By Martin Windrow
Absolutely illustrated all through with many infrequent BW pictures all with well-informed captions, plus eight pages of color profile drawings.
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Extra info for Aircam Aviation Series №S8: Luftwaffe Colour Schemes and Markings, 1935-45 Volume 2
Figure 3-16. Coupling the FMS to navigation instruments. Awareness: Mode Awareness Mode awareness refers to the pilot’s ability to keep track of how an advanced avionics cockpit system is configured. As shown in Figure 3-16, every advanced avionics system offers an annunciation of which mode is currently set—somewhere in the cockpit! There is no guarantee that you will notice these annunciations in a timely manner. The configuration of these systems must remain part of your mode situational awareness at all times.
Higher performance piston engines usually require descent scheduling to prevent engine shock cooling. Either the engines must be cooled gradually before descent, or power must be constant and considerable in the descent to prevent excessive cooling. In such instances, a much longer deceleration and gradual engine cooling must be planned to prevent powerplant damage. Additionally, the turbulence penetration or VA speeds should be considered with respect to weather conditions to avoid high speeds in turbulent conditions, which could result in overstressing the airframe.
Another technique for calculating descents is to use the formula shown in Figure 3-29. S. Terminal Procedures on page D-1. Working through the formula for the ECA VOR crossing restriction example, 8 minutes is needed to descend 8,000 feet at the planned descent rate of 1,000 fpm. At your planned descent speed of 180 knots, you will cover 3 NM per minute. Thus, in 8 minutes, you will cover 24 NM. Once again, you must start the descent 24 NM prior to ECA to meet the crossing restriction. Coordinating Calculations with Aeronautical Charts Regardless of which method is used, it is always a good idea to locate the top-of-descent point chosen on the aeronautical chart.