An accurate barometer reading QFE can be used to determine altitude by obtaining the QNH from an airport's ATIS service. The difference between QNH and QFE can be used to calculate the height of the air column, using the formula h = (QNH - QFE) / ρ, where ρ is the air density. It's important to consider density variations and use empirical equations for better accuracy in atmospheric pressure calculations. The simplest equation for pressure at altitude is P = 29.92 - 0.001H, but adjustments are needed when converting units. Ultimately, knowing the QNH allows for accurate altitude readings when set on an altimeter.