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Engine out practice



 
 
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  #91  
Old October 16th 07, 04:45 AM posted to rec.aviation.piloting,rec.aviation.homebuilt
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Posts: 1,130
Default Engine out practice

On Oct 15, 8:49 am, Bertie the Bunyip wrote:

The examiner wouldn't allow him to slip because he reckons they are
dangerous with the flaps out and that he should wiggle the ailerons back
and forth to lose height. He didn't even want him to slip clean.

Jesus wept.

This examiner had had a fright in a 172 (this was an archer anyway) and
did not alow anyone to slip with flaps out.
While I am firmly in the camp that says some cessnas can get a litle
fuzzy in pitch with full flaps, this is just stupidity incarnate.


Shoot. We do slips with full flaps all the time in 172s, have
done so for years, and never had a scare. I wonder if that "Avoid
Slips With Flaps Extended" applied to some earlier models? I'll have
to check the TCDS sometime.

Dan

  #92  
Old October 16th 07, 06:19 AM posted to rec.aviation.piloting,rec.aviation.homebuilt
Steve Hix
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Posts: 340
Default Engine out practice

In article .com,
wrote:

On Oct 15, 8:49 am, Bertie the Bunyip wrote:

The examiner wouldn't allow him to slip because he reckons they are
dangerous with the flaps out and that he should wiggle the ailerons back
and forth to lose height. He didn't even want him to slip clean.

Jesus wept.

This examiner had had a fright in a 172 (this was an archer anyway) and
did not alow anyone to slip with flaps out.
While I am firmly in the camp that says some cessnas can get a litle
fuzzy in pitch with full flaps, this is just stupidity incarnate.


Shoot. We do slips with full flaps all the time in 172s, have
done so for years, and never had a scare. I wonder if that "Avoid
Slips With Flaps Extended" applied to some earlier models? I'll have
to check the TCDS sometime.


It affected at least some 172s.

Back when dinosaurs still roamed the taxiways...well, around 1971, a
couple of the instructors who worked for the FBO for which I was a very
lowly minion were wondering why the sole 172 was placarded against slips
with full flaps. (We operated mostly Pipers, various Cherokees and a
Navajo, and this one slightly elderly 172, I don't recall which year it
was.)

So they went out one morning, got plenty of cushion between themselves
and the ground, set the 172 into a landing configuration with full
flaps, and slipped it.

It shook a bit and then went inverted on them. They recovered and came
back home.

It may have only done that in some specific CG configurations, but they
were satisfied, and didn't wonder any longer.

Didn't do it again, either.
  #93  
Old October 16th 07, 07:43 AM posted to rec.aviation.piloting,rec.aviation.homebuilt
Bertie the Bunyip[_19_]
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Posts: 3,851
Default Engine out practice

wrote in news:1192492570.300275.289550
@i38g2000prf.googlegroups.com:

On Oct 15, 8:49 am, Bertie the Bunyip wrote:

The examiner wouldn't allow him to slip because he reckons they are
dangerous with the flaps out and that he should wiggle the ailerons back
and forth to lose height. He didn't even want him to slip clean.

Jesus wept.

This examiner had had a fright in a 172 (this was an archer anyway) and
did not alow anyone to slip with flaps out.
While I am firmly in the camp that says some cessnas can get a litle
fuzzy in pitch with full flaps, this is just stupidity incarnate.


Shoot. We do slips with full flaps all the time in 172s, have
done so for years, and never had a scare. I wonder if that "Avoid
Slips With Flaps Extended" applied to some earlier models? I'll have
to check the TCDS sometime.

