50 minute video... is there a summary / highlights article anywhere?
What the heck does that mean?single lever operation a near certainty
Actually goes further. From what I have previously seen, FAA is considering constant speed prop as a part of a true single level control only.I guess that means constant speed props that are controlled like the cirrus with the throttle control, but not where throttle and prop are two separate controls?
OICActually goes further. From what I have previously seen, FAA is considering constant speed prop as a part of a true single level control only.
Currently most LSA are two levers, throttle and mixture. To get the constant speed prop, FAA is looking at requirements which only allow a single lever. Historically this meant FADEC.
Tim
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Variable pitch - the FADAC picks the pitch/throttle/rpm combination according to the demand from the "throttle" lever. Not really "constant speed" - more like an automatic transmission that will downshift when you thump the pedal and put you in overdrive when cruising.I guess that means constant speed props that are controlled like the cirrus with the throttle control, but not where throttle and prop are two separate controls?
Currently most LSA are two levers, throttle and mixture.
That would be an elegant, simple solution.I’m a simple guy. Align the future of LSA to the equipment and capability allowed under BasicMed today. Six place, day/night, IFR outside of Class A airspace.
That would require an act of congress. Literally.Eliminate the requirement of a medical prior to getting basic med.
Yep - you’re right.That would require an act of congress. Literally.
I’m a simple guy. Align the future of LSA to the equipment and capability allowed under BasicMed today. Six place, day/night, IFR outside of Class A airspace.
That would require an act of congress. Literally.
I. That's dogwhistle for non-retroactive line items. There goes your cost savings proposition (aka the retroactive inclusion of old fac builts). This is part 23 re-write all over again..
First post. Considering sport pilot. Not in a hurry. Sorry if this is a naive question.
If rules did change, does the above mean to imply that all existing aircraft that fit into any new rules (4 seat, <XXXX lbs GW, etc, whatever they are) would not be eligible to be flown with a sport pilot license. How exactly would that work? It would only apply to new planes that were certified to meet the new requirement?
The way it works now is that any aircraft that meets the requirements for speed / seats/ weight /etc.can be flown with a sport pilot certificate. How the airplane is/was originally certificated is totally irrelevant - that's why you can fly Cubs, Champs, E-AB, etc. with your sport ticket.If rules did change, does the above mean to imply that all existing aircraft that fit into any new rules (4 seat, <XXXX lbs GW, etc, whatever they are) would not be eligible to be flown with a sport pilot license. How exactly would that work? It would only apply to new planes that were certified to meet the new requirement?
No way will it be as simple as power to weight. We're talking FAA here.This would be a power to weight ratio? Are different ratio's easier/safer to fly? I
See the power index discussion here:
https://www.bydanjohnson.com/faas-proposed-regulation-mosaic-lamas-spring-2020-update-report/
Algebraically, that reduces to Ip = P/(3 S). So, in that equation, weight is irrelevant.Ip = {(W/S)/(W/P)}1/3, where:
W = maximum takeoff weight (MTOW) in pounds,
S = wing area in square feet,
P = maximum rated power in horsepower at sea level and standard temperature.
Do yourself a favor and go EAB as soon as you can.
Not super excited about the A in EAB. What advantage would this have over ELSA if I only had a sport pilot license?...its till has to meet LSA requirements, correct?
Looks like the power index equation has something wrong (or they are not using horsepower / square feet) with it as printed on that web page. A 182 comes out at 0.34, a DC-3 is 0.81... One heck of an LSA.it looks unlikely that this metric (power index) would be limiting in many cases.
Looks like the power index equation has something wrong (or they are not using horsepower / square feet) with it as printed on that web page. A 182 comes out at 0.34, a DC-3 is 0.81... One heck of an LSA.
But it is the FAA after all.