Limitations & Memory Items Flashcards

1
Q

Memory item

Loss of Breaking

A

1) Thrust levers……….……Max reverse (as reqd)
2) Break pedals…………..……….………release
3) A/SKID & NWS switch………………………….OFF
4) Brake pedals…………….APPLY (max 1000psi)
5) Parking Brake (if required)……………………USE
NOTE: Use short successive parking brake applications to stop the aircraft.

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2
Q

Memory Item

CAB PR EXCESS CAB ALT
or
Rapid Depressurization

A

1) Oxygen mask……………………On
2) Crew Communications………Establish

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3
Q

Maximum Takeoff and Landing Tailwind Component

A

10 knots, or as permitted by the Company Pages. (A319/320)

15 knots, or as permitted by the Company Pages. (A321/A321NEO)

Note: Flaps FULL recommended when landing with tailwinds greater than 10 knots.

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4
Q

Delta A319/A320/321 crosswind limit for takeoff and landing

A

38 kts (including gust)

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5
Q

Maximum operating altitude

A

39,100 feet pressure altitude

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6
Q

Simultaneous use of AC packs and _________ is prohibited.

A

LP ground air
(External A/C)

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7
Q

Minimum Altitude For Use of Autopilot(s)

A

The minimum altitude for autopilot engagement during takeoff and manual go-around is 100 feet AGL and at least 5 seconds after lift off.

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8
Q

Flight Controls

A

Do not extend the flaps/slats above FL200.

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9
Q

Emergency Evacuation Flow/Philosophy

These evacuation flow items are not included within the EVACUATION checklist. They are meant to refresh the logical pattern and procedures that must occur for a successful evacuation. In the unlikely event that the checklist cannot be read due to smoke/fire, darkness, injury or incapacitation, this simple flow or philosophy should lead the pilot to completion of all critical task contributing to the safe as possible evacuation.

A

STOP
CONFIGURE
SHUTDOWN
EVACUATE

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10
Q

Severe Turbulent Air Penetration

A

Below 20,000 feet:
A319 255 Kts
A320 250 Kts
A321 270 Kts
A321NEO 275 Kts

At or above 20,000 feet:
A319 280 Kts
A320 275 Kts
A321 300 Kts
A321NEO 305 Kts
*until intercepting 0.76 Mach.

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11
Q

Memory Item

Unreliable Airspeed Indication

A

> If the safe conduct of the flight is impacted:
1)AP…………………………..……………..……..,OFF
2) A/THR……………………………………….…………OFF
3) FD………………………………………………..………OFF
4) PITCH/THRUST
Below THR RED ALT………………….…15°/TOGA
Above THR RED ALT & Below FL100…10/CLB
Above THR RED ALT & Above FL100….5/CLB
5) FLAPS
{If CONF 0(1)(2)(3)}…..MAINTAIN CURRENT CONFIGURATION
6) FLAPS
{If CONF FULL}………….SELECT CONF 3 & MAINTAIN
7) SPEEDBRAKES…………….CHECK RETRACTED
8) L/G…………………………………………………………UP
9) When at or above MSA or pattern altitude:
Level off for troubleshooting.

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12
Q

Engine warm-up and cooldown times

A

Warm-up is 2 and 5 minutes (more than 2hrs after shutdown)

Cool down is 3 minutes (mandatory for the NEO)

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13
Q

Min engine oil quantities

A

CEO (All models):
9.5 qts + .5 qts per hour of flight for est. consumption

NEO:
14 qts (ambient temps above -30° C)
16.5 qts (ambient temps below -30° C)

ENG FADEC GND PWR button on overhead to view

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14
Q

CG Speedbreaks limitation for decent

A

On decent in A319/A321NEO speedbreaks not authorized below 240 kts if CG is above 35%.

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15
Q

LO/ECON PACK flow limits

A

A319/320- Pack flow to LO if 138 SOB or less
A321/A321NEO- Pack flow to ECON if 168 SOB or less

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