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Treatise > 11-251 > Flashcards

11-251 Flashcards

1
Q

On student training sorties, the students are expected to obtain _______. (AETCMAN 11-251V1 1.2.2.2)

A
  1. Relevant NOTAMs
  2. Weather
  3. Airfield Status
  4. Threat of the Day
  5. Emergency Procedure of the Day
  6. Lineup Card
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2
Q

Keep hands clear anytime someone is ________. (AETCMAN 11-251V1 2.4)

A

Underneath the aircraft.

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3
Q

To reduce the risk of FOD during ground operations, do not place object on the ____________ during engine start or while engines are running. (AETCMAN 11-251V1 2.5)

A

Cockpit glareshields

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4
Q

Normally, a power setting less than ______% RPM should be enough to taxi. (AETCMAN 11-251V1 2.6.1)

A

80% RPM

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5
Q

Aircrews should taxi at a moderate speed, normally not greater than ______ knots groundspeed.

A

25 knots GS. (AETCMAN 11-251V1 2.6.2)

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6
Q

When using the brakes, ensure the throttles are in _______. (AETCMAN 11-251V1 2.6.3)

A

Idle

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7
Q

Do not taxi within _____ feet of any obstacle. Do not taxi within ____ feet of an obstacle without a wingwalker. (AETCMAN 11-251V1 2.6.4)

A

10 feet, 25 feet

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8
Q

The maximum allowable error of each altimeter at a known elevation point is _____ feet.

A

75 feet. (AETCMAN 11-251V1 2.7.7)

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9
Q

NAVAID Ground Checkpoint Checks allows a max of ______o CDI error from the depicted course, DME error no greater then ____ NM or ____% of the distance to the facility, whichever is greater.

A

+/- 4o CDI error, DME error no greater than ½ NM or 3% of the distance. (AETCMAN 11-251V1 2.7.11.5)

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10
Q

Ensure the Magnetic Compass is within ____o of a known heading and within ______o of the EHSI readout.

A

5o of a known heading, within 8o of the EHSI. (AETCMAN 11-251V1 2.7.6)

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11
Q

When inspecting the flight control surfaces during the before-takeoff checks, what are the two separate tasks that must be accomplished? (AETCMAN 11-251V1 2.8.3)

A
  1. Visually confirm free and proper movement of the flight control surfaces
  2. Confirm the flight control surfaces return to neutral
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12
Q

Rolling takeoffs can increase takeoff distance by _____ to _____ feet. (AETCMAN 11-251V1 3.2.1)

A

150-300 feet

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13
Q

Pilots should normally initiate backstick pressure at approx. _____ KCAS and set the boresight cross to ______o nose-high on the pitch ladder. (AETCMAN 11-251V1 3.2.4.2)

A

145 KCAS, 7o NH

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14
Q

Nosewheel liftoff will occur at approx. _____ KCAS, and the aircraft should fly off the runway at approx. _____ KCAS, depending on gross weight. (AETCMAN 11-251V1 3.2.4.2)

A

155 KCAS, 165KCAS

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15
Q

Smoothly reduce power out of MAX between _____ and _____ KCAS, and terminate afterburner by _____ KCAS. (AETCMAN 11-251V1 3.3.1)

A

220-280 KCAS, 300KCAS

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16
Q

Accelerate to 300KCAS in MIL power using approx. _____o NH pitch until passing 10,000’ MSL

A

12o NH (AETCMAN 11-251V1 3.3.1)

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17
Q

You may combine the climb check with the level-off check when cruise altitude is at or below _____.

A

FL180. (AETCMAN 11-251V1 3.3.5)

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18
Q

As a technique, begin levelling off upon reaching ____% of the Vertical Velocity Indicator (VVI).

A

10% 🡪 with a VVI of 4000, level off would begin at 400’ prior to altitude. (AETCMAN 11-251V1 3.4)

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19
Q

The priorities for maintaining directional control during an abort are ___________. (AETCMAN 11-251V1 3.6.2)

A
  1. Rudder
  2. Differential Braking
  3. Nose Wheel Steering as a last resort
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20
Q

Can you taxi the T-38 single-engine? Can you exit the runway single-engine if you have downside hydraulics or the landing gear is pinned (barring no greater emergency)? (AETCMAN 11-251V1 3.6.6)

A

No, Yes

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21
Q

Initiate the break turn between _________ and the first ______ feet of the runway. (AETCMAN 11-251V1 4.5.1)

A

The approach end of the runway, 3000’

22
Q

Before initiating the break turn, ensure traffic is ____o off for 3000’ separation or _____ for 6000’.

A

45o off for 3000’, abeam (90o) for 6000’. (AETCMAN 11-251V1 4.5.1)

23
Q

Begin the closed pull-up with a minimum of _____ KCAS and maintain a minimum of _____ until wings-level on downwind. (AETCMAN 11-251V1 4.5.2)

A

240 KCAS, 200 KCAS

24
Q

What is normal no-wind spacing of inside downwind for a 1500’ AGL traffic pattern?

