E175 Limitations & Memory items Flashcards
1
Q
Max Ramp Weight
A
LL = 85,450 lbs
LR = 85,870 lbs
2
Q
Max Takeoff Weight
A
LL = 85,098 lbs
LR = 85,517 lbs
3
Q
Max Landing Weight
A
LL = 74,957 lbs
LR = 74,957 lbs
4
Q
Max Zero Fuel Weight
A
LL = 69,467 lbs
LR = 69,886 lbs
5
Q
Minimum Runway Width
A
LL = 100 ft (SW)
LR = 100 ft (SW)
6
Q
Minimum Taxiway Width
A
LL = 50 ft (SW)
LR = 50 ft (SW)
7
Q
Wing Span
A
93’ 11”
8
Q
Aircraft Length
A
103’ 11”
9
Q
Tail Height
A
32’ 4”
10
Q
Max Operations Altitude
A
41,000 ft
11
Q
Max Takeoff and Landing Altitude
A
10,000 ft
12
Q
Max Temperature for Takeoff and Landing
A
ISA +35C (52C at 1,000 ft below sea level)
13
Q
Minimum Temperature for Takeoff and Landing
A
-40*C
14
Q
Max Runway Slope
A
+/- 2*
15
Q
Max Tailwind
A
15 kts
16
Q
Max Altitude for Single Pack Operations
A
31,000 ft
17
Q
Vmo
A
SL - 8,000’ = 300 kias
10,000’ - Mach Transitions Altitude = 320 kias
18
Q
Mmo
A
0.82M
19
Q
Va
A
240 kias
20
Q
VLO Ext
A
250 kias
21
Q
VLE Ret
A
250 kias
22
Q
VLE
A
250 kias
23
Q
V Tire
A
195 kias
24
Q
V RAT Deploy Max
A
Vmo/Mmo
25
Vmin (to provide electrical power)
130 kias
26
Vb
Below 10,000' = 250 kias
10,000' and above = 270 or 0.76M, whichever is lower
27
V wiper operations max
250 kias (SW)
28
V window
160 kias
29
What needs to happen if a landing below -40*C occurs?
The airplane can't take off again until a maintenance inspection is completed
30
Vfe Speeds
Vfe 1 = 230 kias
Vfe 2 = 215 kias
Vfe 3 = 200 kias
Vfe 4 = 180 kias
Vfe 5 = 180 kias
FULL = 165 kias
31
Maximum altitude for flaps/slats extended?
20,000 ft
32
What is the mandatory flaps setting for a CAT 2 approach?
Flaps 5
33
Landing Flaps Full, Go-Around Flaps
Flaps 4
34
Landing Flaps 5 Go-Around
Flaps 2
35
Battery Minimum Voltage
22.5 V
36
Maximum ITT during engine start
815* C
37
Engine Starter Cranking Limits (Ground)
Starts 1 and 2:
90 secs ON, 10 secs OFF
Starts 3, 4, 5:
90 secs ON, 5 mins OFF
38
Engine Starter Cranking Limits (In Flight)
Starts 1 and 2:
120 secs ON, 10 secs OFF
Starts 3, 4, 5:
120 secs ON, 5 mins OFF
39
For engine starts, the maximum cumulative starter run time per engine start is 90 seconds on the ground and 120 seconds in flight. These time limits include...
motoring plus start time.
40
DRY MOTORING CYCLE DUTY LIMITS
Motoring # 1 = 90 secs ON, 5 mins OFF
Motoring # 2-5 = 30 secs ON, 5 mins OFF
41
DRY MOTORING CYCLE DUTY LIMITS
After ______ sequential motoring cycles, the process may be __________ following a ___ minute cool down period.
five
repeated
15
42
When it is necessary to perform an engine start with a tailwind, when must the engine start be manually aborted?
When there is no positive increase of N1 before starter cutout at 50% N2
43
Is takeoff with Automatic Takeoff Thrust Control System (ATTCS) OFF authorized?
No
44
Maximum Fuel Capacity
20,935 lbs
45
What kind of fuel do we use?
Jet A
Jet A1
46
Maximim Fuel Imbalance
794 lbs
47
Minimum Fuel Tank Temperature
-37*C
48
Is it permissable to takeoff and land with a FUEL IMBALANCE caution message?
Yes, as long as the actual imbalance doesn't exceed 794 lbs
49
How long do you need to wait to start the APU?
30 seconds after the EICAS is energized
50
What postion must Fuel XFEED be in during takeoff and landing?
OFF position
51
How long can you leave the aircraft unattended with the APU running?
No more than 5 mins (SW)
52
Simultaneous use of the _____ Bleed and ___ cart is ___________.
APU
HP
prohibited
53
APU STARTER DUTY CYCLE LIMITS
Start attempts 1 & 2:
60 secs OFF
Start attempt 3:
5 mins OFF
54
APU Start Minimum Temperature
-54*C
55
APU Start Maximum Temperature
ISA +35*C
56
APU Start Maximum Altitude
30,000 ft
57
APU Continuous Operation Minimum Temperature
-54*C
58
APU Continuous Operation Maximum Temperature
ISA +35*C (52*C)
59
APU Continuous Operation Maximum Altitude
33,000 ft
60
APU Continuous Operation Electrical Generator Use Maximum Altitude
33,000 ft
61
APU Continuous Operation Engine Start Maximum Altitude
21,000 ft
62
APU Continuous Operation Bleed Use Maximum Altitude
15,000 ft
63
Maximum Differential Pressure
8.4 psi
64
Maximum Differential Overpressure
8.8 psi
65
Maximum Differential Negative Pressure
-0.5 psi
66
Maximum Differential Pressure for Takeoff and Landing
0.2 psi
67
Minimum Hydraulic Reservoir Temperature for Engine Start
-18*C
68
Brake temperature must be what for takeoff?
