Limitations Flashcards
(84 cards)
1
Q
Max Takeoff Weight
A
85,517lbs
2
Q
Max Landing weight
A
74,957lbs
3
Q
Max Zero fuel weight
A
69,886lbs
4
Q
Max Aft Cargo
A
2,535lbs
5
Q
Max Forward Cargo
A
3,306lbs
6
Q
Minimum runway width
A
100 Feet (SW)
7
Q
Wing Span
A
93ft 11in
8
Q
Aircraft length
A
103ft 11in
9
Q
Tail Hieght
A
32ft 4in
10
Q
Max Operation Altitude
A
41,000ft
11
Q
Max Takeoff and landing altitude
A
8,000ft
12
Q
Max temp takeoff and landing
A
ISA +35•C (52•C)
13
Q
Min temp takeoff and landing
A
-40•C
14
Q
Runway Slope
A
+/- 2%
15
Q
Max Tailwind
A
15kt
16
Q
Max single pack operation
A
31,000ft
17
Q
VMO SL-8,000’
A
300
18
Q
VMO SL-10,000’- Mach Transition
A
320
19
Q
MMO
A
.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
V Tire
A
195
25
V RAT Deploy Max
VMO/MMO
26
Vmin (to provide electrical power)
130
27
Vb (below 10,000ft)
250
28
Vb (10,000ft and above)
270/.76m (whichever is lower)
29
Vwiper operation max
250 (SW)
30
Vwindow
160
31
VFE 1
230
32
VFE 2
215
33
VFE 3
200
34
VFE 4
180
35
VFE 5
180
36
Flaps Full
165
37
Dry Runway Croswind
38kt
38
Wet Runway Crosswind
31kt
39
Runway with compact snow crosswind
20kt
40
Runway with standing water, slush, wet snow, dry snow crosswind
18kt
41
Runway with ice crosswind
12kt
42
Max altitude flaps/ slats extended
20,000ft
43
Enroute operation slats/ flaps
Prohibited
44
Minimum spoiler speed
180kt
45
Cat II approach slats/ flaps
| What setting?
Mandatory flaps 5
46
Go Around
| Landing Flaps Full
Go around flaps 4
47
Go Around
| Landing flaps 5
Go around flaps 2
48
Battery minimum voltage
22.5v
49
Engine start temp limit max
815c
50
Oil temp start temp minimum
-40c
51
Oil pressure start minimum
25psi
52
Engine start ground cranking limits
Starts 1-2
-90 sec on/ 10 sec off
Starts 3-5
-90 sec on/ 5 min off
53
Starter cranking limits engines (in flight)
Starts 1-2
-120 sec on/ 10 sec off
Starts 3-5
-120 sec on/ 5 min off
54
Dry motoring limits
Motor 1
-90 sec on/ 5 min off
Motor 2-5
-30 sec on/ 5 min off
After 5 cycles the process may be repeated after 15 minutes
55
No N1 % increase manual abort (ground start)
50% N2
56
Fuel capacity total
20,935lbs
57
Max fuel imbalance
794lbs
58
Minimum fuel tank temp
-37c
59
Wait 30 seconds after the EICAS is energized to start the APU
True
60
Simultaneous use of the APU bleed and the HP cart is prohibited
True
61
APU Starter duty cycles
Attempt 1-2
60 sec off
Attempt 3
5 min off
62
APU start temperature min/max
-54c/ ISA + 35
63
APU max start altitude
30,000 ft
64
APU continuous operation min/ max temps
-54c / ISA + 35 (52c)
65
APU operation Max altitude
33,000 ft
66
APU GEN use Max altitude
33,000 ft
67
APU Max altitude bleed use
15,000 ft
68
APU Max altitude engine start
21,000 ft
69
Max differential pressure up to FL370
7.8psi
70
Max differential pressure above FL370
8.34psi
71
Max differential over pressure
8.77psi
72
Max differential negative pressure
-0.5psi
73
Max differential pressure takeoff and landing
0.2 psi
74
Min reservoir temp for engine start (hydraulics)
-18c
75
Autopilot minimum engagement height
400ft
76
Autopilot minimum use height
50ft
77
Autopilot minimum use height on a non precision approach
MDA
78
Between 5-10c the MCDU dataset menu must be set to ENG when visible moisture will be encountered up to 1,700 ft or on the ground at all.
True
79
The MCDU data set menu must be set to ALL if the OAT is less than 5c. Moisture below 1,700ft or on the ground at all
True
80
Max Ramp Weight
85,870lbs
81
LL Max Ramp Weight
85,450
82
LL Max T/O Weight
85,098
83
LL Max Landing Weight
74,957
84
LL Max Zero Fuel Weight
69,467
