33.3 Fuel Planning - Operational Requirements_在线真题试卷与模拟练习_33.3 Fuel Planning

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Given the information below:

160 Imp.GAL

Fuel density: 0.81 kg/L

The fuel mass is:

Given the information below:

Fuel mass 180 kg

Fuel density: 0.80 kg/L

The fuel volume is:

Given the information below:

Fuel mass 240 kg

Fuel density: 0.78 kg/L

The fuel volume is:

In case a crew plans to pre-position fuel at the next airport to re-fill a quantity of 1200 lbs, how many of 40-Imperial gallon fuel drums have to be ordered, assuming a specific gravity of 0.78 kg/L?

If the fuel density increases due to temperature change, with all other flight conditions remain unchanged, the fuel flow of a turbine engine given in kg/h will...

At 0.8 relative fuel density the fuel flow of a turbine engine is 200 kg/h.

With all other in-flight conditions constant, at 0.75 density the fuel flow will be:

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:

(See attachment IC-033-046)

Gross Mass 45000 kg

Racetrack Pattern Press. Alt. 1500 ft

Holding Time 30 min.

The Holding Fuel is:

（含图）

(See attachment IC-033-097 or CAP697 Table 2.2.1)

Power setting: 25 in.Hg (or Full throttle) @ 2500 RPM

Pressure Altitude: 9000 ft

OAT -23° C

The fuel flow is:

（含图）

(See attachment IC-033-098 or CAP697 Figure 2.4)

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:

（含图）

(See attachment IC-033-098 or CAP697 Figure 2.4)

Aeroplane mass, fuel load and Take-off altitude: as stated in the graph

Power setting: Full throttle 2500 RPM (20°C LEAN of peak EGT)

Headwind: 30 kt

Cruising altitude: 8000 ft

Determine the air range in NAM:

（含图）

At a checkpoint on a VFR flight, the remaining usable fuel is 60 US gal.

Reserve fuel 12 US gal. Flight time remaining 1 h 35 min.

To complete the trip, the max. consumption in US gal/h is...

(See attachment IC-033-099)

Mass: 52500 kg

Flight Level: 340

Headwind component: 40 kt

TAT: -42° C

Determine fuel required for ground distance 100 NM at LRC speed:

（含图）

(See attachment IC-033-099)

Mass: 62500 kg

Flight Level: 350

Headwind component: 20 kt

TAT: -42° C

Determine fuel required for ground distance 200 NM at LRC speed:

（含图）

Given the following values:

Ground distance: 360 NM

TAS 240 kt

Average Tailwind component: 40 kt

Average Fuel Flow: 3300 kg/h

Calculate the Trip Fuel:

Given the following values:

Ground distance: 240 NM

TAS 220 kt

Average Tailwind component: 30 kt

Average Fuel Flow: 2200 kg/h

Calculate the Trip Fuel:

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)

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: 2400 kg

Planned Fuel Flow for Holding: 1800 kg/h

Alternate no. 1 Fuel: 1200 kg

Alternate no. 2 Fuel: 1400 kg

Taxi Fuel: 200 kg

(no Additional Fuel or Extra Fuel required)

Trip fuel 3800 kg

Contingency fuel 230 kg

Alternate fuel 1200 kg

Final reserve fuel 1300 kg

The Minimum Fuel at destination is:

A piston-engined aircraft arrives at the destination airport and performs one single-engine approach with go-around, and is then required to proceed to the alternate aerodrome.

Calculated Trip Fuel: 440 liters

Alternate Fuel: 120 liters

Fuel Flow cruise: 90 liters/hour

Fuel Flow holding: 60 liters/hour

Fuel for single-engine approach and go-around: 20 liters

The minimum fuel required (1) at the destination and (2) at the alternate is:

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