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What weight do you think the GA pitch angle is calculated for? Most likely it is the maximum landing weight or less. So what good does it do you to fly a pitch angle and power setting for an unknown weight that is almost certainly less than your takeoff weight?
I just feel that using the FD for unkown values that are "close enough" is sloppy.
The only thing close that I know of is a requirement to use a F/D or A/P on certain RNAV DP's.
Where did you see that? The only requirement is that you have your PFD/HSI set with a CDI needle (not a Map/course track) to varify any deviation. If that's what you ment then excuse me.
Where did you see that? The only requirement is that you have your PFD/HSI set with a CDI needle (not a Map/course track) to varify any deviation. If that's what you ment then excuse me.
Also depends on the airplane. Most newer aircraft, like the Challenger 300, set the TOGA pitch based (more or less) on actual aircraft weight - so it is providing useful guidance. It also adjusts the pitch based on whether or not both engines are making power.
It's another example of "every airplane is different" - fly the one you got, not the one you used to fly...
Where did you see that? The only requirement is that you have your PFD/HSI set with a CDI needle (not a Map/course track) to varify any deviation. If that's what you ment then excuse me.