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LIMITATIONS - MEMORY ITEMS -PROFECIENCY > Proficiency items > Flashcards

Proficiency items Flashcards

1
Q

Aircraft type versus tail number

COM 3.1.7

A

A319 502NK to 536NK

A320 601NK to 656 NK
A320 NEO 901NK to 905NK
A320 690NK to 694NK

A321 657NK to 687NK

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2
Q

Wingspans

COM 3.1.8

A

Not sharklets 111 feet 10 inches

Sharklets 117 feet 5 inches

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3
Q

Tailstrikes Pitch attitudes

COM 3.1.8

A

A310-320 Pitch 10’
A321 Pitch 7.5’

                   Compress.           
A319              13.9                       
A320              11.7
A320 NEO    11.7                     
A321                9.7
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4
Q

Max Certified Alt

COM 3.1.9

A

FL 398

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5
Q

Minimum runway width

COM 3.1.12

A

148 feet (45 meters)

98 feet reduced ops

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6
Q

Maximum Runway alt

COM 3.1.12

A

9200 feet

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7
Q

Runway Slope

Com 3.1.12

A

+2 /-2 %

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8
Q

Maximum X-wind

COM 3.1.12

A

For To and Lnd

38 kts

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9
Q

Max tailwind for TO

COM 3.1.12

A

15kts

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10
Q

Max Tailwind for Lnd

COM 3.1.12

A

10kts

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11
Q

Max wind for Passengers door operations

A

65 kts

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12
Q

Max Speed with gear extended

COM 3.1.16

A

280 kts or .67M

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13
Q

Max speed for gear extension

COM 3.1.16

A

250kts or .60M

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14
Q

Max speed gear retraction

COM 3.1.16

A

220 kts .54M

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15
Q

Max altitude for gear

COM 3.1.16

A

25.000 feet

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16
Q

Max Tire speed

COM 3.1.16

A

195 kts

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17
Q

Max speed for cockpit window

A

200 kts

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18
Q

Taxi Speed

COM 3.1.17

A

10 kts if making a 90’ or more turn
30 kts straight
20 kts in turn if weight <167.550 pounds

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19
Q

max windshield wipers speed

COM 3.1.17

A

230kts

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20
Q

Max landing weight

A

A319 137.788
A320 145.505
A320 NEO 148.591
A321 171.519

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21
Q

APU Bleed Use with Air Start unit

A

The Flight Crew must not use bleed air from the APU BLEED and from
the HP Air Start Unit at the same time, to prevent any adverse effect
on the Bleed Air System.

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22
Q

Cabin Pressure

A
  • Max positive differential pressure. . . . . . . . . . . . . . . . . . 9.0 PSI
  • Max negative differential pressure . . . . . . . . . . . . . . . . . -1.0 PSI
  • Safety relief valve setting . . . . . . . . . . . . . . . . . . . . . . . . . . 8.6 PS
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23
Q

Packs Use With LP Air Conditioning Unit

A

The Flight Crew must not use conditioned air from the packs and
from the LP Air Conditioning Unit at the same time, to prevent any
adverse effect on the Air Conditioning system.

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24
Q

Autopilot

Minimum Height For Use Of Autopilot

Take Off with SRS mode

A

100 ft AGL

Note: Takeoff with SRS mode - An internal FMGS logic prevents the
autopilot from engaging during the 5 seconds after liftoff.

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25
Q

Autopilot

Straight in non precision app

COM 3.1.44

A

Applicable minimum

26
Q

Autopilot

ILS app when CAT2 or CAT3 not display

COM 3.1.44

A

160 ft AGL

27
Q

Autopilot

Go Around

COM 3.1.44

A

AP or FD engagement 100 Ft AGL

28
Q

Autopilot

All other phase

COM 3.1.44

A

500 feet AGL (A319-A320)

900 feet AGL (A321)

29
Q

Autopilot

Use of AP or FD in OPEN DES or DES mode is not permitted in APP unless the FCO is set at or above

COM 3.1.44

A

Highest of:

Minimum or 500 ft AGL (319-320)
Minimum or 900 ft AGL (321)

30
Q

FD must be selected off when

A

Reaching MDA
Or
300 ft AGL on a RNAV visual

31
Q

Nag Mode may be used in terminal area provided that:

A
  • GPS Primary is available, or
  • The appropriate RNP is checked or entered on the MCDU, and
    HIGH accuracy is displayed, or
  • FMS navigation is crosschecked with navaid raw data.
32
Q

One Engine Inop approach Limitations:

A

A319 &A321

If one engine is inoperative, it is not permitted to use the autopilot to
perform NPAs in the following modes: FINAL APP, NAV V/S, NAV/
FPA.
Only FD use is permitted

33
Q

APU Start Limitations:

COM 3.1.57

A

After three consecutive APU start attempts, the Flight Crew must wait
60 min before a new start attempt.

