Hi all,
on my last flight I had a real challenge to climp for 7000 ft (airplane was loaded by 80%). Finally I ended up with a very low climb rate and the airplane didn't "felt good" (high angle) and speed cruise speed was very low (2700 rpm --> about 100 knots). The wind was very calm (haven't noted the values, but nothing worse, just a few knots).
I decided to familiar myself with the performance sheet, but I cannot get trough it.
Questions:
- Why is density altitude increased by decreased power? e.g. Power 75 %, 2400 rpm --> max density altitude 8000; Power 59 %, 2000 rpm max density altitude 14000
- Is the shown density altitude (after calculation) the max. possible altitude I can reach in the flight?
Many thanks and KR
Itchy2