EMB limitations Flashcards
(104 cards)
1
Q
Max Ramp Weight
A
40530 kg
2
Q
Max Takeoff Weight
A
40370 kg
3
Q
Max Landing weight
A
34100 kg
4
Q
Max zero fuel weight
A
32000 kg
5
Q
The takeoff weight is limited by:
A
Structural (MTOW) Field length Brake Energy Climb En-route Landing
6
Q
The landing weight is limited by:
A
Structural (MLW)
Altitude, temperature
Approach
Climb Gradient
7
Q
Alt CG for increased TOW
A
16% - 27%
8
Q
Min and Max Temp and Alt for Takeoff
A
- 1,000’ to 8,000’
- 40C to 52C
9
Q
Min and Max temp in flight
A
-65C to ISA + 35C
10
Q
When landing below _______ the airplane may not takeoff without a mx inspection
A
-40C
11
Q
Max Alt Flap extended
A
20,000’
12
Q
Vlo - retraction
Vlo - extension
Vle - extended
A
250 KIAS
250 KIAS
250 KIAS
13
Q
Max speed to open cockpit window
A
160 KIAS
14
Q
Max Speed
A
0’ to 8,000’ - 300 KIAS
8,000’ to 12,000’ - increasing to 320 KIAS
12,000’ to FL410 - 320 KIAS / M0.82
15
Q
Va - Maneuvering Speed
A
250 KIAS - 270 KIAS
16
Q
Max Flaps Speed: Flaps 1 Flaps 2 Flaps 3 Flaps 4 Flaps 5 Flaps Full
A
1 - 230 KIAS 2 - 215 KIAS 3 - 200 KIAS 4 - 180 KIAS 5 - 180 KIAS Full - 165 KIAS
17
Q
Max Tire speed
A
195 Kts - 225mph
18
Q
Max Takeoff and landing Tailwind
A
10kts
19
Q
Max Crosswind: Dry Wet Compacted Snow Standing Water and Slush/Dry Snow ice
A
Dry - 38 kt Wet - 31 kt Compacted Snow - 20 kt Standing Water and Slush/Dry Snow - 18 kt ice - 12 kit
20
Q
Max crosswind for static Takeoff
A
25 kts
21
Q
Kinds of operations
A
Visual - VFR
Instrument -IFR
Icing conditions
RVSM
22
Q
Min Crew
A
2 - Pilot + copilot
23
Q
maneuvering flight load limits
Flaps UP
Flaps Down
A
UP -1 to 2.5g
Down 0 to 2g
24
Q
Runway Surfaced type
A
paved
25
Runway slope
+/-2%
26
Max water equivalent depth for takeoff
19mm
27
Improved Go Around Performance - IGAP
| Flaps ______ are prohibited
3
28
EGPWS
Not for Navigation
Situational Tool only
Deviate from ATC as necessary to comply with EGPWs
Turn off when landing at an airport not in the database
NA with Qfe
29
TCAS
Deviate from ATC as necessary to comply with RA
30
Max useable fuel per tank
4714 KG
31
Unusable fuel per tank
34 kg
32
Max Total Fule
9496 kg
33
Max Fuel imbalance between tanks
360 kg
34
Cross Feed must be off during
Takeoff and Landing
35
Apu Type
Sunstrand APS 2300
36
APU Max and Min temp for starting and operation
-54C to ISA + 35C
37
APU Max alt for Start
30,000'
38
APU max Alt
Elec
Bleed
Assist engine start
Elec - 33,000'
Bleed - 15,000'
Assist - 21,000'
39
APU Max rotor speed
108%
40
APU Max EGT for Start
1032C
41
APUT MAx EGT continuous
717C
42
In Flight there is ________ Auto shutdown if APU EGT exceeds limits
There is ______ time limitation for operating the APU in the amber range between ______ and _____
NO
No, 662C - 717C
43
APU starter limit
1st / 2nd - 60 sec on, 60 sec off
| 3rd - 60 sec on, 5 min off
44
What type of Engine
General Electric CF34-8E5A1
45
Max N1
99.5%
46
Min and Max N2
58.5% - 99.4%
47
Max ITT Start
815C
48
Normal limit ITT Takeoff
989C - 2 min
| 973C - 3 min
49
Normal limit ITT GA
965C - 2 min
| 949C - 3min
50
Max ITT T/O and GA
1006C - 2 min
| 990C - 3 min
51
Oil Pressure Max and Min PSI
25 - 95 PSI
52
Max Oil Temp Continuous and Transient
Cont. - 155C
| Trans - 163C (15 min)
53
Dry Motor
1 - 90 sec on / 5 min off
2 to 5 - 30 sec on / 5 min
after 5th attempt - 15 min cool down
54
Starter Duty Cycle
1st and 2nd - 90(ground)/120(flt) sec on / 10 sec off