Dan



Dunno. the manual in a 172 makes reference to a possibility of degraded
elevator control, but I think it's only a bit of a nod, really.
The Bird dog suffers from this ailment big time, though. it has,
essentially, the 172's wing, but the flaps go to 60 degrees. I can tell you
first hand that blanking of both the rudder and elevator are a very real
characteristic of that airplane if you slip it ith full flaps. I did it
once close to the ground and never even thought about it again..
  #94  
Old October 16th 07, 07:46 AM posted to rec.aviation.piloting,rec.aviation.homebuilt
Bertie the Bunyip[_19_]
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Posts: 3,851
Default Engine out practice

Ernest Christley wrote in news:47142123$0$32479
:

Bertie the Bunyip wrote:

It's the same either way. Cooling and heating are two sides of th
esame coin. It takes time to disapate heat and it's not so much the
passage of heat from one area to another (or the disappation, it's
irrelevant) but the speed at which the cooling or heating is taking
place and thus the gradient across the material.
In short, you take a frozen lump of metal and apply a torch to one
side you have a problem.
Take a cherry red pice of metal and put some ice on side and you have
the same problem (more or less, and disregading crystalisation)
It is the same if the same delta T is present, but my point is that it
is easier to heat something quickly than cool it quickly. Even at 250
C, you are only 523 degrees above absolute zero. So, this the
absolute largest delta T you can induce for cooling, and it is very
hard to get absolute zero, so you are more likely to have a cool temp
closer to 0 C yielding a delta T of only 250 degrees.

On the hot side things are more open-ended. It isn't too hard to get
450 C exhaust gas temperatures. For an engine that is started at say
20 C ambient temperature, you now have a delta T of 430 degrees which
is much greater than the 250 likely on the cooling side of the cycle.


With the heating, you only have the few hundred CFM of air passing
through the engine to heat it. With the cooling, you have all of the
great outdoors to do the trick. To tie it into your anology, you have a
butane lighter to heat the metal, and the Atlantic Ocean to cool it.


Kind of besides th point. you coudl say the same thing about an oxy
acetylene setup and we all know what that will do to a bit of metal.


Bertie
  #95  
Old October 16th 07, 07:47 AM posted to rec.aviation.piloting
Bertie the Bunyip[_19_]
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Posts: 3,851
Default Engine out practice

"Morgans" wrote in news:LdUQi.347$SQ2.280
@newsfe12.lga:


"Bertie the Bunyip" wrote

Seriously, though, they will increase engine life considerably.


'Specially for the guy that is only flying his plane 50 or 100 hours per
year.


Yes, absolutely.

Bertie
  #96  
Old October 16th 07, 02:52 PM posted to rec.aviation.piloting,rec.aviation.homebuilt
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Posts: 1,130
Default Engine out practice

On Oct 16, 12:43 am, Bertie the Bunyip wrote:
wrote in news:1192492570.300275.289550
@i38g2000prf.googlegroups.com:



On Oct 15, 8:49 am, Bertie the Bunyip wrote:


The examiner wouldn't allow him to slip because he reckons they are
dangerous with the flaps out and that he should wiggle the ailerons back
and forth to lose height. He didn't even want him to slip clean.


Jesus wept.


This examiner had had a fright in a 172 (this was an archer anyway) and
did not alow anyone to slip with flaps out.
While I am firmly in the camp that says some cessnas can get a litle
fuzzy in pitch with full flaps, this is just stupidity incarnate.


Shoot. We do slips with full flaps all the time in 172s, have
done so for years, and never had a scare. I wonder if that "Avoid
Slips With Flaps Extended" applied to some earlier models? I'll have
to check the TCDS sometime.


Dan


Dunno. the manual in a 172 makes reference to a possibility of degraded
elevator control, but I think it's only a bit of a nod, really.
The Bird dog suffers from this ailment big time, though. it has,
essentially, the 172's wing, but the flaps go to 60 degrees. I can tell you
first hand that blanking of both the rudder and elevator are a very real
characteristic of that airplane if you slip it ith full flaps. I did it
once close to the ground and never even thought about it again..


Here's what the Type Certificate Data Sheet says:
.................................................. ...................................

D. On flap handle, Models 172 through 172E

(1) "Flaps - Pull to extend
Takeoff Retract 0°
1st notch 10°
Landing 0° - 40°

(2) "Avoid slips with flaps down."

