Limitations 2023 Flashcards

1
Q

Wingspans A319,A320

A

111 feet, 10 inches

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2
Q

Wingspan A320 Sharklet and A321 Sharklet

A

117 Feet, 5 inches

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3
Q

Tailstrike A319 Strut Compressed

A

13.9 degrees

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4
Q

Tailstrike A320,A320 NEO Strut Compressed

A

11.7 degrees

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5
Q

Tailstrike A321 Strut Compressed

A

9.7 degrees

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6
Q

Tailstrike A319 Strut Extended

A

15.5 degrees

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7
Q

Tailstrike A320 Strut Extended

A

13.5 degrees

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8
Q

Tailstrike A320 NEO Strut Extended

A

13.7 degrees

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9
Q

Tailstrike A321 Strut Extended

A

11.2 degrees

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10
Q

Maximum certified altitude

A

FL398

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11
Q

Runway slope (mean)

A

+/- 2%

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12
Q

Runway Altitude

A

9,200 feet

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13
Q

Normal runway width

A

45m (148 feet)

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14
Q

Maximum demonstrated crosswind (takeoff and landing)

A

38 knots (guest included)

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15
Q

Maximum tailwind for takeoff

A

15 knots

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16
Q

Maximum tailwind for landing

A

10 knots

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17
Q

Maximum wind for passenger door operation

A

65 knots

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18
Q

Cockpit window open max speed

A

200 knots

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19
Q

Maximum speed with landing gear extended (VLE)

A

280 knots / M.67

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20
Q

Maximum speed landing gear extension (VLO)

A

250 Knots / M.60

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21
Q

Maximum speed landing gear retraction (VLO retract)

A

220 Knots / M.54

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22
Q

Maximum tire speed (ground speed)

A

195 knots

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23
Q

When the taxi weight is higher than 167,550 pounds (76,000kg) taxi speed should not exceed during a turn

