Limitations 2023 Flashcards
(113 cards)
1
Q
Wingspans A319,A320
A
111 feet, 10 inches
2
Q
Wingspan A320 Sharklet and A321 Sharklet
A
117 Feet, 5 inches
3
Q
Tailstrike A319 Strut Compressed
A
13.9 degrees
4
Q
Tailstrike A320,A320 NEO Strut Compressed
A
11.7 degrees
5
Q
Tailstrike A321 Strut Compressed
A
9.7 degrees
6
Q
Tailstrike A319 Strut Extended
A
15.5 degrees
7
Q
Tailstrike A320 Strut Extended
A
13.5 degrees
8
Q
Tailstrike A320 NEO Strut Extended
A
13.7 degrees
9
Q
Tailstrike A321 Strut Extended
A
11.2 degrees
10
Q
Maximum certified altitude
A
FL398
11
Q
Runway slope (mean)
A
+/- 2%
12
Q
Runway Altitude
A
9,200 feet
13
Q
Nominal runway width
A
45m (148 feet)
14
Q
Maximum demonstrated crosswind (takeoff and landing)
A
38 knots (guest included)
15
Q
Maximum tailwind for takeoff
A
15 knots
16
Q
Maximum tailwind for landing
A
10 knots
17
Q
Maximum wind for passenger door operation
A
65 knots
18
Q
Cockpit window open max speed
A
200 knots
19
Q
Maximum speed with landing gear extended (VLE)
A
280 knots / M.67
20
Q
Maximum speed landing gear extension (VLO)
A
250 Knots / M.60
21
Q
Maximum speed landing gear retraction (VLO retract)
A
220 Knots / M.54
22
Q
Maximum tire speed (ground speed)
A
195 knots
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
24
Q
Wipers maximum operating speed
A
230 knots
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(N657NK-N687NK)
A321 NEO (N702NK-N715NK)
A321 171,519 pounds
A321 NEO 174,606 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 at takeoff with SRS
100 feet AGL and at least 5 s after takeoff.
35
Minimum hight Auto Pilot usage Straight-in non-precision approach
250 ft
36
Minimum hight Auto Pilot usage Circling Approach
600 ft
37
Minimum hight Auto Pilot usage ILS approach with CAT 2 or 3 (single or dual) is displayed on the FMA
0ft AGL if autoland
38
Minimum hight Auto Pilot usage at Go-Around (AP or FD engagement)
100 feet AGL
39
Minimum hight Auto Pilot usage All other phases of flight
500 feet AGL
40
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.
500ft
41
Takeoff with SRS mode
An internal FMGS logic prevents auto pilot from engaging during the 5 seconds after liftoff
42
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
43
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
44
Honeywell APU Maximum altitude assisted engine start
20,000 feet
45
Hamilton APU maximum altitude engine start
20,000 feet
46
Hamilton APU maximum altitude air conditioning and pressurization single pack
20,000 feet
47
Hamilton APU maximum altitude air conditioning and pressurization dual pack
15,000
48
Is APU bleed air able to be used for wing anti ice
NO
49
Honeywell APU maximum altitude air conditioning and pressurization single pack
22,500 feet
50
Honeywell APU maximum altitude air conditioning and pressurization dual pack
15,000
51
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
52
Power plant EGT limits for (657-687) A321
Takeoff go around All engines 5 min, EGT 650
Takeoff go around One engine 10 min, EGT 650
Takeoff go around MCT No limit, EGT 610
Start on the ground 635
Start in flight 635
53
Power plant EGT limits for (901-986) A320 NEO
Takeoff go around all engines 5 min, EGT 1083
Takeoff go around one engine 10 min, EGT 1083
Takeoff go around MCT no limit EGT 1043
Start on the ground 1083
Start in the air 1083
54
Minimum oil temperature (N502NK-N698NK) (901-986)
-40 c
55
Minimum oil temperature before IDLE (N502NK-N698NK)
-10 c
56
Minimum oil temperature before takeoff (N502NK-N698NK)
50 c
57
Max continuous oil temperature (502-698)
155 c
58
Maximum transient oil temperature (502-698) for 15 Minutes
165 c
59
Maximum oil pressure (502-698)
60 PSI
60
Maximum continues oil temperature (901-986)
151 c
61
Minimum oil temperature before takeoff (901-986)
52 c
62
Minimum oil pressure (901-986)
65 PSI
63
Maximum oil pressure (901-986)
270 PSI
64
What is considered a engine start cycle for (502-698)
A standard automatic start that includes only one start attempt, is considered one cycle
65
Starter limits (502-698)
- For ground starts (automatic or manual), a 15 second pause is required between successive cycles
- A 30 minute cooling period is required, subsequent to 3 failed cycles, or 4 minutes of continuous crank, or 5 min cumulated crank.
