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Why do we let an ATC rule over ride aerodynamics? If the airplane needs to climb at 300 fpm why do we let the 500fpm notification rule put us in a position of high drag? ALPA should lobby to get this rule thrown out.
I don't think its a ATC rule that you have to climb at 500 fpm. The rule( As I understand it)is if you can't climb at least 500 fpm, you have to notify ATC. Right GCD?
There really is a reason the FMS displays
UNABLE CRZ ALT
Its refreshing to hear from someone who actually knows what they are talking about and not just wanting to "hear" themselves.
That's not correct...at least not on the -700. If you're too heavy for the altitude you pop in (like FL400 or 410), it'll give that message.As I understand, all that message means is that your TOC is past your TOD. I don't think it necessarily means that you can't reach your planned altitude, that's what the climb capability charts are for.
Climbing at 250 KIAS to planned cruise altitude is not a good technique, unless it is to a lower FL. Here's why.
FAR Part 25 cruise altitude requiremnts:
At such altitude that the airplane must be able to:
1. Maintain designed cruise speed at maximum cruise thrust;
2. Be able to have a 1.3G buffet margin;
3. Still have climb capability to climb at 300 FPM at max continuous thrust / climb thrust.
If you climb to a higher FL at 250 KIAS and cannot accelerate to designed cruise speed at max cruise thrust, you've screwed yourself out of that altitude. The only way you can get to cruise speed is to descend.
When you go through the higher FL's, you should be transitioning from KIAS to Mach climb, anyway.
Keeping the deck agle lower for the climb will keep your kenectic energy higher and it will also help your thrust available by keeping the engines at a lower angle. The key word is intake. If the engine's angle is steep, it doesn't have as much intake to produce thrust with.
One question though: What if the CRJ 200 is on a giant treadmill?