Nova FACTOR 2, Руководство пользователя

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Vers.1.0
01.06.2011
S. 37 / 39
8G
The breaking load of the line equates to the LTF threshold. The lines should be
replaced, because the strength of the lines would soon be below the LTF limit.
If the breaking load is in between 8g and 10g we strongly recommend
scheduling the next NFS after just one year instead of two. If the wing is used
for Acro flying or for more than 100hours a year, the lines have to be replaced.
> 10G
The breaking load is well above the LTF limit of 8 G. For normal use (less than
400 flights and 200 hours per 2 years, no Acro) we recommend the next NFS
after two years.
Note:
The values in the table above for the mid lines are valid for all gliders which
have two mid lines per lower line. For gliders with three mid lines per lower
line (e.g. Carbon) you have to calculate the strength limit as follows:
Get the value for the lower line from the table and divide it by three. Then
multiply this value by 1.2 to get the strength limit for the mid line. For
example:
If the limit for the lower line is 120 daN, the limit for the mid line (in case of
three mid lines) is 48 daN. = (120 / 3) * 1.2
If you want to perform a ripping test on the top lines (not obligatory), the
calculation is as follows: Multiply the max. Take-off weight by the G-load.
Then divide this value by the number of all A and B top lines. (no stabile lines!)
This value has to be multiplied by 1.2.
For example:
Maximum take-off weight=110kg
Number of A & B top lines=40
Necessary G load= 10g
Minimum strength= [(110*10)/40]*1.2=33 daN