a different speed in the MCP window that provides a steeper climb angle

Vmcg sped would be increased most by which of the following ambient air value combinations ?

Humidity low, OAT low, QNH high

Use of de-rated thrust rateher than full thrust would affect Vmca speed value how?

it would reduce it

The auto brakes are set to position "2" After touchdown if the thrust reversers are engaged the target rate of deceleration will?

Essentially remain at the "2" datum setting

Spiral stability is greatest when ?

Lateral stability is high compared to directional stability

When operating at locations on earth that are outside of the B767 FMC navigation database a waypoint can be entered ?

Only as a latitude and longitude

In the B767 the FMC route is cancelled?

Automatically after landing as the aircraft groundspeed reduces to 10kts

For the sane conditions of flight level, gross weight, mach number and temperature, the most forward allowable CoG position compared to the most aft CoG would produce?

A higher fuel flow

The greatest 'reduction' in takeoff distance would be with which of the following ambient air temperature combinations ?

humidity low, OAT low, QNH high

The source of field excitation current to a three phase alternator in a large jet powered transport aircraft electrical system is ?

the PMG

Which of the following factors will produce low thrust value for takeoff?

high density altitude

The use of high voltage AC generation systems in large transport aircraft produces what advantage?

low current levels

Which answer describes the best CoG position to preserve elevator authority if you are faced with a jammed stabiliser trim whilst in flight ?

An aft position

A change in value of which element would increase the amount of thrust available ?

Temperature decrease

Lift dumpers (ground spoilers) are most effective if deployed at ?

As soon as possible after touchdown and before brake application

To apply the parking brake on a heavy transport aircraft the pilot?

First applies toe brake pressure and the pulls the park brake handle

The level for absolute aerodynamic ceiling is reduced as ?

Bank angle increases

Which statement best represents the effects of severe ice formation on an aircraft structure

Stall speed will be higher, stick shaker stall warning may be compromised, lift reduced, drag increased

A cabin humidifier is incorporated in aircraft with pressurised cabins, and utilised?

At high altitude

ATPL Systems

Will Erwin · 50問 · 1年前

ATPL Systems