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A Note About Moding G's instead of Weight
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Gig Giacona



Joined: 10 Jan 2006
Posts: 1416
Location: El Dorado Arkansas USA

PostPosted: Fri Jul 10, 2009 12:48 pm    Post subject: A Note About Moding G's instead of Weight Reply with quote

The following was written by Andy Elliot and posted on the Zenith Aircraft Builder's & Flyer's forum. Since he doesn't post to this list any more he gave me permission to post this here.

Planes obey the laws of physics like nearly everything else. It is not just the weight of the plane that produces flight loads, it is the weight x G loading. So if the plane's design somehow suddenly became weaker (which seems illogical), and now is limited to +4 G's at 1255#, you could still safely fly it at 1320# if you limit yourself to just +3.8 G's. Not so bad, eh?

In fact, I certified my 601XL (non-LSA) to 1450# max gross weight, but at reduced G limits of +3.6, -1.6. Not much of a restriction in my book, and I tested the gear (Grove) at the higher weight during Phase 1 and found it acceptable. A PDF copy of the flight load limit diagram that appears in my POH is attached.

For reference, I am also attaching the CG most forward and max aft limit pages from my POH, which show how the CG range also changes at various weights. You should have, or will be, required by your DAR to produce similar diagrams for your plane for certification.

As for the 140 MIAS VNE change, well if that effects you directly, Congratulations!

The net result is that if you fly the plane within its limits, either old or "temporarily recommended" you still have a highly useful machine.

Andy Elliott
N601GE/ TD / Corvair


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PostPosted: Fri Jul 10, 2009 1:09 pm    Post subject: A Note About Moding G's instead of Weight Reply with quote

On Fri, Jul 10, 2009 at 1:48 PM, Gig Giacona<wrgiacona(at)gmail.com> wrote:
Quote:
Planes obey the laws of physics like nearly everything else. It is not just the
weight of the plane that produces flight loads, it is the weight x G loading.

Yes, but gusts and turbulence may impose a G loading on your aircraft
that is independent of your control inputs. For example, would you
also not need to reduce your Va?

Ihab

ps "Nearly" everything? *Nearly*? Hmmm.... Smile

--
Ihab A.B. Awad, Palo Alto, CA


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PostPosted: Fri Jul 10, 2009 1:37 pm    Post subject: A Note About Moding G's instead of Weight Reply with quote

Things which do not obey the laws of physics:

- Wile E. Coyote
- my bank account
- nearly everything in Sci-Fi movies

-- Craig

Do not archive

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jetboy



Joined: 22 Jul 2006
Posts: 233

PostPosted: Fri Jul 10, 2009 1:47 pm    Post subject: Re: A Note About Moding G's instead of Weight Reply with quote

I asked Andy about changing limit speeds and he agreed there should be a reduction to Va
Actually this subject is more complicated dependent on which category of operation the aircraft is registered for.

In New Zealand CH601, HD and XL and CH701 are only eligible to be registered as a microlight if they comply with the design rules of Canadian Advanced Ultralight spec. TC10141E (now DS10141E) or the British BCAR-S which is a more stringent rule. Both these design rules require flutter testing which it seems the LSA (ASTM) does not.
These aircraft cannot be modified without designer approval and must continue to comply with the design rules subsequent to any modification.
The DS10141E spec includes a clause requiring design limit load of not less than 4G. I have no idea what the ASTM allows for LSA because that information is not publicly available.
Therefore if you were to operate over the design gross there would need a restriction on the various limit airspeeds Vfe, Vc, Va, Vne ?
Most countries would only allow operations above design gross wt. if the aircraft was being operated in Experimental category and the test pilot had proved it safe.
Ralph


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PostPosted: Fri Jul 10, 2009 2:43 pm    Post subject: A Note About Moding G's instead of Weight Reply with quote

Hi Ralph,

Oddly, it has been common practice in my flying experience to nearly
always fly some planes over the MTOW. I don't know the formal
treatment of this question, but the informal treatment I have heard
from several instructors suggests the FAA's version of MTOW is
ultra-conservative and should only be considered a serious limit at
high density altitudes.

