I didn't read the entire thread so forgive me if I missed some pertinent comments, but I have a suggestion.
From a "Systematic Approach to Safety" standpoint, it's important for the pilot in command to look at takeoff performance on every flight and ensure the aircraft as loaded, the runway length and condition, and atmospheric conditions are all compatible. However, there are a few ways to accomplish this. They don't all require the pilot of a Cessna 172 to crunch the numbers down to the decimal point when departing from sea level on a dry, 9,000 ft. long runway.
In my case I took a cue from the Citation 510 (the "Mustang") AFM which provides "Takeoff Performance Simplified Criteria."
View attachment 93597
The idea here is that V1, Vr, V2, and Vse will all "work" provided the weight of the aircraft, the altitude of the airport, and length of runway fit into "the box," along with some configuration requirements, consideration of obstacle in the flight path, etc. etc. 9+ times out of 10, I can get a Citation Mustang to easily fit into this criteria. It's a nice tool.
I decided to do something like that with my Twin Comanche. I spent some time parsing performance data and came up with this table, which is on the bottom of my QRC:
View attachment 93598
You probably get the idea here pretty quickly, but since I
do fly from shorter runways, particularly here in the NE, I ran three common weights (3600 lbs = max gross, 3400, and 3200) along with temps and a headwind correction for each.
Those numbers are all for S.L. so after doing some crunching, I was able to determine that all of the runway lengths at 2000 ft. PA would be increased by less than 500 feet. So the first note in grey bar, bottom left, states "add 500 ft. to rwy" if the airport PA is 2000 ft. For 4000 ft, I need to add 1000 ft. These are conservative numbers. The actual increases are always less, sometimes substantially so. The idea is that as soon as I get "close" it's time to crack open the AFM and do the actual calculation.
The very last, bottom right field is my "catch-all" which I glance at any time I'm flying out of a runway 4500 feet or longer, which is often enough. I can prove with my performance charts that if the runway length is 4500 ft. or great, and the airport PA is 4000 ft. or less, I'll have the accelerate stop performance needed to safely depart. That's sort of an equivalent of the Citation 510 data.
No reason anyone couldn't do the same for their personal aircraft. Of course this is for a twin, so I'm looking at accelerate stop, and that wouldn't be the case for single engine airplanes.