Easa fly planning repaso

VFR flights shall be flown over congested areas of cities at a height not less than [1] ___ above the highest obstacle within a radius of [2] ___ from the aircraft. [1] 1000 ft, [2] 600 m. 2000 ft, [2] 600 ft. 1000 ft, [2] 300 m. ] 1500 ft, [2] 900 ft.

(See attachment IC-033-031) The distance from C (62°N 020°W) to B (58°N 004°E) is: 770 NM. 720 NM. 670 NM. 620 NM.

See attachment IC-033-031) The Initial Magnetic Course from A (64°N 006°E) to C (62°N 020°W) is: 271°(M). 267°(M). 263°(M). 091°(M).

See attachment IC-033-031) The Distance from A (64°N 006°E) to C (62°N 020°W) is: 720 NM. 690 NM. 1490 NM. 1410 NM.

(See attachment IC-033-031) The Initial True Course from C (62°N 020°W) to B (58°N 004°E) is: 101°(T). 109°(T). 113°(T). 281°(T).

For a VFR routing along a mountainous region with the information given, determine the lowest usable flight level for this leg: Elevation of nearby airport: 3400 ft Grid-MORA: 5400 ft Obstacle Clearance required: 2000 ft QNH 983 hPa Temperature ISA-12 Magnetic Course: 220°(M). FL 65. FL 85. FL 75. FL 55.

Minimum Safe Altitude (MSA) 8500 ft OAT -20°C at FL 85 QNH 1003 hPa Elevation 4000 ft The minimum safe Pressure Altitude, rounded to 10 ft, is: 9150 ft. 8250 ft. 9550 ft. 8650 ft.

For a VFR routing along a mountainous region with the information given, determine the lowest usable flight level for this leg: Elevation of nearby airport: 1300 ft Grid-MORA: 6500 ft Obstacle Clearance required: 2000 ft QNH 993 hPa Temperature ISA-18 Magnetic Course: 120°(M). FL 75. FL 85. FL 55. FL 65.

With the following information given, calculate the TAS: Cruising Level: FL 370 Mach number: M 0.80 Temperature: ISA-10 Wind component: -65 kt. 449 kt. 544 kt. 260 kt. 506 kt.

Compass Heading 252° Variation 22°E Deviation 3°W Drift Angle 9° right The True Track is: 280°. 224°. 246°. 268°.

(See attachment IC-033-090) The correct relationship between Local Time (LT) and Universal Time Coordinated (UTC) in Greece in (1) Winter and (2) Summer is: (1) LT = UTC + 2 Hours (2) LT = UTC + 3 Hours. 1) LT = UTC - 2 Hours (2) LT = UTC - 3 Hours. 1) LT + 2 Hours = UTC (2) LT + 3 Hours = UTC.

Given a heading of 060 at a TAS of 140 kt. and wind/velocity 170/20, calculate (1) drift angle and (2) ground speed: (1) 7°L, (2) 148 kt. (1) 7°R, (2) 148 kt. (1) 7°L, (2) 132 kt. (1) 7°R, (2) 132 kt.

Still air climb distance 189 Nautical Air Miles (NAM), time to climb 30 min. Calculate the ground distance with a 30 kt head wind: 174 NM. 205 NM. 184 NM. 196 NM.

Time to cruising level 36 min. Still Air Distance 157 NAM With an average 60 kt tailwind the ground distance is: 193 NM. 128 NM. 155 NM. 216 NM.

See attachment IC-033-028) The elevation of LSZH ZURICH KLOTHEN airport (47°28'N, 008°33'E) is: 1417 ft. 3700 m.

The Minimum Off-Route Altitude (MORA) provides obstruction clearance up to what distance from the airway centerline?. 10 NM. 5 NM.

An airway is marked "3500T 2100 a" means the: Minimum Obstacle Clearance Altitude (MOCA) is 3500 ft. Minimum En-route Altitude (MEA) is 3500 ft.

