C207 Fox Exam Review Questions with Verified
Correct Answers
Describe C207 engine
Teledyne Continental IO-520-F
Horizontally Opposed
Air Cooled
Naturally Aspirated
Direct Drive
*Fuel Injected, 6 cylinder piston engine.
Describe C207 airframe
All-metal, seven seat, high-wing, single-engine airplane designed for general utility purposes.
Semi-monocoque design covered with aluminum skin
How much fuel can the C207 hold?
Two, 40g tanks for a total of 80g, 73g usable
Describe the C207 fuel system
Fuels flows from
Wing tanks
Reservoir tanks
Fuel selector
Auxiliary fuel pump
Fuel strainer
Engine driven fuel pump
Fuel air control unit
Fuel manifold
What does Fuel Injection consist of?
Engine driven fuel pump
Fuel/Air control unit
Fuel manifold
, Fuel flow indicator
Air bleed type injector nozzles
What should you do if you run one tank completely dry?
PSS (Pitch Switch Switch)
What is PSS acronym?
Pitch - for best glide - (80 KIAS w/flaps up or 85 with 10º)
Switch - the fuel selector to the opposite tank
Switch - turn on the emergency fuel pump for 3-5 seconds with throttle ½ open
Describe C207 electrical system
28v direct current electrical system driven by a 60amp alternator with a 12v battery
What does the Primary BUS power?
All aircraft lights
Pitot heat/stall system
Turn coordinator Ignition switch
Fuel quantity indicators
CHT indicators
Flap system
Aux fuel pump
What does the Electronic BUS power?
GPS
Capstone
Com 1 & 2
Nav 1 & 2
Describe C207 flaps
Electric single slotted flaps 0-30deg powered by 15amp circuit breaker
Describe C207 trim tab
Servo trim tab meaning it moves opposite of elevator
Describe C207 landing gear
Fixed tricycle landing gear, steerable nose wheel, hydraulically actuated disc brakes and oleo
struts
Correct Answers
Describe C207 engine
Teledyne Continental IO-520-F
Horizontally Opposed
Air Cooled
Naturally Aspirated
Direct Drive
*Fuel Injected, 6 cylinder piston engine.
Describe C207 airframe
All-metal, seven seat, high-wing, single-engine airplane designed for general utility purposes.
Semi-monocoque design covered with aluminum skin
How much fuel can the C207 hold?
Two, 40g tanks for a total of 80g, 73g usable
Describe the C207 fuel system
Fuels flows from
Wing tanks
Reservoir tanks
Fuel selector
Auxiliary fuel pump
Fuel strainer
Engine driven fuel pump
Fuel air control unit
Fuel manifold
What does Fuel Injection consist of?
Engine driven fuel pump
Fuel/Air control unit
Fuel manifold
, Fuel flow indicator
Air bleed type injector nozzles
What should you do if you run one tank completely dry?
PSS (Pitch Switch Switch)
What is PSS acronym?
Pitch - for best glide - (80 KIAS w/flaps up or 85 with 10º)
Switch - the fuel selector to the opposite tank
Switch - turn on the emergency fuel pump for 3-5 seconds with throttle ½ open
Describe C207 electrical system
28v direct current electrical system driven by a 60amp alternator with a 12v battery
What does the Primary BUS power?
All aircraft lights
Pitot heat/stall system
Turn coordinator Ignition switch
Fuel quantity indicators
CHT indicators
Flap system
Aux fuel pump
What does the Electronic BUS power?
GPS
Capstone
Com 1 & 2
Nav 1 & 2
Describe C207 flaps
Electric single slotted flaps 0-30deg powered by 15amp circuit breaker
Describe C207 trim tab
Servo trim tab meaning it moves opposite of elevator
Describe C207 landing gear
Fixed tricycle landing gear, steerable nose wheel, hydraulically actuated disc brakes and oleo
struts