| 3rd to 5th - 90(ground)/120(flt) sec on /5 min
55
Powerback is __________
prohibited
56
Max thrust reduction is ________
25%
57
Do not move TR back to forward thrust unless ________
REV icon are amber or green
58
Max Press up to 37,000'
7.8 psi
59
Max press above 37,000'
8.4 psi
60
Max Overpressure
8.8 psi
61
Max negative pressure
-0.5 psi
62
Max pres t/o and landing
0.2
63
Icing Conditions exist when
OAT is 10C or less on the ground with snow, ice, standing water, slush may be ingested by the engine or freeze on the engines, nacelles or engine probes
TAT is 10C or less and visible moisture in any form such as clouds, fog, vis less than 1 mile, rain, snow, sleet, ice crystals
64
On Ground select ENG Ice when _______
OAT is 5C to 10C and
vis moisture up to 1,700'
Ramp, taxiways, runways have snow, ice, standing water, slush may be ingested by the engine or freeze on the engines, nacelles or engine probes
65
On the Ground select ALL ice when _______
OAT is 5C or less and
vis moisture up to 1,700\0'
Ramp, taxiways, runways have snow, ice, standing water, slush may be ingested by the engine or freeze on the engines, nacelles or engine probes
66
Max windshield wiper speed
253 KIAS
67
Min engagement height AP
400'
68
Min in use height AP
Cruise
App
Cruise - 1,000'
| App - 50'
69
TAS, TAT and SAT are valid above _____
60 KIAS
70
while transmitting on _______ the standby mag compass indication is _______
VHF 1
| Not valid
71
Baro Alt must be used for
CAT 1 approaches
72
Back course IESS is
prohibited
73
RVSM equipment
2 RVSM ADS
1 AP with holdover mode
1 alt alerter
1 transponder
ADS 1, 2 and 3 are compliant with RVSM
ADS 3 is NOT compliant when ADS 3 SLIPCOMP fail is displayed on the EICAS
74
Max Fwd Cargo
Max Aft Cargo
Fwd - 1500KG
Aft - 828 KG
75
Min Fuel Temp Jet A
Min Fuel Temp Jet A1
- 37C(EMB) / -40C
| - 44C(EMB) / -47C
76
GE CF348E5A1 engines with Takeoff Thrust is limited to __________
5 min
77
Max N1 with brakes applied
60%
78
There is ______ temp limit for the auto A/I sys
no
79
ACARS is limited to transmission and receipt of messages that ____________
NOT create an unsafe conditions if the message is improperly received
80
Max diff between charts and FMS for RNP navigation si ______
3 deg
81
Best Angle of Climb
Green Dot
82
Best Rate of Climb
Green Dot + 50 until M0.63
83
Elec PBIT last ____
3 min
84
HYD PBIT last ____-
1 min
85
Max GE cf348E5A1 Eng Thrust
14,200 lb per eng
28,4000 lb of thrust total
86
Elec AC power voltage
115 +3/-2 VAC
87
Factored landing Dry and Wet
Dry 1.67
Wet 1.92
88
Flap Man Seed
```
up
1
2
3
4
5
Full
```
```
up - 210
1 - 180
2 - 160
3 - 150
4 - 140
5 - 140
Full - 130
```
89
Taxi Fuel
8kg/min
90
App and Landing Fuel
18kg/min
91
GA fuel
73kg/min
92
Cruise fuel burn
30kg/min
93
APU on ground
2.5kg/min
94
Max Alt Diff
-2000 to 10,000'
10,000 to 20,000'
20,000 t FL410
-2000 to 10,000' : 50'
10,000 to 20,000': 120'
20,000 t FL410: 180'
95
Min Battery Voltage for APU start
21 V
96
Min press Xbleed pneumatic start
40 psi -0.5 per 1,000'
97
Opening closing door max wind
40 kts
65 kts Gust
98
Min O2 press
3 - 1150 psi Green
2 -842 psi Cyan
Amber = no dispatch
99
Service ceiling
41,000'
100
Min Temp for Hyd sys
-18C
101
Min Temp use of dual ignition
-2C
102
Turb air penetration
Below 10,000' - 250
| Above 10,000' 270/M0.76 whichever is lower
103
Min Runway width for 180
18m
104
Wingspan
26m