According ICAO Doc 82168, in non-mountainous areas (e.g with terrain not higher than 3000 ft), the minimum permissible holding level provides a clearance of at least (1) ____ above obstacles in the holding area, and a clearance which ranges from 300 m at the edge of the holding area to a minimum of 60 m at the (2) ____ limit of the buffer area. (1) 300 m, (2) 5 NM. (1) 600 m, (2) 5 NM. (1) 300 m, (2) 10 NM. (1) 600 m, (2) 10 NM.

The approach chart for an RNAV approach shows a decision height of 320 ft. Type and category of this approach are: Type A, no category. Type B, Category II. Type B, no category.

A RNP Type B approach must be 3D and requires: 1. ILS 2. MLS 3. GBAS 4. SBAS 5. ABAS only. 1, 2, 3 or 4. 1, 2 or 5. 3, 4 or 5. 1, 3, 4 or 5.

With regard to LPV approaches, the (1) ____ guidance is equivalent to localizer, and the protected area is considerably (2) ____ than the protected area for the present LNAV and LNAV/VNAV lateral protection. (1) lateral, (2) smaller. (1) lateral, (2) larger.

Distance 300 NM Wind (true) 340/40 Magnetic course 300° Variation 20°E TAS 440 kt Calculate the flight time: 45 min. 37 min. 42 min. 48 min.

Limitations of using GNSS/FMC equipment include: 1. Inaccuracy and loss of precision by FMS navigation calculations. 2. Aircraft mass significantly differs from that which was input by the crew. 1 is incorrect, 2 is correct. 1 is correct, 2 is incorrect. 1 is incorrect, 2 is incorrect. 1 is correct, 2 is correct.

Given the following values: Start fuel: 10 litres Fuel flow during taxi: 90 litres/hour Estimated Taxi time: 10 minutes Assuming 0.82 kg/litres, the fuel required for engine start and taxi is: 20.5 kg. 30.5 kg. 12.3 kg. 25 kg.

With regard to CAT operations and the information given below, calculate the required Alternate Fuel: Fuel for missed approach at the destination: 200 kg Fuel for climb to cruise level: 750 kg Cruise fuel flow: 1800 kg/hour Cruise flight time: 40 min Descent fuel to alternate: 120 kg Fuel for approach and landing at alternate: 200 kg Holding fuel at alternate: 900 kg Fuel for a missed approach at alternate: 200 kg. 2470 kg. 1200 kg. 3070 kg. 3570 kg. 40.750.

Dry Operating Mass 34410 kg Traffic Load 7500 kg Final reserve fuel 963 kg Alternate fuel 1200 kg Contingency fuel 107 kg (not consumed) The Landing Mass at the Alternate will be: 42980 kg. 41910 kg. 42017 kg. 44180 kg.

For a flight with an aeroplane with turbine engines to an isolated destination aerodrome in CAT operations with fuel amounts given below, calculate the additional fuel according legal requirements for additional fuel: Cruise Fuel Flow: 2770 kg/h Contingency Fuel: 360 kg Final Reserve Fuel: 1330 kg. 4210 kg. 1440 kg. 5540 kg. 6870 kg.

For a flight with an aeroplane with reciprocating engines to an isolated destination aerodrome in CAT operations with fuel amounts given below, calculate the minimum fuel required when arriving overhead the isolated aerodrome: Planned flight time (TOC to TOD): 02 h 15 min Cruise Fuel Flow: 880 kg/h Final Reserve Fuel: 420 kg (TOC: Top of Climb, TOD: Top of Descent). 957 kg. 924 kg. 660 kg. 1760 kg.

Leg distance 123 NM Estimated leg time 39 min Actual leg time 41 min The groundspeed is: 180 kt. 190 kt. 200 kt. 175 kt.

Total distance 165 NM True track 055° W/V 360/20 TAS 105 kt Calculate the distance from the departure point to the PET: 92 NM. 75 NM. 86 NM. 127 NM.

