Originally posted by Viking
Of course flying at high altitude in mountainous terrain demands respect. However considering the Twin-Otter has about twice the service ceiling of your H500 it has a lot more reserve power at 9000 feet than your heli. Considering the DHC-6 has a landing speed of 80 knots at sea level, at 9000 feet it would still be less than the normal landing speed of jet airliners at sea level.
I have a feeling Lukla is a good-weather only airport.
I wasn't comparing the power reserves of a H500 to the Twin-Otter... It's all relevant even the mighty Otter isn't going to have the same performance at 9,000ft the pilot taking off at sea level is going to have to make considerable calculations to allow for the higher altitude landing then if he was landing at another field at or near sea level.
Even a Harrier Jump Jet is going to suffer operating at higher altitudes for example Afghanistan. Then it would operating from a ship.
I can't remember the maths calculation (and can't be bothered to google it)but for every 1,000ft there is a performance degredation for any aircraft/helicopter. Same as for every deg increase in temp or increase in moisture content in the air. Get a very hot/humid day and you have double the problems.
It's just basic met and aircraft tech papers, even PPL theory covers it.
...-Gixer