The prime example of this issue is the Cessna 150. Many of us
learned to fly with dual instruction in this humble plane. When it
carries two adult males it is almost certainly a couple of hundred
pounds over gross weight. It still flies just fine, but the climb
rate is very low. Even solo with a teenager at the controls the
climb rate on this fine old plane is not very impressive.

Historically, I have always considered CG to be a much more important
specification than gross weight. Of course this thinking only works
if you fly the plane gently. (On the other hand, all the aerobatic
maneuvers I learned were done with two adults in a C-152 . . .).

I don't know about Vne, Va or other performance limits. From my
point of view these only come into play when you fly the plane in
very harsh conditions or with a very heavy hand on the stick or throttle.

Paul
XL grounded
At 02:47 PM 7/10/2009, you wrote:
Quote:
Most countries would only allow operations above design gross wt. if
the aircraft was being operated in Experimental category and the
test pilot had proved it safe.
Ralph


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Juan Vega Jr



Joined: 13 Jan 2009
Posts: 157

PostPosted: Fri Jul 10, 2009 2:54 pm    Post subject: A Note About Moding G's instead of Weight Reply with quote

Paul,
Ignoring MTOW is playing Russian roullette. PLay at your own peril.
Juan

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PostPosted: Fri Jul 10, 2009 3:06 pm    Post subject: A Note About Moding G's instead of Weight Reply with quote

OK, Juan. I'll bite.

What outcome would you expect from flying over gross weight?

We all know it will reduce the climb rate. We also know that Va
increases with increased weight. This would seem to suggest that
structure failures are less likely with excess weight rather than
more likely (the plane is more likely to stall than sustain high G's).

So, what is the big problem with excess weight?

Paul
do not archive

At 03:52 PM 7/10/2009, you wrote:
Quote:
Paul,
Ignoring MTOW is playing Russian roullette. PLay at your own peril.
Juan


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PostPosted: Fri Jul 10, 2009 3:25 pm    Post subject: A Note About Moding G's instead of Weight Reply with quote

My Zenith is an" EXPERIMENTAL".. I can make my MTOW 10,000  lbs if I want.
do not archive.
Ben Haas
N801BH
www.haaspowerair.com

--------


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Juan Vega Jr



Joined: 13 Jan 2009
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PostPosted: Sat Jul 11, 2009 5:39 am    Post subject: A Note About Moding G's instead of Weight Reply with quote

Paul,
your shitting me right?
Juan

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Juan Vega Jr



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Posts: 157

PostPosted: Sat Jul 11, 2009 6:09 am    Post subject: A Note About Moding G's instead of Weight Reply with quote

Ladies,

I am headed to Wickee Wachee SPrings with the Kids, in the Mean Time, chew on this piece from a n article from Mr. McGee. It starts on the basics of Overweight issues on a lite wing loaded aircraft. Very Basic info but to the point.
ASk your self the questions after you read it,"do I want to deal with an over maxed aircraft, and do I have the hours flown to understand how the plane will behave at manuvering speeds at over gross" "WHat is my new stall speeds?".
As quoted from an article by Art Mcgee;

Aside from building a light plane, there is another option to achieve a reasonable useful load. Under the FAA's Amateur Built Experimental aircraft guidelines, the manufacturer (the builder) sets the gross weight of the aircraft. With this flexibility you can increase the maximum gross weight to more than 800lbs. Although the builder can assign any weight he feels appropriate, when doing so he should keep in mind the original design load and the G load factor used to determine the designed gross weight.

As you increase your gross weight, you must decrease the G rating of the aircraft to keep from going over the design load of the aircraft. With this in mind, let's go back to the information provided earlier about G rating, gross weight and design load.

If you are willing to reduce your G ratings and use more precautions in rough conditions, then you can increase your gross weight. Let's look back to the example airplane. The gross weight was 800 lbs. and the empty weight was 472-lbs. and left room after pilot fuel, and oil for 117.2 lbs. of passenger. If I were to increase the gross weight to 900 pounds that would give me room for a 217.2-pound passenger, which would give more flexibility in passengers.

