5826517
Description
Quiz by tsampikos pompou, updated more than 1 year ago
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Created by tsampikos pompou
over 8 years ago
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Question 1
Question
179 Pressure altitude is frequently employed as the datum for measuring aircraft performance. Given an aerodrome elevation as 1010ft amsl and a QFE of 990hPa.
What is the aerodrome pressure altitude? [1mb = 30ft]
Answer
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O 1700ft
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O 1500ft
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O 1244ft
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O 1623ft.
Question 2
Question
180 The take-off distance safety factor, mandatory for all public transport flights is recommended by the CAA to be applied to all flights. After all other variable factors have been taken into account when calculating the take-off distance required, that figure should be increased by:
Answer
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O 33% or the original take-off distance factored by 1.33.
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O 25% or the original take-off distance factored by 1.25,
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O 45% or the original take-off distance factored by 1.45.
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O 20% or the original take-off distance factored by 1.20.
Question 3
Question
181 Flight for maximum range in a piston engined normally aspirated aircraft is achieved by flying:
Answer
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O at just above the minimum drag speed.
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O at the lowest density altitude that is safely possible.
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O just below that speed which provides the maximum power/airspeed ratio.
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O at the same speed, where minimum difference between power required and power available exist.
Question 4
Question
182 Under what conditions is carburettor icing likely to occur?
Answer
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O During descent power setting or idle when the throttle butterfly opening is minimal.
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O When climb power is selected and the throttle butterfly is fully open.
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O At high altitude in very cold air before the fuel is correctly leaned for the cruise.
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O During cruise power settings when the throttle butterfly is half open.
Question 5
Question
183 The remaining fuel weight available for computing mass and balance, is 285 Kgs AVGAS of specific gravity 0.70. Determine how many litres the pump will indicate to be within limits.
Answer
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O 407 lts.
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O 1995 lts.
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O 355 lts.
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O 500 lts.
Question 6
Question
184 In a constant IAS climb in the troposphere?
Answer
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O TAS increases.
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O TAS decreases.
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O TAS increases, then remains constant.
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O TAS decreases, then remains constant.
Question 7
Question
185 In a constant TAS climb?
Answer
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O IAS decreases, then decreases rapidly.
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O IAS increases.
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O IAS decreases.
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O IAS increases rapidly.
Question 8
Question
186 The relationship between Vx and Vy?
Answer
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O Vx is always less than or equal to Vy.
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O Vx is always less than Vy.
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O Vx is always greater than Vy,
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O There's no between them.
Question 9
Question
187 As altitude increases?
Answer
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O Vy decreases and Vx remain almost constant.
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O Vx and Vy both increase.
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O Vx and Vy both decrease.
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O Vx and Vy is zero at service ceiling.
Question 10
Question
188 Loading icreases, then……………………
Answer
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O Vx and Vy increase.
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O Vx increases and Vy decreases.
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O Vx decreases and Vy increases.
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O both Vx and Vy decrease.
Question 11
Question
189 Take-off performance is best with?
Answer
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O Low altitude, low temperature, low humidity.
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O High altitude, high temperature, high humidity.
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O Low altitude, low temperature, high humidity.
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O High altitude, low temperature, low humidity.
Question 12
Question
191 When flying close to the max. operating altitude?
Answer
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O Manouevrability is degraded.
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O Manouevrability is improved.
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O Manouevrability is possible.
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O None of them is possible.
Question 13
Question
192 A RW slope contaminated with 5 mm of dry snow, will …………………… landing distance compared to a dry runway?
Answer
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O increase.
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O decrease.
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O increase or decrease, depending on pilot's skills.
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O increase or decrease depending on flap setting.
Question 14
Question
193 If a pilot decides to use 40? flaps on his Cessna 172, instead of the standard of 30,? when landing?
Answer
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O LDR is decreased and go-around performance degraded.
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O LDR is increased and go-around performance improved.
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O LDR is increased and go-around performance degraded.
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O LDR is decreased and go-around performance improved.
Question 15
Question
194 5 mm of snow will………………………………………. the LDR?
Answer
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O increase.
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O decrease.
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O increase or decrease -depending on PA-
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O not affect.
Question 16
Question
197 Observe Fig. 29, carefully and spot Vx and Vy at S.L.
Answer
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O 59kt and 73kt,
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O 61kt and 68kt.
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O 75kt and 70kt.
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O 70kt and 80kt.
Question 17
Question
199 If the aeroplane in Fig. 27 quits engine at 8.000 ft, the distance will cover in still air conditions, is:
Answer
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O 12 nm
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O 10 nm
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O 14 nm
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O 13 nm.
Question 18
Question
200 An aircraft with full tanks has 500 litres on board. Given that the fuel specific gravity is 0.750, the weight of the fuel will be:
Answer
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O 825 lbs or 375 Kgrs.
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O 800 lbs. or 362 Kgrs
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O 820 lbs or 372 Kgrs.
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O 900 lbs or 407 Kgrs.
Question 19
Question
201 From the illustratiom in Fig.28, select the initial climb profile, with take-off flap set.
Answer
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O A to B, blue line.
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O Γ to Δ, red line.
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O Νοne of them.
Question 20
Question
203 What effect has a centre of gravity close to the forward limit?
Answer
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O A reduce rate of climb
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O A better rate of climb capability
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O A reduction in the specific fuel consumption
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O A decreased induced drag
Question 21
Question
206 Consult Fig.30 that's in accordance with CAP 696
Where is the reference datum?
Answer
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O 39 inches forward of the firewall
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O 74 inches aft of the fwd CG position
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O 80.4 inches aft of the rear CG position
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O 87.7 inches aft of the rear CG position
Question 22
Question
207 Consult Fig.30 that's in accordance with CAP 696
What are the CG limits?
Answer
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O fwd limit = 74 inches to 80.4 inches and aft limit = 87.7 inches
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O fwd limit = 74 inches to 80.4 inches
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O fwd limit = 74 inches, aft limit = 80.4 inches
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O fwd limit = 74 inches, aft limit = 87.7 inches
Question 23
Question
208 Consult Fig.30 that's in accordance with CAP 696
What is the CG at the BEM?
Answer
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O 77.7 inches
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O 77 inches
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O 87 inches
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O 77.7 centimetres
Question 24
Question
209 Consult Fig.30 that's in accordance with CAP 696
What is the distance of the main undercarriage from the firewall?
Answer
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O 58 inches
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O 97 inches
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O 87.7 inches
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O 39 inches
Question 25
Question
210 Consult Fig.30 that's in accordance with CAP 696
The aircraft has six seats. Assuming no other cargo or baggage, what is the maximum fuel (in 74USG capacity version), that can be carried if all six seats are occupied and the mass of each occupant is 180 lb?
Answer
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O 155 lbs but the CG would be dangerously out of limits
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O 296 lbs but the CG would be dangerously out of limits
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O 444 lbs and the CG would be dangerously out of limits
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O 1551bs and the CG would be in limits since tank fuel capacity is 74USG
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