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Cirrus SR22 - Landing Gear; Brake System

Cirrus SR22
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7-24 P/N 13772-004
Section 7 Cirrus Design
Systems Description SR22
Vertical speed must exceed 100 feet/min before digits will appear in
the VSI pointer. If the rate of ascent/descent exceeds 2000 fpm, the
pointer appears at the corresponding edge of the tape and the rate
appears inside the pointer.
Serials 4164 & subs w/ MD302 Standby Attitude Module:
The Altitude Trend Bar is located along the right margin of the Altitude
Display. This feature is optional and can be turned on or off by the
user.
Magnetic Compass
A conventional, internally lighted, liquid filled, magnetic compass is
installed on the cabin headliner immediately above the windshield. A
compass correction card is installed with the compass.
• Note •
Refer to FAA Advisory Circular (AC) 43.13-1B for a list of
occasions requiring a compass swing. If a compass swing is
required, perform Operational Test - Magnetic Compass
Calibration (refer to AMM 34-20, Attitude and Direction).
Revision 1

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