0
Q
Max. T/O Wt.
A
85,517 lb
1
Q
Max. Ramp Wt.
A
85,870 lb
2
Q
Max. Lnd. Wt.
A
74,957 lb
3
Q
Max. Zero Fuel Wt.
A
69,886
4
Q
Max. Aft. Cargo
A
2,535 lb
5
Q
Max. Fwd. Cargo
A
3,306 lb
6
Q
Min. Runway Width (SW)
A
100’
7
Q
Max. Ops. Altitude
A
41,000 ft
8
Q
Max. T/O & Lnd.
A
8,000 ft
9
Q
Max. Temp. T/O & Lnd.
A
ISA + 35 C (52 C)
10
Q
Min. Temp. T/O & Lnd.
A
-40 C
11
Q
RWY Slope
A
+/- 2%
12
Q
Max. Tailwind
A
15 kt
13
Q
Max. Single Pack Operations
A
31,000 ft
14
Q
VMO SL- 8,000 ft
A
300
15
Q
VMO 10,000 - Mach Transition.
A
320
16
Q
MMO
A
M 0.82
17
Q
Va
A
240
18
Q
Vlo Ext.
A
250
19
Q
Vle
A
250
20
Q
Vle RET
A
250
21
Q
V Tire
A
195
22
Q
V Rat Deploy Max
A
Vmo/Mmo
23
Q
Vmin (to provide electrical power)
A
130
24
Vb (Below 10,000 ft)
250
25
Vb (10,000 ft and above)
270 / .76M (Whichever is lower)
26
V Wiper Ops. Max. (SW)
250
27
V Window
160
28
VFE 1
230
29
VFE 2
215
30
VFE 3
200
31
VFE 4
180
32
VFE 5
180
33
Flaps Full Speed
165
34
Maximum Recommended Crosswind
38 kt
35
Maximum Recommended Crosswind Wet Runway
31 kt
36
Maximum Recommended Crosswind with Compacted Snow
20 kt
37
Maximum Recommended Crosswind with Standing Water/Slush/Wet Snow/Dry Snow
18 kt
38
Maximum Recommended Crosswind with Ice
12 kt
39
Max. Alt. Flaps/Slats Extended
20,000 Ft
40
Slats/Flaps Enroute Ops.
Prohibited
41
Slats/Flaps Cat II Approach
Mandatory Flaps 5
42
Min. Spoiler Speed
180 kt
43
Slats/Flaps go-Around Landing Flaps Full
Go-Around Flaps 4
44
Slats/Flaps Go-Around Flaps 5
Go-Around Flaps 2
45
Battery Min. Voltage
22.5 V
46
Battery Min. Temp.
-20 C
47
Engine Start ITT Max Temp
815 C
48
Min Oil Temp. Start
-40 C
49
Min. Oil Pressure Start
25 psi
50
Starter Cranking Limits for Start 1 & 2 (Ground)
90 Seconds on 10 seconds off
51
Starter Cranking Limits for Start 3 & 5 (Ground)
90 Seconds On 5 min off
52
Engine Start 1 & 2 Cranking Limits (In Flight)
120 seconds ON 10 seconds OFF
53
Engine Start 3 - 5 Cranking Limits (In Flight)
120 Seconds ON 5 minutes OFF
54
Dry Motoring # 1 Cycle Limit
90 seconds ON 5 minutes OFF
55
Dry Motoring #2-5 cycle limits
30 seconds ON 5 Minutes OFF
56
Ground Start with a Tailwind Limitation.
If no increase in N1 before Starter Cutout (50% N2) Start must be Manually Aborted.
57
Automatic Takeoff Thrust Control System (ATTCS) Limitation.
Takeoff with the ATTCS OFF is not authorized.
58
Max. fuel capacity
20,935 lb
59
Max. Fuel Imbalance
794 lb
60
Min. Fuel tank temp.
-40 C
61
Fuel Crossfeed for Takeoff and Landing Limitation.
Fuel crossfeed must be OFF during take off and landing
62
EICAS Must be Energized for ( ___ ) Before Starting the APU.
30 seconds
63
Simultaneous use of HP air cart and APU bleeds limitation
Not authorized
64
APU Starter Duty Cycle Limit For Start Attempt 1 & 2
60 seconds off
65
APU Starter Duty Cycle Limit For Start Attempt 3
5 minutes OFF
66
APU START Min. And Max. Temperatures.
-54 C and ISA +35 C
67
APU Max. START Altitude Limit
30,000 ft
68
APU Max. Operational Altitude
33,000 ft
69
APU Max. Operational Altitude for Bleed Use.
15,000 ft
70
APU Max. Operational Altitude for Electrical Generator Use
33,000 ft
71
APU Max. Operational Altitude for Engine Start Use
21,000 ft
72
Max. Differential Pressure Up To 37,000
7.8 psi
73
Max. Differential Pressure Above 37,000 ft
8.34 psi
74
Max Differential Over Pressure
8.77 psi
75
Max. Differential Neg. Pressure
-0.5 psi
76
Max. Differential Pressure T/O and Land
0.2 psi
77
Min. Hydraulic Temp. For Engine Start.
-18 C
78
Thrust Reverser Limit for Go-Around Maneuver.
Do not attempt.
79
Reverse Thrust Stowage Movement Limitation.
No not move the thrust levers into the forward range until the REV icon on the EICAS is shown in AMBER or GREEN
80
Operation in Icing Conditions ON THE GROUND when the Temp. Is Between 5 C and 10 C
The TO DATASET MENU on the MCDU must be set to ENG.
When:
Any chance of encountering visible moisture below 1,700 ft. OR contaminated ramp or taxi ways.
81
Operation in Icing Conditions ON THE GROUND when the OAT Is Less Than 5 C
The TO DATASET MENU on the MCDU must be set to ALL if any possibility of visible moisture may be encountered up to 1,700 ft. Or with contaminated ramp, taxi ways or runways.
82
Autopilot Min. Engagement Height
400 ft
83
Min. Auto Pilot Use Height
50 ft
84
Min. Use height - Non-Precision Approach
MDA
85
TAS, TAT, and SAT information limitation
Only valid above 60 kt
86
While transmitting on VHF 1 the Standby Magnetic Compass limitation.
Compass information not valid
87
Altimeter limitations for CAT I approaches
Barometric altimeter settings must be used
88
Back Course Approach limitations
B/C approaches using IESS are prohibited.
89
EGPWS limitations (3)
1. Do not navigate using the EGPWS.
2. Predictive EGPWS needs to be disabled for approaches to airports not yet in the database.
3. Predictive EGPWS needs to be manually inhibited for QFE operations if the GPS data is unavailable or inoperative.
90
FMS limitations (2)
1. RNP approaches Not Authorized. (SW)
| 2. Use of speed mode prohibited in the event of an Engine Failure.
91
APU Continuous Operational Min. And Max. Temperature.
Min. -54 C and Max. ISA +35 C (52 C)
92
Wing Span (old wing)
85' 4"
93
Aircraft Length
103' 11"
94
Tail Height
32' 3"
95
Main Landing Gear Width Center to Center
17'
96
In the event of landing below -40 C
Must have a maintenance inspection performed.
97
Crosswind component greater than 25
Static takeoff not recommended
98
After five sequential motoring cycles
Must wait 15 minutes for a cool down period.
99
BTMS limit for takeoff
Must be in the green
ERJ 175
flashcards
Decks in class (4)
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