MauleSkinner
Well-known member
- Joined
- Sep 4, 2005
- Posts
- 638
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For Small, non-transport 135 aircraft, (King Air 90, 200, Baron, etc), do you have to have single-engine climb gradient performance?
Don't confuse certification rules with operational rules...there are a LOT of things that aren't required for certification that ARE required under various operational regulations.It has nothing to do with whether you're Part 135 or not. A Part 23 aircraft is not required to show SE climb performance.
Don't confuse certification rules with operational rules...there are a LOT of things that aren't required for certification that ARE required under various operational regulations.
Again, don't confuse issues...just because it's "not required for certification" doesn't mean that it "can't". Some can, some can't...you just can't use the ones that can't for that particular operation if it's required.Absolutely right, but one would think that an aircraft that can't do something won't magically become capable of that something due only to the type of operation.
Check out my OpSpecs post above.In other words, are you saying that there is a gradient requirement for Part 23 aircraft when operating under 135? I'm not saying there isn't, only that I don't see it in the FARs. Can you point me to the pertinent reg?
Again, don't confuse issues...just because it's "not required for certification" doesn't mean that it "can't". Some can, some can't...you just can't use the ones that can't for that particular operation if it's required.
Check out my OpSpecs post above.
Fly safe!
David
Check out Appendix A to part 135
119.7 mandates OpSpecs.Yes, I understand about Ops Specs. My question is, is there anything in the FARs that mandates a Part 23 aircraft to demonstrate SE climb performance while under 135 and, if there is, can you point me to it?
Much obliged.
Granted, it's not a regulation specifically requiring engine-out performance, but effectively it does.For takeoffs when the RVR is less than touchdown zone RVR and rollout RVR authorized in subparagraph b(2) (if selected), each airplane used must be operated at a takeoff weight which permits the airplane to achieve the performance equivalent to the takeoff performance specified in 14CFR section 135.367 for reciprocating power airplanes...