9 FLIG. PER. EXAM. PREP.

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236 The total weight of an airplane together with its total contents at any particular time is referred to as:

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239 If air density is increased above ISA conditions, the take-off distance required at full throttle compared with that for standard conditions will be:

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240 The performance tables of an aircraft for take off and climb are based on:

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241 What is the maximum zero fuel mass ?

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242 TORA is the:

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244 The take-off mass of an airplane is:

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245 What is the balance arm?

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246 The part of run way available to an aircraft and capable of supporting its weight during the take-off phase is:

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247 In comparison to the true airspeed in still air conditions, the TAS for the best range in strong tailwind will be:

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248 Which of the following items are included in the Dry Operating Mass?

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250 In respect of all runway surfaces:

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251 The maximum range in a glide path will be achieved by:

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253 If the aircraft C of G is on the forward centre of gravity limit:

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254 When gliding for maximum range, the greater the aircraft weight:

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255 In comparison to gliding in still air conditions, the rate of descent will be …..(i)….. and the distance llown will be …(ii)…… in a tailwind:

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257 The distance covered when gliding headwind compared with gliding in still air will result in ….. (i)…….. distance traveled over the ground together with ….. (ii)…… descent:

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258 Increasing an aircraft's gross weight will …….(X)…… the stall speed, ….(Y)….. the take-off run required and ….(Z)….. the landing distance required.
Select the correct combination.

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259 Why is full flap selected during the approach and landing phase of a flight?

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260 Light twin aircraft, for the purpose of aircraft performance, are certified under JAR 25 as:

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261 If the approach and landing speeds are increased above the recommended in the Pilot's Operating Handbook:

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262 Flight for the maximum range in a piston engined aircraft is achieved by flying:

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263 With an increase of flap setting angle from 50 to 120 , both angles are within limits, what will be effect on:
(I) the required take-off run to lift off
(II)the mean drag during the take-off

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264 An aircraft cruising at 3000 ft is cleared to climb to 8000 ft. See the table and calculate the time taken in minutes, the used fuel in gallons and the distance flown during the climb, (Fig.1).Temperature is standard, wind is calm).

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265 An aircraft cruising at 5000 ft is cleared to climb to 10000 ft. See the table and calculate the time taken in minutes, the used fuel in gallons and the distance flown during the climb, (Fig.1). (Temperature is standard, wind is calm).

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266 The primary reason for making a take-off into the wind is to: (i) reduce the take-off run available (TORA) (ii) reduce the take-off distance required and (iii) reduce the ground speed at which the aircraft will take off.
Select from he following:

9 FLIG. PER. EXAM. PREP.

9 FLIG. PER. EXAM. PREP.

236 The total weight of an airplane together with its total contents at any particular time is referred to as:

239 If air density is increased above ISA conditions, the take-off distance required at full throttle compared with that for standard conditions will be:

240 The performance tables of an aircraft for take off and climb are based on:

241 What is the maximum zero fuel mass ?

242 TORA is the:

244 The take-off mass of an airplane is:

245 What is the balance arm?

246 The part of run way available to an aircraft and capable of supporting its weight during the take-off phase is:

247 In comparison to the true airspeed in still air conditions, the TAS for the best range in strong tailwind will be:

248 Which of the following items are included in the Dry Operating Mass?

250 In respect of all runway surfaces:

251 The maximum range in a glide path will be achieved by:

253 If the aircraft C of G is on the forward centre of gravity limit:

254 When gliding for maximum range, the greater the aircraft weight:

255 In comparison to gliding in still air conditions, the rate of descent will be …..(i)….. and the distance llown will be …(ii)…… in a tailwind:

257 The distance covered when gliding headwind compared with gliding in still air will result in ….. (i)…….. distance traveled over the ground together with ….. (ii)…… descent:

258 Increasing an aircraft's gross weight will …….(X)…… the stall speed, ….(Y)….. the take-off run required and ….(Z)….. the landing distance required. Select the correct combination.

259 Why is full flap selected during the approach and landing phase of a flight?

260 Light twin aircraft, for the purpose of aircraft performance, are certified under JAR 25 as:

261 If the approach and landing speeds are increased above the recommended in the Pilot's Operating Handbook:

258 Increasing an aircraft's gross weight will …….(X)…… the stall speed, ….(Y)….. the take-off run required and ….(Z)….. the landing distance required.
Select the correct combination.

263 With an increase of flap setting angle from 50 to 120 , both angles are within limits, what will be effect on:
(I) the required take-off run to lift off
(II)the mean drag during the take-off

266 The primary reason for making a take-off into the wind is to: (i) reduce the take-off run available (TORA) (ii) reduce the take-off distance required and (iii) reduce the ground speed at which the aircraft will take off.
Select from he following: