POH

Question 1

What are the engine specs for the SR20?

Answer 1

Lycoming: IO-390-C3B6
Fuel injected
Air Cooled
Horizontally opposed
Direct Drive
Normally Aspirated
215 Horsepower
2700 RPM (max)

Question 2

What are the propeller specs for the SR20?

Answer 2

Hartzell 74.0” three blade metal constant speed.

Question 3

What is the maximum oil capacity for the SR20?

Answer 3

7 quarts

Question 4

What is the maximum gross weight for T/O?

Answer 4

3,150 lbs

Question 5

What is the maximum baggage compartment load weight?

Answer 5

130 lbs

Question 6

What are the fuel specs for the SR20?

Answer 6

-Approved Fuel Grades: 100LL and 100
-Total Fuel capacity: 58.5 gallons
-Total Fuel each tank: 29.3
-Total Usable Fuel: 56.0

*Maximum allowed fuel imbalance: 7.5 gallons

Question 7

Is the SR20 rated for flight into known icing conditions?

Answer 7

No

Question 8

Max oil temperature?

Answer 8

235 F

Question 9

Minimum oil temperature for takeoff?

Answer 9

100 F

Question 10

Oil pressures at different stages.

Answer 10

Minimum (idling): 25 psi
Normal Operating Range: 55-95
Maximum (starting, warmup, taxi, takeoff): 115

Question 11

What oil does the SR20 use?

Answer 11

SAE 15W-50

Question 12

Where is the reference datum?

Answer 12

100 inches forward of firewall

Question 13

What maneuvers are not allowed?

Answer 13

Acrobatic maneuvers and spins are prohibited.

Question 14

Flight Load Factor Limits

Answer 14

Flaps up (0%): +3.8g, -1.9g
Flaps 50%: +1.9g, 0g
Flaps 100%: +1.9g, 0g

Question 15

Maximum T/O altitude?

Answer 15

10,000’ MSL

Question 16

Maximum operating altitude?

Answer 16

17,500’ MSL

Question 17

Max occupancy?

Answer 17

1+4. 1 pilot and 4 passengers.

Question 18

What is the minimum crew needed for the SR20?

Answer 18

1

Question 19

Why does the Garmin 1,000 Manual need to be in the plane?

Answer 19

It says it in the POH, 2-20.

Question 20

How long should the ignition system be cranked?

Answer 20

10 seconds with 30 seconds breaks between uses.

Question 21

What kind of fuselage does the SR20 have?

Answer 21

Monocoque

Question 22

How are the flight controls connected to the flight surfaces?

Answer 22

The control system uses a combination of push rods, cables, and bell cranks for control of the surfaces.

Question 23

What kind of elevator does the SR20 have?

Answer 23

Conventional

Question 24

What kind of Rudder does the SR20 have?

Answer 24

Conventional

Question 25

What kind of Ailerons does the SR20 have?

Answer 25

Conventional

Question 26

How is the elevator trim system powered/operated?

Answer 26

Elevator (pitch) trim operates on 28 VDC supplied through the 2 amp pitch trim circuit breaker on ESS BUS 2.

Question 27

What kind of Flaps does the SR20 have?

Answer 27

Electrically controlled single slotted flaps.

Question 28

How is the Aileron trim powered/operated?

Answer 28

Aileron trim operates on 28 VDC supplied through the 2 amp Roll Trim circuit breaker on ESS BUS 2.

Question 29

What are the three positions Flaps can be deflected to (include degrees with percentages).

Answer 29

0% = 0 degrees 50% = 16 degrees 100% = 32 degrees

Question 30

How do the flaps move?

Answer 30

by operating the Flap control switch this positions the Flaps through a motorized linear actuator mechanically connected to both flaps by a torque tube.

Question 31

What are the specs for the main wheel tires?

Answer 31

Each main gear wheel has a 15 X 6.00 X 6 tubeless tire.

Question 32

What are the specs for the Nose Gear Tires?

Answer 32

Each nose wheel has a 5.00 X 5 tubeless tire.

Question 33

How many degrees can the nose wheel move?

Answer 33

Through 170 degrees. 85 degrees for each side.

Question 34

Brake System

Answer 34

Hydraulically operated, single disc type brakes, individually activated by floor mounted toe pedals at both pilot stations. Note: a parking brake mechanism hold induced hydraulic pressure on the disc brakes for parking.

Question 35

What is SLICKSTART?

Answer 35

The ignition and starter system includes SlickSTART, which changes the ignition timing and adds energy to the spark to aid in starting. Note: 28 VDC for Starter operation is supplied through the 2 amp STARTER circuit breaker on NON-ESSENTIAL BUS.

Question 36

What kind of oil system does the SR20 have?

Answer 36

Wet sump.

Question 37

How does the oil move through the engine?

Answer 37

SPSCFP Sump, Pump, Strainer, Cooler, Filter, Pressure Relief Valve

Question 38

What are the four purposes of oil?

Answer 38

Cool Clean Seal Lubricate

Question 39

What are the components of the Fuel system?

Answer 39

tanks, collectors, three position selector valve, an electric fuel pump, and an engine driven fuel pump.

Question 40

What is ALT 1 regulated to?

Answer 40

27.7 Volts

Question 41

What is ALT 2 regulated to?

Answer 41

28.7 Volts

Question 42

How many amps is Alt 1?

Answer 42

100

Question 43

How many amps is Alt 2?

Answer 43

70

Question 44

How many torque pounds of force does it require to pull the CAPS handle?

Answer 44

45

Question 45

How is CAPS initiated?

Answer 45

Blue, Red, Red Activate Autopilot, pull the lever, cut the mixture.

Question 46

Does the Airworthiness Cert need to be displayed?

Answer 46

Yes

Question 47

Does the Registration need to be displayed?

Answer 47

No, but it needs to be in the aircraft for all operations.

Question 48

What is the PSI for the Nose and Main tires?

Answer 48

Nose: 30-35 Mains: 60-65

Question 49

What is the minimum amount of oil allowed?

Answer 49

The engine must not be operated with less than six quarts of oil in the sump. Seven is recommended for extended operations.

Question 50

How many quarts does the oil filter hold?

Answer 50

1