Dash One Sxn 6 Flashcards

1
Q

What does the stab augmentor system do?

A

Automatically damps out yaw short period oscillations

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2
Q

In what Mach range may abrupt forward or aft ddeflection (pulsing) of the stick cause over-G?

A

Mach 0.80-0.95

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3
Q

What does the bobweight do?

A

It is a part of the horizontal tail control system and it increases stick forces under g loads but the pilot will not feel the effect of it until the aircraft responds to the stick movement.

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4
Q

How much stick travel provides 1/2 aileron deflection? Full aileron deflection?

A

4.5 inches for 1/2 aileron; 1.5 inches more for full deflection (6 inches total)

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5
Q

What does having an external store do?

A

Shifts CG forward, which results in increased rotation and liftoff speeds, less trim authority, less aerobraking and flare deceleration, and higher aft stick forces

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6
Q

What is the best airspeed to maintain at a minimum until configuring for maneuvering and handling qualities?

A

300 KCAS

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7
Q

Where do minimum stick forces per g occur?

A

At approximately Mach 0.9

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8
Q

Where can you have severe pilot induced oscillations?

A

High subsonic low altitude flight

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9
Q

How should you fix pilot induced oscillations if you encounter them?

A

Release the stick to allow the aircraft to damp itself out, or if at low altitude or close to another aircraft, hold back pressure on the stick. Also reducing a/s will help

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10
Q

What’s more effective at low AOA?

A

Ailerons

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11
Q

What’s more effective at high AOA?

A

Rudders

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12
Q

What’s a caution with using rudder with the gear down?

A

Using sustained 30 deg rudder deflection at high AOA may result in violent roll and engine flameout

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13
Q

What limits should you use to evaluate an over-g for jetwash?

A

Asymmetric

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14
Q

What indicates the stall for this aircraft the most?

A

A very high sink rate and airframe buffet

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15
Q

How should you correct post stall gyrations?

A

Neutralize the controls smoothly until the aircraft recovers

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16
Q

How do you do a high-speed dive recovery?

A

Throttles IDLE, open speed brake, level wings, pull with sufficient g to recover

17
Q

Do spins every happen in this aircraft?

A

No. Test pilots couldn’t do it Would need abrupt application of aft stick at close to maximum rates within an impossible envelope.

18
Q

What is the primary anti-spin control?

A

Aileron

19
Q

How do you recover from an impossible-to-get-into spin?

A

Full aileron in direction of spin and as much aft stick as possible, rudder full opposite of turn, do not change configuration, and neutralize controls after recovery

20
Q

How do you recover from an inverted spin?

A

Neutralize all flight controls

21
Q

For a high Mach 60 deg dive altitude loss includes what time allowance?

A

4 sec for load factor to build up to 4 Gs

22
Q

Initiate dive recovery for a high speed dive recovery NLT what?

A

26,400’ for 45,000’ entry and 27,800’ for 50,000’ entry

23
Q

What determines the subsonic lift limit? Supersonic lift limit?

A

Buffet; horizontal tail deflection