Flight planning easa 1

. Given the information below: Fuel mass 240 kg Fuel density: { 0.78}kg/L The fuel volume is: -. 81.3 US GAL.. 67.7 US GAL. 307.7 US GAL. 187.2 US GA.

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. [1] 2000 ft, [2] 600 ft. [1] 1000 ft, [2] 300 m. [1] 1500 ft, [2] 900 ft.

See attachment IC-033-031) The Average True Course from A (64°N 006°E) to C (62°N 020°W) is: 259°(T). 243°(T). 275°(T). 079°(T).

The Initial Magnetic Course from C (62°N 020°W) to B (58°N 004°E) is: 113°(M). 101°(M). 089°(M). 293°(M).

The Average Magnetic Course from C (62°N 020°W) to B (58°N 004°E) is: 115°(M). 109°(M. 103°(M). 195°(M).

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.

Compass Heading 2{5}2° {parece un ocho} Variation 22°E Deviation 3°W Drift Angle 9° right The True Track is: 280. 224. 246°. 268°.

Given a heading of 220 at a TAS of 130 kt. and wind/velocity 280/30, calculate (1) drift angle and (2) ground speed. {pal lado que no tiene sentido }. (1) 13°L, (2) 118 kt. (1) 13°R, (2) 118 kt. (1) 13°L, (2) 142 kt. (1) 13°R, (2) 142 kt.

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.

Cruise Level FL95 GS {155 kt }TAS Constant Wind component Negligible OAR ISA QNH 1030 hPa Rate of Descent 500 ft/min To arrive at 2000 ft overhead the airfield, descent must commence at a distance of: 41 NM. 47 NM. 36 NM. 44 NM.

Departure elevation 1500 ft Cruise Level FL075 QNH 1023 hPa OAT ISA 1 hPa 30 ft What vertical distance do you have to climb to Cruise Level? 300 pies más por el QNH. 6300 ft. 6100 ft. 6500 ft. 7800 ft.

For a VFR routing along a mountainous region with the information given, determine obstacle clearance in the situation: Elevation of nearby airport: 8800 ft Cruising Level: FL 120 Minimum Grid-Area-Altitude: 10500 ft QNH 983 hPa Temperature: ISA-12 {10500 a 12000 = 1500+900 de QNH más un pelo por temperatura }. 2490 ft. 4490 ft. 2190 ft. 9810 ft.

Excluding RVSM, an appropriate flight level (FL) for an IFR flight in accordance with the semi-circular height rules on a Magnetic Course 180 is: {margarita }. FL100. FL90. FL85. FL115.

According GM1 CAT.OP.MPA.145 (b), the lowest MOCA to be indicated is... {1000 flat 2000 mountains aquí supongo que se refiere a montañas}. 2000 ft (600 m). 1000 ft (300 m). 500 ft (150 m). 5000 ft (450 m).

According SERA.5015, an IFR flight shall be flown at a level which is not below the minimum flight altitude, or, where no such minimum flight altitude has been established: if NOT over high terrain or in mountainous areas, at a level which is at least (1) ____ above the highest obstacle located within (2) ____ of the estimated position of the aircraft. (1) 300 m (1000 ft), (2) 8 km. (1) 600 m (2000 ft), (2) 8 km. (1) 300 m (1000 ft), (2) 5 km. 1) 600 m (2000 ft), (2) 5 km.

Given the following information, calculate the minimum flight level to be flown under IFR: MOCA: 4400 ft Magnetic course: 233(M) Elevation of nearby airport: 1500 ft Magnetic variation: 12°W Temperature: ISA-18 QNH reported at airport: 993 hPa Transition Altitude: 5000 feet. FL 60. FL 70. FL 80. FL 50.

With regard to RNAV and conventional STARs, which of the following statements is correct? 1. "RNAV STAR overlay" charts provide RNAV information to support flying a conventional STAR. 2. An "RNAV STAR" must NOT be flown with reference to conventional sources only. 1 is correct, 2 is correct. 1 is correct, 2 is incorrect. 1 is incorrect, 2 is correct. 1 is incorrect, 2 is incorrect.

With regard to RNAV and conventional SIDs, which of the following statements is correct? 1. A "RNAV STAR overlay" provides shortcuts compared to a STAR using ground-based navigational aids. 2. A "SID RNAV only" is limited to aircraft with approved RNAV equipment only. is incorrect, 2 is correct. 1 is correct, 2 is correct. 1 is correct, 2 is incorrect. 1 is incorrect, 2 is incorrect.

