by Heber98 » Fri Mar 07, 2003 2:22 am
450 knots is a True Airspeed (TAS) reference, not to be confused with Indicated Airspeed (IAS).
At altitude, in the 30,000's, the 747 can do 450 knots True Airspeed (similar to groundspeed), but the indicated airspeed is closer to 260 knots. That's why you have to reference your speed as Mach when you're that high, because airspeed becomes too difficult to gauge.
Basically, using indicated airspeed hold on jets is useful up to 320 knots. While climbing at 320 knots you can watch the mach reading gradually increase. The air is getting thinner and thinner so the aircraft actually moves faster and faster to hold 320 as it climbs. When the mach get's to .84 you set speed hold to M.84. The autopilot then holds your mach cruising speed, and as you continue to climb the airspeed reading will begin to drop which is a sign that the air is REALLY thin.
Last edited by
Heber98 on Fri Mar 07, 2003 2:29 am, edited 1 time in total.