A-320 Performance Question Paper

Flight Simulation Technique Centre A-320 Aircraft Performance final Test: Pilots Total Marks: 100

Time: 1:30

Select the correct answer. Q.1 In the case of refuelling refuelling with one engine running A) Point the A/C in to wind where the slope is negligible B) Carry out gravity refuelling. C) Both A & B are correct.

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Q.2 Take-off optimisation is calculated in an airport analysis chart for a given R/W and obstacle for A) Temp., wind, & config. B) Temp., config. & QNH C) Config., QNH, wind, & temprature

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Q.3 On typical runway performance of twin engine aircraft is is generally limited by A) Two engines operative at T/O. B) One engine out at T/O C) Both A & B are correct.

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Q.4 Conservative correction correction for weight if T/O T/O is performed with with full thrust with with engine anti-ice is on is A) Subtract 1850 Kgs B) No correction C) Subtract 90 Kgs

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Q.5 In case flex T/O A) Thrust must not be reduced by more than 35% of full rated thrust B) The flex T/O EPR cannot be lower than m ax climb EPR at same flight conditions C) Both A & B are correct

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Q.6 RLD dry is equal to A) ALD dry x 1.15 B) ALD dry x 1.67 C) ALD dry x 0.6

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Q.7 Find the ALD landing wt 64t, config full, PA 2000ft, App speed VLS+5, surface wet, tail wind 5 kts, two reverser operative. A) 1360M B) 1260M, C) 1570M

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Q.8 Find RLD for manual landing wt 60t surface dry, CG forward, head wind 10kts PA 3000ft config full A) 1510M B) 1730M C) 1780M

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Q.9 What is the wt. penalty to dry R/W T/O wt when taking-off from R/W covered with 5 mm of  water,config 1+f , R/W length 3000M without Clearway A) 9.7t B) 10.9t C) 11.8t

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Q.10 In case of without cabin Pressurization rate of descent must be limited to A) 500ft/min. B) 1000ft/min. C) 750ft/min.

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Q.11 Fuel for flight without cabin pressurisation at flight level 100, LRC at wt 65t, with 50kts tailwind, ISA +10deg, air-conditioning off anti-icing off at a ground distance of 579 NM is A) 4350Kgs B) 4340Kgs C) 4400Kgs

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D) 4040 Kgs

Q.12 For a flight with gear down for second segment gradient conditions in config 1+f, the wt reduction calculated from RTOW charts is A) 22% B) 18% C) No Reduction

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Q.13 Trip fuel for cruise for an air-distance of 700NM from quick determination of flight plan for flight level 310 with landing wt of 64t at 0.78 Maunder ISA condition is

A) 4490 Kgs B) 4590 Kgs C) 4280 Kgs

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Q.14 Fuel required for alternate planning at destination with a ground distance 240NM wind calm F/L 200 ISA +20, with ref landing wt of 60t is A) 1990 Kgs B) 1830 Kgs C) 1910 Kgs

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Q.15 Find T/O EPR when OAT is +30 deg., P A 2000ft, Air-conditioning on A) 1.430 B) 1.420 C) 1.440

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Q.16 Time fuel & distance to climb from F/L 15 to F/L270 with brew 72t ISA +20 with normal airconditioning and anti-ice off at max. Climb thrust is A) 19mts 1453Kgs 118NM B) 21mts 1682 Kgs 123NM C) 13mts 1155Kgs 83NM

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Q.17 Optimum altitude for 0.78M T/O wt. 70 t at ISA+20 is A) 34000 B) 34500 C) 34700

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Q.18 Given winds at F/L 350 are 40Kts headwind wt. is 62.5t flying at .78M.What should be wind at F/L 310 to have same effect. A) 40k TW B) Nil wind C) 17k HW

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Q.19 Find ALD when landing wt. 64t, TW 5k, elevation 3000ft CG normal, surface wet with reverser, flap-3, s