Limitations 2017 Flashcards
1
Q
Flight Maneuvering Load Acceleration Limits
A
Clean configuration. . . . . . . . . . . . . . . . . . . . -1.0g to +2.5g
• Slats and flaps extended . . . . . . . . . . . . . . . . . 0g to +2.0g
• Slats extended and flaps retracted . . . . . . . . 0g to +2.0g
2
Q
Maximum Certified Altitude
A
FL398
3
Q
Runway slope
A
+/-2%
4
Q
Runway Altitude
A
9,200 ft
5
Q
Nominal Runway Width
A
45 m (148 ft)
6
Q
Maximum demonstrated crosswind at landing
A
38 kt (gust included)
7
Q
Maximum tailwind for takeoff
A
15 kt
8
Q
Maximum tailwind for landing
A
10 kt
9
Q
Maximum wind for passenger door operation
A
65 kt
10
Q
Maximum certified crosswind for takeoff NEO
A
35 kt (gust included)
11
Q
Max with landing gear extended (VLE)
A
280 kt/M.67
12
Q
Max landing gear extension (VLO Extension)
A
250 kt/M.60
13
Q
Max landing gear retraction (VLO Retraction)
A
220 kt/M.54
14
Q
Maximum Tire Speed
A
Ground speed. . . 195 kt
15
Q
Windshield Wipers In Use
A
Max speed . . . . . . . 230 kt
16
Q
Cockpit Window Open
A
Max speed. . . . 200 kt
17
Q
Airflow supplied by the ground cart shall not exceed
A
2.60 lb/s.
18
Q
Max positive differential pressure
A
9.0 PSI
19
Q
Max negative differential pressure
A
-1.0 PSI
20
Q
Safety relief valve setting
A
8.6 PSI
21
Q
Minimum Height For Use Of Autopilot
A
- After take/off with SRS mode 100 ft AGL
- Straight-in non-precision approach Applicable Minimum
- Circling Approach
- Applicable Circling Minimums - 100 ft.
- ILS approach when CAT 2 or CAT 3 is not displayed on the FMA 160 ft AGL
- Go-Around (AP or FD engagement) 100 ft AGL
- All other phases 500 ft AGL (A319/A320) 900 ft AGL (A321)
- 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 ft (A319/A320) Minimum or 900 ft (A32
22
Q
Takeoff with SRS mode
A
An internal FMGS logic prevents the autopilot from engaging during the 5 seconds after liftoff.
23
Q
NAV mode may be used in the terminal area, provided:
A
- GPS PRIMARY is available, or
- HIGH accuracy is displayed, and the appropriate RNP is
checked or entered on the MCDU, or - FMS navigation is cross-checked with NAVAID raw data.
24
Q
Minimum decision height CATII
A
100ft
25
CATIII Minimum Runway Visual Range
75m
26
MAX continuous load per generator
100% (90 KVA)
27
MAX continuous load per TR (continuous)
200 A
28
Max operating altitude with slats and/or flaps extended is
20,000ft
29
The minimum fuel quantity for takeoff is
3307 lb and the WING TK LO LVL warning must not be displayed on the ECAM.
30
Tanks must be emptied in the following order:
Center tank then wing tanks. T/O on center tank prohibited
31
Hydraulic system normal operating pressure
3,000 PSI ± 200
32
Maximum brake temperature for takeoff (brake fans (if installed) off)
300°C
33
The nosewheel steering angle is limited to
75° when using the handwheels
34
For towing and pushback, the nosewheel steering angle is limited to
95 degrees
35
Towbarless towing and pushback on the nose landing gear is approved for the “accepted towbarless towing vehicles,” but the nosewheel steering angle must be limited to
85 degrees
36
APU Starter
After 3 starter motor duty cycles, wait 60 min before attempting 3 more cycles.
