E190/195 LIMITATIONS Flashcards by Paulino Cicero | Brainscape

Q

Max Taxi & Ramp Weight 190

A

51,960 Kg

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Q

Max Taxi & Ramp Weight 195LR

A

50,950 Kg

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Q

Max Takeoff Weight 190

A

51,800 Kg

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Q

Max Takeoff Weight 195LR

A

50,790 Kg

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Q

Max Landing Weight 190

A

44,000 Kg

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Q

Max Landing Weight 195LR

A

45,000 Kg

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Q

Max Zero Fuel Weight 190

A

40,900 kg

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Q

Max Zero Fuel Weight 195LR

A

42,500 Kg

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Q

Max Headwind (for CAT II and LVO)

A

25 Kt

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Q

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

A

15 Kt (AD)

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Q

Max 90 degree crosswind component (STEADY)

Takeoff and Landing
DRY RWY

A

25 Kt

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Q

Max 90 degree crosswind component (STEADY)

Takeoff
WET RWY

A

20 Kt

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Q

Max 90 degree crosswind component (STEADY)

Landing
WET RWY

A

15 Kt

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Q

Max 90 degree crosswind component (STEADY)

Takeoff and Landing
STANDING WATER GROOVED RWY

A

10 Kt

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Q

Max 90 degree crosswind component (STEADY)

Takeoff and Landing
STANDING WATER NON-GROOVED RWY

A

05 Kt

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Q

Max 90 degree crosswind component (STEADY)

Takeoff and Landing
DRY RWY or TAXIWAYS (1700m X40m or less)

A

15 Kt

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Q

Max 90 degree crosswind component (STEADY)

Takeoff and Landing
WET RWY or TAXIWAYS (1700m x 40m or less)

A

05 Kt

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Q

Max takeoff and landing tailwind component

A

10 Kt (AD)

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Q

Max takeoff tailwind component for LVO

A

5 Kt (AD)

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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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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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Q

RUNWAY SLOPE

Max (up hill, down hill)

A

+2.0%, -2.0%

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Q

Min fuel temperature

A

-37°C

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Q

Max fuel imbalance left/right

A

360 kg

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Q

Max operating airspeed

A

VMO

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Q

Max operating mach number

A

.82 (MMO)

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Q

Max airspeed for RAT operation

A

VMO/MMO

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Q

Max Turbulent airspeed below 10,000 ft

A

250 Kt

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Q

Max Turbulent airspeed at or above 10,000 ft

A

270 Kt/.76 M

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Q

Tire limit ground speed

A

195 Kt

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Q

Max speed with windshield wiper failed in non-parked position

A

320 Kt

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Q

Max windshield wiper operation speed

A

250 Kt

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Q

Max gear extension speed VLO

A

265 Kt

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Q

Max gear retraction speed VLO

A

235 Kt

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Q

Max gear extended speed VLE

A

265 Kt

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Q

Max speed flap position 1

A

230 Kt

Q

Max speed flap position 2

A

215 Kt

Q

Max speed flap position 3

A

200 Kt

Q

Max speed flap position 4 and 5

A

180 Kt

Q

Max speed flap position FULL

A

165 Kt

Q

Maximum Speed to open side (Direct Vision) window

A

160 KIAS

Q

Design maneuvering speed

A

240 Kt

Q

Max operating ALTITUDE

A

41,000 ft

Q

Max takeoff and landing ALTITUDE

A

10,000 ft

Q

Max flap extension ALTITUDE

A

20,000 ft

Q

Max ambient TEMPERATURE for takeoff and landing

A

52°C

Q

Min ambient TEMPERATURE approved for takeoff

A

-54°C

Q

Max altitude for single pack operation

A

31,000 ft

Q

Max differential pressure

A

8.4 psi

Q

Max negative differential pressure

A

-0.5 psi

Q

Max differential pressure for takeoff & landing

A

0.2 psi

Q

Positive pressure relief valve

A

8.6 psi

Q

Maximum Differential Overpressure

A

8.8 psi

Q

Min altitude for autopilot use

Precision approach

A

50 ft below
DH/DA

Q

Min altitude for autopilot use

Nonprecision approach

A

MDA

Q

Min altitude for autopilot use

En route

A

500 ft
AGL

Q

Min altitude for autopilot use

Visual Approach not backed up by instrument procedure

A

500 ft
AGL

Q

Min Engagement AUTOPILOT Height

Takeoff

A

Acceleration Altitude

Q

Min Engagement AUTOPILOT Height

All Other

A

400 ft AGL

Q

LIMIT MANEUVERING LOAD FACTORS

Flaps up

A

-1.0 to +2.5 G

Q

LIMIT MANEUVERING LOAD FACTORS

Flaps down (1, 2, 3, 4, 5 and full)

A

0.0 to +2.0 G

Q

ENGINE

Max N1

A

100%

Q

ENGINE

Max N2

A

100%

Q

ENGINE

Max ITT During engine start

(on ground)

A

740°C

Q

ENGINE

Max ITT During engine start

(In flight)

A

875ºC

Q

ENGINE

Max ITT Takeoff and Go-Around

A

983°C (time timited to 5 min)

Era 943°C, mas foi alterado na RT-OPS-42_23

Q

ENGINE

RSV Takeoff & Go-Around (5 min)

A

983°C

Q

ENGINE

Max Continuous ITT

A

960°C

Q

ENGINE

Min Oil Pressure

A

25 psi

Q

ENGINE

Max Oil Temperature

A

155°C

Q

ENGINE STARTER DUTY CYCLE (E1)

1st and 2nd attempt ON GROUND

A

90 seconds ON
10 seconds off

Q

ENGINE STARTER DUTY CYCLE (E1)

3rd through 5th attempt ON GROUND

A

90 seconds ON
5 minutes off

Q

ENGINE STARTER DUTY CYCLE (E1)

1st and 2nd attempt IN FLIGHT

A

120 seconds ON
10 seconds off

Q

ENGINE STARTER DUTY CYCLE (E1)

3rd through 5th attempt IN FLIGHT

A

120 seconds ON
5 minutes off

Q

ENGINE STARTER DUTY CYCLE (E1)

Dry-Motoring Cycle

A

1st attempt
90 seconds ON
5 minutes off

2nd attempt
30 seconds ON
5 minutes off

Q

APU

Starter Duty Cycle (E1)

1st and 2nd attempt

A

60 seconds ON
60 seconds off

Q

APU

Starter Duty Cycle (E1)

3rd and subsequent

A

30 seconds ON
5 minutes off

Q

APU

Min temperature

A

Start ………………… -54°C

Operation ………… -62ºC

Q

APU

Max temperature for operations

A

ISA +35°C

Q

APU

Max altitude for Start

A

30,000 ft

Q

APU

Max altitude for electrical supply

A

33,000 ft

Q

APU

Max altitude for bleed supply

A

15,000 ft

Q

APU

Max altitude to assist engine start

A

21,000 ft

Q

APU

Max rotor speed

A

108%

Q

APU

Max EGT start

A

1032°C

Q

APU

Max EGT Continuous

A

717°C

Q

Maximum USABLE FUEL quantity

A

13100 kg

Q

Unusable FUEL quantity

A

92 kg