Checkrid

Question 1

What engines are on N6914L?

Answer 1

Continental IO-470V6B, 260HP each

Question 2

What is the useable fuel?

Answer 2

130 U.S. Gallons
50 in each main tank
15 in each AUX tank

Question 3

What is Vso?

Answer 3

Stall Speed in Landing Configuration
Bottom of white arc
75 mph

Question 4

What is the max gross weight?

Answer 4

5200lbs

Question 5

What is Vmca?

Answer 5

Minimum Control speed with critical engine out, out of ground effect. (Red Radial)

80 mph

Question 6

What is Vr?

Answer 6

Rotation Speed (max performance)
84 mph

Question 7

What is Vs1?

Answer 7

Clean
Stall speed
85 mph

Question 8

Vr (Normal Takeoff)?

Answer 8

Rotation Speed

90 mph

Question 9

What is Vx?

Answer 9

Best Angle of Climb

97 mph

Question 10

What is 1.3 Vso?

Answer 10

Reference Speed for final approach 1.3 x Vso

98 mph

Question 11

What is Vapp?

Answer 11

Approach Speed

105 mph

Question 12

What is Vxse?

Answer 12

Best Single Engine angle of climb

108 mph

Question 13

What is Vapp (se)?

Answer 13

Approach Speed Single Engine

110 mph

Question 14

What is Vglide?

Answer 14

Glide speed with both props feathered

110 mph

Question 15

What is 1.3 Vs1?

Answer 15

1.3x

111mph

Question 16

What is Vyse (blue line)

Answer 16

Best Single Engine Rate-of-Climb

120 mph

Question 17

What is Vy?

Answer 17

Best Rate-of-Climb
124 mph
Decreasing to 122 mph @ 10,000ft

Question 18

What is Vcc?

Answer 18

Cruise climb

140mph

Question 19

What is Vlo/le

Answer 19

Landing gear operation or extension.

140 mph

Question 20

What is Va?

Answer 20

Maneuvering Speed?

170 mph at 5200 lbs

Question 21

What is Vfle?

Answer 21

Flaps extended 15 degrees

180 mph

Question 22

Explain Maximum Performance Takeoff

Answer 22

15 degrees flaps
Full rich
Fuel pumps on low
Hold the brakes
Full throttles
Lean to rise
Engine instruments in the green
Release brakes
Rotate at 84 mph
Lift off at 93 and climb till clear of obstacles
Gear up, flaps up, pumps off

Question 23

Explain Procedure for Engine Failure During Flight

Answer 23

?

Question 24

Explain Single Engine Approach and Landing

Answer 24

Approach @ 110 mph
Delay Extension of Landing Gear until within Gliding Distance of Field
Avoid use of flaps until landing is assured
Only decrease speed below 105 if landing is certain

Question 25

10 Factors used to determine Vmc?

Answer 25

1. Critical engine windmilling
2. Rt engine is producing max power
3. Airplane is at max gross weight
4. CG is at the rear most limit
5. Flaps in the takeoff configuration
6. Cowl flaps in takeoff configuration
7. Aircraft trimmed for takeoff
8. Aircraft is not in ground effect
9. The gear is up
10. Less than 5 degrees if bank into the good engine.

Question 26

What is the procedure for the Vmc Demo?

Answer 26

Full power
Critical engine to idle
Slow aircraft and pitch up till yaw
Power to idle on good engine
Pitch for Blue Line
Add power on good engine to stop descent
Pitch for Blue Line

Question 27

What is the procedure for engine failure on takeoff?

Answer 27

Power up (forward, forward, forward)

Clean up (flaps and gear)

Identify
Verify
Feather