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?

25
Load Factor Limit (G loads) with fFaps Down (1, 2, 3 & FULL
2.0 G
26
Max T/O and LDG tailwind component?
10 kts
27
Max x-wind component to apply static T/O power?
18 kts
28
Hydraulic sys. accumulator pre-charge check interval?
Every 15 days or before the next flight, whichever occurs last
29
Stall Warning and Protection system must be tested?
before each flight
30
Synthetic Vision System prohibitions
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
Max operating altitude?
45,000 feet
32
Maximum take off and landing altitude?
8,300 feet (or 14,000 feet with AFM supplement 2)
33
Minimum Battery Voltage required for engine start
24V
34
Minimum GPU voltage for battery charging
27V
35
Maximum generator load on Ground
330 Amps each
36
Max generator load in Flight
390Amps each
37
Max usable fuel per tank
399.4 US Gal (2,676 lb)
38
Unusable fuel per tank
3.75 US Gal (25.13 lb)
39
Max fuel capacity
806.2 US Gal (5,401 lb)
40
Min Fuel tank temperature
-37 C
41
Max permitted imbalance between tanks
33 US Gal (220 lb)
42
Min Fuel tank temperature
-37
43
Max Fuel tank temperature (on the ground)
52 C NOTE Max temp can be exceeded up to 80 C in flight
44
Position of 'XFEED' Knob during Takeoff & Landing
'OFF'
45
46
47
48
49
50
For air conditioning system operation on ground _______
the GPU must be used or one engine generator must be turned ON
51
52
When must the crew activate the Ice Protection System?
when icing conditions exist or are anticipated, per Section 3, Normal Procedures
53
Define: "when icing conditions exist or are anticipated"?
54
55
What is the limitation regarding contaminated aircraft surfaces?
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
In what environmental condition is flight prohibited?
Flight in freezing drizzle or freezing rain The pilot must immediately exit the area by changing altitude or course
57
What are the limitations regarding the use of the Autopilot in icing conditions?
58
When must the Wing Inspection Light be operative?
Prior to flight into known or forecast icing at night
59