Limitations

Question 1

Weight limitations E190 LR

Answer 1

ZFW 40.8
MRW 50.46
MTOW 50.0
MLW 43.0

Question 2

Weight limitations E190 AR

Answer 2

ZFW 40.9
MRW 51.96
MTOW 50.0/51.8
MLW 44.0

Question 3

Operational Envelope

Answer 3

Max altitude - 41000ft

Max altitude for flaps extended - 20000ft

Question 4

Gear Speeds

Answer 4

VLO retraction - 235kts
VLO extension - 265kts

VLE - 265kts

Question 5

Max airspeed to open direct vision window

Answer 5

160kts

Question 6

VMO≤8000ft
VMO≥10000ft
MMO

Answer 6

300kts
320kts
M0.82

Question 7

MAXIMUM FLAP EXTENDED SPEED (VFE)

Answer 7

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

Question 8

Maximum Tire Ground Speed

Answer 8

195kts

Question 9

WINDSHIELD WIPER OPERATION

Answer 9

253kts

Question 10

Turbulent Air Penetration: Below 10000ft

Turbulent Air Penetration: Above 10000ft

Answer 10

250kts Below 10000ft

270kts/M0.76 Above 10000ft

Question 11

VX

VY

Answer 11

VX - Green Dot

VY - Green Dot + 50

Question 12

Dual engine failure minimum speed

Answer 12

265kts

Below 10,000ft pitch for Green Dot

Question 13

Minimum speed in the cruise

Answer 13

Green Dot

Question 14

Minimum speed if STALL PROT ICE SPEED is annunciated

Answer 14

Green Dot + 10

Question 15

Minimum speed on approach with RAT deployed

Answer 15

130kts

Question 16

Wind Limitations

Answer 16

Maximum tailwind for take-off and landing - 10kts

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

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

Question 17

MANOEUVRING FLIGHT LOAD
FACTORS

Answer 17

FLAPS UP +2.5g to -1.0g

Flaps extended +2.0g to 0.0g

Question 18

Fuel
Maximum fuel quantity

Maximum usable quantity per wing

Maximum fuel imbalance

Answer 18

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

Question 19

APU - OPERATIONAL LIMITS

Answer 19

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.

Question 20

APU Starter: Duty cycles

Answer 20

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

Question 21

Autopilot Usage heights

Answer 21

Minimum engagement height 400ft AGL

Latest disconnect height 50ft AGL

Question 22

RUNWAY

Answer 22

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

Question 23

ENGINE - STARTER DUTY CYCLE LIMITS

Answer 23

Question 24

PRESSURISATION

Maximum differential pressure?

Maximum differential overpressure?

Answer 24

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

Question 25

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

Answer 25

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.

Question 26

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

Answer 26

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.

Question 27

AUTOPILOT USAGE

Answer 27

Minimum Engagement Height. ..... 400 ft Minimum Use Height...................... 50 ft

Question 28

NAVIGATION EQUIPMENT

Answer 28

* 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