11-251 Flashcards

(52 cards)

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
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)
Landing gear, 60%
26
Normally, the rollout point is approximately _____ to _____ feet AGL at _____ to _____ NM from the threshold. (AETCMAN 11-251V1 4.5.4)
300-390 feet AGL, 1.0-1.3 NM from the threshold
27
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)
2/3 to ensure 3000’, abeam to ensure 6,000’
28
The vertical velocity will eventually indicate _____ the pattern altitude. (AETCMAN 11-251V1 4.5.4.1.3)
Double
29
What three criteria must be met to consider the final turn “made”? (AETCMAN 11-251V1 4.5.4.1.3)
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
Once established on final, what is normal vertical velocity? (AETCMAN 11-251V1 4.5.4.2)
700-900 fpm
31
How far down the runway is the normal “shift”? (AETCMAN 11-251V1 4.7.1.2)
100-200 feet
32
How far from the threshold is the normal power reduction to idle? (AETCMAN 11-251V1 4.7.2.1.3)
300-500 feet
33
What is considered “fully flared”? (AETCMAN 11-251V1 4.7.2.1.4)
20-25 KCAS below approach speed
34
What is the normal landing zone? (AETCMAN 11-251V1 4.7.2.3)
150-1000 feet down the runway
35
How is normal landing distance calculated? (AETCMAN 11-251V1 4.8.3)
2500+Gas+Touchdown distance
36
What are the T-38 Groundspeed checks at the 3/2/1 boards? (AETCMAN 11-251V1 4.9.2)
90 GS / 60 GS / 30 GS
37
Keep the stick full aft until _____ KIAS to maximize aerodynamic deceleration. (AETCMAN 11-251V1 4.9.2)
50 KIAS
38
When do crosswind procedures go into effect? What are crosswind procedures? (AETCMAN 11-251V1 4.11)
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
For a crosswind landing, what flight control inputs should be made? (AETCMAN 11-251V1 4.11)
Aileron into the wind, rudder to maintain centerline/proper track down the runway.
40
Applying crosswind landing procedures may increase landing distance by approx. ______%.
50%. (AETCMAN 11-251V1 4.11)
41
Normal spacing for a No-Flap Pattern is approx. ____ NM. (AETCMAN 11-251V1 4.12.1)
1.5 NM
42
What does No-Flap configuration do to your landing distance? (AETCMAN 11-251V1 4.12.3.3)
Doubles the landing distance i.e. [2500+Gas+Landing Dist.] x2
43
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)
500 feet
44
During a practice single-engine approach, the simulated inoperative engine is set to no less than _____% RPM. (AETCMAN 11-251V1 4.14.1)
60%
45
If a single-engine pattern is practiced from an overhead, use both engines until _______.
Rolling out on final. (AETCMAN 11-251V1 4.14.2)
46
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)
MIL
47
An actual stall may be preceded by what two aerodynamic indications? (AETCMAN 11-251V1 4.16.2.1
1. Heavy, low frequency buffet | 2. Moderate wing rock (in most cases)
48
An actual stall may indicated by what three things? (AETCMAN 11-251V1 4.16.2.1)
1. Very high sink rate 2. Heavy buffet 3. High AoA (Above 1.0)
49
Describe the different types of typical Airframe Buffet: (AETCMAN 11-251V1 4.16.2.2)
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
What situations would require an immediate stall recovery in the pattern? (AETCMAN 11-251V1 4.16.3.1)
1. Definite Increase in Buffet Intensity (DIBI) 2. Aural, HUD, or MFD stall warning 3. Excessive Sink Rate
51
What are the immediate actions of the stall/sink recovery? (AETCMAN 11-251V1 4.16.3.1)
1. Advance both throttles to MAX 2. Relax backstick pressure as required 3. Roll wings level
52
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)
Rolling flaps to 60%