An approach designated as "APV Baro" or "APV SBAS" is a (1) ____ down to minima published as (2) ____. (1) 3D approach, (2) MDH or DH. (1) 2D approach, (2) LNAV/VNAV or LPV. (1) 3D approach, (2) LNAV/VNAV or LPV. (1) 2D approach, (2) LNAV or LP.

Distance 300 NM Wind (true) 340/40 Magnetic course 300° Variation 20°E TAS 440 kt {4+1} Calculate the flight time. 45 min. 37 min. 42 min. 48 min.

Given the information below: 160 Imp.GAL Fuel density: 0.81 {1} kg/L The fuel mass is: 589.2 kg. 898.0 kg. 490.6 kg. 747.7 kg.

During the pre-flight preparation, the crew decides to re-fuel an amount of 24 US gallons, fuel density is (6)lb / US gallon. This amount is equal to approximately. 65 kg. 72 kg. 144 kg. 317 kg.

Gross Mass 45000 kg Racetrack Pattern Press. Alt. 1500 ft Holding Time {30}min . The Holding Fuel is: 1090 kg. 1280 kg. 1020 kg. 2040 kg.

Power setting:{25} in.Hg (or Full throttle) @ 2500 RPM Pressure Altitude: 9000 ft OAT {-23}° C The fuel flow is: 13.25 GPH. 76.3 GPH. 12.25 GPH. 79.3 GPH.

Aeroplane mass, fuel load and Take-off altitude: as stated in the graph Power setting: Full throttle 2300 RPM (20°C LEAN of peak EGT) Headwind: 40 kt Cruising altitude: 10000 ft Determine the ground range in NM: 657 NM. 876 NM. 629 NM. 839 NM.

Mass: 62500 kg Flight Level: 350 Headwind component: {20} kt TAT: -42° C Determine fuel required for ground distance 200 NM at LRC speed: 1019 kg. 1044 kg. 510 kg. 930 kg.

A flight is planned according to the basic fuel policy procedure as stated in AMC1 CAT.OP.MPA.150(b)(a). Due to payload restrictions, planning required minimum possible Block Fuel. With the values given below, calculate the total fuel required: Trip Fuel: 3300 kg Planned Fuel Flow for Holding: 2200 kg/h Alternate no. 1 Fuel: 1200 kg Alternate no. 2 Fuel: 1600 kg Taxi Fuel: 220 kg (no Additional Fuel or Extra Fuel required) ( the lower 03). 6403 kg. 6385 kg. 6183 kg. 7603 kg.

Using the attached graph, determine the Nautical Air Miles (NAM) with the following values given: TAS 350 kt Headwind Component 40 kt Ground Distance: 440 NM { the higher 400}. 497 NAM. 395 NAM. 400 NAM. 480 NAM.

APU usage (planned) at the ramp: 30 minutes prior to taxi Taxi time at departure airport: 25 minutes Taxi time at destination airport: 20 minutes Determine the Taxi Fuel required for a Commercial Air Transport flight: 333 kg. 275 kg. 553 kg.

Operation Single Engine Aeroplane. Start and Taxi Fuel 10 lb Climb Fuel 3 min. plus 10 lb additional fuel Desecent Fuel 10 min. with no correction for the descent. Flight Time {3 h 12}min. overhead to overhead Reserve Fuel 30 % of trip fuel. Power Setting 23 in.HG (or full throttle), 2300 RPM, 20°C lean. Cruise Level FL70 OAT ISA + 20°C. The minimum Block Fuel. 325 lb. 308 lb. 352 lb. 294 lb.

Trip fuel : 1. Block position to holding point 2. Take-off to landing, including expected departure 3. End of the departure route to beginning of the arrival route, no departure and arrival 4. Climb, cruise (including any step climb) and descent 5. Arrival, approach and landing 6. Holding for 15 minutes at 1500 ft above destination aerodrome elevation (lower). 2, 4 and 5. 1, 2, 4 and 5. 1, 3, 4 and 5. 2, 4, 5 and 6.

Multi-engine Piston (MEP) Departure aerodrome elevation {3000}ft OAT -1°C To climb with Mixture Rich to FL110 with OAT ISA-10, the Fuel required is: 6 US GAL. 9 US GAL. 12 US GAL. 15 US GAL.

