g450cpt
I really can't believe...
Let's begin by examining some authoritative references.
By all means, feel free to cite your own.
FAA AIM 5-2-8:
FAA AC 120-91:
The AC is quite clear --
Thus, one-engine-inoperative obstacle clearance requirements and the all-engines-operating TERPS requirements are independent, and one- engine-inoperative procedures do not need to meet TERPS requirements.
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Without a performance engineering analysis, how would you determine the maximum allowable takeoff weight for your G450 (if that is indeed your current ride) at KLAS:
350'/nm to 11,000 MSL.
Per the AC,
"...any gradient requirement, specified or unspecified, will be treated as a plane which must not be penetrated from above until reaching the stated height, rather than as a gradient which must be exceeded at all points in the path."
If you are going to insist that it's necessary to fly the COWBY4 with OEI -- and without using a performance engineering analysis:
- How would you calculate the correct acceleration height and know with certainty that the airplane would not penetrate the plane from above?
- How would you propose to comply with time limits on takeoff thrust?