These pages are a collection of the ideas and impressions of the
Cardinal pilots who frequent this site. This information is anecdotal
and informal, and may not be completely accurate.
As always, the Cessna operations and flight manual, and the advice
of a certified flight instructor, should be your primary source of
information regarding the safe operation of your aircraft.
Contents:
Where to cruise?
Low altitude cruise
Middle altitude cruise
High altitude cruise
What profile to fly?
Where (what altitude) should I expect to Cruise at?
There is much personal choice and opinion on this subject, so
we put this question before the CFO membership.
The results are as shown here:
What is the *highest* cruise altitude you use (in MSL?)
| RG |
Votes |
Approximate % |
| RG: 8,000 or less |
51 |
25% |
|
| RG: 10,000 |
74 |
36% |
|
| RG: 12,500 |
55 |
26% |
|
| RG: 14,000 |
15 |
7% |
|
| RG: 16:000 |
13 |
6% |
|
| FG |
Votes |
Approximate % |
| FG: 8,000 or less |
61 |
30% |
|
| FG: 10,000 |
71 |
35% |
|
| FG: 12,000 |
53 |
26% |
|
| FG: 14,000 |
15 |
7% |
|
| FG: 16,000 |
1 |
0% |
|
To summarize the conclusion, they are remarkably similar. I was surprised that I should clearly have added an altitude below 8,000 feet.. evidently some folks just don't climb, even on a long trip with a tailwind.
One would expect the RG to have a much higher normal cruise, but the shift seemed to be about 6%.. that is, the lower altitude was 6% lower for the RG, and that 6% translated through to show up at the top of the RG altitude.
Also note that only the RG was normally turbocharged (other than the two exceptions.) That may almost account for the 6% in our sample, which based on the comments seemed to include a number of Turbo owners.
So it appears that the average Cardinal owner would expect to use 10,000 feet as a possible cruise altitude if their trip and conditions suggested that they fly as high as possible.
So what should one expect at each cruise level, up to that maximum?
Low Altitude Cruise
Anything below about 5000 feet can be thought of as
low altitude cruise. In these altitudes you will be
using some throttle to reduce the manifold pressure
to a selected level.
Most Cardinal pilots pick a manifold pressure and
RPM combination that simply feels right for their airplane.
Usually that starts with RPM. Most Cardinals (or other
airplanes, for that matter) will have a 'sweet spot',
an RPM where the engine is simply happier.
When you get an overhaul or a prop balance this can
change. If you don't like where yours is 'sweet' it
could be worth a try.
Once the RPM is picked, just look up the power setting
you want in the operations manual and set your manifold
pressure from that. The book is pretty
accurate in the Cardinal.
The book is also pretty accurate about cruise numbers.
(Note that I refer to post-1970 books... I've heard bad
rumors and don't have personal experience with the
earlier books.)
There is a power computer available that does the same
thing, but it's results are really the same as the
tables. It's a nice tool if you are short of other
instrumentation or like such gadgets.
Most people cruise at 65% to 75% power, unless you are
trying to resolve engine compression or blowby problems.
I need to write a page on that process...
As always, the best measure of power (until someone
invents a % power gauge, as many are trying to do) is
read directly from fuel flow. If you have a direct reading
fuel flow system, once the system is leaned you can set
the power with hi accuracy from that indicator. Check out
this page for details.
Middle Altitude Cruise
Without applying too much science to this choice, I'd
call the middle altitudes those in which you are able
to run 'normal' power settings with full throttle.
I've heard, and it makes sense to me, that full throttle
operation is the most efficient. No turbulence around the
throttle plate, a smoother flow through the distribution
box under the oil pan... I try for full throttle as soon
as I can.
At this point you only have one way to set power: by
changing RPM. Higher RPM will result in higher power,
although it's not quite linear. Again the book or power
computer will help you sort out where you are.
And again, the best measure of power is
read directly from fuel flow. Check out
this page for details.
Mid altitude cruise will give you the highest airspeeds,
short of a turbocharger. Click
Here for the page on Turbo cruise.
Keep in mind that the RG fuel flow gauge is actually a
pressure gauge calibrated in Gallons Per Hour. If you
have dirty injectors or other non-standard flow, it will
not be accurate. This is not a common problem.
It has been said by some Cardinal owners that the ideal
cruise settings are full throttle and an RPM setting at
the bottom of the green. It's suggested that the lower
number of turns of the engine results in less friction
and loss.
I'm not sure that science supports that argument, but if
your engine runs smoothly at low RPM you might find some
remarkable efficiencies at those settings.
High Altitude Cruise
As you climb higher you will start to lose power, but
the fuel flow will go down as well. And your fuel efficiency
will be higher as you are flying in thinner (lower drag)
air.
Of course your prop will also be less efficient, but their
is a net gain in fuel efficiency.
For most high altitude flights, you will want full throttle
and top of the green RPM. As the power drops you may feel
better about operations lean of peak, more about that on
This page.
As an example of a high altitude flight, our trip back from
Colorado Springs to the Chicago area last summer was done
at 12,500 in our stock '76 RG. True airspeed was around
136, and the fuel flow,
lean of peak, was around 8.2 GPH. We flew home, with some
headwinds, in 6:20 and landed with 17 gallons on board.
I have detailed data from other flights, but not here. In
the future I'll add to this section with that information.
What Profile to fly?
There has been a lot of speculation about the benefits of
flying higher: is the improved efficiency worth the extra
time and fuel to climb?
People who have set out to prove this one way or the other
usually come up with a dead heat: no real benefit either
way.
My personal experience is that high altitudes are good when
you are not in a hurry an have a long way to go.
Of course the overriding influence is the wind. I usually
go for a slow cruise climb and level off every so often to
get an actual wind impact reading. When I find a peak, I
either go back to the peak or stop where I am.
There is also a difficult to quantify benefit to going just
slightly downhill for as long as possible for arrival. I
find that when I'm not staying high for smooth air, I can
gain an extra 10 knots with just a slight descent. Some
day someone will do the math to prove or disprove this as
an efficiency trick.
Copyright Keith Peterson 1999
|