
Never left in the dark
An example explanation
Question
The QNH is 999hPa. An aircraft is flying over terrain at an altitude of 4500ft. The OAT is minus 10°C. What is the true altitude of the aircraft (assume 1hPa = 30ft)?
- A4230ft Right answer
- B4555ft
- C4720ft
- D4900ft
Explanation
This is a straightforward true altitude question, using the altitude window on the whizz-wheel.
In the altitude window of the whizz-wheel, you'll see that the inputs are air temperature and pressure altitude.
The pressure altitude is what the altimeter would read if the pilot set a sub-scale pressure setting of 1013hPa. The aircraft is at 4500ft, but on a sub-scale setting of 999hPa.
To work out the pressure altitude, we turn the sub-scale up from 999 to 1013, an increase of 14hPa. The question says to assume 1hPa = 30ft, so the altimeter reading increases by 14 × 30ft = 420ft, from 4500ft to 4920ft. Our pressure altitude is therefore 4920ft.
The temperature is −10°C. With both pressure altitude and actual temperature, we use the whizz-wheel to convert indicated altitude to true altitude:
- In the altitude window, set −10°C against 4920ft.
- Against the actual altitude (inner scale) of 4500ft, read the true altitude of 4230ft on the outer scale.
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