rockeye1
11th Mar 2011, 02:19
Hoping to get some performance help. I searched the forums, but couldn't quite find the answer to my questions concerning twin-engine approach climb gradient performance requirements.
I fly almost exclusively off of US DoD approach plates, so I don't have the luxury of being provided a required missed approach climb gradient, an alternate, higher MDA/DH that provides a 2.5% climb path clear of obstacles, or a company provided OEI escape maneuver.
Question 1: Am I doing this math correctly? Published missed approach requires 360ft vertical climb/min for every 60kts of groundspeed. I calculate a missed approach climb gradient of approx 5.9% [(360 ft/NM)/(6076 ft/NM)].
Question 2: At my intended landing weight my flight performance manual shows my aircraft is capable of achieving a greater than 2.5%, but less than 5.9%, One Engine Inop Go-Around climb gradient. Am I overweight to initiate this approach under IMC on two engines?
Thanks!
I fly almost exclusively off of US DoD approach plates, so I don't have the luxury of being provided a required missed approach climb gradient, an alternate, higher MDA/DH that provides a 2.5% climb path clear of obstacles, or a company provided OEI escape maneuver.
Question 1: Am I doing this math correctly? Published missed approach requires 360ft vertical climb/min for every 60kts of groundspeed. I calculate a missed approach climb gradient of approx 5.9% [(360 ft/NM)/(6076 ft/NM)].
Question 2: At my intended landing weight my flight performance manual shows my aircraft is capable of achieving a greater than 2.5%, but less than 5.9%, One Engine Inop Go-Around climb gradient. Am I overweight to initiate this approach under IMC on two engines?
Thanks!