A

20 knots

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24
Q

Wipers maximum operating speed

A

230 knots

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25
Maximum landing weight A320 NEO
148,591 pounds
26
Maximum landing weight A320
145,505 pounds
27
Maximum landing weight A319
137,788 pounds
28
Maximum landing weight A321
171,519 pounds
29
APU bleed use with air start unit
APU bleed should not be used at the same time when using a HP air start unit.
30
Maximum cabin pressure positive differential pressure
9.0 PSI
31
Maximum cabin pressure negative differential pressure
-1.0 PSI
32
Cabin pressure safety relief valve pressure setting is
8.6 PSI
33
Pack use with LP air conditioning unit
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.
34
Minimum hight Auto Pilot usage Circling Approach
600ft AGL | -100 feet
35
Minimum height Auto Pilot usage ILS approach with CAT 2 or 3 (single or dual) is displayed on the FMA
0ft AGL if autoland
36
Minimum hight Auto Pilot usage at Go-Around (AP or FD engagement)
100 feet AGL
37
Minimum hight Auto Pilot usage All other phases of flight
500 feet AGL (A319,A320) 900 feet AGL (A321) | 900 feet AGL (A321)
38
Use of the AP or FD in open DES or DES mode is not permitted in approach, unless the FCU altitude is set at or above.
Highest of: Minimum or 500 feet (A319,A320) 900 feet (A321)
39
NAV mode maybe used in the terminal area provided that
- GPS primary is available - The appropriate RNP is checked or entered on the MCDU, and high accuracy is displayed or - FMS navigation is cross checked with nav aid raw data
40
If one engine is inoperative, it is NOT permitted to use the autopilot to perform non-precision approaches in the following modes
FINAL APP, NAV V/S, NAV/FPA only FD use is permitted
41
Power plant EGT limits for (502-656,690-694) | A319,A320
Takeoff go around All engines 5 min, EGT 635 Takeoff go around One engine 10 min, EGT 635 Takeoff go around MCT No limit EGT 610 Starting on ground 635 Starting in air 635
42
Power plant EGT limits for (657-687) A321 ceo
Takeoff go around All engines 5 min, EGT 650 Takeoff go around One engine 10 min, EGT 650 MCT No limit, EGT 610 Start on the ground 635 Start in flight/ground 635
43
Power plant EGT limits for (901-986) A320 NEO
Takeoff go around all engines 5min, EGT 1083 Takeoff go around one engine 10 min, EGT 1083 Takeoff go around MCT no limit EGT 1043 Start on the ground/air 1083
44
Minimum starting oil temperature (N502NK-N698NK) (901-986)
-40 c
45
Minimum oil temperature before IDLE is exceeded (N502NK-N698NK)
-10 c
46
What is considered a engine start cycle for (502-698)
A standard automatic start that includes only one start attempt, is considered one cycle
47
Starter limits (502-698) CEO
- One start is one cycle - ground starts (automatic or manual), 15 s pause between successive cycles - 30 minute cooling period after 3 failed cycles or 5 minutes of continuous crank - For manual start, observe a 2 minute maximum cycle time - For crank, observe a 5 minute maximum cycle time - The starter must not be run when N2 is above 10% on the ground and 18% inflight
48
What is considered a engine start cycle for (901-986)
A standard automatic start that includes up to 2 start attempts, is considered one cycle
49
Starter limits (901-986) NEO
- 2 starts is 1 cycle - For ground start (automatic or manual) a 35 second pause is required between successive cycles - A 15 minute cooling period is required, subsequent to 3 failed cycles, or 15 minute of continuous or cumulative crank - Starter must not be run when N2 is above 20%
50
Minimum speed for max reverse
70 knots, Idle reverse is permitted down to aircraft stop.
51
Maximum fuel imbalance INFLIGHT and at LANDING Inner tanks (outer tanks balanced) Tank fuel quantity (heavier tank) (502-536 / 601-656 / 690-698 / 901-928)
3,306 pounds
52
Maximum fuel imbalance at TAKEOFF Wing Tanks (657-687) A321
882 pounds
53
Minimum fuel quantity for TAKEOFF
3,307 pounds
54
Maximum brake temperature for takeoff
300 c
55
CG limits
Clean configuration.........-1.0g to +2.5g Other configuration............0g to +2.0g
56
Takeoff is NOT permitted on which runway conditions
Wet Ice
57
Takeoff is NOT recommended on which runway conditions
Water on top compact snow Dry snow Wet snow over ice
58
Maximum Operating speed Vmo/Mmo
Vmo............350kt Mmo.............M0.82 | Mom............M0.82
59
Can the APU be started and operated even if the LOW OIL LEVEL ECAM advisory is displayed
Yes, maintenance action is required within the next 10 hours of APU operation
60
How many start attempts on the APU
After three consecutive APU start attempts, the Flight Crew must wait 60 min before a new start attempt.
61
Engine Start crosswind max speed
Engine is able to start in crosswind up to 35kt
62
Maximum operating altitude with slats and/or flaps extended
20,000ft
63
Fuel Imbalance at TAKEOFF: Inner Tanks (Outer Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-990)
Maximum Asymmetry 1,102 LB
64
Fuel Temperature
For JET A only, if TAT reaches -34 c, monitor on FUEL SD page that fuel temperature remains higher than -36 C
65
Automatic Approach, Landing, and Rollout ILS Category II Minimum Decision height?
100 feet AGL
66
Special Authorization CAT II (SA CAT II) Minimum decision height?
100 feet AGL
67
Other than standard CAT II (OTS CAT II) minimum decision height?
100 feet AGL
68
ILS Category III FAIL Passive (single) minimum decision height?
50 feet AGL
69
ILS Category III Fail Operational (DUAL) Alert height?
100 feet AGL
70
CAT III without DH: Minimum Runway Visual Range?
300 RVR
71
Maximum one tire per gear is deflated (consider three gear) Maximum taxi speed during turn?
7 knots
72
If two tires are deflated on the same main gear (maximum one main gear) Maximum taxi speed?
3 knots
73
For the nose wheel steering (NWS) angle Maximum NWS angle with damage tire?
30 degrees
74
Nosewheel steering (NWS) Maximum NWS angle?
+/- 85 degrees
75
ENG oil quantity 502-698 CEOs
(V2500): Check that the oil quantity is at or above 11 qt. + estimated consumption (average estimated consumption ~ 0.3 qt./h).
76
ENG oil quantity check for (PW1100G):
Above 14 quarts, if OTS -30 Check that the oil quantity is at, or above 16.5 quarts
77
Airflow supplied by the ground cart shall not exceed?
2.60 lb/s
78
MAX continuous load per TR?
200 AMP
79
Hydraulic system normal operating pressure?
3,000 PSI +/- 200 PSI
80
Max altitude for APU start (on A/C power) and operations?
FL410
81
Minimum use of autopilot ILS approach when CAT1 is displayed on the FMA
160 ft AGL
82
Minimum use of autopilot in approach with FINAL APP, V/S, or FPA mode?
250 ft AGL
83
When is reduced thrust at takeoff not permitted?
Contaminated runways, when outside temperature is within 10 degrees of flex temperature.
84
Autopilot Minimum ILS CAT 1 on FMA
160 AGL
85
A321 NEO Max Landing Weight
**174,606**