Limitations 2019 Flashcards
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
5
Q
Tailstrike A321 strut Compressed
A
9.7
6
Q
Tailstrike A319 strut extended
A
15.5
7
Q
Tailstrike A320 strut extended
A
13.5
8
Q
Tailstrike A320 NEO strut extended
A
13.7
9
Q
Tailstrike A321 strut extended
A
11.2
10
Q
Maximum certified altitude
A
FL398
11
Q
Runway slope (mean)
A
+/- 2%
12
Q
Runway Altitude
A
9,200 feet
13
Q
Normal 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 altitude landing gear may be extended
A
25,000 feet
23
Q
Maximum tire speed (ground speed)
A
195 knots
24
Q
When the taxi weight is higher than 167,550 pounds (76,000kg) taxi speed should not exceed during a turn
A
20 knots
25
Wipers maximum operating speed
230 knots
26
Maximum landing weight A320 NEO
148,591 pounds
27
Maximum landing weight A320
145,505 pounds
28
Maximum landing weight A319
137,788 pounds
29
Maximum landing weight A321
171,519 pounds
30
APU bleed use with air start unit
APU bleed should not be used at the same time when using a HP air start unit.
31
Maximum cabin pressure positive differential pressure
9.0 PSI
32
Maximum cabin pressure negative differential pressure
-1.0 PSI
33
Cabin pressure safety relief valve pressure setting is
8.6 PSI
34
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.
35
Minimum hight Auto Pilot usage at takeoff with SRS
100 feet AGL
36
Minimum hight Auto Pilot usage Straight-in non-precision approach
Applicable minimums
37
Minimum hight Auto Pilot usage Circling Approach
Applicable circling minimums
| -100 feet
38
Minimum hight Auto Pilot usage ILS approach with CAT 2 or 3 is NOT displayed on the FMA
160 Feet AGL
39
Minimum hight Auto Pilot usage at Go-Around (AP or FD engagement)
100 feet AGL
40
Minimum hight Auto Pilot usage All other phases of flight
500 feet AGL (A319,A320)
| 900 feet AGL (A321)
41
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)
42
Takeoff with SRS mode
An internal FMGS logic prevents auto pilot from engaging during the 5 seconds after liftoff
43
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
44
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
45
Honeywell APU Maximum altitude assisted engine start
20,000 feet
46
Hamilton APU maximum altitude engine start
20,000 feet
47
Hamilton APU maximum altitude air conditioning and pressurization single pack
20,000 feet
48
Hamilton APU maximum altitude air conditioning and pressurization dual pack
15,000
49
Is APU bleed air able to be used for wing anti ice
NO
50
Honeywell APU maximum altitude air conditioning and pressurization single pack
22,500 feet
51
Honeywell APU maximum altitude air conditioning and pressurization dual pack
15,000
52
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
53
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
54
Power plant EGT limits for (901-928) 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
55
Minimum oil temperature (N502NK-N698NK) (901-928)
-40 c
56
Minimum oil temperature before IDLE (N502NK-N698NK)
-10 c
57
Minimum oil temperature before takeoff (N502NK-N698NK)
50 c
58
Max continuous oil temperature (502-698)
155 c
59
Maximum transient oil temperature (502-698)
165 c
60
Maximum oil pressure (502-698)
60 PSI
61
Maximum continues oil temperature (901-928)
151 c
62
Minimum oil temperature before takeoff (901-928)
52 c
63
Minimum oil pressure (901-928)
65 PSI
64
Maximum oil pressure (901-928)
270 PSI
65
What is considered a engine start cycle for (502-698)
A standard automatic start that includes only one start attempt, is considered one cycle
66
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 three 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
67
What is considered a engine start cycle for (901-928)
A standard automatic start that includes up to 2 start attempts, is considered one cycle
68
Starter limits (901-928)
- For ground start (automatic or manual) a 35 second pause is required between successive cycles
- A 15 minute cooling period is required, subsequent to three failed cycles, or 15 minute of continuous or cumulative crank
- Starter must not be run when N2 is above 20%
69
When should max reverse thrust not be used
Below 70 knots, Idle reverse is permitted down to aircraft stop.
70
Maximum altitude flaps/slats extended
20,000 feet
71
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
72
Maximum fuel imbalance at TAKEOFF Wing Tanks (657-687)
882 pounds
73
Minimum fuel quantity for TAKEOFF
3,307 pounds
74
Maximum brake temperature for takeoff
300 c
75
Flight Maneuvering Load Acceleration Limits
Clean configuration.................-1.0g to +2.5g
| Other configuration.................0g to +2.0g
76
Takeoff is NOT permitted on which runway conditions
Wet Ice
77
Takeoff is NOT recommended on which runway conditions
Water on top compact snow
Dry snow
Wet snow over ice
78
Maximum Operating speed Vmo/Mmo
Vmo............350kt
| Mom............M0.82
79
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
80
APU Maximum N Speed
107%
81
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.
82
Engine Start crosswind max speed
Engine is able to start in crosswind up to 35kt
83
Maximum operating altitude with slats and/or flaps extended
20,000ft
84
Fuel Imbalance at TAKEOFF: Inner Tanks (Outer Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-928)
Maximum Asymmetry 1,102 LB
85
Fuel Imbalance at TAKEOFF: Outer Tanks (Inner Tanks Balanced) (502-536 / 601-656 / 690-698 / 901-928)
Maximum Asymmetry 815 LB
86
Fuel Temperature
For JET A only, if TAT reaches -34 c, monitor on FUEL SD page that fuel temperature remains higher than -36 C
