# 2001 SR22 G1 Deicing

**URL:** <https://forum.cirruspilots.org/t/2001-sr22-g1-deicing/89349>\
**Category:** Guest Discussion\
**Created:** [November 29, 2017, 7:43am UTC](https://forum.cirruspilots.org/t/2001-sr22-g1-deicing/89349 "2017-11-29T07:43:08Z")\
**Posts on this page:** 1\
**Page:** 2

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**Author:** ![NWflyer](https://sea1.discourse-cdn.com/copa/user_avatar/forum.cirruspilots.org/nwflyer/32/85682_2.png) [@NWflyer](https://forum.cirruspilots.org/u/NWflyer)\
**Post date:** [September 19, 2018, 7:41am UTC](https://forum.cirruspilots.org/t/2001-sr22-g1-deicing/89349/21 "2018-09-19T07:41:21Z")

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> [@](#):
>
> And the system has been tested on composite and it’s not a problem

Agreed, but all composites like metals have different elastic regions. The system has to be installed with a known elasticity of the materials.

I’m guessing our leading edges were not tested to be bent in the direction of this system.

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