EMB 505 Limitations GrandView Flashcards

first two pages of the the Grandview specific limitations

1
Q

Max Ramp Weight

A

18,497 lbs

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2
Q

Max Take off Weight

A

18,387 lbs

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3
Q

Max Landing Weight

A

17,042 lbs

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4
Q

Max Zero Fuel Weight

A

14,220 lbs

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5
Q

Left-hand cabinet FWD

A

44 lbs

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6
Q

Lavatory \cabinet

A

33 lbs

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7
Q

AFT bag compartment

A

463 lbs

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8
Q

FWD bag compartment

A

110 lbs

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9
Q

Refreshment center

A

71 lbs

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10
Q

Side facing couch stowage compartment stowage

A

36 lbs

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11
Q

max speed LDG ext. / retr. (Vlo)M

A

250 kias

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12
Q

Max speed LDG extended / locked?

A

250 kias

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13
Q

Minimum Control Speed (Vmc) for takeoff (takeoff flaps):

A

97 kias

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14
Q

Minimum Control Speed (Vmc) for landing, (landing flags) in “No Icing Conditions”:

A

91 kias

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15
Q

Minimum Control Speed (Vmc) for landing, (landing flags) in “Icing Conditions”:

A

95 kias

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16
Q

Operating Maneuvering Speed Vo?

A

205 kias

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17
Q

Maximum Flap Extension Speed (Vfe)

Flap 1

A

180 kias

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18
Q

Maximum Flap Extension Speed (Vfe)

Flap 2

A

170 kias

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19
Q

Maximum Flap Extension Speed (Vfe)

Flap 3

A

170 kias

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20
Q

Maximum Flap Extension Speed (Vfe)

Flap Full

A

160 kias

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21
Q

Max altitude with flaps extended?

A

18,000 feet

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22
Q

Max tire ground speed?

A

182 kts

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23
Q

Runway slope max / min gradient?

A

-2% / +2%

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24
Q

Load Factor Limit (G loads) with flaps up?

A

3.0 G

25
Q

Load Factor Limit (G loads) with fFaps Down (1, 2, 3 & FULL

A

2.0 G

26
Q

Max T/O and LDG tailwind component?

A

10 kts

27
Q

Max x-wind component to apply static T/O power?

A

18 kts

28
Q

Hydraulic sys. accumulator pre-charge check interval?

A

Every 15 days or before the next flight, whichever occurs last

29
Q

Stall Warning and Protection system must be tested?

A

before each flight

30
Q

Synthetic Vision System prohibitions

A

Use of the SVS as primary information to base decisions and/or plan maneuvers, to navigate, or to avoid terrain, obstacles, or traffic is prohibited.

31
Q

Max operating altitude?

A

45,000 feet

32
Q

Maximum take off and landing altitude?

A

8,300 feet

(or 14,000 feet with AFM supplement 2)

33
Q

Minimum Battery Voltage required for engine start

A

24V

34
Q

Minimum GPU voltage for battery charging

A

27V

35
Q

Maximum generator load on Ground

A

330 Amps each

36
Q

Max generator load in Flight

A

390Amps each

37
Q

Max usable fuel per tank

A

399.4 US Gal (2,676 lb)

38
Q

Unusable fuel per tank

A

3.75 US Gal (25.13 lb)

39
Q

Max fuel capacity

A

806.2 US Gal (5,401 lb)

40
Q

Min Fuel tank temperature

A

-37 C

41
Q

Max permitted imbalance between tanks

A

33 US Gal (220 lb)

42
Q

Min Fuel tank temperature

A

-37

43
Q

Max Fuel tank temperature (on the ground)

A

52 C
NOTE Max temp can be exceeded up to 80 C in flight

44
Q

Position of ‘XFEED’ Knob during Takeoff & Landing

A

‘OFF’

45
Q
A
46
Q
A
47
Q
A
48
Q
A
49
Q
A
50
Q

For air conditioning system operation on ground _______

A

the GPU must be used or one engine generator must be turned ON

51
Q
A
52
Q

When must the crew activate the Ice Protection System?

A

when icing conditions exist or are anticipated, per Section 3, Normal Procedures

53
Q

Define: “when icing conditions exist or are anticipated”?

A
54
Q
A
55
Q

What is the limitation regarding contaminated aircraft surfaces?

A

Take-off is prohibited with frost (polished or not), ice, snow, or slush adhering to wings, control surfaces, engine inlets, or other critical surfaces

56
Q

In what environmental condition is flight prohibited?

A

Flight in freezing drizzle or freezing rain
The pilot must immediately exit the area by changing altitude or course

57
Q

What are the limitations regarding the use of the Autopilot in icing conditions?

A
58
Q

When must the Wing Inspection Light be operative?

A

Prior to flight into known or forecast icing at night

59
Q
A