1
Q
Max. Ramp Wt. (ERJ 175 LL)
A
85,450 lb
2
Q
Max. Ramp Wt. (ERJ 175 LR)
A
85,870 lb
3
Q
Max. T/O Wt. (ERJ 175 LL)
A
85,098 lb
4
Q
Max. T/O Wt. (ERJ 175 LR)
A
85,517 lb
5
Q
Max. Lnd. Wt. (ERJ 175 LL & ERJ 175 LR)
A
74,957 lb
6
Q
Max. Zero Fuel Wt. (ERJ 175 LL)
A
69,467 lb
7
Q
Max. Zero Fuel Wt. (ERJ 175 LR)
A
69,886 lb
8
Q
Min. Runway Width
A
100 ft (SW)
9
Q
Min. Taxiway Width
A
50 ft (SW)
10
Q
Wing Span
A
93’ 11’’
11
Q
Aircraft Length
A
103’ 11’’
12
Q
Tail Height
A
32’ 4’’
13
Q
Max. Ops. Alt.
A
41,000 ft
14
Q
Max. T/O & Lnd. Alt.
A
10,000 ft
15
Q
Max. Temp. T/O & Lnd.
A
ISA + 35 C (52 C)
16
Q
Min. Temp. T/O & Lnd.
A
-40 C
17
Q
RWY Slope
A
+/- 2 %
18
Q
Max. Tailwind
A
15 kt
19
Q
Max. Single Pack Operations
A
31,000 ft
20
Q
VMO (SL - 8,000’)
A
300 kt
21
Q
VMO (10,000’ - Mach Transition)
A
320 kt
22
Q
MMO
A
0.82 M
23
Q
VA
A
240 kt
24
Q
VLO EXT
A
250 kt
25
VLE RET
250 kt
26
VLE
250 kt
27
V Tire
195 kt
28
V RAT Deploy Max.
VMO / MMO
29
V Min. (to provide electrical power)
130 kt
30
VB (below 10,000')
250 kt
31
VB (10,000' and above)
270 kt / 0.76 M
32
V Wiper Ops. Max.
250 kt (SW)
33
V Window
160 kt
34
VFE 1
230 kt
35
VFE 2
215 kt
36
VFE 3
200 kt
37
VFE 4
180 kt
38
VFE 5
180 kt
39
VFE Full
165 kt
40
Due to engine compressor stall possibility, static takeoff is not recommended with crosswind component greater than _____?
25 kt
41
T/O Max. Crosswind (Dry)
38 kt (SW)
42
T/O Max. Crosswind (Wet)
31 kt (SW)
43
T/O Max. Crosswind (Compact Snow)
20 kt (SW)
44
T/O Max. Crosswind (Dry Snow / Wet Snow / Slush / Standing Water)
18 kt (SW)
45
T/O Max. Crosswind (Ice)
12 kt (SW)
46
T/O Max. Crosswind (Wet Ice)
Prohibited
47
Lnd. Max. Crosswind
(RCC - 6;
Dry;
BA - Dry)
38 kt
48
Lnd. Max. Crosswind
(RCC - 5;
Frost /
Wet /
1/8'' Depth or Less of: Slush / Dry Snow / Wet Snow;
BA - Good)
31 kt
49
Lnd. Max. Crosswind
(RCC - 4;
Compact Snow (-15 C OAT and colder);
BA - Good to Medium)
20 kt
50
Lnd. Max. Crosswind
(RCC - 3;
Slippery When Wet /
Dry Snow over Compact Snow /
Wet Snow over Compact Snow /
> 1/8'' Depth: Dry Snow / Wet Snow / Compact Snow (Warmer than -15 C);
BA - Medium)
15 kt
51
Lnd. Max. Crosswind
(RCC - 2;
> 1/8'' Water or Slush;
BA - Medium to Poor)
12 kt
52
Lnd. Max. Crosswind
(RCC - 1;
Ice;
BA - Poor)
8 kt
53
Lnd. Max. Crosswind
(RCC - 0;
Wet Ice / Slush over Ice / Water over Compact snow / Dry Snow over Ice / Wet Snow over Ice;
BA - Nil)
Prohibited
54
Max. Alt. Flaps/Slats Extended
20,000 ft
55
CAT II Approach
Mandatory Flaps 5
56
Landing Flaps Full
Go-Around Flaps 4
57
Landing Flaps 5
Go-Around Flaps 2
58
Min. Voltage
22.5 V
59
Max. ITT Start Temp.
