Lim A320 Flashcards
(96 cards)
1
Q
FLIGHT MANEUVERING LOAD ACCELERATION LIMITS. Clean configuration?
A
-1 g to +2.5 g
2
Q
FLIGHT MANEUVERING LOAD ACCELERATION LIMITS. Other configuration?
A
0g to +2 g
3
Q
Runway slope (mean) limitation
A
±2 %
4
Q
Runway altitude limitation
A
9200 ft
5
Q
Nominal runway width
A
45 m
6
Q
Minimal runway width
A
30 m
7
Q
Maximum demonstrated crosswind (takeoff and landing)
A
38kn (gust included)
8
Q
Maximum tailwind for takeoff.CEO
A
15 kn
9
Q
Maximum tailwind for takeoff. NEO
A
10 kn
10
Q
Maximum tailwind for landing. All
A
15 kn
11
Q
The maximum wind for passenger door operation is
A
65kn
12
Q
The maximum wind for FWD and AFT cargo door operation is
A
40 kt (or 50 kt, if the aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side)
13
Q
The FWD and AFT cargo doors must be closed before the wind speed exceeds
A
65 kn
14
Q
COCKPIT WINDOW OPEN MAXIMUM SPEED
A
200 kn
15
Q
Maximum speed with the landing gear extended (VLE)
A
280 kn/M 0,67
16
Q
Maximum speed at which the landing gear may be extended (VLO extension)
A
250 kn/M.60
17
Q
Maximum speed at which the landing gear may be retracted (VLO retraction)
A
220 kn /M 0.54
18
Q
Maximum ground speed
A
195kn
19
Q
MINIMUM CONTROL SPEED FOR LANDING (VMCL)
A
115 kn
20
Q
MINIMUM CONTROL SPEED FOR LANDING (VMCL) CEO
A
114 kn
21
Q
WIPERS MAXIMUM OPERATING SPEED
A
230 kn
22
Q
With passengers on board, it is not recommended to exceed ____ min without air conditioning supply.
A
20 min
23
Q
The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time?
A
Yes
24
Q
Maximum positive differential pressure
A
9,0 PSI
25
Maximum negative differential pressure
-1,0 PSI
26
Safety relief valve setting
8,6 PSI
27
The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time?
Yes
28
The autopilot can be used with the following minimum values: at take off
100 ft AGL and at least 5 s after liftoff
29
The autopilot can be used with the following minimum values: In approach with F-G/S mode
200 ft AFL
30
The autopilot can be used with the following minimum values: In approach with FINAL APP, V/S or FPA mode
250 ft AGL
31
The autopilot can be used with the following minimum values: in circling approach
500 ft AGL for aircraft category C (600 ft AGL for aircraft category D)
32
The autopilot can be used with the following minimum values: After a manual go-around
100 ft AGL
33
The autopilot can be used with the following minimum values: In all other phases
900 ft AGL. The AP or FD in OP DES or DES mode can be used in approach. However, its use is only permitted if the FCU selected altitude is set to, or above, the higher of the two: MDA/MDH or 900 ft AGL
34
NAV mode may be used after takeoff provided that:
‐ GPS PRIMARY is available, or
‐ The flight crew checked the FMGS takeoff updating.
35
NAV mode may be used in terminal area provided that:
‐ 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.
36
DEGRADED SITUATION
If GPS PRIMARY LOST is displayed on the ND and MCDU, the navigation accuracy remains sufficient for RNP operations provided that…
the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed.
37
RNAV APPROACH
An RNAV(RNP) approach may be performed, with GPS PRIMARY not available…3
…only if the radio navaid coverage supports the RNP value and HIGH accuracy is displayed on the MCDU with the specified RNP, and an operational approval is obtained.
38
ILS CATEGORY II. Minimum decision height.
100 ft
39
S CATEGORY II. At least one autopilot must be engaged in APPR mode, and…
…CAT 2 or CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA.
40
ILS CATEGORY II. For manual landing, AP should be disconnected no later than…
80 ft AGL
41
ILS CATEGORY III FAIL PASSIVE (SINGLE). Minimum decision height…
50 ft. A/THR must be used in selected or managed speed.
42
ILS CATEGORY III FAIL PASSIVE (SINGLE). At least one autopilot must be engaged in APPR mode, and…
…CAT 3 SINGLE or CAT 3 DUAL must be displayed on the FMA.
43
ILS CATEGORY III FAIL OPERATIONAL (DUAL). Alert height…A/THR…, autopilots…
100 ft AGL. A/THR must be used in selected or managed speed. Both autopilots must be engaged in APPR mode, and CAT 3 DUAL must be displayed on the FMA
44
ILS CATEGORY III FAIL OPERATIONAL (DUAL). CAT III without DH:
Minimum Runway Visual Range(NEO)…
75 m
45
ILS CATEGORY III FAIL OPERATIONAL (DUAL). CAT III with DH:
Minimum Decision Height (CEO)…/CAT III without DH:
Minimum Runway Visual Range
22ft/75m
46
ENGINE-OUT. CAT II and CAT III fail passive autoland are only approved in
configuration 3 and FULL, and if engine-out procedures are completed before reaching 1 000 ft in approach.
47
MAXIMUM WIND CONDITIONS FOR ILS/MLS CAT II OR CAT III AND FOR GLS CAT I(CEO) HEADWIND?
