Checkrid Flashcards

1
Q

What engines are on N6914L?

A

Continental IO-470V6B, 260HP each

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2
Q

What is the useable fuel?

A

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

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3
Q

What is Vso?

A

Stall Speed in Landing Configuration
Bottom of white arc
75 mph

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4
Q

What is the max gross weight?

A

5200lbs

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5
Q

What is Vmca?

A

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

80 mph

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6
Q

What is Vr?

A
Rotation Speed (max performance)
84 mph
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7
Q

What is Vs1?

A

Clean
Stall speed
85 mph

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8
Q

Vr (Normal Takeoff)?

A

Rotation Speed

90 mph

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9
Q

What is Vx?

A

Best Angle of Climb

97 mph

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10
Q

What is 1.3 Vso?

A

Reference Speed for final approach 1.3 x Vso

98 mph

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11
Q

What is Vapp?

A

Approach Speed

105 mph

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12
Q

What is Vxse?

A

Best Single Engine angle of climb

108 mph

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13
Q

What is Vapp (se)?

A

Approach Speed Single Engine

110 mph

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14
Q

What is Vglide?

A

Glide speed with both props feathered

110 mph

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15
Q

What is 1.3 Vs1?

A

1.3x

111mph

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16
Q

What is Vyse (blue line)

A

Best Single Engine Rate-of-Climb

120 mph

17
Q

What is Vy?

A

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

18
Q

What is Vcc?

A

Cruise climb

140mph

19
Q

What is Vlo/le

A

Landing gear operation or extension.

140 mph

20
Q

What is Va?

A

Maneuvering Speed?

170 mph at 5200 lbs

21
Q

What is Vfle?

A

Flaps extended 15 degrees

180 mph

22
Q

Explain Maximum Performance Takeoff

A
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
23
Q

Explain Procedure for Engine Failure During Flight

A

?

24
Q

Explain Single Engine Approach and Landing

A

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

25
Q

10 Factors used to determine Vmc?

A
  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.
26
Q

What is the procedure for the Vmc Demo?

A
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
27
Q

What is the procedure for engine failure on takeoff?

A

Power up (forward, forward, forward)

Clean up (flaps and gear)

Identify
Verify
Feather