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Takeoff and Landing chart

 
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rv10flyer(at)live.com
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PostPosted: Wed Jun 19, 2013 11:38 am    Post subject: Takeoff and Landing chart Reply with quote

Anyone have a chart for their POH that covers runway takeoffs at different altitudes, over the 50 foot obstacles, landing distances, etc.
Thank you!

Pascal

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dave.saylor.aircrafters(a
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PostPosted: Wed Jun 19, 2013 4:58 pm    Post subject: Takeoff and Landing chart Reply with quote

I don't have graphs and tables but I did record some empirical information in the POH, as follows:
***********************************
Take-off Performance

Safe takeoff has been demonstrated at 10,000 foot density altitude conditions. At a takeoff weight of 2600 pounds, the aircraft was 100 feet AGL after 4000 feet of runway. There was no headwind.
The aircraft was run up and leaned for best performance before starting the ground roll. Flaps were set at 1/3.

Typical sea level takeoff generally requires less than 1000 feet.

***********************************

That's not a ton of information but it's a useful data point.  We did this on the way back from OSH at KEMM.  4000' was approximately mid-field.

Dave Saylor
831-750-0284 CL


On Wed, Jun 19, 2013 at 12:38 PM, Pascal <rv10flyer(at)live.com (rv10flyer(at)live.com)> wrote:
[quote] Anyone have a chart for their POH that covers runway takeoffs at different altitudes, over the 50 foot obstacles, landing distances, etc.
Thank you!
 
Pascal
 
Quote:


get="_blank">http://www.matronics.com/Navigator?RV10-List
tp://forums.matronics.com
_blank">http://www.matronics.com/contribution


[b]


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rv10flyer(at)live.com
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PostPosted: Wed Jun 19, 2013 5:21 pm    Post subject: Takeoff and Landing chart Reply with quote

Thank you Dave. Any information is helpful.
Pascal

From: Dave Saylor (dave.saylor.aircrafters(at)gmail.com)
Sent: Wednesday, June 19, 2013 5:57 PM
To: rv10-list(at)matronics.com (rv10-list(at)matronics.com)
Subject: Re: Takeoff and Landing chart


I don't have graphs and tables but I did record some empirical information in the POH, as follows:
***********************************
Take-off Performance

Safe takeoff has been demonstrated at 10,000 foot density altitude conditions. At a takeoff weight of 2600 pounds, the aircraft was 100 feet AGL after 4000 feet of runway. There was no headwind.
The aircraft was run up and leaned for best performance before starting the ground roll. Flaps were set at 1/3.

Typical sea level takeoff generally requires less than 1000 feet.

***********************************

That's not a ton of information but it's a useful data point. We did this on the way back from OSH at KEMM. 4000' was approximately mid-field.


Dave Saylor
831-750-0284 CL
On Wed, Jun 19, 2013 at 12:38 PM, Pascal <rv10flyer(at)live.com (rv10flyer(at)live.com)> wrote:
Quote:
Anyone have a chart for their POH that covers runway takeoffs at different altitudes, over the 50 foot obstacles, landing distances, etc.
Thank you!

Pascal

Quote:


get="_blank">http://www.matronics.com/Navigator?RV10-List
tp://forums.matronics.com
_blank">http://www.matronics.com/contribution





[quote]

href="http://www.matronics.com/Navigator?RV10-List">http://www.matronics.com/Navigator?RV10-List
href="http://forums.matronics.com">http://forums.matronics.com
href="http://www.matronics.com/contribution">http://www.matronics.com/c
[b]


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