General Description Flashcards

1
Q

How tall is the Legacy 600?

A

22’ 2”

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2
Q

What is the Wingspan of the Legacy 600?

A

68’ 11”

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3
Q

How Long is the Legacy 600?

A

86’ 5”

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4
Q

Max Ramp Weight?

A

49,758 Lbs

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5
Q

Max Take-off weight?

A

49,604 Lbs

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6
Q

Max Landing Weight

A

40, 786 Lbs

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7
Q

Max Zero Fuel Weight

A

35, 274 Lbs

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8
Q

Max Operating Altitude of N317LL?

A

41,000’

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9
Q

Max Pressure Altitude for Take-Off and Landing

A

9,500’

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10
Q

MMO

A

.80 Mach

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11
Q

VMO

A

250 below 8,000 ft

320 above 10,000 ft

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12
Q

Maneuvering Speed

A

200 Knots

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13
Q

Flap Speeds

A

Flaps 9 - 250 Knots
Flaps 22- 200 Knots
Flaps 45- 145 Knots

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14
Q

Max Demonstrated Crosswind

Dry Runway

A

30 Knots

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15
Q

Max Demonstrated Crosswind

Wet

A

25 Knots

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16
Q

Max Demonstrated Crosswind

Compacted Snow

A

20 knots

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17
Q

Max Demonstrated Crosswind

Standing Water, Slush, Loose Snow

A

15 Knots

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18
Q

Max Demonstrated Crosswind

Ice

A

10 Knots

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19
Q

How long does Passenger Oxygen Masks last once mask is pulled

A

Legacy 600 has Central Gaseous Oxygen for Pax. Duration depends on configuration

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20
Q

Minimum Internal Oxygen Pressure for 2 Pilots? 2 Pilots & Jumpseater?

A

1130 PSI- 2 Pilots

1570 PSI - with Jumpseater

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21
Q

How Many Batteries Power the Emergency Lights and for how long?

A

2 Batteries, 10 Minutes

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22
Q

What Powers the ISIS and for how long?

A

The Backup Hot Battery for 240 Minutes

23
Q

What Engine does the Legacy 600 have?

A

AE3007A1E

24
Q

What is the Horsepower of the AE3007A1E Engine?

A

8,810 Lbs per engine

25
Q

Max Differential Cabin Pressure

A

8.1 PSI

26
Q

Max Cabin Overpressure Differential

A

8.4 PSI

27
Q

How many Fuel Tanks does the Legacy 600 have? Where are they located?

A

4, One in each wing, one is Located beneath the FWD Fuselage, and one is located behind the Baggage Compartment

28
Q

How much fuel can the Legacy 600 hold?

A

18,328 Lbs Total

29
Q

What type of APU does the Legacy 600 Have?

A

C-14

30
Q

Max Start Altitude for the APU?

A

30,000’

31
Q

Max Altitude for Operation of the APU (C-14)

A

41,000’

32
Q

What Controls the APU (C-14), and the Overspeed Test?

A

The FADEC Automatically Controlls the APU

33
Q

Legacy 600 (Post Mod) Max Ramp Weight?

A

49,758 Lbs

34
Q

Max Take-off Weight

A

49,604 Lbs

35
Q

Max Landing Weight

A

40,786 Lbs

36
Q

May Zero Fuel Weight

A

35,274 Lbs

37
Q

Maximum Altitude for Flap Extension

A

20,000’

38
Q

Maximum Airspeed after Takeoff/During

Climb without Retrimming

A

160 Knots

39
Q

Maximum Takeoff and Landing

Tailwind Component

A

10 Knots

40
Q

Maximum recommended speed to remove direct vision window

A

140 Knots

41
Q

Maximum altitude for operation after an in-flight depressurization

A

10,000’

42
Q

TURBULENT AIR PENETRATION SPEED

A

Below 10,000’- 200 Knots

Above 10,000’ -250 Knots or .63 Mach, whichever is lower

43
Q

Max G load on the Legacy 600?

A

Flaps 0: Positive= 2.51Gs Negative = -1 G

Flaps 9,22,45: Positive= 2 Gs Negative = 0 Gs

44
Q

Maximum Electrical Load on the Main Generators?

A

400 Amps

45
Q

Max Electrical Load on the APU Generator

A

Up to 30,000’ = 400 Amps

Above 30,000’ = 300 Amps

46
Q

Maximum Battery Temperature

A

70* Celsius

47
Q

How much Fuel does each wing hold?

A

5703.4 Lbs

48
Q

How much fuel does FUSE 1 (Fwd & Aft) , and FUSE2 (FWD & AFT) hold?

A

3461 Lbs in FUSE 1, and 3461 in FUSE 2

49
Q

At what point do you hear a “Cabin” Aural Warning?

A

At 9,900’ +/- 100’ Cabin Altitude

50
Q

If landing altitude is not entered in the digital controller, what happens?

A

The Controller Assumes 8,000’ as landing altitude

51
Q

What Cabin Altitude does the Cabin hold after takeee-off, and why? For how long?

A

750 below take off Altitude, for 15 minutes, in case of need for return to Airport

52
Q

What is the depressurization sequence on the ground?

A

On touchdown, the cabin is pressurized at 650’above landing altitude and then a gradual decrease until the outflow valves are completely open.

53
Q

What Happens when you hit dump button in automatic,ode?

A

Dumps the Cabin to 14,500’

54
Q

How are the outflow valves powered?

A

Bleed air coming through the ejector valve creates suction through the static lines which provides the air to physically open and close the outflow valves.