Memory Items Flashcards

1
Q

Circle to Land approach maneuver.

A

Wx mins 1000’ ceiling & 3 SM Vis
Or higher if published
MDA of 1,000 ft above the field or higher if published

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2
Q

With engine bleed air switches on, can we operate the packs?

A

With Engine bleed air switches on, do not operate packs in high for takeoff, approach, and landing.

Note: fire protection non-normal procedures take precedence

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3
Q

Holding in icing conditions.

A

No holding in icing conditions with flaps extended

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4
Q

Wing anti ice on the ground.

A

Do not operate wing anti ice on the ground when oat is above 10C

Do not use wing anti ice as a substitute for deicing/anti icing

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5
Q

WX radar on the ground.

A

Do not operate WX radar on the ground during fueling, near fuel spills, or near people

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6
Q

How many amps is one generator limited to on the ground?

A

NG - 215 amps
Max - 215 amps on the ground or in the air

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7
Q

How long to wait after removing power from the aircraft before shutting down the IRS?

A

At least 30 Secs

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8
Q

When can a circuit breaker be reset in-flight?

A

Should only be accomplished when directed by the QRH.

Wait two minutes for cooling before resetting.

May only be reset once.

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9
Q

Maximum EGT for ground start?

A

NG - 725 C
Max - 753 C

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10
Q

Engine warm-up and cooldown time?

A

NG - 2 min warm-up, 1 min cooldown
Max - 3 min warm-up, 3 min cooldown

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11
Q

When is reverse thrust prohibited?

A

In flight
With flaps greater than 10
Below 1,000’ AGL

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12
Q

Max altitude for APU operation?

A

FL410

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13
Q

Max altitude to use APU for Bleed Air & Electric?

A

10,000’

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14
Q

Max altitude for APU for electric only?

A

FL410

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15
Q

Max altitude for APU Bleed Air only?

A

17,000’

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16
Q

Limits on alternate flaps.

A

Alternate flap duty cycle in flight is one complete cycle, then 5 mins off.

(Complete cycle- movement from 0 to 15 and back to 0.

The alternate flap position switch must be in off position for 15 seconds before reversing direction of flap movement.

17
Q

Flap Limitations?

A

Do not extend flaps above 20,000’

18
Q

Speedbrake wing load alleviation system limitation?

A

-700W, do not operate the aircraft in excess of 320 kt at weights over 143,000 lb if the speedbrake wing load alleviation system is inop.

19
Q

Max and min fuel tank temperatures?

A

Max +49 C

Min -37 C

21
Q

How is an upset defined?

A

● Pitch attitude greater than 25° nose up
● Pitch attitude greater than 10° nose down
● Bank angle greater than 45°
● Within above parameters but flying at airspeeds inappropriate for the conditions

22
Q

Terrain Avoidance Manuever

A

● Disengage autopilot (if engaged).
● Disengage autothrottle (if engaged).
● Aggressively apply emergency thrust.
● Simultaneously roll wings level and rotate to an initial pitch
of 20°.
● Retract speedbrakes (if extended).
● If terrain contact is still a threat, continue rotation up to pitch
limit indicator (if installed) or respect the stick shaker or
initial buffet.
● Do not change gear or flap configuration until terrain
separation is assured.
● Monitor radio altimeter for sustained or increasing terrain
separation.
● When clear of terrain, slowly decrease pitch attitude and
accelerate.

23
Q

Wind shear Escape Manuever

A

● Disengage autopilot (if engaged).
● Disengage autothrottle (if engaged).
● Press either TO/GA switch.
● Aggressively apply emergency thrust.
● Simultaneously roll wings level and rotate to an initial pitch
of 15°.
● Retract speedbrakes (if extended).
● Follow flight director TO/GA guidance (if available)1
.
● Do not change flap or gear configuration until windshear
is no longer a factor.
● Monitor vertical speed and altitude.
● Do not attempt to regain lost airspeed until windshear is
no longer a factor

24
Q

What deviations define wind shear?

A

● + or - 15 knots indicated airspeed
● + or - 500 fpm vertical speed
● + or - 5° pitch attitude
● + or - 1 dot displacement from the glideslope
● Unusual thrust lever position for a significant period of time