Limitations Flashcards

1
Q

Max operating Alt
Max Alt w/ flaps/slats
Max Alt for gear extension

A

39,000
20,000
25,000

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2
Q

RVSM MAX in flight difference between captain and FOs

A

200

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3
Q

Max Op AS (SL-FL246)
Max Op Mach# (>FL246)

A

350kts
.82

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4
Q

Max wind for TO &Landing
Max Tailwind for TO
1. 320/321 w/IAE
2. 319/320/321 w/CFM
Max Tailwind for landing
1. Sharklet
2. Non-Sharklet

A

50kts

10kts
15kts

15kts
10kts

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5
Q

Min height for AP
TAKEOFF
LANDING

A

100’
80’ on ILS W/ CAT2,CAT3 single/dual on FMA

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6
Q

What Temperature is the bench mark for engine run ups in icing conditions

A

3C

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7
Q

How long are Engine run-ups when in icing conditions and below 3C.

A

Check AOM 15.8 for different Eng

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8
Q

What is the difference between a blue and red depression route?

A

Blue-elevation < 15000
Red-elevation > 15000

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9
Q

Depression routes allow aircraft to descend to what altitude in what amount of time

A

10000msl
12 min

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10
Q

With A/THR engaged when is A/THR available and Manual Thrust Availabe

A

A/THR— CLB to FLIGHT IDLE
MAN THRUST— Above CLB

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11
Q

Why is APU required for single engine taxi

A

If there was an engine fire electrical power would be only battery power after ENG FIRE button pushed. This results in only 1 fire bottle being available

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12
Q

When is the reactive wind shear detection available?

A

3sec after liftoff to 1300’
1300’ to 50’ RA

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13
Q

Where is CB PANEL GUIDE

A

QRH 21-3

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14
Q

EMERGENCY EQUIPMENT DIAGRAMS ARE FOUND

A

AIM Chapter 20

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15
Q

WHEN DONWE NEED TO ALTERNATE & what are DISTANCES
319
320/321

A

WX is to bad to return to airport single engine or using temporary electric lights
373
368

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16
Q

RTO Prior to 80kts and after

A

Before 80kts reject for engine fire, failure, warning, tire failure, exam warning or caution, strange vibration or noise

After 80kts to V1 engine failure, fire, PWS,or if aircraft feels unsafe to fly

17
Q

After RTO Consider

A

AOM 6.4.5
Aircraft condition
Clear runway
Disarm brakes by releasing spoilers
Brake cooling
AML entry

18
Q

Auto thrust changes to Descent when

A

•With in 200nm of Des
•If Descent is selected below 200’
•at TODescent

19
Q

When App Phase is activated the managed target speed becomes?

A

VAPP but in managed speed it will not decelerate below configuration speed
Clean=GD
CONF 1= S
CONF 2/3=F
FULL= VAPP

20
Q

Thrust lock activates when

A

When 1 TR is in CLB with 2 eng running or MCT with 1 eng running and A/THR button is pushed or disconnects due to failure

21
Q

Incorrect altimeter settings affect altitude in what way?

A

Alt setting is lower than published you will be high if alt setting is higher than published you will be low.