Cirrus SR20 - Page 262

7-78 P/N 21399-004
Section 7 Cirrus Design
Airplane and Systems Description SR20
Figure 7-17
Pitot-Static System - Serials w/o MD302 (1 of 2)
STATIC
BUTTONS
PITOT HEAT
AIR DATA COMPUTER
PFD Air Data
AIR DATA COMPUTER 2 (optional)
AIRSPEED
INDICATOR
PITOT MAST
Annunciation
PITOT-STATIC
WATER TRAPS
ALTERNATE
STATIC
AIR SOURCE
ALTIMETER
ENGINE AIRFRAME UNIT
LOGIC
CURRENT
SENSOR
HEATER
7.5A
PITOT
HEAT
CB
PITOT HEAT SW
SR20_FM07_2793B
Revision A1