The details of an aircraft flight from M to N ( no fuel is available at N ) are given below:-Distance M to N 750 nmAverage TAS 380 KWind component M to N 30 K HWAverage fuel flow 5700 Kg/hrFuel reserve (assume unused) 500 Kg Ac weight less fuel & pay load 52000 KgMax T/O weight at M 91000 KgMax T/O weight at N 88000 KgMax Landing weight at M 77500 KgMax Landing weight at N 75000 Kg

Find max payload from M to N and N to M:-a. 14500, 22500 b. 15800, 25000 c. 15800, 14500 d. 25000, 22500.

2. Max take off weight 45000 lbs.Max landing weight 40000 lbs.Flight fuel 4000 lbs.Reserve fuel 800 lbs.Empty weight 25000 lbs.Find pay load and state if a/c can carry additional reserve fuel without affecting pay load, and if so how much?a. 15200, yes, 1000 lbs. b. 15200, no, 0 lbs c. 14200, yes, 1000 lbs d. 14200, no, 0 lbs.

3. From P to Q ( where fuel is not available) & return to P. Maximum payload is to be off loaded at Q & maximum pay load is to be uplifted from Q The data given is:

Distance P to Q 610 nm.Weight no fuel & no payload 36500 kg.Max landing weight 52400 kg.Max take off weight 63000 kg.Reserve fuel unused 4000 kg.Additional fuel for each flight 500 kg.(T/O circuit landing etc)Mean Fuel consumption 1350 kg/Hr.Mean ground speed P to Q 240 KMean ground speed Q to P 280 K

Find fuel to be up lifted at P, maximum pay load P to Q, maximum pay load Q to P.a. 7425, 8475, 11900 b. 4000, 11900, 9075.c. 11345, 8475, 11900 d. 2925, 11345, 9075.

4. Given:-Maximum take off weight 82000 lbsMaxing landing weight 64500 lbs

Basic operating weight 50000 lbsFlight fuel 16000 lbsReserve Fuel 1500 lbs.

Find the pay load that can be carried.a. 13000. b. 14500.c. 14000. c. 13500.

5. An a/c is to fly from A to B.Max T/O Weight 82000 lbsMax Weight without fuel 50000 lbs& pay loadMax. landing weight 64000 lbsFuel for flight A to B 16000 lbsReserve Fuel 8000 lbsIf the a/c lands at B after having consumed 500 lbs of reserve fuel what is max. payload that can be carried?a. 6000 . b. 6500.c. 7000. d. 7500.

6. An a/c is to fly from A to B.Max permissible take off weight 82000 lbsMax weight without fuel and payload 50000 lbsMax permissible landing weight 69000 lbsFuel required for flight from A to B 16000 lbs

. Reserve 3000 lbs.

What is the max payload that can be carried? Is it possible to carry additional reserve fuel without affecting the pay load?a. 13000, yes, 1000. b. 14000, no, 0.c. 1300, no, 0. d. 14000, yes, 0.

7. A flight is to be made from M to N and return to M carrying max. payload in each direction, Fuel is not available at N.Given:-Distance to M to N 80 NMMean ground speed M to N 70 KMean ground speed N to M 110 KMean fuel consumption 410 Kg/hrMax take off wt. at M 6180 KgMax landing wt. at N 5740 KgMax take off wt. at N 5800 Kg.Max landing wt. at M 5460 Kg.Max zero fuel wt. 5180 Kg.Aircraft wt less fuel and pay load 4400 Kg.Reserve fuel ( assume not used) 250 Kg.

Calculate: Max payload which can be carried from M to N and Max payload which can be carried from N to M.

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a. 780, 764. b. 764,780.c. 794, 780. d. 780,810.

8. Max T/O weight 51.00 Tons.RTOW 50.00 Tons.Max Landing Weight 43.25 Tons.Max Zero Fuel Weight 39.10 TonsAPS Weight 27.50 TonsTrip Fuel 4.2 TonsReserve Fuel 1.00 Ton

Find the payload that can be carrieda. 14.75. b. 18.30.c. 17.30. d. 11.60.

9. Max Take off weight 80000 LbsMaximum Landing Weight 60000 LbsBasic Weight 48000 LBSTAS 200 KTrack 350W/V 350/20Distance 1350 nmFuel consumption 2500 Lbs/HrReserve Fuel 3500 Lbs

Find the pay load that can be carrieda. 9750. b. 8500.c. 9500. d. 8750.

10. Max T/O Weight 55000 kgMax Landing Weight 52000 KgMax Zero Fuel Weigh t 38000 KgA/C weight without Fuel & pay load 29000 KgFuel Cons 1600 Kg/HrDistance 1500 nmReserve Fuel 2750 KgTAS 260 K

Find max pay load in still and max pay load with a head wind of 90 K.a. 10000, 10000. b. 11000, 11000.c. 9000, 9000. d. 10000, 9000.

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