Limitations Flashcards
Weight limitations E190 LR
ZFW 40.8
MRW 50.46
MTOW 50.0
MLW 43.0
Weight limitations E190 AR
ZFW 40.9
MRW 51.96
MTOW 50.0/51.8
MLW 44.0
Operational Envelope
Max altitude - 41000ft
Max altitude for flaps extended - 20000ft
Gear Speeds
VLO retraction - 235kts
VLO extension - 265kts
VLE - 265kts
Max airspeed to open direct vision window
160kts
VMO≤8000ft
VMO≥10000ft
MMO
300kts
320kts
M0.82
MAXIMUM FLAP EXTENDED SPEED (VFE)
VFE Flap 1 - 230kts
VFE Flap 2 - 215kts
VFE Flap 3 - 200kts
VFE Flap 4 - 180kts
VFE Flap 5 - 180kts
VFE Flap FULL - 165kts
Maximum Tire Ground Speed
195kts
WINDSHIELD WIPER OPERATION
253kts
Turbulent Air Penetration: Below 10000ft
Turbulent Air Penetration: Above 10000ft
250kts Below 10000ft
270kts/M0.76 Above 10000ft
VX
VY
VX - Green Dot
VY - Green Dot + 50
Dual engine failure minimum speed
265kts
Below 10,000ft pitch for Green Dot
Minimum speed in the cruise
Green Dot
Minimum speed if STALL PROT ICE SPEED is annunciated
Green Dot + 10
Minimum speed on approach with RAT deployed
130kts
Wind Limitations
Maximum tailwind for take-off and landing - 10kts
Maximum crosswind for take-off/Landing DRY - 38kts
Maximum crosswind for take-off/Landing WET - 31kts
MANOEUVRING FLIGHT LOAD
FACTORS
FLAPS UP +2.5g to -1.0g
Flaps extended +2.0g to 0.0g
Fuel
Maximum fuel quantity
Maximum usable quantity per wing
Maximum fuel imbalance
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
APU - OPERATIONAL LIMITS
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.
APU Starter: Duty cycles
1st attempt 60sec OFF
2nd attempt 60sec OFF
3rd attempt 5min OFF
Autopilot Usage heights
Minimum engagement height 400ft AGL
Latest disconnect height 50ft AGL
RUNWAY
Runway Slope…………………..-2% TO +2%
Runway Surface Type …………….PAVED
ENGINE - STARTER DUTY CYCLE LIMITS
PRESSURISATION
Maximum differential pressure?
Maximum differential overpressure?
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
OPERATION IN ICING CONDITIONS
On ground:
The TO DATASET MENU on the MCDU must be set to ALL when OAT is from?
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.
OPERATION IN ICING CONDITIONS
On ground:
The TO DATASET MENU on the MCDU must be set to ENG when OAT is from?
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.
AUTOPILOT USAGE
Minimum Engagement Height. ….. 400 ft
Minimum Use Height…………………. 50 ft
NAVIGATION EQUIPMENT
- 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