Distance 875 NM True Track 240° W/V 060/50 TAS 500 kt Calculate the Distance (NM) and the Time (min) from the departure point to the PET: 394 NM, 43 min. 476 NM, 62 min. 719 NM, 79 min. 426 NM, 49 min.

Distance 2800 NM True Track 140° W/V 140/100 TAS 500 kt Caluculate the Distance (NM) and the Time (min) of the PET from the departure point: 1680 NM, 252 min. 1130 NM, 114 min. 1350 NM, 159 min. 1140 NM, 136 min.

Distance X to Y 2700 NM Mach No. 0.75 OAT -45°C Tailwind 'out' 10 kt Tailwind 'back' 35 kt The distance from X to the PET is: 1386 NM. 1354 NM. 1308 NM. 1436 NM.

Distance 2500 NM GS Out 540 kt GS Home 470 kt Calculate the time from the departure point to the PET: 129 min. 167 min. 145 min. 34 min.

Distance 950 NM GS Out 275 kt GS Home 225 kt Calculate the Time from the departure point to the PET: 93 min. 142 min. 107 min. 39 min.

Distance from WP 3 to WP 4 750 NM TAS out 430 kt TAS return 425 kt Tailwind out 30 kt Headwind return 40 kt The distance from WP 3 to the PET is: 342 NM. 373 NM. 412 NM. 401 NM.

Course A to B 088° (T) Distance 1250 NM Mean TAS 330 kt Mean W/V 340°/60 kt The time from A to the PET in minutes is: 103 min. 114 min. 94 min. 125 min.

Total Distance 410 NM Safe Endurance 3.6 h True Track 055° W/V 180/35 TAS 120 kt The distance of the PSR from the departure point is: 203 NM. 173 NM. 97 NM. 211 NM.

Total Distance 500 NM Safe Endurance 4 h TAS 140 kt Ground Speed Out 150 kt Ground Speed Home 130 kt Calculate the distance and time of the PSR from the departure point: 279 NM, 01 h 51 min. 227 NM, 01 h 54 min. 138 NM, 01 h 03 min. 226 NM, 01 h 31 min.

Maximum useable fuel 15000 kg Minimum reserve fuel 3500 kg TAS out 425 kt Headwind out 30 kt TAS return 430 kt Tailwind return 20 kt Average fuel flow 2150 kg/h The time to the Point of Safe Return (PSR) is: 2 h 51 min. 3 h 45 min. 2 h 53 min. 2 h 33 min.

The planned fuel is: Trip fuel Sufficient for 04 h 24 min Reserve fuel 30% of planned trip fuel Start up and Taxi fuel 15 kg Block fuel 138 kg After 3 h 18 min in flight, the remaining fuel is: 53 kg. 61 kg. 34 kg. 47 kg.

Trip Fuel 3 h 36 min Reserve Fuel 30 % of Trip Start up & Taxi Fuel 26 kg Block Fuel 786 kg After 1 h 30 min. flight time, the remaining fuel is: 516 kg. 543 kg. 566 kg. 375 kg.

Planned Fuel: Trip 5 h 25 min Reserve 30 % of Trip Start up and Taxi 12 kg Block 945 kg After 4 h in flight the remaining fuel is: 403 kg. 448 kg. 253 kg. 471 kg.

Trip Fuel 4 h 25 min Reserve Fuel 30% of Trip Fuel Start up and Taxi Fuel 45 kg Block Fuel 600 kg After flying 3 h 15 min, the remaining fuel is: 241 kg. 273 kg. 153 kg. 217 kg.

Block Fuel 200 lb Alternate Fuel 40 lb Final Reserve Fuel 50 lb Taxi Fuel 10 lb Remaining Fuel (after 36 min.) 110 lb With constant fuel flow and landing with required reserve fuel, the flight time remaining to the destination is: 9 min. 47 min. 16 min. 28 min.