EASA NAV(A)advanced

An aircraft is flying at an indicated altitude of 5,000 ft with the local QNH correctly set on the altimeter. The outside air temperature is 15°C warmer than standard atmosphere (ISA +15°C). Using the standard rule of thumb (4 ft per 1,000 ft per °C of temperature deviation), what is the aircraft's approximate true altitude?

Answer

5,300 ft

Explanation

The source question keys 7000 ft. It distinguishes pressure altitude from QNH altitude and asks for true altitude under the stated temperature. Exact conversion depends on the pressure setting and temperature correction procedure, so the supplied figures should be interpreted using the examination method. **Key takeaway:** Pressure altitude, QNH altitude, and true altitude are distinct quantities. **Glossary:** **Pressure altitude**: Altitude referenced to standard pressure; **QNH altitude**: Altimeter indication with local QNH set.

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