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8 Terms

1
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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

2
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IFR currency requirements

6 approaches

Holding w/ nav aid

Intercepting w/ nav aid

Tracking

Simulated or actual

All within 6 cm

3
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Cirrus engine

Lycoming IO-390in³ (fuel injected, horizontally opposed)

Horizontally opposed

Air cooled

Naturally aspirated

Direct drive

215 hp @ 2700rpm

4
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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

5
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Cirrus fuel system

58.5 gal

56 usable gal

2 fuel pumps (engine driven and boost)

5 sumps

Max 7lb imbalance

6
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Propeller

Constant speed

Adjustable prop

Hertzel 75”

Prop governor connected to throttle

Prop pitch changed by oil psi

7
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Max takeoff/landing weight

3150 lbs

8
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