Limitations Flashcards

1
Q

Rwy Slope

A

+/- 2%

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2
Q

Max Tail Wind

A

10Kts

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3
Q

Turbulent Air Penetration

A

280Kt / 0.73M

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4
Q

Max Operating Altitude

A
FL 370 
FL 250 (single Pack)
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5
Q

Max TKFF and Ldg Altitude

A

8.400’

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6
Q

Max Altimeter Variation

A

In Flight: 200’
On Ground: 40’
Field Elevation Difference: 75’

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7
Q

Max Ramp Weight

A

63.049Kg

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8
Q

MTOW

A

62.822Kg

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9
Q

MLW

A

54.884Kg

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10
Q

MZFW

A

51.225Kg

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11
Q

Flap Maneuvering

A
220Kts
                    / 
   53.070Kg
                    \
                     210Kts
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12
Q

Max Cabin Press. Diferential

A

8,65psi

(On ground): 0,125psi

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13
Q

Autopilot

A

Departing: 1.000’
Approaching: 50’

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14
Q

Max Generator Oil Drive

A

157°C / 20°C Rise

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15
Q

Pneumatic

A

Min. 30psi -0,5psi/1.000’ of elevation

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16
Q

TKFF Thrust

A

5 minutes

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17
Q

Max N1:

A

106%

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18
Q

Max. N2:

A

105%

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19
Q

Engine Type

A

CFM56-3-C3

20
Q

Max. EGT

A

TKF : 930°C (940°C for 20 seconds)
Continuous: 895°C
Start: 725°C

21
Q

Min Oil Press

A

13psi

22
Q

Max Oil Temperature:

A

165°C - Max
165°C ~ 160°C - 15 minutes
160°C - Continuous

23
Q

EGT Alive:

A

10 seconds - Ground Start

30 seconds - In Flight Start

24
Q

Generators

A

160A - In Fligh

140A - Ground

25
Q

APU Altitude Limitation:

A

Bleed + Elec : 10.000’
Bleed : 17.000’
Electrical : 37.000’

26
Q

APU EGT

A

760°C - Max

710°C - Continuous

27
Q

APU Start

A

3 Starts then 30 minutes of cooling

28
Q

APU AutoShuttdown

A

110%

29
Q

APU Cooling/ Warming

A

1 Minute - For Electric

3 Minutes - For Bleed Air

30
Q

Max Fuel Imbalance

A

453 Kg

31
Q

Central Tank

A

Tank 1 and 2 must be Full , for Central having 453Kg or more on central.

32
Q

Flap Retraction/Extension Speed:

A

Flap: <53.070<
Up. 210Kt. 220Kt
1. 190Kt. 200Kt
5. 180Kt. 190Kt
10. 170Kt. 180Kt
15. 150Kt. 160Kt
25. 140Kt. 150Kt
30/40. VRef 30/VRef 40

33
Q

Fuel Temperature, Max and Min.

A

Max : 49°C

Min: -45°C or Freezing Point +3°

34
Q

Starter CutOut at ….. % N2

A

45% N2

35
Q

Max Flap altitude.

A

20.000’

36
Q

Speed Brake Limit.

A

Not beyond Flight Detent In Flight

37
Q

Landing Gear Speed Limit

A

Extension: 270Kt/0.82M
Extended: 320Kt/0.82M
Retraction: 235Kt

38
Q

Engine 5th and 9th Stage Bleed Temperature:

A

5th: 350°C
9th: 580°C

39
Q

SOP Landing and Takeoff Crosswind Limits

A

TKFF LNDG
Dry 25Kt. 25Kt
Wet. 20Kt. 15Kt
Standing(Grooved) 10Kt. 10Kt
Standing(Ungrooved) 5kt. 5Kt

Rwy Less then 40m width
And/or 1.700m Length

Dry. 15Kt. 15Kt
Wet. 5Kt. 5Kt

40
Q

Max SOP Taxi Speed.

A

Max 20Kts , in turns 10Kts.

If wet 1/2 of the limit

41
Q

Hyd Pump Cooling Limit.

A

Min of 760Kg of Fuel on Tank 1 and 2 (respectively)

42
Q

Cargo Door Wind Limit

A
  • Full Open: 30Kt->
43
Q

Electric Sistem:
A/C : Volts ?
Frequency: ?
DC : Volts ?

A

A/C : 115V +/- 5V
Frequency: 400Hz +/- 10Hz
DC: 26V +/- 4V

44
Q

Hydraulic Pressure:

A

Min: 2.800psi
Normal: 3.000psi
Max: 3.500psi
Pre-charge: 1.000psi

45
Q

Fuel Capacity:

Tank 1 , Center, Tank 2 and Total:

A

Tank 1 : 4.555Kg
Central: 7.029Kg
Tank 2 : 4.555Kg

Total: 16.139Kg

46
Q
Aircraft Dimensions:
Span
Length 
Height 
Stab Span
Landing Gear Span 
Distance Gears
180° Turning Radius
A
Span: 28,88m
Length: 35,22m
Height: 11,13m
Stab Span: 12,70m
Landing Gear Span: 5,23m
Distance Gear: 14,27m
180° Turning Radius: 22,25m