I'm interested to know what factors are used to determine what the rate of climb will be after the wheels leave the ground.
Sometimes the aircraft seems to climb very steeply and it feels like I'm being pushed back into my seat quite a lot (almost uncomfortable).
Other times the climb into the sky is quite gentle.
Basically the initial pitch attitude is a result of the power used vs the aircraft weight. So, the more power is used in the take off, the steeper the initial climb. More power could be used for lots of reasons...short runway would be the most likely seen in Oz domestic ops.
A specific target speed is required (around V2 plus 15 to 25 knots) from lift off to clean up (when the flap retraction is started). That gets you away from the ground, with very clearly defined obstacle clearance requirements. The angles required for the obstacle clearance (and some of the statutory climb angles) will be as likely to define the maximum take off weight as the runway length. There are two techniques controlling just when the power reduction from take off to climb happens. Normally clean up starts at 1500, with the pitch being reduced to control acceleration as the flaps are retracted, and the power changed from take off to climb once clean. The second method is mandated for noise reasons (note it doesn't make any less noise, but has the different spread), and that involves power reduction at 1500 feet, and clean up at 3000.
If I had to have a stab at answering my own question I'd say steeper climbs are used when: a) Airports are close to residential areas. b) The pilot wants to spend less time flying in low winds. c) The distance to the destination airport is quite short.
Residential areas can throw up different departure procedures for noise control, though, more than anything else, that normally involves a thrust reduction at 1500' and clean up at 3000'. So, it certainly doesn't make the initial climb steeper.
Low level winds can certainly be a factor. If you have any thoughts at all about possible wind shear, then it's best to use no derate for the take off. In a 767 that will give pitch attitudes that are up around 20 degrees, and perhaps appreciably more.
Short sectors imply light fuel loads, and so lighter overall weight. There is a limit to just how much power you can derate. Aircraft like the 767 have to be able to fly on one engine, generally at much higher weights than what they are operated at on most occasions. Upshot of that, is that the big twins tend to be very powerful, and so need quite high pitch attitudes to keep the initial climb speed under control. In the the 767 the initial pitch targets is around 20 degrees, vs, 15 in the 747 and 12 in the 380.
Also, JB, will you be flying the A380 on the SYD-HKG route?
Probably, though it won't be high on my list. I prefer longer trips, that either start or finish in Melbourne...which basically means London or London.