E. Near flap indicator Models 172F (electric flaps) through 17271034,
excluding 17270050)

"Avoid slips with flaps extended."
.................................................. .........................................

The applicable models, 172 through 172F, were built between
1956 and 1964 ('65 model?). There's no mention of the slip with flaps
thing for later models. I wonder if the addition of the back window
changed the airflow enough to keep the elevator flying?

Dan

  #97  
Old October 16th 07, 04:06 PM posted to rec.aviation.piloting,rec.aviation.homebuilt
Bertie the Bunyip[_19_]
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Posts: 3,851
Default Slips with Flaps, was: Engine out practice

Souns about right. The Bird dog's reaction was anything but mild, but with
60 degrees of flap it's not surprising really. Teh 172 this DE claims to
have had problems with was a relatively late one, but I could have been
anything that caused it. Some turbulence or maybe his mimagination coupled
with the horrow stories about it.
  #98  
Old October 16th 07, 06:25 PM posted to rec.aviation.piloting,rec.aviation.homebuilt
Scott[_1_]
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Posts: 367
Default Slips with Flaps, was: Engine out practice

Seems if one must use full flaps AND slip in landing, I would say the
approach was an abortion that lived. I prefer slips to flaps as you can
instantly remove a slip but the same can't be said for flaps...

Just MY personal opinion...not trying to slam anybody.

Scott


Bob Moore wrote:
Bertie the Bunyip wrote

This examiner had had a fright in a 172 and
did not alow anyone to slip with flaps out.
While I am firmly in the camp that says some
cessnas can get a litle fuzzy in pitch with
full flaps, this is just stupidity incarnate.



About once-a-year I post the following excerpt from "Cessna, Wings for
the World", a book by William D. Thompson.

Bill Thompson is an Aeronautical engineer from Purdue University and
worked for Cessna Aircraft Company for 28 years as an engineering test
pilot and later as the Manager of Flight Test & Aerodynamics.

-------------------------------------------------------------------
"With the advent of the large slotted flaps in the C-170, C-180, and C-
172 we encountered a nose down pitch in forward slips with the wing
flaps deflected. In some cases it was severe enough to lift the pilot
against his seat belt if he was slow in checking the motion. For this
reason a caution note was placed in most of the owner's manuals under
"Landings" reading "Slips should be avoided with flap settings greater
than 30° due to a downward pitch encountered under certain combinations
of airspeed, side-slip angle, and center of gravity loadings". Since
wing-low drift correction in cross-wind landings is normally performed
with a minimum flap setting (for better rudder control) this limitation
did not apply to that maneuver. The cause of the pitching motion is the
transition of a strong wing downwash over the tail in straight flight to
a lessened downwash angle over part of the horizontal tail caused by the
influence of a relative "upwash increment" from the upturned aileron in
slipping flight. Although not stated in the owner's manuals, we
privately encouraged flight instructors to explore these effects at high
altitude, and to pass on the information to their students. This
phenomenon was elusive and sometimes hard to duplicate, but it was
thought that a pilot should be aware of its existence and know how to
counter-act it if it occurs close to the ground.
When the larger dorsal fin was adopted in the 1972 C-172L, this side-
slip pitch phenomenon was eliminated, but the cautionary placard was
retained. In the higher-powered C-172P and C-R172 the placard was
applicable to a mild pitch "pumping" motion resulting from flap
outboard-end vortex impingement on the horizontal tail at some
combinations of side-slip angle, power, and airspeed."
--------------------------------------------------------------------
1959 C-172
Notice that this prohibition appears in Section III, Operating Details
of the C-172Owner's Manual and NOT in Section IV, Operating Limitations.
It is NOT an FAA limitation. Sounds more like "Lawyer" talk to me.

"LANDING
Normal landings are made power off with any flap setting. Slips are
prohibited in full flap approaches because of a downward pitch
encountered under certain combinations of airspeed and sideslip angle."
---------------------------------------------------------------------

I wear my "Slips with Flaps" T-Shirt proudly!