- For manual start, Do not exceed the 2 minute maximum cycle time
- The starter must not be run when N2 is above 10% on the ground and 18% inflight
66
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
67
Starter limits (901-986)
- 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%
68
When should max reverse thrust not be used
Below 70 knots, Idle reverse is permitted down to aircraft stop.
69
Maximum altitude flaps/slats extended
20,000 feet
70
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
71
Maximum fuel imbalance at TAKEOFF Wing Tanks (657-687)
882 pounds
72
Minimum fuel quantity for TAKEOFF
3,307 pounds
73
Maximum brake temperature for takeoff
300 c
74
Flight Maneuvering Load Acceleration Limits
Clean configuration.................-1.0g to +2.5g
| Other configuration.................0g to +2.0g
75
Takeoff is NOT permitted on which runway conditions
Wet Ice
76
Takeoff is NOT recommended on which runway conditions
Water on top compact snow
Dry snow
Wet snow over ice
77
Maximum Operating speed Vmo/Mmo
Vmo............350kt Mmo.............M0.82
| Mom............M0.82
78
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
79
APU Maximum N Speed
107%
80
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.
81
Engine Start crosswind max speed
Engine is able to start in crosswind up to 35kt
82
Fuel Imbalance at TAKEOFF: Inner Tanks (Outer Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-986)
Maximum Asymmetry 1,102 LB
83
Fuel Imbalance at TAKEOFF: Outer Tanks (Inner Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-986)
Maximum Asymmetry 815 LB
84
Fuel Temperature
For JET A only, if TAT reaches -34 c, monitor on FUEL SD page that fuel temperature remains higher than -36 C
85
Automatic Approach, Landing, and Rollout ILS Category II Minimum Decision height?
100 feet AGL
86
Special Authorization CAT II (SA CAT II) Minimum decision height?
100 feet AGL
87
Other than standard CAT II (OTS CAT II) minimum decision height?
100 feet AGL
88
ILS Category III FAIL Passive (single) minimum decision height?
50 feet AGL
89
ILS Category III Fail Operational (DUAL) Alert height?
100 feet AGL
90
CAT III without DH: Minimum Runway Visual Range?
300 RVR
91
Maximum one tire per gear is deflated (consider three gear) Maximum taxi speed during turn?
7 knots
92
If two tires are deflated on the same main gear (maximum one main gear) Maximum taxi speed?
3 knots
93
For the nose wheel steering (NWS) angle Maximum NWS angle with damage tire?
30 degrees
94
Nosewheel steering (NWS) Maximum NWS angle?
+/- 85 degrees
95
ENG oil quantity check (V2500)?
(V2500): Check that the oil quantity is at or above 11 qt. +
estimated consumption (average estimated consumption
~ 0.3 qt./h).
96
ENG oil quantity check for (PW1100G):
Above 14 quarts, if OTS -30 Check that the oil quantity is at, or above 16.5 quarts
97
Airflow supplied by the ground cart shall not exceed?
2.60 lb/s
98
MAX continuous load per generator?
100% (90KVA)
99
MAX continuous load per TR?
200 AMP
100
Hydraulic system normal operating pressure?
3,000 PSI +/- 200 PSI
101
Max altitude for APU start (on A/C power) and operations?
FL410
102
Minimum use of autopilot ILS approach when CAT1 is displayed on the FMA
160 ft AGL
103
Minimum use of autopilot in approach with FINAL APP, V/S, or FPA mode?
250 ft AGL
104
When is reduced thrust at takeoff not permitted?
Contaminated runways, when outside temperature is within 10 degrees of flex temperature.
105
Minimal Runway Width
30m, (99ft)
106
The maximum wind for FWD and AFT cargo door operation?
40 Knots, or 50 Knots if aircraft nose is into the wind or if the FWD and AFT cargo doors are on the leeward side. The FWD and AFT cargo doors must be closed before wind exceeds 65 Knots.
107
Maximum Flaps/Slats Speed flaps 1
230kt Holding
108
Maximum Flaps/Slats Speed flaps 1+F
215kt Takeoff
109
Maximum Flaps/Slats Speed flaps 2
200kt Takeoff/Approach
110
Maximum Flaps/Slats Speed flaps 3
185kt Takeoff/Approach/Landing
111
Maximum Flaps/Slats Speed flaps Full
177kt Landing
112
Minimum Control Speed for Landing (VMCL)
VMCL 109kt
113
If the wing fuel temperature exceeds 30C at engine start?
The altitude must be limited to 25,000ft until the center tank is empty.