815 C
60
Starter Cranking Limit
Engine Start (Ground)
Start # 1 & 2
90 sec ON / 10 sec OFF
61
Starter Cranking Limit
Engine Start (Ground)
Start # 3 - 5
90 sec ON / 5 min OFF
62
Starter Cranking Limit
Engine Start (In Flight)
Start # 1 & 2
120 sec ON / 10 sec OFF
63
Starter Cranking Limit
Engine Start (In Flight)
Start # 3 - 5
120 sec ON / 5 min OFF
64
Dry Motoring Cycle Limit
Motoring # 1
90 sec ON / 5 min OFF
65
Dry Motoring Cycle Limit
Motoring # 2 - 5
30 sec ON / 5 min OFF
66
After five sequential motoring cycles, the process may be repeated following a ____ cool down period.
15 min
67
When it is necessary to perform an engine start with tailwind, monitor ____ indication. When there is no positive increase of ____ indication before starter cutout (____ N2), the engine start must be manually aborted.
N1 / N1 / 50%
68
Takeoff with the Automatic Takeoff Thrust Control System (ATTCS) OFF is ____.
No authorized
69
Max. Fuel Capacity
20,935 lb
70
Max. Imbalance
794 lb
71
Min. Fuel Tank Temp.
-37 C
72
Fuel crossfeed must be selected ____ during takeoff and landing.
OFF
73
Wait ____ after the EICAS is energized to start the APU
30 sec
74
Do not leave the aircraft unattended more than ____ with the APU running (SW).
5 min
75
Simultaneous use of the APU bleed and the ____ is prohibited.
HP cart
76
APU Starter Duty Cycle
Start Attempt 1 & 2
60 sec OFF
77
APU Starter Duty Cycle
Start Attempt 3
5 min OFF
78
Max. APU Start Temp.
ISA + 35 C
79
Min. APU Start Temp.
-54 C
80
Max. APU Start Alt.
30,000 ft
81
Max. APU Continuous Operation Temp.
ISA + 35 C (52 C)
82
Min. APU Continuous Operation Temp.
-54 C
83
Max. APU Continuous Operation Alt.
33,000 ft
84
Max. APU Electrical Generator Use Alt.
33,000 ft
85
Max. APU Engine Start Alt.
21,000 ft
86
Max. APU Bleed Use (for Packs) Alt.
15,000 ft
87
Max. Differential Pressure
8.4 psi
88
Max. Differential Overpressure
8.8 psi
89
Max. Differential Pressure for T/O and Landing
0.2 psi
90
Max. Negative Differential Pressure
-0.5 psi
91
Min. Hydraulic Reservoir Temp. for ENG Start
-18 C
92
Brake temperature indication must be ____ for takeoff
in the green range
93
After selecting reverse thrust, do not move the thrust levers into the forward thrust range until the ____ on the EICAS is shown in ____.
REV icon / amber or green
94
The TO DATASET MENU on the MCDU must be set to ____ when OAT is from 5 C to 10 C and:
- When there is any possibility of encountering visible moisture up to 1,700 ft AFE.
- When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes.
ENG
95
The TO DATASET MENU on the MCDU must be set to ____ when OAT is less than 5 C and:
- When there is any possibility of encountering visible moisture up to 1,700 ft AFE.
- When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engines, nacelles, or engine sensor probes.
ALL
96
In flight, when either one or both ice detectors are failed, the crew must set the anti-ice mode selector to ON when icing conditions exist or are anticipated below ____ with visible moisture.
10 C TAT
97
Min. Autopilot Engagement Height
400 ft
98
Min. Autopilot Use Height on Approach
50 ft HAT
99
TAS, TAT, and SAT information are only valid above ____.
60 kt
100
While transmitting in VHF1, the standby magnetic compass is ____.
not valid
101
The use of predictive EGPWS functions should be ____ when landing at an airport that is not in the database to avoid unwanted alerts.
manually inhibited
102
The use of predictive EGPWS functions must be ____ during QFE operations, when GPS data is unavailable or inoperative. Press in the ____ button to inhibit predictive EGPWS functions.
manually inhibited / GND PROX TERR INHIB
103
RNAV (GPS) LP minima are ____.
not authorized
104
Minimum Fuel (SW)
2,250 lbs (45 min)
105
Emergency Fuel (SW)
1,500 lbs (30 min)
106
Red single side fuel indication
Fuel 660 lbs or less
107
Amber single side fuel indication
Fuel 1,320 lbs or less
108
Red total quantity fuel indication
Fuel 1,320 lbs or less
109
Amber totally quantity fuel indication
2,640 lbs or less
ERJ 175
flashcards
Decks in class (7)
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