7 FLIG. PER. EXAM. PREP.

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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]

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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:

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181 Flight for maximum range in a piston engined normally aspirated aircraft is achieved by flying:

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182 Under what conditions is carburettor icing likely to occur?

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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.

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184 In a constant IAS climb in the troposphere?

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185 In a constant TAS climb?

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186 The relationship between Vx and Vy?

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187 As altitude increases?

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188 Loading icreases, then……………………

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189 Take-off performance is best with?

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191 When flying close to the max. operating altitude?

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192 A RW slope contaminated with 5 mm of dry snow, will …………………… landing distance compared to a dry runway?

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193 If a pilot decides to use 40? flaps on his Cessna 172, instead of the standard of 30,? when landing?

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194 5 mm of snow will………………………………………. the LDR?

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197 Observe Fig. 29, carefully and spot Vx and Vy at S.L.

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199 If the aeroplane in Fig. 27 quits engine at 8.000 ft, the distance will cover in still air conditions, is:

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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:

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201 From the illustratiom in Fig.28, select the initial climb profile, with take-off flap set.

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203 What effect has a centre of gravity close to the forward limit?

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206 Consult Fig.30 that's in accordance with CAP 696
Where is the reference datum?

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207 Consult Fig.30 that's in accordance with CAP 696
What are the CG limits?

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208 Consult Fig.30 that's in accordance with CAP 696
What is the CG at the BEM?

1

209 Consult Fig.30 that's in accordance with CAP 696
What is the distance of the main undercarriage from the firewall?

1

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?

7 FLIG. PER. EXAM. PREP.

7 FLIG. PER. EXAM. PREP.

7 FLIG. PER. EXAM. PREP.

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]

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:

181 Flight for maximum range in a piston engined normally aspirated aircraft is achieved by flying:

182 Under what conditions is carburettor icing likely to occur?

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.

184 In a constant IAS climb in the troposphere?

185 In a constant TAS climb?

186 The relationship between Vx and Vy?

187 As altitude increases?

188 Loading icreases, then……………………

189 Take-off performance is best with?

191 When flying close to the max. operating altitude?

192 A RW slope contaminated with 5 mm of dry snow, will …………………… landing distance compared to a dry runway?

193 If a pilot decides to use 40? flaps on his Cessna 172, instead of the standard of 30,? when landing?

194 5 mm of snow will………………………………………. the LDR?

197 Observe Fig. 29, carefully and spot Vx and Vy at S.L.

199 If the aeroplane in Fig. 27 quits engine at 8.000 ft, the distance will cover in still air conditions, is:

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:

201 From the illustratiom in Fig.28, select the initial climb profile, with take-off flap set.

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]

206 Consult Fig.30 that's in accordance with CAP 696
Where is the reference datum?

207 Consult Fig.30 that's in accordance with CAP 696
What are the CG limits?

208 Consult Fig.30 that's in accordance with CAP 696
What is the CG at the BEM?

209 Consult Fig.30 that's in accordance with CAP 696
What is the distance of the main undercarriage from the firewall?

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?