Limitations Flashcards
1
Q
Max ramp weight
A
84,450 lb (LL) 85,870 lb (LR)
2
Q
Max T/O weight
A
85,098 lb (LL), 85,517 lb (LR)
3
Q
Max Landing weight
A
74,957 lb
4
Q
Max Zero Fuel weight
A
69,467 lb (LL), 69,886 lb (LR)
5
Q
Min Runway Width
A
100 ft (SKW)
6
Q
Min Taxiway Width
A
50 ft (SKW)
7
Q
Wing Span
A
93 ft 11 in
8
Q
Aircraft Length
A
103 ft 11 in
9
Q
Tail Height
A
32 ft 4 in
10
Q
Max Ops Alt
A
41,000 ft
11
Q
Max T/O & Land Alt
A
10,000 ft
12
Q
Max Temp T/O & Land
A
ISA +35C (52C)
13
Q
Min Temp T/O & Land
A
-40*C
14
Q
Runway Slope
A
+/- 2%
15
Q
Max tailwind
A
15 knots
16
Q
Max single pack operations (altitude)
A
31,000 ft
17
Q
Vmo SL - 8000’
A
300 knots
18
Q
Vmo 10,000 ft - Mach Transition
A
320
19
Q
Mmo
A
0.82
20
Q
Va
A
240
21
Q
Vlo ext
A
250
22
Q
Vle ret
A
250
23
Q
Vle
A
250
24
Q
Vtire
A
195
25
V rat deploy max
Vmo/Mmo
26
Vmin (to provide electrical power)
130
27
Vb (below 10,000 ft)
250
28
Vb (10,000 ft and above)
270/0.76M (whichever is lower)
29
V wiper ops max
250 (SKW)
30
Vwindow
160
31
Vfe 1
230
32
Vfe 2
215
33
Vfe 3
200
34
Vfe 4
180
35
Vfe 5
180
36
Vfe FULL
165
37
Crosswind limitation; dry runway
38 kt (SKW)
38
Crosswind limitation; wet
31 kt (SKW)
39
Crosswind limitation; compact snow
20 kt (SKW)
40
Crosswind limitation T/O; dry snow, wet snow, slush, standing water
18 kt (SKW)
41
Crosswind limitation T/O; ice and wet ice
12 kt (SKW)
42
Max Alt Flaps/Slats Extended
20,000 ft
43
CAT II Approach flap setting
Mandatory Flaps 5
44
Min battery voltage
22.5V
45
Engine Start Max ITT
815*C
46
Starter cranking limits: Engine start on the ground
Start 1&2: 90 seconds ON, 10 seconds OFF. Start 3-5: 90 seconds ON, 5 minutes OFF.
47
Starter cranking limits: engine start in flight
Start 1&2: 120 seconds ON, 10 seconds OFF. Start 3-5: 120 Seconds ON, 5 minutes OFF.
48
Dry motoring duty cycle limits
Motoring #1: 90 seconds ON, 5 minutes OFF. Motoring #2-5: 30 seconds ON, 5 minutes OFF. After this the process may be repeated following a 15 minute cool down period.
49
Max fuel capacity
20,935 lb.
50
Max fuel imbalance
794 lb
51
Min fuel tank temperature
-37* C
52
How long to wait before starting the APU after EICAS is energized?
30 seconds.
53
Simultaneous use of the APU bleed and the HP cart?
Prohibited.
54
APU starter duty cycle
Start attempt 1&2: 60 seconds OFF. Start attempt 3: 5 minutes OFF.
55
APU min and max temp: start
-54*C -/ ISA+35
56
APU start max altitude
30,000 ft
57
APU continuous operation min/max temp
-54*C / ISA+35 (52*C)
58
APU continuous operation max altitude
33,000 ft
59
APU continuous operation electrical generator use max altitude
33,000 ft
60
APU continuous operation engine start max altitude
21,000 ft
61
APU continuous operation max altitude bleed use
15,000 ft
62
Max Differential Pressure
8.4 psi
63
Max Differential Overpressure
8.8 psi
64
Max Differential Negative Pressure
-0.5 psi
65
Max Differential Pressure for T/O and Landing
0.2 psi
66
Min hydraulic reservoir temp for engine start
-18*C
67
Go-around after deployment of thrust reversers?
Prohibited
68
When must the TO DATASET MENU be set to ENG?
OAT is from 5*C to 10*C, there is possibility of encountering visible moisture up to 1700 ft AFE , and when operating on ramps, taxiways, runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes. TO DATASET MENU on the MCDU must be set to ENG.
69
When must TO DATASET MENU on the MCDU must be set to ALL?
OAT is less than 5*C, there is possibility of encountering visible moisture up to 1700 ft AFE , and when operating on ramps, taxiways, runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes. TO DATASET MENU on the MCDU must be set to ALL.
70
AP minimum engagement height
400 ft
71
AP minimum use height
50 ft
72
AP minimum use height - Non-Precision Approach
MDA
73
When are TAS, TAT and SAT information valid?
Only valid above 60 knots
74
When is the standby magnetic compass indication not valid?
While transmitting in VHF1.
75
What to verify prior to joining a published segment of an instrument approach?
Verify the NAVAID identification visually displayed matches the chart being used. When the identification is not visually displayed, very that the ID matches the chart being used.
