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pbuttles(at)charter.net
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 Posted: Fri Nov 21, 2008 4:41 pm Post subject: gross weight |
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I know there is a formula in the plans for g load over gross.
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cscsail(at)gmavt.net
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| Posted: Sat Nov 22, 2008 5:15 am Post subject: gross weight |
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This is the entry from my the manual I wrote:
Warning: If operating the aircraft at a weight over the gross weight:
1) The load factor will decrease as follows: 1100
“g”
over gross = 6 x ------------------
Weight in lbs. (1100 +excess)
(for example at 1150lbs the limit load factor will be 3.8
Ultimate load factor = limit load factor divided by the standard aircraft
safety factor of 1.5)
2) Reduced performance:
-Stall speed will be higher.
-Rate of climb and
controllability will deteriorate.
3) The center of gravity must always stay within the design limits.
Gordon
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cscsail(at)gmavt.net
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| Posted: Sat Nov 22, 2008 5:31 am Post subject: gross weight |
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Tommy Walker
Joined: 12 Jan 2006
Posts: 442
Location: Anniston, AL 36207
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| Posted: Sun Nov 23, 2008 1:50 pm Post subject: Re: gross weight |
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I agree with you Gordon.
Tommy Walker in Alabama.
Do Not Archive
| cscsail(at)gmavt.net wrote: | This is the entry from my the manual I wrote:
Warning: If operating the aircraft at a weight over the gross weight:
1) The load factor will decrease as follows: 1100
“g”
over gross = 6 x ------------------
Weight in lbs. (1100 +excess)
(for example at 1150lbs the limit load factor will be 3.8
Ultimate load factor = limit load factor divided by the standard aircraft
safety factor of 1.5)
2) Reduced performance:
-Stall speed will be higher.
-Rate of climb and
controllability will deteriorate.
3) The center of gravity must always stay within the design limits.
Gordon
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| | - The Matronics Zenith701801-List Email Forum - | | | Use the List Feature Navigator to browse the many List utilities available such as the Email Subscriptions page, Archive Search & Download, 7-Day Browse, Chat, FAQ, Photoshare, and much more:
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_________________
Tommy Walker
N25A - Anniston, AL |
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