viserfly

Questions for MEASUREMENT OF ELEMENTS

Answer the following questions

1. From "A" to "B" distance 2,000 nm. Track 080°, TAS 180K WIND 290/20 for first 1000 nm & 320/20 for rest of flight, endurance 15 Hrs. find a) Time of flight. b) Distance to PNR c) ETA to PNR (ETD 1000 IST)
2. Find G/S and Drift. Trk - 090°, TAS(kts) - 160, W/V - 330/18, G/S - ________ , HDG - 0.84°, DRIFT - ________ .
3. On a flight from A to B: Tr 317 WIND 205/35 TAS 185 K DPNR 732 nm Fligh Fuel 1200 lbs find: a) Fuel consumption b) SAR c) If CP is reached 45 min before PNR, find excess fuel carried on board.
4.
Dist = 1,250 nm. TRK = 030° FOB = 1,400 kg, Winds = 360/30 kts, Reserve = 150 kg TAS = (N) = 298 kts, F/C (N) = 200 kg/hr. (R) = 250 kts F/C (R) = 150 kg/hr. Find DCP and TCp ; DPNR and TPNR (ii) SAR ; Fuel required to go to destination.
5.
Dist. = 800 nm TRK 330° W/V = 270°/30 kts TAS (N) = 240 kts TAS (R) = 180 kts DCP and Tcp = ?
6.
Dist = 2000 nm Track = 090° W/V = 090°/30 kts for first 1,000 nm for remaining . = 330°/18 kts TAS (4 engine) = 380 TAS (3 engine) = 260 kts FOB = 2,500 kg Reserve = 350 kg FC (4 engine) = 360 kg/hr FC (3 engine) = 280 kg/hr.
7. The effect of an increasing strength of wind at 90° to track on the time and distance to the PET will be
8. From P to Q distance 2000 nm. Track 090, TAS 4 Eng. 180 K TAS 3 Eng. 150 K, WIND 090/20 for first 1000 nm. & 150/20 for rest of the flight. FOB 1600 gal, reserve 200 gal. fuel consumption 4 engine 100 GPH, 3 Eng 80 GPH. Find: a) Time & distance to CP b) Time & distance to PNR, return on 3 Eng. a) Time & distance to CP b) Time & distance to PNR, return on 3 Eng.
9. Distance 1015 nm. TAS 180 K, head wind 10 K, fuel cons 1200 lbs/hr Max AUW 90,000 lbs operational mass 50,000 lbs reserve fuel 3,000 lbs (to be added for PNR) find a) Time & distance to CP b) Time & distance to PNR
10. Find G/S and Drift. Trk - 220°, TAS(kts) - 310, W/V - 330/42, G/S - ________ , HDG - 227°, DRIFT - ________ .
11.
Dist = 1,500 nm TAS (4 engines) = 360 kts TAS (3 engines) = 300 kts TRK = 090° W/V = 33°/30 kts FOB = 4,500 kg Reserve = 500 kg F/C (4 engines) = 800 kg/ hr F/C (3 engines) = 600 kg / hr Find
12. From "A" to "B" distance 1500 nm. Track 347, TAS 4 Eng - 175 K TAS 3 Eng. 152K WIND 270/20 for first 1000 nm. & 245/20 for rest of the flight. FOB 1200 G. Reserve 100G, fuel cons 4 Eng. 120 GPH, 3 Eng 100 GPH. Find a) Time & distance to CP b) Time & distance to PNR return on 3 Engines
13. On a flight from A to B dist. 1100 nm. Track020° WIND 220÷°×/30. F/C 1200 lbs/hr FOB 10000 lbs reserve 1500 lbs, TAS 210 K (4-eng) TAS 185 K (3 eng) find: a) Time & distance to CP b) Time distance to PNR c) SAR
14.
Trk = 270°, TAS = (N) = 240 kts (R) = 150 kts , W/V = 090°/20 up to CP = 330×°/38 after CP , Dist = 1,100 nm FOB = 1,800 kg, Res = 200 kg FC (N) = 450 kg/hr, FC(R) = 300 kg/ hr.
15. Flight distance 1500nm, wind component out +40kt, back - 50kt, TAS 320kt, endurance - flight time +15%. The distance to the PNR will be
16.
In question 12, FF = 3,000 kg, Calculate Drives and True.
17.
Trk = 330° W/V = 290°/25 kts up to GP, 330°/15 kts after CP TAS (N) = 220 kts TAS(R) = 160 kts, Dist = 750 nm, POB = 1,500 kg Res = 100 kg, FC (N) = 180 kg/hr. FC (R) = 120 kg/hr. (i) DCP and TCP (ii) DPR and TPNR (assume engine failure at PNR)
18. Full TAS 500 kt. Engine failure TAS 400 kt. Total distance 1000 nm. Along track wind component 40 kt. The distance to the engine failure CP will be
19. On a flight from Y to X : Track 210, WIND 270/35. TAS 200 kts FF 1100 lbs DPNR 785 nm. Find a) fuel consumption b)SAR c) If CP is reached 45 min before PNR, find excess fuel carried on board
20. On a flight from A to B: Track 155, TAS 200 K WIND 260/35 DPNR 1050 nm, F/C 141 GPH find: a) fuel on board b) SAR c) If CP lies one hour 15 min before PNR, find find excess fuel carried on board
21. In flight it is discovered that the winds used have been reversal, the effect will be
