azure said:
Why without reducing MP? I was taught to pull out the MP, prop, and mixture controls (in that order) to bring the MP, RPM, and fuel flow gauges down to top of green on climbout.
This is a topic that can spark a 'religious' debate, so I'll try to present the information simply and with as little bias as possible.
In my experience as a flight instructor, aircraft owner, and ferry pilot, most folks, through no fault of their own, are 'taught' poorly when it comes piston powerplant management. There are so many ways to move all those multicolored knobs/levers, and nearly all combinations work - they don't have any immediate noticable consequence to the pilot. Poor powerplant management is largely evident in a reduction of engine longevity and increase in mx bills in the long run. As such, renter pilots may never be aware of the cause and effect nature of their actions, i.e. when the levers/knobs are moved to the wrong positions at the wrong times. After all, they're not responsible for the maintenance and overhaul bills (and maybe some just don't care.) And CFIs may not know or care either; most don't own airplanes, and most were taught by those who came before, who might also not have actually ingested any data on the subject. But I guarantee all aircraft owners do care, and in my view owners are the ones who take it upon themselves to learn more about managing piston engines. It is surely a more complicated and technical process than managing any turboprop/shaft or turbofan engine I've ever flown.
The first caveat I have to throw into the mix, prior to going any further, is that every engine's different. What I'm advising applies to 'most' normally aspirated Continental and Lycoming engines used in typical GA airplane installations. However, there are exceptions.
The second caveat with which you must be aware is that the AFM or POH may not always directly agree with some of these 'facts.' Most engines on the market today, particularly brand A & B engines, were certified decades ago. Guidance on power settings for takeoff climb, cruise, etc. is sometimes vague and murky; other times it's directly 'wrong;' and sometimes it's about it right. That's just the way it is, and the manufacturers aren't going to reverse course after all this time and endorse new ways to operate their engines, despite test-stand evidence which clearly indicates better ways to do things. That could start a legal liability nightmare; it'll never happen.
With all that outta the way...
There's this old "oversquare" myth that's still alive today, which suggests that operating with the manifold pressure at a higher " of Hg. setting than RPM can damage the engine. I.e., don't use 28" and 2500 RPM, use "25 squared." Ugh, just the mention of it makes me feel grouchy. Almost any POH will include power settings that include "oversquare" combinations of MAP and RPM. This is the first data you should show to your CFI if he/she tells you to reduce manifold pressure on the climbout to some setting lower than fully open. (If he/she can show you an actual
limitation on METO - maximum except takeoff power - accept that.)
So we've gotten this idea that it's somehow easier on the engine to reduce MAP during initial climbout. That's actually not the case for
most naturally-aspirated engines. One of the most important tenets to understand about piston powerplant management is that internal temperatures and pressures are what's important, not necessarily the power setting. Of course, temps and pressures are largely derived from power settings, so they're important. But it's the results, not the cause, that we're most interested in.
Problem is, powering back in the climb is not good for our theoretical generic normally-aspirated engine. These powerplants are designed to run "extra rich" with wide open throttle settings. By bringing the throttle all the way forward, you allow this to occur, usually via a second fuel inlet which increases fuel flow. The reason for this is twofold; first, you provide more fuel to the engine, which via slower compression events, leads to cooler CHTs and lower internal pressures (particularly important during climbout due to the higher AOA and lower indicated airspeeds involved.) Second, and probably more importantly, you prevent detonation, the number one enemy of all engines at high power settings (for emphasis, see the Reno Air Races.)
In other words, when you bring MAP back but leave the RPMs up at 2700 during takeoff, you're taking air and fuel away from an engine thirsty for both. You're defeating the fuel-enrichening feature mentioned above, and you're increasing temps and pressures inside the engine. If you have a properly calibrated digital engine monitor, you can verify this for yourself.
Reducing RPM from 2700 to 2500RPM only costs 5-15HP in most GA engines and tremendously reduces noise. Won't do all that much for temps and pressures.
Another excellent Deakin tip is to note EGT right at takeoff and adjust mixture to keep it there during the climb. You CAN'T hurt the engine this way. So I've always taught that after rotation, pull the props back to 2500RPM at 500 feet or so, and just keep tweaking the mixtures back to match takeoff EGT. When you reach 75% power (usually around 23 or 24") and dropping you can start thinking about tweaking them back further.
So, in normally-aspirated piston airpolanes, I leave throttles fully forward all the way to cruise altitude. There's no better way to do it, in terms of engine care and longevity. Going partial power just doesn't do anything good at all for your hot little bucket of bolts trying to thrash itself apart with every stroke. Give it all the air and fuel it wants in the climb, and your repair bills will go down. For heaven's sake, the WORST thing you can do is reduce MAP AND fuel-air mixture during the initial climb. Don't do that. (This is assuming near sea-level ambient pressures and standard or higher temps. If you're taking off out of a high elevation airport, you may not be able to hurt the engine regardless of how you feed the fuel and air - below 65% power, it's mostly a matter of not running too
rich, which can foul plugs and cause some other relatively minor, nuisance related problems.)
The real question at the end of the day is, "Why do we learn to do it the wrong way?" When I first starting flying airplanes with constant speed props, I was told to reduce power to 25-25 on the climbout. No one knew why, but that's just what we did. When the size of my wallet started depending on the health of my two IO-320s, I started looking into the subject a bit more. Glad I did... these engines have been trouble-free for years with compressions in the high 70s. (Of course, the fact that they're products of Charlie Melot's shop in Zephyr Hills doesn't hurt matters either.)
-Ryan