Limitations Flashcards

1
Q

Max Ramp weight
(MRW) lb

A

190 Lr- 111,245
190 Ar-114,552

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2
Q

Max Takeoff weight
(MTOW)

A

190 LR-110,892
190 Ar-114,199

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3
Q

Max landing weight
(MLW)

A

190 Lr-94,798
199 Ar- 97,003

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4
Q

Max zero fuel weight
(MZFW)

A

190 Lr-89,948
190 Ar- 90,169

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5
Q

Max altitude for flap extended

A

20,000 ft

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6
Q

Minimum crew

A

2 pilots

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7
Q

Load factor limit positive

A

Flaps up 2.5 g
Flaps down 2.0 g

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8
Q

Load factor limit negative

A

Flaps up -1.0 g
Flaps down 0 g

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9
Q

Runway slope

A

-2% to +2%

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10
Q

Runway surface type

A

Paved

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11
Q

Towing

A

Towbarless towing is prohibited, unless it is conducted in accordance with the procedures presented in the AMM chapter 9

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12
Q

Max tire ground speed

A

225 mph (195 kt)

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13
Q

Wind limitations

A

Max t/o and landing tailwind component 10 kt

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14
Q

Max recommended crosswind

A

-Dry runway 38kt
-Wet rwy 31 kt
-Rwy whit frost 31 kt
-Rwy whit compacted snow 20kt
-Specially prepared winter rwy (RWYCC 4) 20kt
-Rwy whit standing water/slush/wet snow/dry snow 18kt
-slippery when wet rwy 15kt
-specially prepared winter rwy (RWYCC 3) 15kt
-rwy whit ice 12kt

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15
Q

Maximum usable quantity per wing tank

A

2134 gal
14,440 lb

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16
Q

Unusable quantity per wing tank

A

15 gal
101.5 lb

17
Q

Max fuel capacity

A

4298 gal
29,083 lb

18
Q

Max permitted imbalance between wing tanks

A

794 lb

19
Q

Fuel specifications

A

Brazilian specification QAV1
ASTM specification D1655-JET A AND JET A-1
American specification MIL-T-83133A-JP8

20
Q

Fuel tank temperature

A

Minimum -37 Celsius

21
Q

Crossfeed operation

A

Crossfeed selector knob must be set OFF during takeoff and landing

22
Q

APU starter limits

A

Cooling period after each starting attempt
First and second attempt 60s off
Third attempt 5min off

23
Q

Engine

A

Two General Electric CF34-10E6

24
Q

Take off thrust

A

Hasta 20,000 lb

25
Q

Range

A

LR 2,400 Nm
AR 2,450 Nm

26
Q

Altitud de operación

A

-Techo de servicio 41,000 ft
-Max para despegues/aterrizajes en tierra 10,000 ft
-mi. Para despegues/aterrizajes en tierra 1,000 ft

27
Q

Autopilot

A

Alt mínima de engarzado 400 ft
Mínima altura de uso 50 ft

28
Q

Presurizacion

A

-Max diferencia de presión arriba de 37,000 ft: 8.4 psi
-Max diferencia de sobre presión: 8.8 psi
-Max diferencia de presión negativa -0.5 psi
-Max diferencia de presión en to/landing 0.2 psi

29
Q

Eléctrico

A

-Temperatura máxima de batería 70 Celsius
-Mínima temperatura de batería para arranque de apu -20 celsius
-tiempo de uso con falla eléctrica total: 10 minutos

30
Q

Back course approach using IESS

A

Prohibited

31
Q

Powerback

A

Prohibited

32
Q

Navigation limitations

A

Differences between the charts and the FMS information up to 3 degrees are acceptable

33
Q

Ice and rain protection

A

Engine: OAT 5-10 Celsius
All: OAT less than 5 Celsius

34
Q

Operation temperatures

A

-54/52 centígrados

35
Q

Kinds of operations

A

Visual
Instruments
Icing conditions
Category 1-2
RVSM
EXTENDED OVERWATER OPERATION
RNP