Today's Message Index:
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1. 03:44 AM - Re: Flight Load Factors (Barry Collman)
2. 04:51 PM - Re: Re: Flight Load Factors (nico css)
3. 05:03 PM - Re: Re: Flight Load Factors (BobsV35B@aol.com)
Message 1
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| Subject: | Re: Flight Load Factors |
Hi Richard,
Grateful thanks!
Very Best Regards,
Barry
----- Original Message -----
From: Richard & Jacqui Thompson
To: commander-list@matronics.com
Sent: Saturday, May 03, 2008 11:32 PM
Subject: RE: Commander-List: Flight Load Factors
Hi Barry,
My 680E manual states a positive limit load factor is 3.5 Gs.
Cheers
Richard
-----Original Message-----
From: owner-commander-list-server@matronics.com
[mailto:owner-commander-list-server@matronics.com] On Behalf Of Barry
Collman
Sent: Saturday, 3 May 2008 10:14 PM
To: commander-list@matronics.com
Subject: Commander-List: Flight Load Factors
Hi Guys,
I need some help.
I haven't got a copy of numerous Flight Manuals for the Commander
Models and will really appreciate your help.
I understand that somewhere within these Manuals are the "Flight Load
Factors" for the Model.
Could I ask that you take the proverbial "5 minutes" to look in your
Manual and let me know the 'Positive G' and 'Negative G' figures,
together with the Model concerned.
Your help will, of course, be very much appreciated.
Very Best Regards,
Barry
http://www.matronics.com/Navigator?Commander-Listhttp://forums.matronics.
com
Message 2
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| Subject: | Re: Flight Load Factors |
Wouldn't turbulence easily exceed the load when the flaps are down? +2 isn't
much and no negative?
-----Original Message-----
From: owner-commander-list-server@matronics.com
[mailto:owner-commander-list-server@matronics.com] On Behalf Of KORY
Sent: Saturday, May 03, 2008 7:49 AM
Subject: Commander-List: Re: Flight Load Factors
FOR THE 685
FLAPS UP POSITIVE 3.36 NEGATIVE 1.35
FLAPS DOWN POSITIVE 2.00 NEGATIVE 0.00
KORY
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=180894#180894
Message 3
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| Subject: | Re: Flight Load Factors |
Good Evening Nico,
Chances are that the airplane is actually much stronger than that, but 2 Gs
is all that they have to prove to the FEDs. Same thing is true with the
other listed load factors. It has been a long time so somebody please correct me
where I am wrong, but I THINK the required structural strength on the tail is
only 1.5 Gs!
Happy Skies,
Old Bob
AKA
Bob Siegfried
Ancient Aviator
628 West 86th Street
Downers Grove, IL 60516
630 985-8502
Stearman N3977A
Brookeridge Air Park LL22
In a message dated 5/4/2008 6:53:07 P.M. Central Daylight Time,
nico@cybersuperstore.com writes:
Wouldn't turbulence easily exceed the load when the flaps are down? +2 isn't
much and no negative?
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