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Atlas > EMB limitations > Flashcards

EMB limitations Flashcards

1
Q

Max Ramp Weight

A

40530 kg

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2
Q

Max Takeoff Weight

A

40370 kg

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3
Q

Max Landing weight

A

34100 kg

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4
Q

Max zero fuel weight

A

32000 kg

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5
Q

The takeoff weight is limited by:

A 
Structural (MTOW) 
Field length
Brake Energy
Climb
En-route
Landing
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6
Q

The landing weight is limited by:

A

Structural (MLW)
Altitude, temperature
Approach
Climb Gradient

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7
Q

Alt CG for increased TOW

A

16% - 27%

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8
Q

Min and Max Temp and Alt for Takeoff

A
  • 1,000’ to 8,000’

- 40C to 52C

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9
Q

Min and Max temp in flight

A

-65C to ISA + 35C

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10
Q

When landing below _______ the airplane may not takeoff without a mx inspection

A

-40C

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11
Q

Max Alt Flap extended

A

20,000’

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12
Q

Vlo - retraction
Vlo - extension
Vle - extended

A

250 KIAS
250 KIAS
250 KIAS

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13
Q

Max speed to open cockpit window

A

160 KIAS

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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

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15
Q

Va - Maneuvering Speed

A

250 KIAS - 270 KIAS

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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
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17
Q

Max Tire speed

A

195 Kts - 225mph

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18
Q

Max Takeoff and landing Tailwind

A

10kts

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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
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20
Q

Max crosswind for static Takeoff

A

25 kts

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21
Q

Kinds of operations

A

Visual - VFR
Instrument -IFR
Icing conditions
RVSM

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22
Q

Min Crew

A

2 - Pilot + copilot

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23
Q

maneuvering flight load limits
Flaps UP
Flaps Down

A

UP -1 to 2.5g

Down 0 to 2g

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24
Q

Runway Surfaced type

A

paved

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25
Q

Runway slope

A

+/-2%

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26
Q

Max water equivalent depth for takeoff

A

19mm

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27
Q

Improved Go Around Performance - IGAP

Flaps ______ are prohibited

A

3

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28
Q

EGPWS

A

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

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29
Q

TCAS

A

Deviate from ATC as necessary to comply with RA

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30
Q

Max useable fuel per tank

A

4714 KG

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31
Q

Unusable fuel per tank

A

34 kg

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32
Q

Max Total Fule

A

9496 kg

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33
Q

Max Fuel imbalance between tanks

A

360 kg

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34
Q

Cross Feed must be off during

A

Takeoff and Landing

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35
Q

Apu Type

A

Sunstrand APS 2300

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36
Q

APU Max and Min temp for starting and operation

A

-54C to ISA + 35C

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37
Q

APU Max alt for Start

A

30,000’

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38
Q

APU max Alt
Elec
Bleed
Assist engine start

A

Elec - 33,000’
Bleed - 15,000’
Assist - 21,000’

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39
Q

APU Max rotor speed

A

108%

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40
Q

APU Max EGT for Start

A

1032C

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41
Q

APUT MAx EGT continuous

A

717C

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42
Q

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 _____

A

NO

No, 662C - 717C

43
Q

APU starter limit

A

1st / 2nd - 60 sec on, 60 sec off

3rd - 60 sec on, 5 min off

44
Q

What type of Engine

A

General Electric CF34-8E5A1

45
Q

Max N1

46
Q

Min and Max N2

A

58.5% - 99.4%

47
Q

Max ITT Start

48
Q

Normal limit ITT Takeoff

A

989C - 2 min

973C - 3 min

49
Q

Normal limit ITT GA

A

965C - 2 min

949C - 3min

50
Q

Max ITT T/O and GA

A

1006C - 2 min

990C - 3 min

51
Q

Oil Pressure Max and Min PSI

A

25 - 95 PSI

52
Q

Max Oil Temp Continuous and Transient

A

Cont. - 155C

Trans - 163C (15 min)