Bob Moore
12 years instructing in Skyhawks


--
Scott
http://corbenflyer.tripod.com/
Gotta Fly or Gonna Die
Building RV-4 (Super Slow Build Version)
  #99  
Old October 16th 07, 07:52 PM posted to rec.aviation.piloting,rec.aviation.homebuilt
[email protected]
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Posts: 1,130
Default Engine out practice

On Oct 16, 7:52 am, wrote:
On Oct 16, 12:43 am, Bertie the Bunyip wrote:



wrote in news:1192492570.300275.289550
@i38g2000prf.googlegroups.com:


On Oct 15, 8:49 am, Bertie the Bunyip wrote:


The examiner wouldn't allow him to slip because he reckons they are
dangerous with the flaps out and that he should wiggle the ailerons back
and forth to lose height. He didn't even want him to slip clean.


Jesus wept.


This examiner had had a fright in a 172 (this was an archer anyway) and
did not alow anyone to slip with flaps out.
While I am firmly in the camp that says some cessnas can get a litle
fuzzy in pitch with full flaps, this is just stupidity incarnate.


Shoot. We do slips with full flaps all the time in 172s, have
done so for years, and never had a scare. I wonder if that "Avoid
Slips With Flaps Extended" applied to some earlier models? I'll have
to check the TCDS sometime.


Dan


Dunno. the manual in a 172 makes reference to a possibility of degraded
elevator control, but I think it's only a bit of a nod, really.
The Bird dog suffers from this ailment big time, though. it has,
essentially, the 172's wing, but the flaps go to 60 degrees. I can tell you
first hand that blanking of both the rudder and elevator are a very real
characteristic of that airplane if you slip it ith full flaps. I did it
once close to the ground and never even thought about it again..


Here's what the Type Certificate Data Sheet says:
.................................................. ..................................

D. On flap handle, Models 172 through 172E

(1) "Flaps - Pull to extend
Takeoff Retract 0°
1st notch 10°
Landing 0° - 40°

(2) "Avoid slips with flaps down."

E. Near flap indicator Models 172F (electric flaps) through 17271034,
excluding 17270050)

"Avoid slips with flaps extended."
.................................................. ........................................

The applicable models, 172 through 172F, were built between
1956 and 1964 ('65 model?). There's no mention of the slip with flaps
thing for later models. I wonder if the addition of the back window
changed the airflow enough to keep the elevator flying?

Dan


Wait a minute. I just noticed something, and it's not clear
from the way Cessna put it on the TCDS. It says under "E" that the
avoid slips thing applies to the 172F through 17271034. That serial
number is the end of the 1978 172 N production, so the warning applies
to a lot more that I though it did. I hope nobody's gone out and hurt
themselves, now.
But we still slip with full flaps.

Dan

  #100  
Old October 16th 07, 07:58 PM posted to rec.aviation.piloting,rec.aviation.homebuilt
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Posts: 1,130
Default Slips with Flaps, was: Engine out practice

On Oct 16, 11:25 am, Scott wrote:
Seems if one must use full flaps AND slip in landing, I would say the
approach was an abortion that lived. I prefer slips to flaps as you can
instantly remove a slip but the same can't be said for flaps...

Just MY personal opinion...not trying to slam anybody.


Need to know how to do it for forced approaches. The stress
of an actual failure (I've had two) will make things difficult enough,
and slipping with flap might be the only way to get down soon enough
in the only field available.
I miss manual flaps. They were handy. You could dump them
right at touchdown and get weight on the mains for braking. Electric
flaps are so slow that they are passing through 20°, the max-lift/min
drag position, just when you want to brake, so it's better to leave
them alone. My old Auster had huge Zap flaps that lowered the stall by
a wide margin, and dumping them right at a minimum-speed touchdown
allowed full braking and stopping in unbelievably short spaces.

Dan

 




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