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Required IFR equipment
G enerator/alternator
R adio
A ltimeter
B all inclinometer
C lock
Artificial horizon
Rate of turn indicator
Directional gyro
DME/gps substitute
IFR currency requirements
6 approaches
Holding w/ nav aid
Intercepting w/ nav aid
Tracking
Simulated or actual
All within 6 cm
Cirrus engine
Lycoming IO-390in³ (fuel injected, horizontally opposed)
Horizontally opposed
Air cooled
Naturally aspirated
Direct drive
215 hp @ 2700rpm
Cirrus electrical system
28v direct current
2 alternators (Alt 1: 27.7 v 100 amp Alt 2: 28.7v 70 amps)
2 batteries (Batt 1: 24v 10 amps Batt 2: two 12v 7 amps)
Buses
Diodes
Cirrus fuel system
58.5 gal
56 usable gal
2 fuel pumps (engine driven and boost)
5 sumps
Max 7lb imbalance
Propeller
Constant speed
Adjustable prop
Hertzel 75”
Prop governor connected to throttle
Prop pitch changed by oil psi
Max takeoff/landing weight
3150 lbs