34
Q

ENGINE ITT limits:

A

A319 & A320 - 635 TO/GA (5 min/10 min), 610 MCT, 635 start.
A321 - 650 TO/GA (5 min/10min0,610 MCT, 635 Start.
A320 NEO - 1083 TO/GA (5 min/10 min), 1043 MCT, 1083 Start.

35
Q

Oil Temperature

A

-40 Start
-10 Idle
+50 To
+155 max
+165 Transiant (15min)

36
Q

Oil Pressure

COM 3.1.69 & 3.1.70

A

60 Psi Classic

65 Psi NEO

37
Q

Starter engagement

A
  • A standard automatic start that includes only one start attempt, is considered one cycle
  • For ground starts (automatic or manual), a 15 s pause is required
    between successive cycles
  • A 30 min cooling period is required, subsequent to three failed
    cycles or 5 min of continuous crank
  • For manual start, observe a two-minute maximum cycle time
  • For crank, observe a 5 min maximum cycle time
  • The starter must not be run when N2 is above 10 % on-ground and
    18 % in-flight
38
Q

Starter engagement NEO

A
  • A standard automatic start that includes up to three start
    attempts, is considered one cycle
  • For ground starts (automatic or manual), a 35 s pause is required
    between successive cycles
  • A 15 min cooling period is required, subsequent to three failed
    cycles, or 15 min of continuous or cumulated crank
  • The starter must not be run when N2 is above 20%.
39
Q

Reverse Thrust

A

Maximum reverse should not be used below 70 kt. Idle reverse is
permitted down to aircraft stop

40
Q

Flex To not permitted:

A

On contaminated runway.
More than 25% derated
Temp is within 10’c of Flex
APG says so

41
Q

Max X-wind for engine start

A

35kts

42
Q

Max altitude for flaps

A

20.000 ft

43
Q

Fuel temperature

COM 3.1.76

A

For JET A only, if TAT reaches -34 °C, monitor on FUEL SD page
that fuel temperature remains higher than -36 °C

44
Q

Max fuel imbalance at TO

COM 3.1.80 & 3.1.81

A

882 (A321) or 1102

45
Q

Max fuel imbalance at LND

COM 3.1.80 & 3.1.81

A

2910 (A321) or 3306

46
Q

Brake Temp

A

Maximum brake temperature for takeoff . . 300 °C

150 if brake fan ON

47
Q

Takeoff at reduced thrust is not permitted:

A
  • On contaminated runways.
  • For known windshear conditions.
  • When a Special Departure Procedure specifies
    full thrust for takeoff.
  • When a deferred maintenance item per the MEL
    requires full thrust for takeoff.
  • When the flex temp is within 10 0C of actual OAT.
48
Q

AOM 2.121.26

Takeoff Performance Data Validity

A
  • If there is a tailwind component, takeoff performance data must
    indicate tailwind data.
  • Actual QNH is no less than takeoff data QNH minus 0.10”.
  • Actual OAT is no less than takeoff data OAT minus 10°C.
  • Actual takeoff weight is less than or equal to MTOW.
49
Q

Emergency Descent

A

MEMORY ITEMS

  1. CREW OXY MASKS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .USE
  2. SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
  3. EMER DESCENT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . INITIATE
  4. THR LEVERS (if A/THR not engaged). . . . . . . . . . . . . . . . . . . . IDLE
  5. SPD BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FULL

6 min to descend to 18.000 then 12min @ 18000 then 30 min at 14.000

50
Q

EGPWS WARNING

A

Simultaneously:
- Pull to full backstick and maintain in that position.
- Aircraft achieve the best climb performance when the wings
are as level as possible.
- If the “TERRAIN TERRAIN PULL UP” or “TERRAIN AHEAD
PULL UP” or “OBSTACLE OBSTACLE PULL UP” or
“OBSTACLE AHEAD PULL UP” aural alert triggers, a turning
maneuver can be initiated if the Flight Crew concludes that
turning is the safest action. The PULL UP maneuver must be
performed before the turn toward the safe direction, as climbing
increases the terrain clearance.
Apr 16, 2018MEMORY & PROFICIENCY ITEMS
A320 Series 3.2.4
MEMORY ITEMS

• AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• PITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL UP
(Pull to full backstick and maintain in that position.)
• THRUST LEVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TOGA
• SPEED BRAKES lever . . . . . . . . . . . . . . . CHECK RETRACTED
• BANK . . . . . . . . . . . . . . . . . . . . . . . . . WINGS LEVEL or ADJUST

51
Q

Loss of Braking

A

• REV . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX
• BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE
• A/SKID & N/W STRG. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• BRAKE PEDALS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
• MAX BRK PR. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1,000 PSI
• PARKING BRAKE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. . . . . . . . . . . . . . .SHORT AND SUCCESSIVE APPLICATIONS

52
Q

TCAS RA

A

• AP (if engaged) . . . . . . . . . . . . . . . . .. . . . . . .OFF
• BOTH FDs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . .OFF
• ATC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .NOTIFY
Note: Respect stall, GPWS, or windshear warning

53
Q

Unreliable Speed Indication/ADR Check Procedure

A

If the safe conduct of the flight is impacted:
• AP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• A/THR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• FD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
• PITCH/THRUST:
- Below THRUST RED ALT . . . . . . . . . . . . . . . . . . . . . . . .15°/TOGA
- Above THRUST RED ALT and Below FL 100. . . . . . . . .10°/CLB
- Above THRUST RED ALT and Above FL 100. . . . . . . . . . 5°/CLB
• FLAPS (if CONF 0(1)(2)(3)). . . . . . MAINTAIN CURRENT CONF
• FLAPS (if CONF FULL) . . . . . SELECT CONF 3 AND MAINTAIN
• SPEEDBRAKES . . . . . . . . . . . . . . . . . . . . CHECK RETRACTED
• L/G . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP

54
Q

Windshear Ahead

A

Before TO & TO roll: Delay/reject

When airborne: Thrust Lever … TOGA
AP (if engaged) … Keep On
SRS orders … Follow

Landing: Go Around … Initiate
AP (if engaged) … Keep On

Note: - Autopilot disengages if the angle of attack value goes
above α prot.
- If the FD bars are not displayed, move toward an initial
pitch attitude of 17.5°. Then, if necessary, to prevent a
loss in altitude, increase the pitch attitude

55
Q

WINDSHEAR

RED “windshear, windshear,windshear”

A

If before V1: Reject

After V1: Thrust levers … TOGA
At Vr … Rotate
SRS orders … Follow

Airborne, Initial climb or landing:
Thrust Levers … TOGA
AP (if engaged) … Keep On
SRS orders … Follow

Note: - Autopilot disengages if the angle of attack value goes
above α prot.
- If the FD bars are not displayed, move toward an initial
pitch attitude of 17.5°. Then, if necessary, to prevent a
loss in altitude, increase the pitch attitude

56
Q

STALL WARNING AT LIFT OFF

A
  1. THRUST. . . . . . . . . . . . . . . . . . . . . . . . . . TOGA
  2. PITCH ATTITUDE . . . . . . . . . . . . . . . . . . .15°
  3. BANK . . . . . . . . . . .. . . . . . . . . . . . . WINGS LEVEL
57
Q

Stall recovery

A
  1. Nose Down Pitch Control … Apply
  2. Bank … Wings Level
    when out of Stall:
    Thrust Increase Smoothly as needed
    Speed brakes … Check Retracted
    Flight Path … Recover Smoothly

if below 20.000 feet: Flaps 1 … Select

58
Q

Severe Turbulence

A
  1. SIGNS . . . . . . . . . . . . . . . . . . . . . . .. . . . . . ON
  2. AUTO PILOT. . . . . . . . . . . .. . . . … . . KEEP ON
  3. A/THR (when thrust changes become excessive) . . DISCONNECT
  4. TURBULENCE SPEED. (275 .76)..SET
    Do Not Chase
  5. Descent……………………………………….Consider
  6. For Approach………AT keep on (in manage speed)
  7. For Landing.
    Flaps 3 less drag more energy, Flaps full better protection
59
Q

Crew Incapacitation

A

Call lead FA

60
Q

One engine INOP Obstacle / STD

A
  1. Thrust set MCT
  2. Auto Thrust disconnect
  3. ATC notify
  4. Decelerate/ Descent: Green Dot / 300 .78M
  5. Engine out cruise altitude figure out.
  6. Start ECAM actions.

LIMITATIONS - MEMORY ITEMS -PROFECIENCY (1 decks)

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