Source material for takeoff performance:
1) weather briefing
2) chapter 5 of the POH
3) chart supplement
Pressure altitude calculation:
(29.92 - Current altimeter setting) * 1000 + field elevation
Density altitude calculation
(120 * temp deviation from standard) + PA
criteria for runway slope to be listed in chart supplement
-The runway has an faa instrument approach procedure
- The slope is 0.3 percent or greater
Runway gradient impact on runway length
rule of thumb: for every 1%: 10% effective change in runway length
When is wake turbulence from wing-tip vortexes the greatest?
When the aircraft is:
-heavy
-clean (flaps up)
-slow