G500_600 Memory Flash Cards

1
Q

Length, height & wingspan G600

A

L: 96’ 1” H: 25’ 3” S: 95’ 0”

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2
Q

Maximum Weights?
Ramp
Takeoff
Landing
Zero fuel

A

Aircraft G600

Ramp 95,000
Takeoff 94,600
Landing 76,800
Zero fuel 57,440

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3
Q

Max approved wt. in baggage comp

A

G600: 2500lbs

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4
Q

Max passengers

A

19 Depending on floor plan

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5
Q

Min taxi strip for 180° turn

A

G600: 65’

135’ no tiller

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6
Q

Cruising Altitudes

Initial

Max

A

Initial: FL430
Max: FL510

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7
Q

High speed cruise

A

0.90M

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8
Q

Internal baggage door altitude restriction

A

Shall remain closed > 45,000’

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9
Q

Max fuel weight

A

G600: 41,500lbs

33,500 over wing

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10
Q

Max approved pressure alt for T/O & Landing

A

15,000’

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11
Q

Max runway slope for T/O & Landing

A

+/- 2%

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12
Q

Max tailwind component for T/O & Landing

A

10kts

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13
Q

Xwind limit for static Takeoff

A

30kts

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14
Q

Max demonstrated xwind for T/O & Landing

A

G600: 30kts

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15
Q

Max tailwind component for landing flaps 10° or less

A

0kts

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16
Q

Max wind speed for landing (including gusts)

A

15kts

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17
Q

Max wind gust for landing

A

5kts

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18
Q

Use of autopilot during single engine go-around

A

Prohibited

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19
Q

Use of autothrottles for approach & landing

A

Required during normal ops

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20
Q

Use of autothrottles during single engine approach, or approach & landing with flaps 10° or 0°

A

Prohibited

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21
Q

Turbulent air penetration speed

A

> = 10,000’: 270 KCAS/.85M
<10,000’: 240 KCAS

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22
Q

Max operating speed

A

0.925M

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23
Q

Don’t operate weather radar within __ft. of refueling ops or within __ft. of ground personnel

A

50

11

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24
Q

Autopilot minimum engage height

A

200’ AGL

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25
Q

Autopilot minimum disengage height from ILS or LPV approach

A

G600: 90’ AGL

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26
Q

Autopilot minimum disengage height for all other ops

A

200’ AGL

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27
Q

Max demonstrated altitude loss for coupled go-around

A

50’

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28
Q

Use of VOR Approach (VORAP) mode

A

Prohibited if VOR station overflight is required during any portion of intermediate or final approach segments, excluding the missed approach point

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29
Q

When should Terrain be inhibited

A

For all airports not contained in EGPWS database

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30
Q

Use of SDF declutter mode

A

Prohibited

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31
Q

Starting APU with external DC power source

A

Prohibited

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32
Q

Max flap extended speed - Vfe
10°
20°
39°

A

250 KCAS
220 KCAS
180 KCAS

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33
Q

Max operating altitude for extension/flight with flaps extend it to 10 or 20°

A

25,000’ MSL

34
Q

Max operating altitude for extension/flight with flaps down

A

20,000’ MSL

35
Q

When is use of Speed breaks prohibited on G500

A

Not approved for extension with flaps at 39° or with landing gear extended in-flight

36
Q

Restrictions when operating in other than normal mode

A
  1. Max speed - 285 KCAS/.90M
  2. Crosswind for landing - 10kts
  3. Flight into known icing conditions is prohibited
37
Q

Maneuvering speed (VA)

A

206 KCAS

38
Q

Max speed if any primary flight control surface or speedbrake panel is failed due to component malfunction or hydraulic system failure

A

= 285 KCAS/.90M

39
Q

Flight attitudes

Negative & zero “g” ops limited to

A

7 sec of operation

40
Q

Max operating altitude for extending landing gear or flying with landing gear extended