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: 550 kg Cruise fuel to alternate: 800 kg Descent fuel to alternate: 150 kg Fuel for approach and landing at alternate: 200 kg {Holding fuel at alternate: 900}kg Fuel for a missed approach at alternate: 150 kg. 1900 kg. 1500 kg. 2800 kg. 2950 kg.

Distance to Alternate {400}NM Landing Mass at Alternate 50000 kg Headwind 25 kt The Alternate Fuel required is: 2800 kg. 2700 kg. 2950 kg. 2550 kg.

Distance to Alternate 450 NM Landing Mass at Alternate {45000} kg Tailwind 50 kt The Alternate Fuel required is: 2500 kg. 2750 kg. 3150 kg. 2800 kg.

With regard to CAT operations and the information given below, calculate the Contingency Fuel: Trip Fuel: 2500 lb {Taxi Fuel: 120}lb Alternate Fuel: 750 lb (En-route alternate NOT available) Fuel for 5 min at 1500 ft above destination: 100 lb Reserve Fuel: 720 lb. 125 lb. 225 lb. 100 lb. 75 lb.

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.

Calculate the total fuel required for a Commercial Air Transport flight (VFR) with a multi-engined piston aircraft, rounded to the higher full GAL: Start-up / Taxi Fuel: 3 GAL Climb Fuel: 8 GAL Cruise Fuel: 24 GAL Final Reserve Fuel Flow: {12 GAL/h Alternate Fuel: 5 GAL}. 51 GAL. 48 GAL. 46 GAL. 54 GAL.

Use the following information from the operational flight plan of a Medium Range Jet Transport Aeroplane (MRJT) to calculate the minimum required Take-Off Fuel, in case the operator has nominated a suitable En-Route Alternate: Flight time: 03:15 Flight time to alternate: 00:25 Cruise fuel flow: { 2490}kg/h Holding fuel flow: 1950 kg/h. 10348 kg. 10268 kg. 9311 kg. 11323 kg.

Calculate the minimum fuel required of a jet aircraft before commencing a Commercial Air Transport flight: Taxi Fuel: 90 kg Trip Fuel: 3350 kg Fuel to alternate: {888}kg Fuel flow at 1500 feet above destination aerodrome: 1900 kg/h. 5446 kg. 5356 kg. 4558 kg. 6396 kg.

Calculate the total fuel required for a Commercial Air Transport flight in a Long-Range Jet Transport (LRJT) aeroplane, rounded to the higher full kg: Startup/Taxi Fuel: 185 kg Trip Fuel: { 48950} kg Contingency Fuel: 5% of Trip Fuel Alternate Fuel: 1880 kg Additional Fuel: 3300 kg Final Reserve Fuel: 2250 kg. 59013 kg. 58828 kg. 55713 kg. 56763 kg.

Calculate the total fuel required for a Commercial Air Transport flight with a Medium-Range Jet Transport (MRJT) aeroplane: Fuel Flow Taxi: 12 kg / min Taxi time at departure: 10 minutes Taxi time at destination: 5 minutes Trip distance: 1350 NM Cruise Fuel flow (average): 2400 kg/h Cruise TAS (average): 433 kt Wind component (average): -15 kt Contingency Fuel: use 5% of Trip Fuel Fuel flow Holding: 2200 kg/h Alternate Fuel: 650 kg. APU fuel flow: 110 kg/h Planned APU usage at the parking position: {10 min}. 10009 kg. 9359 kg. 10559 kg. 9889 kg.

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.

Max.Take-off Mass 64400 kg Max. Landing Mass 56200 kg Max. Zero Fuel Mass 53000 kg Dry Operating Mass 35500 kg Estimated Load 14500 kg Estimated Trip Fuel 4900 kg Min. Take-off Fuel 7400 kg The max. Take-Off Fuel is: una pachanga de unos. 11100 kg. 11400 kg. 14400 kg. 11200 kg.

Dry Operating Mass {33500} kg Traffic Load 10600 kg Max. Take-Off Mass 66200 kg Taxi Fuel 200 kg Tank capacity 22500 l Fuel Density 0.78 kg/l The max. Take-Off Fuel is: 17350 kg. 22300 kg. 17550 kg. 21700 kg.