Limitations Flashcards

1
Q

Flight Maneuvering Load Factor Limits

A

-1 to +2.5 in Clean config
O to +2 in other configs

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2
Q

Runway altitude
Runway Slope
Runway width (nominal and minimal)

A

9200 ft
+/- 2%
45m, min 30 meter

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3
Q

Crosswind

Tailwind

Cargo door
Passenger door

A

38 kt takeoff/landing

15/10 kt tail land/take off

Operations 40kt (50 if nose into wind) closed before 65 kt.
Operations 65kr

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4
Q

MAXIMUM RECOMMENDED CROSSWIND ON WET AND CONTAMINATED RUNWAYS

A

Brake Action - Wind
5 - 38
4 - 29
3 - 25
2 - 20
1 - 15

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5
Q

Max Windows Open speed

A

200kt

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6
Q

VMO/MMO and Max Flaps speed

A

VMO - 350
MMO - M 0.82
1 - 230
1+f - 215
2 - 200
3 - 185
Full - 177

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7
Q

Maximum speed GEAR
VLE
VLO Ex
VLO Re

A

VLE - 280
VLO Ex - 250
VLO Re - 220

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8
Q

Max Tire speed

A

195 kt

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9
Q

Max Wipers speed

A

230 kt

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10
Q

Weight Limitations RGC,RGD,RDE,RGV
Taxi
Takeoff
Landing
Zero Fuel

A

75 900
75 500
62 500
58 500

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11
Q

Avionics Ventilation max temp for no limitation

A

49 C

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12
Q

Max Differential Cabin Pressure

A

9 PSI
-1 PIS
Safety relief Valve 8.6 PSI

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13
Q

Autopilot Function
At takeoff
In Approach Precision
In Approach Non-Precision

A

100 ft AGL or after 5 sec
200 ft AGL
250 ft AGL

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14
Q

Minimum Decision Height
Cat ll
Cat lll Fail Passive (Single)
Cat lll Fail Operational (Dual)

A

100 ft
50 ft
Alert Height 100 ft. 75m vis

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15
Q

Maximum wind for CAT II and III

A

Head 30
Cross 20 (15 for automatic rollout with OEI)
Tail 10

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16
Q

Glide slope for Automatic Landings

A

-2.5° to -3.25°

17
Q

APU Limitations
Attempts (Wait time)
Operational Envelope
Assisted Engine start
For anti-ice

A

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

18
Q

TOGA Time limits

A

All engines 5 min
OEI 10 min

19
Q

Oil Temperature NEO
Max Continuous
Min start
Min before takeoff

A

140°
-40°
-10°

20
Q

Minimum Oil Quantity CEO and NEO

A

9.5 qt + estimated consumption
Average estimated consumption = 0.5 qt/h.

21
Q

Starter Limit NEO and CEO

A

-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 %.

22
Q

Max altitude for Flaps extended

23
Q

JET A1 Fuel Temperature

A

-43° C (Jet A -36)
54° C

24
Q

MAX Fuel Imbalance
Heavier tank - Mas Asymmetry

A

Takeoff
FULL - 500kg
3000kg - 1050kg
1450kg - 1450kg
(Outer 370kg)

Landing
Full - 1500kg
4300kg - 1600kg
2250kg - 2250kg

Outer Max 690kg

25
Minimum Fuel for takeoff
1500kg
26
Definition of Icing Conditions
OAT <= 10°C Visible Moisture (Clouds, fog with less than 1 sm (1600m) vis or less, rain, snow, sleet or ice crystals) Also when taxiways and runways have snow, slush or water that might be ingested into engines
27
Definition of severe ice accretion
Ice accumulation on airframe reaches 5 mm or more
28
Max brake Temp (Fan off)
300° C
29
Taxi speeds with Damages tires
One tire 7kr two tires (on same gear) 3kt Max angle 30°
30
Weight Limitations RGG,RGH, RGV Taxi Takeoff Landing Zero Fuel
77 400 77 000 64 500 61 500