Cirrus SR22T User Manual

3-36 P/N 13772-005
Section 3 Cirrus Design
Emergency Procedures SR22T
Oxygen System Emergencies
Oxygen System Fault - Above 10,000 Ft
OXYGEN FAULT Warning
1.
Oxygen Flow Rate.............................................................. CHECK
If no flow:
2.
Initiate Emergency Descent to below 10,000 ft:
a. Power Lever......................................................................IDLE
b. Mixture............................................................. AS REQUIRED
c. Airspeed .........................................................VNE (205 KIAS)
If flow is normal:
3. Oxygen Flow Rate.......................................................... MONITOR
4. Initiate Normal Descent as soon as practical.
Below 10,000 ft:
5. Oxygen System........................................................................OFF
6. Flight ............................................................................ CONTINUE
Remain below altitudes requiring supplemental oxygen.
Amplification
Annunciation indicates tank solenoid failed (open or closed) or flow
rate is low. If flow is checked and confirmed present, solenoid has
failed OPEN; system will continue to provide oxygen until depleted, but
unnecessary flight at altitudes requiring oxygen is not recommended.
OXYGEN FAULT
Original Issue

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