A

1.0-1.3 NM. (AETCMAN 11-251V1 4.5.3)

25
Q

Prior to beginning the final turn, ensure the _______ is down and locked, and the flaps have travelled a sufficient amount to ensure no asymmetry exists, approx. _____%. (AETCMAN 11-251V1 4.5.3)

A

Landing gear, 60%

26
Q

Normally, the rollout point is approximately _____ to _____ feet AGL at _____ to _____ NM from the threshold. (AETCMAN 11-251V1 4.5.4)

A

300-390 feet AGL, 1.0-1.3 NM from the threshold

27
Q

A preceding T-38 should be ____ of the way through the final turn to ensure 3,000’ spacing or _____ to ensure 6,000’ spacing. (AETCMAN 11-251V1 4.5.4)

A

2/3 to ensure 3000’, abeam to ensure 6,000’

28
Q

The vertical velocity will eventually indicate _____ the pattern altitude. (AETCMAN 11-251V1 4.5.4.1.3)

A

Double

29
Q

What three criteria must be met to consider the final turn “made”? (AETCMAN 11-251V1 4.5.4.1.3)

A
  1. Within 30 degrees of alignment with the runway
  2. Less than 30 degrees of bank required
  3. Less than 0.6 AoA required
30
Q

Once established on final, what is normal vertical velocity? (AETCMAN 11-251V1 4.5.4.2)

A

700-900 fpm

31
Q

How far down the runway is the normal “shift”? (AETCMAN 11-251V1 4.7.1.2)

A

100-200 feet

32
Q

How far from the threshold is the normal power reduction to idle? (AETCMAN 11-251V1 4.7.2.1.3)

A

300-500 feet

33
Q

What is considered “fully flared”? (AETCMAN 11-251V1 4.7.2.1.4)

A

20-25 KCAS below approach speed

34
Q

What is the normal landing zone? (AETCMAN 11-251V1 4.7.2.3)

A

150-1000 feet down the runway

35
Q

How is normal landing distance calculated? (AETCMAN 11-251V1 4.8.3)

A

2500+Gas+Touchdown distance

36
Q

What are the T-38 Groundspeed checks at the 3/2/1 boards? (AETCMAN 11-251V1 4.9.2)

A

90 GS / 60 GS / 30 GS

37
Q

Keep the stick full aft until _____ KIAS to maximize aerodynamic deceleration. (AETCMAN 11-251V1 4.9.2)

A

50 KIAS

38
Q

When do crosswind procedures go into effect? What are crosswind procedures? (AETCMAN 11-251V1 4.11)

A

When the crosswind component exceeds 15 knots:

  1. Touchdown on the upwind side
  2. Do not aerobrake, maintain the landing attitude.
  3. Ensure 6000’ spacing between aircraft
39
Q

For a crosswind landing, what flight control inputs should be made? (AETCMAN 11-251V1 4.11)

A

Aileron into the wind, rudder to maintain centerline/proper track down the runway.

40
Q

Applying crosswind landing procedures may increase landing distance by approx. ______%.

A

50%. (AETCMAN 11-251V1 4.11)

41
Q

Normal spacing for a No-Flap Pattern is approx. ____ NM. (AETCMAN 11-251V1 4.12.1)

A

1.5 NM

42
Q

What does No-Flap configuration do to your landing distance? (AETCMAN 11-251V1 4.12.3.3)

A

Doubles the landing distance i.e. [2500+Gas+Landing Dist.] x2

43
Q

When performing an actual or simulated single-engine landing with 60% flaps, the landing roll with be approx. _____ feet longer. (AETCMAN 11-251V1 4.13.2)

A

500 feet

44
Q

During a practice single-engine approach, the simulated inoperative engine is set to no less than _____% RPM. (AETCMAN 11-251V1 4.14.1)

A

60%

45
Q

If a single-engine pattern is practiced from an overhead, use both engines until _______.

A

Rolling out on final. (AETCMAN 11-251V1 4.14.2)

46
Q

Once the simulated single-engine go-around exercise is complete, advance the simulated inoperative engine to _____ prior to coming out of afterburner on the other engine. (AETCMAN 11-251V1 4.14.2)

A

MIL

47
Q

An actual stall may be preceded by what two aerodynamic indications? (AETCMAN 11-251V1 4.16.2.1

A
  1. Heavy, low frequency buffet

2. Moderate wing rock (in most cases)

48
Q

An actual stall may indicated by what three things? (AETCMAN 11-251V1 4.16.2.1)

A
  1. Very high sink rate
  2. Heavy buffet
  3. High AoA (Above 1.0)
49
Q

Describe the different types of typical Airframe Buffet: (AETCMAN 11-251V1 4.16.2.2)

A
  1. Light Buffet = 0.60 AoA 🡪 Optimum Final Turn AoA
  2. Moderate Buffet = 0.70 through DIBI Intensity 🡪 Red Chevron Above Green Donut
  3. Definite Increase in Buffet Intensity (DIBI) >0.80 AoA 🡺 Increase in Amplitude, Decrease in Rate
  4. Heavy Buffet = Higher than DIBI up to Full Aft Stick
50
Q

What situations would require an immediate stall recovery in the pattern? (AETCMAN 11-251V1 4.16.3.1)

A
  1. Definite Increase in Buffet Intensity (DIBI)
  2. Aural, HUD, or MFD stall warning
  3. Excessive Sink Rate
51
Q

What are the immediate actions of the stall/sink recovery? (AETCMAN 11-251V1 4.16.3.1)

A
  1. Advance both throttles to MAX
  2. Relax backstick pressure as required
  3. Roll wings level
52
Q

For a Go-Around from a No-Flap Final Turn, what steps can be taken to minimize the effects of an overshoot? (AETCMAN 11-251V1 4.17.2.2)

A

Rolling flaps to 60%

Treatise (12 decks)

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