53
Q

Dry Motor

A

1 - 90 sec on / 5 min off
2 to 5 - 30 sec on / 5 min

after 5th attempt - 15 min cool down

54
Q

Starter Duty Cycle

A

1st and 2nd - 90(ground)/120(flt) sec on / 10 sec off

3rd to 5th - 90(ground)/120(flt) sec on /5 min

55
Q

Powerback is __________

A

prohibited

56
Q

Max thrust reduction is ________

57
Q

Do not move TR back to forward thrust unless ________

A

REV icon are amber or green

58
Q

Max Press up to 37,000’

59
Q

Max press above 37,000’

60
Q

Max Overpressure

61
Q

Max negative pressure

62
Q

Max pres t/o and landing

63
Q

Icing Conditions exist when

A

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
Q

On Ground select ENG Ice when _______

A

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
Q

On the Ground select ALL ice when _______

A

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
Q

Max windshield wiper speed

67
Q

Min engagement height AP

68
Q

Min in use height AP
Cruise
App

A

Cruise - 1,000’

App - 50’

69
Q

TAS, TAT and SAT are valid above _____

70
Q

while transmitting on _______ the standby mag compass indication is _______

A

VHF 1

Not valid

71
Q

Baro Alt must be used for

A

CAT 1 approaches

72
Q

Back course IESS is

A

prohibited

73
Q

RVSM equipment

A

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
Q

Max Fwd Cargo

Max Aft Cargo

A

Fwd - 1500KG

Aft - 828 KG

75
Q

Min Fuel Temp Jet A

Min Fuel Temp Jet A1

A
  • 37C(EMB) / -40C

- 44C(EMB) / -47C

76
Q

GE CF348E5A1 engines with Takeoff Thrust is limited to __________

77
Q

Max N1 with brakes applied

78
Q

There is ______ temp limit for the auto A/I sys

79
Q

ACARS is limited to transmission and receipt of messages that ____________

A

NOT create an unsafe conditions if the message is improperly received

80
Q

Max diff between charts and FMS for RNP navigation si ______

81
Q

Best Angle of Climb

82
Q

Best Rate of Climb

A

Green Dot + 50 until M0.63

83
Q

Elec PBIT last ____

84
Q

HYD PBIT last ____-

85
Q

Max GE cf348E5A1 Eng Thrust

A

14,200 lb per eng

28,4000 lb of thrust total

86
Q

Elec AC power voltage

A

115 +3/-2 VAC

87
Q

Factored landing Dry and Wet

A

Dry 1.67

Wet 1.92

88
Q

Flap Man Seed

up
1
2
3
4
5
Full
A 
up - 210
1 - 180
2 - 160
3 - 150
4 - 140
5 - 140
Full - 130
89
Q

Taxi Fuel

90
Q

App and Landing Fuel

91
Q

GA fuel

92
Q

Cruise fuel burn

93
Q

APU on ground

94
Q

Max Alt Diff
-2000 to 10,000’
10,000 to 20,000’
20,000 t FL410

A

-2000 to 10,000’ : 50’
10,000 to 20,000’: 120’
20,000 t FL410: 180’

95
Q

Min Battery Voltage for APU start

96
Q

Min press Xbleed pneumatic start

A

40 psi -0.5 per 1,000’

97
Q

Opening closing door max wind

A

40 kts

65 kts Gust

98
Q

Min O2 press

A

3 - 1150 psi Green

2 -842 psi Cyan

Amber = no dispatch

99
Q

Service ceiling

100
Q

Min Temp for Hyd sys

101
Q

Min Temp use of dual ignition

102
Q

Turb air penetration

A

Below 10,000’ - 250

Above 10,000’ 270/M0.76 whichever is lower

103
Q

Min Runway width for 180

104
Q

Wingspan

Atlas (16 decks)

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