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Gulfstream 550 > G550 Limitations > Flashcards

G550 Limitations Flashcards

1
Q

Speed Limitations

When may the auto throttles be used?

A

The autothrottles are approved for use from takeoff to landing

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2
Q

Runway Slope Limitations

What is the maximum runway slope
Approved for takeoff and landing operations?

A

Runway Slope Limitations

     \+2 % uphill and -2% downhill
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3
Q

Speed Limitations

Turbulent Air Penetration Speed

A

Altitude 10,000 or above: 270 KCAS/.80MT

Below 10,000: 240 KCAS
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4
Q

Maximum Flap Extended Speed

A

10 flaps 250 KCAS
20 flaps 220
39 flaps 170

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5
Q

Maximum landing gear extended speed

A

250/0.70 MT with landing gear doors open or closed.

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6
Q

What is the usable fuel capacity?

A

41,300lbs (6118 gal)

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7
Q

What is the minimum engine fuel temperature?

A

-40 C

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8
Q

What is the minimum fuel tank temperature?

A

-35 to -36 degrees C

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9
Q

What is the maximum fuel tank temperature?

A

+ 54 degrees C

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10
Q

What is the maximum fuel imbalance:

For takeoff?

Inflight?

A

Takeoff - 1000 lbs

In flight - 2000lbs

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11
Q

Minimum holding speed

A

160 KCAS

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12
Q

Maximum operating altitude

A

51,000

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13
Q

Maximum crosswind for takeoff and landing

A

28 kts

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14
Q

Maximum tail wind

A

10 kts

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15
Q

Speed brakes

A

Speed brakes are not approved for extension with flaps at 39 degrees or with landing gear extended in flight.

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16
Q

Auto pilot minimum altitude

Departure and Landing (visual)

A

500 AGL

17
Q

Autopilot minimum altitude

ILS approach

LNAV/VNAN

Other than ILS

A

60 AGL

50 Below MDA

18
Q

Autopilot coupled GO-Around S.E.

A

Not Authorized

19
Q

Power plant

max Starting TGT (ground)

A

700

20
Q

Power plant

Max Starting TGT (AIR)

A

850

21
Q

Power plant

Max Crosswind For Start

A

30

22
Q

Power plant

Max Tailwind For Start

A

20

23
Q

Max zero fuel weight

A

53,500

24
Q

Max landing weight

A

75,300

Gulfstream 550 (3 decks)

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