Limitations Flashcards
Flight Maneuvering Load Factor Limits
-1 to +2.5 in Clean config
O to +2 in other configs
Runway altitude
Runway Slope
Runway width (nominal and minimal)
9200 ft
+/- 2%
45m, min 30 meter
Crosswind
Tailwind
Cargo door
Passenger door
38 kt takeoff/landing
15/10 kt tail land/take off
Operations 40kt (50 if nose into wind) closed before 65 kt.
Operations 65kr
MAXIMUM RECOMMENDED CROSSWIND ON WET AND CONTAMINATED RUNWAYS
Brake Action - Wind
5 - 38
4 - 29
3 - 25
2 - 20
1 - 15
Max Windows Open speed
200kt
VMO/MMO and Max Flaps speed
VMO - 350
MMO - M 0.82
1 - 230
1+f - 215
2 - 200
3 - 185
Full - 177
Maximum speed GEAR
VLE
VLO Ex
VLO Re
VLE - 280
VLO Ex - 250
VLO Re - 220
Max Tire speed
195 kt
Max Wipers speed
230 kt
Weight Limitations RGC,RGD,RDE,RGV
Taxi
Takeoff
Landing
Zero Fuel
75 900
75 500
62 500
58 500
Avionics Ventilation max temp for no limitation
49 C
Max Differential Cabin Pressure
9 PSI
-1 PIS
Safety relief Valve 8.6 PSI
Autopilot Function
At takeoff
In Approach Precision
In Approach Non-Precision
100 ft AGL or after 5 sec
200 ft AGL
250 ft AGL
Minimum Decision Height
Cat ll
Cat lll Fail Passive (Single)
Cat lll Fail Operational (Dual)
100 ft
50 ft
Alert Height 100 ft. 75m vis
Maximum wind for CAT II and III
Head 30
Cross 20 (15 for automatic rollout with OEI)
Tail 10
Glide slope for Automatic Landings
-2.5° to -3.25°
APU Limitations
Attempts (Wait time)
Operational Envelope
Assisted Engine start
For anti-ice
3 Attempts (Wait 60 min)
Bleed Air up to 22 500 ft (Single Pack) 15 000ft (Dual pack) , Elec full envelope
20 000 ft
Not permitted
TOGA Time limits
All engines 5 min
OEI 10 min
Oil Temperature NEO
Max Continuous
Min start
Min before takeoff
140°
-40°
-10°
Minimum Oil Quantity CEO and NEO
9.5 qt + estimated consumption
Average estimated consumption = 0.5 qt/h.
Starter Limit NEO and CEO
-A standard automatic start that includes up to three start attempts, is considered one cycle
‐ For ground starts (automatic or manual), a 20 s pause is required between successive cycles
‐ A 15 min cooling period is required, subsequent to four failed cycles
‐ The starter must not be run when N2 is above 20 %.
Max altitude for Flaps extended
20 000ft
JET A1 Fuel Temperature
-43° C (Jet A -36)
54° C
MAX Fuel Imbalance
Heavier tank - Mas Asymmetry
Takeoff
FULL - 500kg
3000kg - 1050kg
1450kg - 1450kg
(Outer 370kg)
Landing
Full - 1500kg
4300kg - 1600kg
2250kg - 2250kg
Outer Max 690kg