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Embraer > E190/195 LIMITATIONS > Flashcards

E190/195 LIMITATIONS Flashcards

(85 cards)

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1
Q

Max Taxi & Ramp Weight 190

A

51,960 Kg

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2
Q

Max Taxi & Ramp Weight 195LR

A

50,950 Kg

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3
Q

Max Takeoff Weight 190

A

51,800 Kg

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4
Q

Max Takeoff Weight 195LR

A

50,790 Kg

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5
Q

Max Landing Weight 190

A

44,000 Kg

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6
Q

Max Landing Weight 195LR

A

45,000 Kg

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7
Q

Max Zero Fuel Weight 190

A

40,900 kg

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8
Q

Max Zero Fuel Weight 195LR

A

42,500 Kg

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9
Q

Max Headwind (for CAT II and LVO)

A

25 Kt

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10
Q

Max 90 degree crosswind (including gusts) for CAT II and LVO

A

15 Kt (AD)

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11
Q

Max 90 degree crosswind component (STEADY)

Takeoff and Landing
DRY RWY

A

25 Kt

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12
Q

Max 90 degree crosswind component (STEADY)

Takeoff and Landing
WET RWY

A

15 Kt

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13
Q

Max 90 degree crosswind component (STEADY)

Takeoff and Landing
STANDING WATER GROOVED RWY

A

10 Kt

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14
Q

Max 90 degree crosswind component (STEADY)

Takeoff and Landing
STANDING WATER NON-GROOVED RWY

A

05 Kt

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15
Q

Max takeoff and landing tailwind component

A

10 Kt (AD)

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16
Q

Max takeoff tailwind component for LVO

A

5 Kt (AD)

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17
Q

Maximum wind for passenger door operation

A

40 kt, valid for positions between fully closed and fully open

For the open and locked position, the wind load limitation is 65 kt

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18
Q

Maximum wind for cargo door opening

A

40 kt, valid for positions between fully closed and fully open.

For the open and locked position, the wind load limitation is 60 kt.

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19
Q

RUNWAY SLOPE

Max (up hill, down hill)

A

+2.0%, -2.0%

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20
Q

Min fuel temperature

A

-37°C

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21
Q

Max fuel imbalance left/right

A

360 kg

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22
Q

Max operating airspeed

A

VMO

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23
Q

Max operating mach number

A

.82 (MMO)

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24
Q

Max airspeed for RAT operation

A

VMO/MMO

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25
Max Turbulent airspeed below 10,000 ft
250 Kt
26
Max Turbulent airspeed at or above 10,000 ft
270 Kt/.76 M
27
Tire limit ground speed
195 Kt
28
Max speed with windshield wiper failed in non-parked position
320 Kt
29
Max windshield wiper operation speed
250 Kt
30
Max gear extension speed VLO
265 Kt
31
Max gear retraction speed VLO
235 Kt
32
Max gear extended speed VLE
265 Kt
33
Max speed flap position 1
230 Kt
34
Max speed flap position 2
215 Kt
35
Max speed flap position 3
200 Kt
36
Max speed flap position 4 and 5
180 Kt
37
Max speed flap position FULL
165 Kt
38
Maximum Speed to open side (Direct Vision) window
160 KIAS
39
Design maneuvering speed
240 Kt
40
Max operating ALTITUDE
41,000 ft
41
Max takeoff and landing ALTITUDE
10,000 ft
42
Max flap extension ALTITUDE
20,000 ft
43
Max ambient TEMPERATURE for takeoff and landing
52°C
44
Min ambient TEMPERATURE approved for takeoff
-54°C
45
Max altitude for single pack operation
31,000 ft
46
Max differential pressure
8.4 psi
47
Max negative differential pressure
-0.5 psi
48
Max differential pressure for takeoff & landing
0.2 psi
49
Positive pressure relief valve
8.6 psi
50
Maximum Differential Overpressure
8.8 psi
51
Min altitude for autopilot use Precision approach
50 ft below DH/DA
52
Min altitude for autopilot use Nonprecision approach
MDA
53
Min altitude for autopilot use En route
500 ft AGL
54
Min altitude for autopilot use Visual Approach not backed up by instrument procedure
500 ft AGL
55
Min Engagement AUTOPILOT Height Takeoff
Acceleration Altitude
56
Min Engagement AUTOPILOT Height All Other
400 ft AGL
57
LIMIT MANEUVERING LOAD FACTORS Flaps up
-1.0 to +2.5 G
58
LIMIT MANEUVERING LOAD FACTORS Flaps down (1, 2, 3, 4, 5 and full)
0.0 to +2.0 G
59
ENGINE Max N1
100%
60
ENGINE Max N2
100%
61
ENGINE Max ITT During engine start (on ground)
740°C
62
ENGINE Max ITT During engine start (In flight)
875ºC
63
ENGINE Max ITT Takeoff and Go-Around
983°C (time timited to 5 min) | Era 943°C, mas foi alterado na RT-OPS-42_23
64
ENGINE RSV Takeoff & Go-Around (5 min)
983°C
65
ENGINE Max Continuous ITT
960°C
66
ENGINE Min Oil Pressure
25 psi
67
ENGINE Max Oil Temperature
155°C
68
ENGINE STARTER DUTY CYCLE (E1) 1st and 2nd attempt ON GROUND
90 seconds ON 10 seconds off
69
ENGINE STARTER DUTY CYCLE (E1) 3rd through 5th attempt ON GROUND
90 seconds ON 5 minutes off
70
ENGINE STARTER DUTY CYCLE (E1) 1st and 2nd attempt IN FLIGHT
120 seconds ON 10 seconds off
71
ENGINE STARTER DUTY CYCLE (E1) 3rd through 5th attempt IN FLIGHT
120 seconds ON 5 minutes off
72
ENGINE STARTER DUTY CYCLE (E1) Dry-Motoring Cycle
1st attempt 90 seconds ON 5 minutes off 2nd attempt 30 seconds ON 5 minutes off
73
APU Starter Duty Cycle (E1) 1st and 2nd attempt
60 seconds ON 60 seconds off
74
APU Starter Duty Cycle (E1) 3rd and subsequent
30 seconds ON 5 minutes off
75
APU Min temperature
Start ………………… -54°C Operation ………… -62ºC
76
APU Max temperature for operations
ISA +35°C
77
APU Max altitude for Start
30,000 ft
78
APU Max altitude for electrical supply
33,000 ft
79
APU Max altitude for bleed supply
15,000 ft
80
APU Max altitude to assist engine start
21,000 ft
81
APU Max rotor speed
108%
82
APU Max EGT start
1032°C
83
APU Max EGT Continuous
717°C
84
Maximum USABLE FUEL quantity
13100 kg
85
Unusable FUEL quantity
92 kg

Embraer (6 decks)

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