A

20,000’ MSL

41
Q

Max speed for extending or retracting landing gear

A

Vlo = 225 KCAS

42
Q

Max speed for flying with Landing gear extended

A

Vle = 250 KCAS

43
Q

Max nose wheel and pedal steering authority

A

Nose +- 82°
Pedal +- 40°

44
Q

Max cabin pressure differential permitted for taxi, takeoff or landing

A

0.30psi

45
Q

Max normal differential pressure

A

10.69psi

46
Q

ECS duct temperature limit during manual zone temperature control

A

< 200°F

47
Q

FAR 91.211 Supplemental O2

Requirements for donning & using O2

A

> 41,000’ one pilot must mask
35,000’ pilot must mask if other pilot leaves cockpit

48
Q

APU starter duty cycle

A

Limited to max of three consecutive start attempts with one minute cool down period between attempts

After three start attempts, observe a one hour cool down period before attempting another start

49
Q

APU max start altitude

A

37,000’

50
Q

APU Max operating altitude

A

45,000’

51
Q

Altitude at which a APU can provide starter assist for main engine start

A

30,000’

52
Q

When is takeoff with APU operating prohibited

A

OAT > 45°C

53
Q

Max TAT for APU inflight operation

A

47°C

54
Q

Engine starter duty cycle

A

Three start attempts of up to three minutes, with 15 seconds between start cycles, followed by 10 minute cooling period. 

55
Q

Max crosswind component and tailwind component for engine ground start

A

40 kt crosswind
25 kt tailwind

56
Q

Minimum oil temp for ground start

A

-40°C

57
Q

Max start TGT

A

975°C

58
Q

Use of takeoff thrust

A

Limited to 5 minutes with all engines operating or 10 minutes for one engine in event of engine failure

59
Q

Max takeoff TGT

A

965°C for 5 min

60
Q

Max continuous TGT

A

956°C

61
Q

Speed for canceling reverse thrust

A

Initiate to be at reverse Idle by 60 KCAS

62
Q

Requirement if reverse thrust used to bring airplane to halt in emergency

A

Record and report for maintenance action

63
Q

Use of thrust reversers for power back

A

Not approved

64
Q

When is use of both thrust reversers prohibited

A

< 10 kts

65
Q

Temperature at which cowl anti-ice required for taxi and takeoff with visible moisture, precipitation, or wet runway present

A

+10°C

66
Q

When is Takeoff prohibited

A

With frost, ice, snow, or slush adhering to wings, control services, engine inlets, or other critical surfaces

67
Q

Where does automatic anti-ice feature work

A

Between 400’ AGL and 35,000’

68
Q

Use of wing and cowl anti-ice

A

Select when entry into icing conditions is imminent, or immediately upon detection of ice formation on wings, winglets or windshield edges

69
Q

Flight with flaps or landing gear extended in icing conditions

A

Restricted to takeoff, approach and landing only

Select WAI ON and confirm normal operation prior to flap extension when icing conditions exist or may exist during approach or landing

70
Q

Use of flaps in icing > 10 minutes

A

Don’t retract flaps < 10° deflection until verifying that flap leading edge is clear of ice

71
Q

Extended operations in icing conditions

A

Limited to flaps up configuration

72
Q

Operation in forecast or reported severe icing

A

Prohibited

Exit condition as soon as possible if severe icing is encountered and verify anti-ice is ON

73
Q

Ops with WAI on in flaps up configuration

A

Maintain minimum of 200 KCAS until ready to configure for landing

74
Q

When select WAI to on if required for takeoff

A

At least 4 minutes prior to setting takeoff power

20 minutes max cumulative

75
Q

Boost pump operation

A

All boost pumps should be ON for all phases of flight unless balancing fuel

76
Q

Max fuel imbalance

  • Takeoff
  • Inflight
A

Takeoff - 1000lbs

Inflight - 2000lbs

77
Q

Max Altitude with single bleed source and anti-ice on

A

32,000’

78
Q

Engine Type

A

G600: PW815GA
Thrust: 15,681 lbs
6:1 bypass ratio

79
Q

Minimum Tire Pressure

A

185psi Cyan CAS
101psi Amber CAS

80
Q

Capacity of hopper tank

A

1170 lbs