‐ 40 kt for CAT II automatic approach
‐ 30 kt for CAT III and GLS CAT I automatic approach
‐ 30 kt for automatic landing and automatic rollout
48
MAXIMUM WIND CONDITIONS FOR ILS/MLS CAT II OR CAT III AND FOR GLS CAT I (CEO) TAILWIND?
10 kn
49
MAXIMUM WIND CONDITIONS FOR ILS/MLS CAT II OR CAT III AND FOR GLS CAT I (CEO). CROSSWIND
‐ 25 kt for CAT II automatic approach
‐ 20 kt for CAT III and GLS CAT I automatic approach
‐ 20 kt for automatic landing and automatic rollout
50
After ______ consecutive APU start attempts, the flight crew must wait ____min before a new start attempt.
Three attempts…60min
51
APU Maximum N speed
107%
52
Maximum EGT for APU start (below 35 000 ft)
1090 C
53
Maximum EGT for APU start (above 35 000 ft)
1 120 °C
54
Maximum EGT for APU running
675 C
55
During refuel/defuel procedures, APU starts or shutdown are permitted with the following restrictions:
‐ If the APU failed to start or following an automatic APU shutdown, do not start the APU
‐ If a fuel spill occurs, perform a normal APU shutdown
56
APU BLEED
Max altitude to assist engine start
20 000ft
57
APU BLEED. Max altitude for air conditioning and pressurization (single pack operation)
22500 ft
58
APU BLEED. Max altitude for air conditioning and pressurization (dual pack operation)
15000 ft
59
Use of APU bleed air for wing anti-ice is ____ permitted.
NOT
60
The BACF results should not be used in the case of:
‐ Any failure impacting aircraft performance during landing (brakes, engines, aerodynamics...) or,
‐ Runways with an average slope greater than 1 % (uphill or downhill).
61
It is prohibited to use the GSM Onboard System:
‐ Below 3 000 m AGL (approximately 10 000 ft)
‐ In some geographical areas
Note:
The GSM Onboard System is able to identify the above-mentioned flight conditions. If the system identifies any of these conditions, it automatically turns off.
62
THRUST SETTING/EGT LIMITS (NEO). Takeoff (1) and Go-around
All engines operative TIME? EGT?
5 minutes, 1083 C
63
THRUST SETTING/EGT LIMITS (NEO). Takeoff (1) and Go-around. One eng. inoperative. Time? EGT?
10 minutes. 1083 C
64
Maximum Continuous Thrust (MCT) (NEO). Time? EGT?
Not limited. 1043 C
65
(NEO) THRUST SETTING/EGT LIMITS. Engines. Starting. On ground. In flight. EGT?
1083 C
66
(CEO) THRUST SETTING/EGT LIMITS. Takeoff and Go-around. All engines operative. Time? EGT?
5 minutes. 650 C
67
(CEO) THRUST SETTING/EGT LIMITS. Takeoff and Go-around. One engine inoperative. Time? EGT?
10 minutes. 650 C
68
(CEO) Maximum Continuous Thrust (MCT). Time? EGT?
Unlimited. 610 C
69
(CEO) Starting. On ground/in flight . EGT?
635 C
70
(NEO) Maximum N1 in normal operation./ Maximum N1 permitted
100%/105%
71
(NEO) Maximum N2 in normal operation./ Maximum N2 permitted
100%/105%
72
(CEO) Maximum N1/ Maximum N2
100%/100%
73
(CEO) Maximum continuous oil temperature
155 C
74
CEO. Maximum transient oil temperature 15 minutes
165 C
75
CEO. Minimum starting oil temperature
-40 C
76
CEO. Minimum oil temperature before idle is exceeded
- 10 C
77
CEO. Minimum oil temperature before take off
50 C
78
CEO. Minimum oil quantity
11 qt + estimated consumption. Average estimated consumption 0.3q/h
79
CEO. Minimum oil pressure
60 PSI
80
NEO. Maximum temperature
151 C
81
NEO. Minimum starting temperature
- 40 C
82
NEO. Minimum temperature before take off
52 C
83
NEO. Oil quantity (OAT >- 30 C)
14qt
84
NEO. Oil quantity (OAT <- 30 C)
16,5 qt
85
NEO. Minimum oil pressure
65 PSI
86
NEO. Maximum oil pressure
270 PSI
87
A standard automatic start that includes up to two start attempts, is considered ___ cycle
One
88
NEO. For ground starts (automatic or manual), a ___s pause is required between successive cycles
15
89
NEO. A ____min cooling period is required, subsequent to _____failed cycles, or ____ min of continuous or cumulated crank
15/three/15
90
NEO. The starter must not be run when N2 is above____ %.
20
91
CEO. For ground starts (automatic or manual), a ____s pause is required between successive cycles
15
92
CEO. A ____min cooling period is required, subsequent to ______ failed cycles or ___min of continuous crank
30 / three / 5
93
Engines. For manual start, observe a ____-minute maximum cycle time
Two
94
Engines. For crank, observe a ___ min maximum cycle time
5
95
Engines. The starter must not be run when N2 is above ____% on-ground and ____% in-flight.
10/ 18
96
Maximum reverse should not be used below ___ kt. Idle reverse is permitted down to __________.
70/ aircraft stop
