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Assess your knowledge: Correct Answers

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1/10 - By applying Continuous Descent Approach, a single-aisle aircraft such as the A320 or B737 will save between:
❌ 10-30 kg of fuel per flight ✅ 30-70 kg of fuel per flight ❌ 70-100 kg of fuel per flight
 
By applying the Continuous Descent Approach, a single-aisle aircraft such as the A320 or B737 will save between 30 and 70 kg of fuel per flight. For larger aircraft, the benefit can exceed 250 kg.
 
As an example, let’s take an airline operating a fleet of only 20 single-aisle aircraft flying 6 flights a day: since a Continuous Descent Approach allows to save around 50 kg per flight, this will result in more than 2 million kg of fuel saved per year (or more than 700,000 gallons), which represent a significant cost.

>> Learn more about CDA

 

2/10 - Engine-Out Taxi-In is only applicable when taxi-in duration is longer than:
✅ Engine cool-down time ❌ Engine warm-down time
 
To preserve engine life, it is very important to respect the engine cool-down time prescribed by the manufacturer before shutting down an engine.
 
As a consequence, Engine-Out Taxi-In is only applicable when taxi-in duration is longer than engine cool-down time.

>> Learn more about EOTI

3/10: What is "Direct"?
❌The impossibility of flying a specific route. ✅ A shortcut between two waypoints of the flight plan. ❌ A limitation between two waypoints.
 

A direct is a shortcut between two waypoints of the flight plan. For example, on the image below, the standard routing would be to follow the flight plan’s different waypoints, but a direct can be flown from waypoint RAVIA to waypoint TAHAR. By taking this direct route, the aircraft saves time and fuel.


Direct-shema-1

 

 

>> Learn more about Direct

4/10: Compared to Full reverse thrust, Idle Reverse Thrust is better to:
✅Save fuel  ✅Reduce noise ✅ Enhance passenger comfort ❌ Save brakes
 

 


5/10: On average, how much fuel can a single-aisle aircraft save per flight by using reduced-flap landings?
❌ 3–5 kg ✅ 7–10 kg ❌ 15-20 kg ❌ 25 kg
 

A single-aisle aircraft such as the A320 or B737 can save between 7 to 10 kg of fuel per flight by applying this best practice. 
For larger aircraft, the benefits can exceed 25 kg per flight. 

>> Learn more about Reduced Landing Flaps

6/10: What is the main reason to use the minimal thrust required at takeoff?
❌ To achieve a faster takeoff speed.  ❌To reduce the overall weight of the aircraft. ✅ To extend the engine's operational lifespan and decrease maintenance costs.
 

One of the main reasons to use the minimal thrust required at takeoff is to reduce maintenance costs. Regular reduced thrust takeoff applications yield significant cost savings for an airline.

By decreasing internal engine temperatures and the exhaust gas temperature (EGT) at takeoff, it reduces engine wear resulting in a longer engine on-wing life. Most engine wear will occur at the highest temperatures, and a 1% reduction from full take-off thrust will result in a 10% saving in engine life, as the last few degrees are the most damaging. Therefore, less maintenance is required as the engine may achieve more flight cycles between two maintenance actions.

The cost savings depend on the engine type and several other factors, like labor cost and engine age. However, according to the IATA, using reduced thrust instead of full thrust during takeoff saves about 150 US$ per engine and per takeoff.

>> Learn more about Reduced Thrust Takeoff

7/10: What is the estimated fuel consumption rate of a Ground Power Unit (GPU) provided by an airport?
❌ Less than 10 kg/hour ✅ Less than 20 kg/hour ❌ About 50 kg/hour ❌ Similar to the APU
 

According to United Continental, APU uses 150 to 400+ kg of fuel per hour, while Ground Power Units (GPU) provided by the airport use less than 20 kg of fuel per hour.

>> Learn more about APU

8/10: What does RAAL (Reduced Acceleration Altitude) aim to improve during climb?
❌ Engine temperature
❌ Cabin pressure  ✅Drag and aerodynamic efficiency ❌ Passenger comfort
 

When the acceleration starts at this lower height, the plane can switch to the efficient flight mode more quickly and reduce drag. This means it faces less resistance from the air, making it more efficient. In most cases, the altitude is reduced from 3000ft to 800ft. For lighter aircraft, it can go down to 400ft.

>> Learn more about Reduced Acceleration Altitude

9/10: Accelerating at 800 ft altitude during climb corresponds to which noise abatement procedure?
❌ NADP1 ✅ NADP2
 Reduce Acceleration Altitude (NADP 1 vs NADP 2)
In red, the usual NADP1 procedure, where the aircraft accelerates at 3000ft
In green, the perfect application of Reduced Acceleration Altitude, where the aircraft accelerates at 800ft. It is equivalent to NADP2 procedure.

 


>> Learn more about Reduced Acceleration Altitude

10/10: Carrying unused extra fuel increases total fuel burn due to added weight. A good rule of thumb is that the cost of carrying fuel is approximately ......... of its weight per flight hour, which can significantly add up over long flights.
❌ 1.5%
❌ 2.0%  ✅3.5% ❌ 5%
 

The unused extra fuel, which remains at landing, had to be carried during the whole flight and increased the fuel consumption by increasing the aircraft's weight. To compute the impact of carrying this fuel, you must multiply the unused aircraft fuel by the cost of weight (CoW) or cost of carrying the fuel.

A good rule of thumb for computing the cost of weight is to consider that it represents about 3.5% of the flight hours.

For example, 1Tone of extra fuel remaining after a flight of 3 hours will have cost 105kg of additional fuel to carry  to destination.

>> Learn more about Pilot Extra Fuel

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