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Cirrus SR20 - Page 291

Cirrus SR20
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Cirrus Design Section 7
SR20 Airplane and Systems Description
P/N 21399-004 7-107P/N 21399-004 7-107
seats and landing gear are designed to accommodate this
stress, occupants must prepare for it in accordance with
Section 3 - CAPS Deployment Checklist.
• Note •
The CAPS is designed to work in a variety of airplane
attitudes, including spins. However, deployment in an attitude
other than level flight may yield deployment characteristics
other than those described above.
Revision A1

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