General Flashcards

1
Q

What is Gulfstream’s Cabin Essential
design?

A

It’s incorporated into cabin systems to
enhance reliability of entertainment,
lighting and service systems. Major cabin
systems are designed with redundancy so
single-point failure doesn’t result in loss
of cabin functionality.
Ref: Gulfstream’s website

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2
Q

What dampens main entry door during
opening?

A

Trapped fluid in actuator
Ref: AOM 2A

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3
Q

What happens when outside door
switch is selected to CLOSE?

A

Circuit energizes to CLOSE provided
EXTERNAL BATTERY switch is
selected ON, aux pump operates, and the
door closes. Once the door is closed and
electrically latched, circuit deenergizes,
aux pump shuts off, and EXTERNAL
BATTERY is selected to OFF.
Ref: PTH

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4
Q

What’s the purpose of DOOR
SAFETY switch?

A

When depressed, it prevents the door from
closing.

Ref: PTH

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5
Q

How could you investigate baggage
compartment from main cabin without
opening the baggage compartment
door?

A

A peep hole is provided to inspect
baggage compartment in the event of
onboard fire in baggage area.
Ref: AOM 2A

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6
Q

Describe the seal on external baggage
door

A

It features a passive seal to maintain
pressurization.

Ref: AOM 2A

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7
Q

What is EVAS?

A

Emergency Vision Assurance System
(EVAS) is provided in cockpit (one unit
for each pilot). In the event of smoke in
cockpit, Inflatable Vision Unit (IVU) is
deployed to provide improved visibility of
flight displays and aircraft flight path
through windscreen.
Ref: AOM 2A

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8
Q

What are the primary escape routes on
G650

A

Main entry door and four (4) emergency
exit windows

Ref: AOM 2A

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9
Q

What information is stored on cockpit
voice recorder (CVR)?

A

Most recent two (2) hours of all audio
signals transmitted and received by
aircraft crew members, including all
conversation in cockpit: last 30 minutes of
data is safely stored in solid state
memory.
Ref: AOM 2A

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10
Q

What are the requirements for erasing
CVR?

A

Aircraft must be stationary with main
cabin door open and WOW system in
ground mode.
Ref: AOM 2A

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11
Q

Length x Width x Height

A

100x100x26

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12
Q

Maximum weights?
RAMP
TAKEOFF
LANDING
ZERO FUEL

A

G650 G650ER
Max ramp 100,000 lbs 104,000 lbs
Max takeoff 99,600 lbs 103,600 lbs
Max landing 83,500 lbs 83,500 lbs
Max zero fuel 60,500 lbs 60,500 lbs

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13
Q

Max passengers?

A

19

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14
Q

Minimum taxi strip for 180° turn?

A

62ft

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15
Q

Landing light auto extinguish altitude?

A

18,000 to 51,000

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16
Q

Cruising altitudes?
Initial

Max

A

41,000

51,000

17
Q

Range?

A

7,000 NM at Mach 0.85

7,500 NM at Mach 0.85 with ASC 014

18
Q

High speed cruise?

A

Mach .90

19
Q

Internal baggage door altitude
restriction?

A

Most stay closed above 40,000