37
APU Rotor Speed
Maximum N (ECAM display) . . . . . . . . . . . . . 107 %
38
The APU automatically shuts down at
107 % N speed
39
Engine oil temperature minimum prior to exceeding idle
-10 °C
40
Engine oil temperature minimum prior to takeoff
50 °C
41
Engine oil maximum continuous temperature
155 °C
42
Engine oil maximum transient temperature (15 min)
165 °C
43
Minimum Engine oil starting temperature
-40 °C
44
Engine oil minimum Oil Quantity V2500, PW1100G
- 11 quarts, (average estimated consumption
~ 0.3 qt./h)
- (PW1100G) 14 quarts
45
Engine minimum Oil Pressure
65 PSI (N901NK THRU N905NK)
46
Engine maximum oil pressure
270 PSI
47
Reverse Thrust limitations
- Maximum reverse should not be used below 70 kt (or when the airspeed indication starts to fluctuate). Idle reverse is permitted down to aircraft stop.
48
FLEX thrust
Takeoff at reduced thrust is not permitted on contaminated runways.
49
Crosswind Operation on Ground engine start
This engine is capable of starting in crosswinds up to 35 kt.
50
Crosswind Takeoff max CEO
38 kt (gust included)
51
A319, A320 Wingspans
- Wing 111'10
52
A320, A321 Sharklet dementions
- Wing 117'5 Difference
53
How man seats A320/A320 Shark Fins/A320 Neo
- 178/182
| - NEO 182
54
How man seats A319
- 145
55
How man seats A321
- 218
56
How man seats A321 Shark Fins
- 228
57
Max landing weight A320/A320 shark fins
- 145,505
58
Max landing weight A319
- 137,788
59
Max landing weight A321/A21 shark fins
- 171,519
60
Max landing weight A320 Neo
- 148,591
61
Max Taxi Speed
- 167,550 lbs 20 KTS in a turn
62
Air Conditioning with LP Ground unit?
- Do not use conditioned air simultanously from PACKS and LP ground unit (to avoid chattering of non-return values)
63
APU with HP ground unit?
- Do not use HP ground unit when the APU supplies bleed air to avoid bleed system damage.
64
Max tail wind for CAT II, III?
- 5 knots (surface winds)
65
Max head wind for CAT II,III?
- 15 knots (surface winds)
66
Max fuel imbalance takeoff (A320-s, A320-NEO) (Outer tanks balanced)?
- Inner tanks: Heavier tank full 1,102
67
Max fuel imbalance in flight for landing? (A320-S, A320-NEO) (Outer tanks balanced)?
- Inner tanks: Heavier tank full 3,306
68
Max fuel imbalance landing (wing tanks) A321?
- Inner tanks: heavier tank full 2,910
69
Max fuel imbalance takeoff (wing tanks) A321-S?
- Inner tanks heavier tank full 882
70
Max Altitude for APU Start (on A/C power) and Operation
FL410
71
EGT Limit for Starting (CEO)
635 C
72
EGT Limit for Starting (A320-NEO)
1083 degrees C
73
EGT Limit for TOGA (A319/A320-CEO)
635 C (5 min/10 min in case of engine failure)
74
EGT Limit for TOGA (A321)
650 C (5 min/10 min in case of engine failure)
75
EGT Limit for TOGA (NEO)
1083 C (5 min/10 min in case of engine failure)
76
EGT Limit for MCT (CEO)
610 C
77
EGT Limit for MCT (NEO)
1043 C
78
Max Reverse Thrust should not be used below:
70 knots
79
Max reverse should not be used when (A319/A320):
Airspeed indication starts to fluctuate.
80
Reduced thrust takeoff is not permitted:
On contaminated runways.
81
Tailstrike Pitch Attitude A319 L/G Struts Compressed?
13.9 Degrees
82
Tailstrike Pitch Attitude A320 L/G Struts Compressed?
11.7 Degrees
83
Tailstrike Pitch Attitude A320 NEO L/G Struts Compressed?
11.7 Degrees
84
Tailstrike Pitch Attitude A321 L/G Struts Compressed?
9.7 Degrees
85
Max airport elevation for Cat II or Cat III Conf full or 3
5,575 Feet
86
Is Flex takeoff allowed on contaminated runway?
NO TOGA only
