Limitations E1& E2 Flashcards
Limitations study
MAX TAKEOFF WEIGHT E190
51800kg
MAX LANDING WEIGHT E190
44000kg
MAX ZERO FUEL WEIGHT E190
40900kg
MAX TAKEOFF WEIGHT E195
50790kg
MAX LANDING WEIGHT E195
45000kg
MAX ZERO FUEL WEIGHT E195
42500kg
MAX TAKEOFF WEIGHT E2
61500kg
MAX LANDING WEIGHT E2
54000kg
MAX ZERO FUEL WEIGHT E2
51850kg
MAX HEADWIND (for CAT II and LVO)
25kt
Max crosswind (CAT II and LVO)
15kt
Max crosswind Takeoff and Landing (DRY RUNWAY)
25kt
Max crosswind Takeoff (WET RUNWAY)
20kt
Max crosswind Landing (WET RUNWAY)
15kt
Max Takeoff and Landing (standing water - GROOVED)
10kt
Max Takeoff and Landing (standing water - NOT GROOVED)
5kt
Max crosswind Takeoff and Landing (1700mX40m or less - DRY RUNWAY)
15kt
Max crosswind Takeoff and Landing (1700mX40 or less - WET RUNWAY)
5kt
Max takeoff and landing tailwind component
10kt
Max takeoff tailwind component for LVO
5kt
Max wind for passanger AND cargo door operation
40kt
Max (UPHILL, DOWNHILL)
+2.0%, -2.0%
Min fuel temperature
-37°C
Max fuel imbalance
360kg
Max operating airspeed
VMO
MAX OPERATING MACH NUMBER
.82 (MMO)
MAX AIRSPEED FOR RAT OPERATION
VMO/MMO
Max turbulent airspeed below 10.000ft
250kt
Max turbulent airspeed at or above 10.000 ft
270kt/.76M
Tire limit speed
195kt (ground speed)
Max speed with windshield wiper failed non-parked position
320kt
Max windshield wiper operation speed
250kt
Max gear extension speed
265kt (E1) ; 250kt (E2)
Max gear retraction speed
235kt (E1) ; 220kt (E2)
Max gear extended speed
265kt
Design maneuvering speed
240kt
Max speed Flap 1
230kt
Max speed Flap 2
215kt
Max speed Flap 3
200kt
Max speed Flap 4 and 5
180kt
Max speed Flap Full
165kt
Max operating altitude
41.000ft
Max takeoff and landing altitude
10.000ft
Max flap extension altitude
20.000ft
Max ambient temperature for takeoff and landing
52°C
Min ambient temperature for takeoff
-54°C
Max altitude for single pack operation
31.000ft
Max differential pressure
8.4PSI
Max negative differential pressure
-0.5PSI
Max differential pressure for takeoff and landing
0.2PSI
Min altitude for autopilot use (Precision approach)
50ft below DH/DA (E1) ; DH/DA (E2)
Min altitude for autopilot use (Non-Precision approach)
MDA (E1 and E2)
Min autopilot engagement height (Takeoff)
Acceleration Altitude
Limit Load factor (Flap Up)
-1.0G to +2.5G
Limit Load factor (Flap not up)
0.0G to +2.0G
Max OIL TEMP
155°C