Limitations Flashcards
1
Q
Manoeuvring Load Acceleration Limit - Clean configuration
A
-1g to +2.5g
2
Q
Manoeuvring Load Acceleration Limit - Other configurations
A
0g to +2g
3
Q
Runway Slope
A
+/- 2%
4
Q
Runway Altitude
A
9200 ft
5
Q
Nominal Runway Width
A
45m
6
Q
Minimal Runway Width
A
30m
7
Q
Max Crosswind (t.o. and ldg)
A
38kt (incl. gust)
8
Q
Max tailwind (ldg)
A
15kt
9
Q
Max wind for pax door operation
A
65kt
10
Q
Max wind for cargo door operation
A
40kt (closed before 65kt)
11
Q
VMO
A
350kt
12
Q
MMO
A
M 0.82kt
13
Q
VLE - Max speed landing gear extended
A
280kt / M0.67
14
Q
VLO extension - Max speed landing gear can be extended
A
250kt / M0.60
15
Q
VLO retraction - Max speed landing gear can be retracted
A
220kt / M0.54
16
Q
Max ground speed (for tires)
A
195kt
17
Q
Max speed to open cockpit window
A
200kt
18
Q
Max taxi speed in a turn (above 76,000kg)
A
20kt
19
Q
Max wiper speed
A
230kt
20
Q
Max taxi weight
A
73,900kg
21
Q
Max take-off weight
A
73,500kg
22
Q
Max landing weight
A
64,500kg
23
Q
Maximum zero fuel weight
A
61,000kg
24
Q
Minimum weight
A
37,230kg
25
Approach Category
C
26
Max recommended time without air conditioning
20 mins
27
APU Bleed use with HP Air Start Unit
Flight crew must not use bleed air from the APU Bleed and from the HP Air Start Unit at the same time to prevent any adverse effect on the Bleed Air System
28
Max cabin positive differential pressure
9.0 psi
29
Max cabin negative differential pressure
-1.0 psi
30
Safety relief valve setting
8.6 psi
31
Max altitude with flaps and slats
20,000ft
32
Max continuous oil temperature
140 degrees
33
Max transient oil temperature (15 min)
155 degrees
34
Minimum starting oil temperature
-40 degrees
35
Minimum oil temperature before take off
-10 degrees
36
Max N1
104%
37
Max N2
105%
38
Minimum fuel quantity for take off
1500 kg
39
Definition of icing conditions
OAT/TAT is at or below 10 degrees and visible moisture in any form is present OR when OAT is at or below 10 degrees on the ground and operating on ramps, taxiways or runways where surface snow, standing water or slush may be ingested by the engines or freeze on engines, nacelles or engine sensor probes
40
Definition of severe ice accretion
when ice accumulation on the airframe reaches approx 5mm thick or more
41
When to use rain repellent
It has been deactivated on the aircraft
42
Maximum brake temperature for take off
300 degrees
43
Max NWS angle
+/- 85 degrees
44
Max crosswind with good ESF
38kt
45
Max crosswind with good to medium ESF
29kt
46
Max crosswind with medium ESF
25kt
47
Max crosswind with medium to poor ESF
20kt
48
Max crosswind with poor ESF
15kt
49
Max Speed config 1
230kt - HOLDING
50
Max Speed config 1+F
215kt - TAKE-OFF
51
Max Speed config 2
200kt - TAKE-OFF/APPROACH
52
Max Speed config 3
185kt - TAKE-OFF/APPROACH/LANDING
53
Max Speed config FULL
177kt - LANDING
54
Autopilot - Take off
100ft AGL and at least 5s after liftoff
55
Autopilot - in approach with FINAL AP, V/S or FPA mode
250ft AGL
56
Autopilot - circling approach
500ft AGL
57
Autopilot - ILS approach CAT1 displayed on FMA
160ft AGL
58
Autopilot - ILS approach CAT 2/ CAT3 displayed on FMA
0ft AGL if autoland
59
Autopilot - after a manual G/A
100ft AGL
60
Max wind conditions for ILS CAT II or ILS CAT III
Headwind 30kt
Crosswind20kt
Tailwind 10kt
61
How many attempts for an APU Start
After 3 consecutive attempts, flight crew must wait 60 mins before the next attempt
62
Avionics ventilation OAT < 49 degrees
No limitation
63
Avionics ventilation
49 < OAT < 55
2 hours
64
Avionics ventilation
55 < OAT < 60
1 hour
65
Avionics ventilation
60 < OAT < 64
0.5 hours
66
Packs use with LP Air Conditioning
Flight crew must not use conditioned air from the packs and form the LP Air Conditioning Unit at the same time to prevent any adverse effect on the Air Conditioning system
67
ILS CAT III Fail operational (dual) with DH - minimum decision height (Jet2)
25 ft
68
ILS CAT III Fail operational (dual) without DH - minimum Runway Visual Range
75 m
69
APU rotor speed - max N speed
107%
70
Highest Altitude
39,800 ft
71
APU Bleed use with HP Air Start Unit
Flight crew must not use bleed air from the APU bleed and from the HP Air Start Unit at the same time, to prevent any adverse effect on the bleed air system
72
Outflow Valve Closure
15,000 ft
73
Max Cabin Alt Selection
14,000 ft
74
Cabin Alt Warning
9550 ft (+- 350 ft)
75
Max Normal Cabin Alt
8000 ft
76
TO and G/A all engines operative time and EGT limit
5 mins
950 degrees
77
TO and G/A OEI time and EGT limit
10 mins
950 degrees
78
Maximum continuous thrust time and EGT limit
time not limited
915 degrees
79
Oil pressure
9.5 qt + estimated consumption
80
Starter - one cycle
A standard automatic start that includes up to three attempts is considered one cycle
81
Cooling period after four failed cycles
15 minutes
82
Time required for ground starts between successive cycles
20 seconds
83
N2 limit for starter
20%
84
Maximum reverse thrust lower limit
70 kt
85
APU Max altitude to assist engine start
20,000 ft
86
APU max altitude for air con and pressurisation (single pack operation)
22,500 ft
87
APU max altitude for air con and pressurisation (dual pack operation)
15,000 ft
88
Definition of thin hoarfrost
White crystalline deposit which usually develops uniformly on exposed surfaces on cold and cloudless nights
So thin that surface features (lines or markings) can be distinguished beneath it
89
Limit for max reverse?
Limit for idle reverse?
Max - 70 kt
Idle - aircraft stop