I knew that if I lowered the maximum G ratings for my plane, that would increase my gross weight. If you take the positive design load of 4800 lbs. and divide it by the new maximum G rating of +5, that would give a gross weight of 960 lbs. If you take the negative design load of 2400 lbs. and divide it by 960lbs, you get a G rating of -2.5G's.

This change leaves a fairly large margin of safety in turbulence and also gives some increased utility since there is now a higher gross weight. This change would now give me room for a passenger who weighed 277.2 pounds and would allow me to carry anyone that I know who would want to fly. Increasing the gross weight does not come without its drawbacks though.

The Down Side to Increasing Gross Weight
Like anything else in aviation, a gain in one place means a loss in another place. There are some things to consider when raising the gross weight. Among those things are decreased performance, increased fuel consumption, possible center of gravity problems, and, of course, decreased G ratings.

Because of the higher gross weight, the take-off distance, landing distance and stall speed will be increased and the climb rate will decrease. The pilot will have to be aware of the G ratings when flying in turbulence and when doing “yank and bank” flying. The pilot will have to remember when flying at the increased weight to slow down more in turbulence and be easier on the controls. He will also need to remember that stall speed will be higher and it will take more distance to take off and land.

He will also have to pay more attention to the center of gravity. The Challenger has a wide center of gravity envelope, but all of the weight that is placed in the cockpit moves the CG forward. With higher payloads, you may go past the forward limit for center of gravity. The good news is that if you are flying solo, then you are most likely below 800 pound gross weight flying a plane with a designed +6 and -3G range.


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PostPosted: Sat Jul 11, 2009 6:15 am    Post subject: A Note About Moding G's instead of Weight Reply with quote

Juan, I don't think he is.....

For my RV-10, I added 100lbs to my gross weight after looking at the numbers. Had an AE look at it and in the end had to reduce my max G loading by .2 G's at the new gross weight. I tested at that weight to include aft C/G....could not test forward CG "limit" since there is no way of getting up on the forward with that much weight. The only real concern I had was with the gear and what affect the 100 lbs would have. But since I would not be landing at the gross weight and since in almost all scenarios it is nearly impossible to load to max and keep it there, I accepted that risk.

Rene' Felker
RV-10 N423CF Flying
801-721-6080
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PostPosted: Sat Jul 11, 2009 6:17 am    Post subject: A Note About Moding G's instead of Weight Reply with quote

Hi Juan,

No. I am being completely serious. I really believe the impact of
being over gross weight is predictable and reasonably safe. There
are obvious impacts to required runway length and climb rates, but
for the most part a small excess of weight results in a small
reduction in performance.

Of course, this assumes that the CG for the plane is still within
normal limits.

My understanding of the FAA regs on this matter is that the pilot is
required to be aware of the weight situation but he is not required
to remain within the weight specified on the aircraft
documents. Indeed the MTOW specified in the documents is totally
arbitrary - based on a set of conditions that may or may not be the
ones faced for a given flight.

I still await your answer about what happens if you are over gross
weight. (Keep in mind that this happens every day on some aircraft
like the C-150, and will probably also happen on most dual flights of
the new C-162).

Paul
XL grounded
do not archive
At 06:37 AM 7/11/2009, you wrote:
[quote]

Paul,
your shitting me right?
Juan

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jmaynard



Joined: 27 Feb 2008
Posts: 394
Location: Fairmont, MN (FRM)

PostPosted: Sat Jul 11, 2009 6:25 am    Post subject: A Note About Moding G's instead of Weight Reply with quote

On Sat, Jul 11, 2009 at 07:13:34AM -0700, Paul Mulwitz wrote:
Quote:
My understanding of the FAA regs on this matter is that the pilot is
required to be aware of the weight situation but he is not required to
remain within the weight specified on the aircraft documents.

..except for an LSA, which may not be operated contrary to the
amnufacturer's instructions. The POH carries the force of law for an LSA.
--
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http://jmaynard.livejournal.com http://www.tronguy.net
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PostPosted: Sat Jul 11, 2009 6:39 am    Post subject: A Note About Moding G's instead of Weight Reply with quote

Hi Juan,

I agree with everything said in your quoted article except for the
turbulence comment. I'm afraid the author got this point backwards.