In the GREEN range
69
After deployment of the thrust reversers what must you not attempt?
A Go-Around
70
After selecting reverse thrust, when can you move the thrust levers into the forward thrust range?
When the REV icon on the EICAS is amber or green
71
Can you use the thrust reversers during taxi operations?
No
72
Can you use the thrust reversers for power back operations?
No
73
Is there a temperature limitation for anti-icing system AUTO operation?
No
74
When must you set the TO DATASET MENU on the MCDU to ENG?
OAT from 5*C to 10*C and...
- there is the possibility of encountering visible moisture up to 1,700 ft AFE
OR
- when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on the engines, nacelles, or engine sensor probes
75
When must you set the TO DATASET MENU on the MCDU to ALL?
OAT less than 5*C and...
- there is the possibility of encountering visible moisture up to 1,700 ft AFE
OR
- when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on the engines, nacelles, or engine sensor probes
76
In normal flight the engine and wing anti-ice systems mode selector must be set to what position?
Why?
AUTO
In case you encounter icing
77
If either one or both ice detectors are failed, what position should the anti-ice mode knob be in?
The ON position when…
- icing conditions exist
OR
- are anticipated below 10*C TAT with visible moisture
78
When may icing conditions exist on the ground or for takeoff?
OAT is 10*C or below and visible moisture is present, such as clouds, fog with visibility one mile or less, rain, snow, sleet, and ice crystals.
It may also exist when OAT is 10*C or below 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.
79
When may icing conditions exist in flight?
When TAT is 10*C or below and visible moisture is present, such as clouds, fog with visibility one mile or less, rain, snow, sleet, and ice crystals.
80
Autopilot Minimum Engagement Height
(takeoff/initial climb and go-around/missed approach)
400 ft
81
Autopilot Minimum Use Height on an Approach
50 ft HAT
82
What information is only valid above 60 kts?
TAS
TAT
SAT
83
What is not valid while transmitting on VHF1?
Standby magnetic compass
84
What minimums must be used for CAT 1 approaches?
Barometric altimeter minimums
85
Prior to joining a published segment of an instrument approach, what should you verify?
The NAVAID ID visually displayed matches the chart being used
86
If a NAVAID ID is not visually displayed, what should you verify before joining a published segment of an instrument approach?
Verify that the ID matches the chart being used
87
Doing what may cause damage to the digital audio panels?
Plugging in a dual prong headset and an ANR (5-pin) headset into the same jack panel at the same time
88
Can you use EGPWS for navigational purposes?
No
89
What should you do to the EGPWS when landing at an airport that is not in the database?
Why?
Manually inhibit the EGPWS to avoid unwanted alerts
90
GPS data is unavailable or inoperative, and we're conducting QFE operations.
What must you do to the EGPWS?
Manually inhibit the EGPWS during QFE operations
91
What RNAV (GPS) minima are NOT authorized?
LP minima
92
SMOKE EVACUATION
OXYGEN MASKS.................................DON, EMER
CREW COMMUNICATION...................ESTABLISH
PRESSURIZATION DUMP.........................PUSH IN
93
SMOKE / FIRE / FUMES
OXYGEN MASKS..................................DON, 100%
CREW COMMUNICATION...................ESTABLISH
94
CABIN ALTITUDE HI
OXYGEN MASKS..................................DON, 100%
CREW COMMUNICATION...................ESTABLISH
95
JAMMED CONTROL COLUMN - PITCH
ELEVATOR DISCONNECT HANDLE...............PULL
96
JAMMED CONTROL WHEEL - ROLL
AILERON DISCONNECT HANDLE.................PULL
97
PITCH TRIM RUNAWAY
AP / TRIM DISC Button..............PRESS AND HOLD
PITCH TRIM SYS 1 & 2 CUTOUT Buttons...................................PUSH IN
98
ROLL OR YAW TRIM RUNAWAY
AP / TRIM DISC Button..........…….PRESS AND HOLD
99
STEERING RUNAWAY
STEER DISC SWITCH....................................PRESS
*Steer the airplane using differential braking and rudder
100
BATT 1 (2) OVERTEMP
ASSOCIATED BATTERY....................................OFF
101
ENGINE ABNORMAL START
AFFECTED ENGINE:
START / STOP SELECTOR..............................STOP
102
Maximum Crosswind - RCC 6 - Dry
38 kts
103
Maximum Crosswind - RCC 5 - Wet
31 kts
104
Maximum Crosswind - RCC 4 - Compact Snow
20 kts
105
Maximum Crosswind - RCC 3 - Dry Snow, Wet Snow, Slush, Standing Water
18 kts
106
Maximum Crosswind - RCC 2 - Ice
12 kts
107
Maximum Crosswind - RCC 0 - Wet Ice
Prohibited
108
Crosswind landing limitations for wet or contaminated runways are only applicable when _____ values are published or, when operating at a ____-_______ airport, when the surface contaminant covers more than _____ of the effective length and width of the runway.
RCC
non-TALPA
25%
109
Maximum Crosswind - RCC 1 - Ice
8 kts
110
ENGINE FIRE, SEVERE DAMAGE, or SEPERATION
QRC
111
CARGO COMPARTMENT FIRE
QRC
112
CRG FWD (AFT) SMOKE
QRC
113
APU FIRE
QRC
114
EMERGENCY DESCENT
QRC
115
EVACUATION
QRC
116
DUAL ENGINE FAILURE
QRC
117
DUAL EFB FAILURE
QRC
