Also, by setting a constant power, economy in fuel usage is achieved.Ĩ.28 Missed Approach. Control of the rate of descent is achieved by aircraft attitude negating the need for power changes thus reducing noise. So, by ensuring that the subsequent aircraft is always above the preceding aircraft there is no requirement for wake turbulence separation. Wake turbulence separation (see Chapter 16) is only applicable between approaching aircraft where the second aircraft is at the same altitude as, or within 1000 ft below, the preceding aircraft. The procedure requires the aircraft to depart from the IAF and descend at a constant rate throughout the procedure. Primarily for the avoidance of wake turbulence separation but also for economy and noise abatement, a procedure known as stabilized approach has been developed. At some point during the final segment, a fix will be specified where glide path information can be verified.Ĩ.27 Constant Approach Slope (Stabilized Approach).
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