Increasing actual gross weight increases Va rather than decreasing
it. So, in theory, you could fly faster in the same turbulence with
more gross weight rather than needing to fly slower.

OK, it is a small point. The simple answer for most pilots in most
conditions is to keep under gross weight specified in the airplane's
documents. However, I still believe flying over gross weight can be
done safely, and legally, in some planes under some conditions.

Paul
do not archive
At 07:08 AM 7/11/2009, you wrote:
Quote:
The pilot will have to remember when flying at the increased weight
to slow down more in turbulence


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PostPosted: Sat Jul 11, 2009 6:39 am    Post subject: A Note About Moding G's instead of Weight Reply with quote

Folks, there is a pertinent article in Flying (July 2009), page 32, by Peter Garrison: "Aftermath / the myth of gross weight", which you can read here:
http://www.flyingmag.com/accidents/1593/the-myth-of-gross-weight.html


Carlos

2009/7/11 Paul Mulwitz <psm(at)att.net (psm(at)att.net)>
[quote] --> Zenith-List message posted by: Paul Mulwitz <psm(at)att.net (psm(at)att.net)>


Hi Juan,

No.  I am being completely serious.  I really believe the impact of being over gross weight is predictable and reasonably safe.  There are obvious impacts to required runway length and climb rates, but for the most part a small excess of weight results in a small reduction in performance.
[b]


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PostPosted: Sat Jul 11, 2009 6:47 am    Post subject: A Note About Moding G's instead of Weight Reply with quote

Hi Jay,

This is a very interesting distinction.

I wonder how the C-162 will be certified. It seems if it is
certified under part 23 you can do dual instruction in it but if it
is certified as S-LSA you can't do dual legally. If I remember
correctly from my original calculations with full fuel and a normal
adult in one seat the other one will have to weigh 50 pounds or so to
stay under MTOW.

Paul
do not archive
At 07:24 AM 7/11/2009, you wrote:
Quote:


On Sat, Jul 11, 2009 at 07:13:34AM -0700, Paul Mulwitz wrote:
> My understanding of the FAA regs on this matter is that the pilot is
> required to be aware of the weight situation but he is not required to
> remain within the weight specified on the aircraft documents.

...except for an LSA, which may not be operated contrary to the
amnufacturer's instructions. The POH carries the force of law for an LSA.
--


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PostPosted: Sat Jul 11, 2009 7:05 am    Post subject: A Note About Moding G's instead of Weight Reply with quote

Over time, it has been proffered that inane speculation often subtracts from
the sum total of human intelligence.

Regards,
Ken

do not archive


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Joined: 12 Dec 2008
Posts: 16
Location: arizona

PostPosted: Sat Jul 11, 2009 1:10 pm    Post subject: Re: A Note About Moding G's instead of Weight Reply with quote

'Over time, it has been proffered that inane speculation often subtracts from
the sum total of human intelligence.'

Hmm... making the assumptive leap that 'human intelligence' is not a conflict in terms, and those doing the proffering are proven by all to be the Wise, methinks speculation of any sort can be classified either as inane or not - praytell, whom dost say whether inane or not?

so as the river winding to the sea is never direct, but flows inanely across the land to the ocean.....

Let it flow and enjoy the shore a bit, eh? just might find a cove of great surprise

Dave
601XL
building temporarily frozen in the phoenix heat


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PostPosted: Sat Jul 11, 2009 1:43 pm    Post subject: A Note About Moding G's instead of Weight Reply with quote

Quote:
Dave
601XL
building temporarily frozen in the phoenix heat

My garage temperature was over 120. Outside temp just over 113.
Also waiting for heat to subside.
Jerry


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Juan Vega Jr



Joined: 13 Jan 2009
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PostPosted: Sat Jul 11, 2009 2:58 pm    Post subject: A Note About Moding G's instead of Weight Reply with quote

Dave,
Put down the Bong and get back to building:)

Juan

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