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What APG offers is a OEI climb capability for a specific procedure that allows you to clear terrain IAW TERPS terrain seperation criteria vs FAA terrain seperation criteria.
When you refer to APG, are you referring to runway analysis, or some other product?
When using a runway analysis, the actual clearance over every obstacle is 35' (net path). Note, I am not referring to 35' over a gradient, but 35' over an obstacle.
Before using runway analysis numbers to takeoff, think about whether you really want to be in IMC, on a single engine, clearing obstacles by only 35'.
Also, keep in mind that the lateral boundaries when using a runway analysis "escape procedure" are significantly narrower than the lateral boundaries specified in TERPS/PANS-OPS.
When you refer to APG, are you referring to runway analysis, or some other product?
When using a runway analysis, the actual clearance over every obstacle is 35' (net path). Note, I am not referring to 35' over a gradient, but 35' over an obstacle.
Before using runway analysis numbers to takeoff, think about whether you really want to be in IMC, on a single engine, clearing obstacles by only 35'.
Also, keep in mind that the lateral boundaries when using a runway analysis "escape procedure" are significantly narrower than the lateral boundaries specified in TERPS/PANS-OPS.
APG allows you to demonstrate to the FAA that on your very worst day, you could lose an engine at V1 while still on the runway, takeoff and not hit any obstacles, albiet, clearing them only by the TERPS terrain seperation criteria. Lose an engine at 100 feet and one would suppose that your terrain clearance would continue to be 100 feet greater than the TERPS 35ft, lose it at 200 ...... on and on (based on TERPS criteria of 200ft per NM). It does not guarantee that you won't have to replace both pilots seat cushions.:blush:
Runway Analysis has absolutely nothing to do with TERPS criteria.***** They shouldn't even be mentioned in the same sentence.
*****
35 ft of terrain separation up to 1500ft.***** It has nothing to do with "per NM". In other words from the ground up, while using a runway analysis procedure at the weights specified, you will clear obstacles by 35 feet.
You're correct, a runway analysis procedure is nowhere near as safe as waiting for the weather to improve. Also interesting is that the escape procedures are never test flown; they're developed via computer software, and then released.
Also interesting is that the escape procedures are never test flown; they're developed via computer software, and then released.
Runway Analysis has absolutely nothing to do with TERPS criteria.***** They shouldn't even be mentioned in the same sentence.
*****
35 ft of terrain separation up to 1500ft.***** It has nothing to do with "per NM". In other words from the ground up, while using a runway analysis procedure at the weights specified, you will clear obstacles by 35 feet.
You're correct, a runway analysis procedure is nowhere near as safe as waiting for the weather to improve. Also interesting is that the escape procedures are never test flown; they're developed via computer software, and then released.
Seeing the obstacle, doesn't mean that you will be able to avoid it with an engine loss.
Neither does operating an aircraft having 3 or more engines, mean that you will clear those same obstacles with an engine loss either.
That's right! And therein lies the misconception that some people have about a higher ceiling and vis requirement allowing them to return VMC to the field. Try turning back at Eagle, Aspen Sun Valley etc..
Well you will if you meet the required climb gradient in a FAR25 certified jet, even if it only has two engines, and you lose one.
Didn't realize that only jets were certified to Part 25?
Well you will if you meet the required climb gradient in a FAR25 certified jet, even if it only has two engines, and you lose one.
Ohh I get it...flamebait. Good job. I guess that flying the Fokker, makes you a little sensitive to those kinda statements. Please accept my apologies.
Technically I believe that all Part 25 certified airplanes actually have turbo fan engines or turbo props. So thanks for giving me the opportunity to clear that up. I know the distiction between Jet and Turbo Jet has caused confusion here before. So when you said "jet" you actually meant "turbo fan."
Why would flying a Fokker make me sensitive?
So, couldn't a piston aircraft also be certified under Part 25 too? Nothing restricts Part 25 to turbine powered aircraft, now does it?
DC8, DC9, B707 and B727 are non Part 25 aircraft. But they are certified under the same regulations as the DC3 and Convair 240.
Well you will if you meet the required climb gradient in a FAR25 certified jet, even if it only has two engines, and you lose one.
This is getting tiresome. I hate to make any assumptions, but is English your second language? (you know - who flys a Fokker).
Please, you're doing such a great job with explaining Part 25, just who does fly a Fokker?
Oh, and to answer your question: I don't really care what piston aircraft are certified under Part 25, but I do know that not all turbine aircraft, over 12,500 lbs, were Part 25 certified.