Aircraft Systems

Question 1

Archer Engine

Answer 1

Lycoming, 4 cylinder, O-360
Horizontally opposed, air cooled, normally aspirated, direct drive
180 hp

Question 2

Archer Oil

Answer 2

6-8 quarts

Question 3

Archer Propeller

Answer 3

Sensenich two-blade fixed pitch

76 inch diameter

Question 4

Archer Landing gear

Answer 4

Fixed gear tricycle
Óleo struts for shock absorption
Shimmy dampener for nose wheel
20 degrees of deflection

Question 5

Archer Brakes

Answer 5

Hydraulic brakes

Separate braking cylinders with shared reservoir

Question 6

Archer Flaps

Answer 6

Manual flaps

0, 10, 25, 40 settings

Question 7

Archer pitot static

Answer 7

Pitot head below left wing
Alternate static inside cabin, left side
When using alternate static storm window/cabin vents must be closed
The cabin heater and defroster must be on, to minimize error

Question 8

Archer fuel systems

Answer 8

100 LL 
2 x 25 Gallon 
1 gallon unusable both tanks 
1 engine driven fuel pump
1 electrically driven fuel pump
L/R/OFF

Question 9

Archer Electrical system

Answer 9

28 volt DC electric
24 volt lead- acid battery
70- amp engine driven alternator

Question 10

G500 components

Answer 10

PFD: Primary Flight Display (left)
MFD:Multi-Function Display (right)
AHRS: Attitude Heading Reference System 
ADC: Aid Data Commuter
Magnetometer
Temperature probe
Dual Garmin in GNS 430 GPS

Question 11

Standby Instruments

Answer 11

Electrical failure allow 60 seconds to press “STBY PWR” which will continue operation for roughly 1 hour
Test: press “STBY PWR” for 4 seconds amber light should flash, and continuous green indicates a PASS, Red light indicates a FAIL