FAA Task G: Operation of Systems

Question 1

Primary flight controls

Answer 1

Alieron: Long
Stabilator: Lat
Rudder: Verticle

Question 2

Secondary flight controls

Answer 2

Slotted Flaps
Anti Servo Trim

Question 3

Powerplant and propeller

Answer 3

LHAND
L: Lycoming 0-360-A4M
H: Horizontally Opposed
A: Air cooled
N: Naturally Aspirated (no turbo or supercharging)
D: Direct Drive (crankshaft connected directly to the propeller)

180 horsepower at 2700 RPM

Sensenich two-bladed, fixed pitch, metal propeller.
Propeller diameter is 76 inches.
Maximum RPM is 2700 RPM

Question 4

Fuel, oil, and hydraulic

Answer 4

100(Green) or 100LL (Blue)

Oil: W100

Hydraulic: Red mineral based

Question 4

Landing gear

Answer 4

Fixed nose wheel.

Question 5

Electrical

Answer 5

24V battery > 28V 70AMP alternator > VR28V > OVR 32V >

LEEANB
L: Lighting
E:Essential
E:Emergency
A:Avionics
N: Non Essential
B: Battery

Question 6

Avionics

Answer 6

G1000, Aspen Evolution backup.

Question 7

Pitot-static, and associated flight instruments

Answer 7

Pitot Static and ADC = IAS, TAS, VSI, Altimeter

AHRS = Attitude indicator, Rate of turn, and Slip Skid.

Question 8

Environmental

Question 9

Deicing and anti-icing

Answer 9

No deicing
Anti Icing = Windshield defroster, pitot heat and carb heat.

Question 10

Indications of and procedures for managing system abnormalities or failures.

Question 11

Detection of system malfunctions or failures.

Question 12

Management of a system failure.

Question 13

Monitoring and management of automated systems.

Question 14

Fuel Flow

Answer 14

Fuel flows from the tanks to the fuel selector, through the strainer, then the electric fuel pump. It then
goes through the engine driven pump, to the regulator, then the distributor that injects the fuel into all
cylinders.