22. On a flight from S to T dist. 1250 nm. Track 135 TAS (4 eng) 250 k TAS (3 eng) 215 K WIND 090/30 FOB 12000 lbs reserve 2000 lbs F/C (4 eng) 1200 lbs/hr F/C (3 eng) 1000 lbs/hr find: a) Time& distance to CP b) Time & distance to PNR c) Time & distance to PNR (return on 3 engine) d) SAR
23.
Dist = 2,400 nm. Trk = 080° W/V = 030°/25 kts TAS (N) = 440 kts TAS (R) = 360 kts FOB = 10,000 kg, Reserve = 1,000 kg, FC (N) = 1,400 kg/hr, FC(R) = 1,000 / kg / hr.
24.
Distance = 1,200 nm TRK = 090° TAS (Normal) 200 kts TAS (Reduced) = 150 kts Winds = 090°/20 kts. Find Dcp Tcp
25. On a flight from K to L dist 1500 nm. TAS 310 K track 350 WIND 240/30 FOB 12000 lbs. reserve 2000 lbs F/C 1800 lbs/hr find: a) Time & distance to PNR b) Time & distance to CP c) SAR
26. On a flight distance 1073 nm. TAS 170 kts, head wind 20 Kts. a) Find time & distance to CP. b) FOB is just sufficient for flight find the time & distance to PNR.
27. From 'X' to "Y" distance 1250 nm. track 120, TAS 4 Eng. 180 K TAS 3 Eng. 150 K, WIND 090/30 up to CP & 060/30 after CP. FOB 1500 G fuel consumption 4 Eng 100 GPH, 3 Eng 80 GPH. Find a) Time & distance to CP in case of engine failure. b) Time & distance to PNR with 200 G of reserve. Return on 3 engnles
28.
TEK = 0500 W/V 330°/18 kts DPNR = 800 Nm FOB = 1,540 kg Reserve Reqd. = 150 kg TAS = 200 kts. Find (i) Fuel consumption ; SAR (ii) If CP is reached 30 min before PNR, Find excess fuel carried on board on reaching destination.
29.
For flight fuel of 2000 Kg calculated Dpnr = 500 nm. If Flight Fuel is increased by 200 Kg, Dpnr will be: (a) 520 nm (b) 550 nm (c) 450 nm Methods to Solve Questions on CP and PNR: Dcp (Distance to CP) DH / O+H nm Dpnr = E ×GO× GH / Go × GH = NM
30. On a flight from X to Y : track 250, TAS 195, dist 975 nm WIND 330/35, FOB 900 gal reserve 100 gal F/C 150 GPH find: a) Time & distance to PNR b) Time & distance to CP c) SAR
31. From A to B distance 1450 nm. track 132, TAS 4 Eng 190 K, TAS 3 Eng 160 K, WIND 260/40 up to CP & 350/60 after CP, FOB 18000 lbs, reserve 1000 lbs fuel consumption 4 Eng 1850 lbs/hr 3 Eng. 1450 lbs/hr. find a) Time & distance to CP b) Time & distance to PNR return on 3 Eng
32. On a simple flight from A to B, the distance to the PET is 1200nm. The PNR endurance is equal to the flight time +10%. The distance to the PNR will be
33.
In question 5, fuel on board 1,000 kg, F/C = 1550 kg/ hr, Reserve = 100kg. Find Dpnr and Tpnr. WV = 270/30 A ↔ B 800 nm PNR
34. On a flight out to the PET, the GS are found to be less then expected. The PET will be moved along track
35. The distance to the PNR will be greatest
36. For head wind component of 50 Kts calculated DCP is 750 nm for the total route dist of 1200 nm. In actual flight wind component is found to be 50 Kts of tail wind, new position of DCP will be
37. On a flight from A to B dist. 1015 nm. track 083, TAS 190 K on 4 Engines, 160 K on 3 Engines, WIND 190/45 up to CP& 110/40 after CP. FOB 15000 lbs, reserve 2000 lbs, F/C 1800 lbs/hr on 4 engines & 1400 lbs/hr on 3 engines. Find a) Time& distance to CP b) Time & distance to PNR (return on Engines)
38. From X to Y distance 1200 nm TAS 160 K, Tail wind of 10 K for first 600 nm. & head wind of 10 K for rest of flight find time & distance to CP
39. In above question find SAR.
40.
TRK = 350° W/V = 120°/28, TAS (4 engine) = 450 kts (3 engine) = 300 kts, Dist. = 1,500 nm. Find Dcp and Tcp
41. An engine failure PNR is calculated to enable the pilot to make the correct decision in the event of
42. On a flight from A to B : Track 153, TAS 210 K Dist. 925 nm WIND 200/30, FOB 1000 lbs, reserve 200 lbs. F/C 180 lbs/hr. find: a) Time & distance to PNR b) Time & distance to CP c) SAR.
43. Find G/S and Drift. Trk - 120°, TAS(kts) - 180, W/V - 180/15, G/S - ________ , HDG - 124°, DRIFT - ________ .
44.
In question 12, is fuel sufficient to go to B?
45. Find G/S and Drift. Trk - 315°, TAS(kts) - 220, W/V - 090/22, G/S - ________ , HDG - 319°, DRIFT - ________ .