Cirrus DESIGN SR22T User Manual

Cirrus Design Section 7
SR22T Airplane and Systems Description
P/N 13772-003 7-41
Figure 7-8
Fuel System Schematic
ENGINE SPEED
SENSOR
(LOW RPM)
THROTTLE
METERING
VALVE
FIREWALL
FUEL
PUMP
GASCOLATOR
SR22_FM07_3259
NOTE
In HIGH BOOST/PRIME
mode, relay allows fuel
pump operation only when
manifold pressure is greater
than 24 in Hg or, - to
facilitate engine starting
- when engine speed is
less than 500 RPM.
MAP SENSOR
(HIGH in Hg)
ENGINE
AIRFRAME
UNIT
FUEL FLOW
SENSOR
ELECTRIC
AUXILIARY
PUMP
R. WING
COLLECTOR
VENT
FILLER
R. WING TANK
FILLER
OFF
FEED
RETURN
LEFT
RIGHT
FEED
RETURN
FUEL PRESSURE SWITCH
SELECTOR VALVE
OPERATION
FUEL
FLOW
INDICATOR
ANNUNCIATOR
FUEL
FUEL
QUANTITY
INDICATOR
HIGH
BOOST/
PRIME
BOOST
DRAIN
(5 PLACES)
INJECTOR
MANIFOLD
VENT
L. WING TANK
L. WING
COLLECTOR
FUEL
RELAY
ENGINE DRIVEN
FUEL PUMP
MIXTURE CNTL.
FLAPPER
VALVE
FLAPPER
VALVE
SELECTOR
VALVE
Original Issue

Cirrus DESIGN SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Model	SR22T
Seating Capacity	5
Engine	Continental TSIO-550-K
Horsepower	315 hp
Avionics	Cirrus Perspective+ by Garmin
Type	Single-engine piston aircraft
Maximum Speed	213 knots
Cruise Speed	183 knots
Service Ceiling	25, 000 feet
Maximum Takeoff Weight	3, 600 lbs
Wingspan	38 feet 4 inches
Length	26 ft
Height	8 feet 11 inches
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cabin Width	49 inches
Cabin Height	50 inches