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E190 Alliance > Limitations > Flashcards

Limitations Flashcards

1
Q

Weight limitations E190 LR

A

ZFW 40.8
MRW 50.46
MTOW 50.0
MLW 43.0

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2
Q

Weight limitations E190 AR

A

ZFW 40.9
MRW 51.96
MTOW 50.0/51.8
MLW 44.0

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3
Q

Operational Envelope

A

Max altitude - 41000ft

Max altitude for flaps extended - 20000ft

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4
Q

Gear Speeds

A

VLO retraction - 235kts
VLO extension - 265kts

VLE - 265kts

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5
Q

Max airspeed to open direct vision window

A

160kts

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6
Q

VMO≤8000ft
VMO≥10000ft
MMO

A

300kts
320kts
M0.82

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7
Q

MAXIMUM FLAP EXTENDED SPEED (VFE)

A

VFE Flap 1 - 230kts
VFE Flap 2 - 215kts
VFE Flap 3 - 200kts
VFE Flap 4 - 180kts
VFE Flap 5 - 180kts
VFE Flap FULL - 165kts

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8
Q

Maximum Tire Ground Speed

A

195kts

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9
Q

WINDSHIELD WIPER OPERATION

A

253kts

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10
Q

Turbulent Air Penetration: Below 10000ft

Turbulent Air Penetration: Above 10000ft

A

250kts Below 10000ft

270kts/M0.76 Above 10000ft

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11
Q

VX

VY

A

VX - Green Dot

VY - Green Dot + 50

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12
Q

Dual engine failure minimum speed

A

265kts

Below 10,000ft pitch for Green Dot

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13
Q

Minimum speed in the cruise

A

Green Dot

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14
Q

Minimum speed if STALL PROT ICE SPEED is annunciated

A

Green Dot + 10

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15
Q

Minimum speed on approach with RAT deployed

A

130kts

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16
Q

Wind Limitations

A

Maximum tailwind for take-off and landing - 10kts

Maximum crosswind for take-off/Landing DRY - 38kts

Maximum crosswind for take-off/Landing WET - 31kts

17
Q

MANOEUVRING FLIGHT LOAD
FACTORS

A

FLAPS UP +2.5g to -1.0g

Flaps extended +2.0g to 0.0g

18
Q

Fuel
Maximum fuel quantity

Maximum usable quantity per wing

Maximum fuel imbalance

A

Maximum fuel quantity - 13192kg

Maximum usable quantity per wing - 8076L/6550kg

Maximum fuel imbalance - 360kg

Xfeed selector Knob must be OFF for Take-off and Landing

19
Q

APU - OPERATIONAL LIMITS

A

Max altitude 33000ft

Max altitude - Electrical
GEN 33000ft

Start: Max altitude 30000ft

Max altitude - Bleed air for engine
starting 21000ft

Max altitude - Bleed for air conditioning and pressurisation 15000ft

In flight, there is no automatic shutdown if EGT exceeds the limits.

20
Q

APU Starter: Duty cycles

A

1st attempt 60sec OFF
2nd attempt 60sec OFF
3rd attempt 5min OFF

21
Q

Autopilot Usage heights

A

Minimum engagement height 400ft AGL

Latest disconnect height 50ft AGL

22
Q

RUNWAY

A

Runway Slope…………………..-2% TO +2%
Runway Surface Type …………….PAVED

23
Q

ENGINE - STARTER DUTY CYCLE LIMITS

A
24
Q

PRESSURISATION

Maximum differential pressure?

Maximum differential overpressure?

A

Maximum differential pressure 8.4 psi

Maximum differential overpressure 8.8 psi

Maximum differential negative pressure -0.5 psi

Maximum differential pressure for Take-off and Landing 0.2 psi

25
Q

OPERATION IN ICING CONDITIONS

On ground:
The TO DATASET MENU on the MCDU must be set to ALL when OAT is from?

A

The TO DATASET MENU on the MCDU must be set to ALL when OAT is less than 5°C:

– if there is any possibility of encountering visible
moisture up to 1700 ft AFE, or.

– when operating on ramps, taxiways, or runways
where surface snow, ice, standing water, or slush
may be ingested by the engines, or freeze on
engines, nacelles, or engine sensor probes.

26
Q

OPERATION IN ICING CONDITIONS

On ground:
The TO DATASET MENU on the MCDU must be set to ENG when OAT is from?

A

5-10°C and:

– if there is any possibility of encountering visible
moisture up to 1700 ft AFE, or

– when operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on
engines, nacelles, or engine sensor probes.

27
Q

AUTOPILOT USAGE

A

Minimum Engagement Height. ….. 400 ft

Minimum Use Height…………………. 50 ft

28
Q

NAVIGATION EQUIPMENT

A
  • TAS, TAT and SAT information are only valid above 60 KIAS.
  • While transmitting in VHF1 the standby magnetic compass indication is not valid.
  • Baro altimeter minimums must be used for all Cat-I approaches

E190 Alliance (5 decks)

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