Cirrus SR22T Maintenance Manual

CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
24-30
Page 59
Serials 22-1602, 22-1644, 22-1663 & subs w/o Per-
spective Avionics
EFFECTIVITY:
Z. Volt / Amp Meter - Serials 22-1602, 22-1644, 22-1663 & subs w/o Perspective Avionics (See Fig-
ure 24-308)
Note: Voltage and amperage are displayed on the screens of the MFD and PFD.
(1) Operational Test - Volt / Amp Meter
(a) Set BAT1 and AVIONICS switches to ON positions.
(b) On MFD, when PRESS ANY BEZEL KEY TO CONTINUE is displayed, press any key.
(c) If Engine Monitoring is selected, press [Fuel Done] to enter Map
page.
(d) Rotate left knob to select Engine
page.
(e) Verify Main Bus voltage indicates 26 ±2 VDC.
(f) Verify Essential Bus voltage indicates no more than 1 vdc less than the Main Bus voltage.
(g) Verify ALT1 indicates zero amps.
(h) Verify ALT2 indicates zero amps.
(i) Verify BATT indicates Dschg 0 - 10 amps.
(j) Turn on large electrical loads (landing light, nav lights, pitot heat, etc.) to ensure more
amps are drawn when larger electrical loads are introduced.
(k) Verify ammeter indicates an increase in amperage.
(l) Set BAT1 and AVIONICS switches to OFF positions.
01 Jan 2012

Cirrus SR22T Specifications

General

Manufacturer	Cirrus Aircraft
Engine	Continental TSIO-550-K
Horsepower	315 hp
Max Takeoff Weight	3, 600 lbs
Service Ceiling	25, 000 ft
Cabin Width	49 in
Cabin Height	50 in
Seating Capacity	4
Avionics	Cirrus Perspective+ by Garmin
Category	Single-engine piston aircraft
Propeller	Hartzell 3-blade composite
Wingspan	38 ft 4 in
Length	26 ft
Height	8 ft 11 in
Maximum Cruise Speed	213 KTAS
Fuel Capacity	92 gallons
Stall Speed	64 knots
Safety Features	Cirrus Airframe Parachute System (CAPS)
Cruise Speed	183 knots