Limitations Flashcards

1
Q

G500

Ramp Wt.
Takeoff Wt.
Landing Wt.
Zero Fuel Wt.

A

80,000 lbs.
79,600 lbs.
64,350 lbs.
52,100 lbs.

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2
Q

Length, height and wingspan?
G500 / G600

A

G500
Length 91‘2“x span 87’ 1”, height 25‘6“,

91x87x26

G600
Length 96’ 1”x span 95.0”height 26’3”
96x95x26

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3
Q

G600
Max Ramp Wt.
Max Takeoff Wt.
Max Landing Wt.
Max Zero Fuel Wt.

A

95,000 lbs.
94,600 lbs.
76,800 lbs.
57,440 lbs.

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4
Q

Max approved weight in baggage compartment?

A

G500: 2250 lbs
G600: 2500 lbs

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5
Q

Max passengers?

A

19

(depending on floor plan)

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6
Q

Min taxi strip for 180° turn?

A

G500: 57 ft
G600: 60 ft

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7
Q

Cruising altitudes?
Initial
Max

A

Initial FL430
Max FL510

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8
Q

High speed cruise?

A

0.90 M

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9
Q

Internal baggage door altitude

restriction?

A

Shall remain closed > 45,000 ft

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10
Q

Max fuel weight?
G500
G600

A

G500: 30,250 lbs
G600: 41,500 lbs

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11
Q

Max approved airport pressure altitude for takeoff

and landing?

A

15,000 ft

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12
Q

Max runway slope for takeoff
and landing operations?

A

± 2%

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13
Q

Max tailwind component for takeoff

and landing?

A

10 kts

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14
Q

Crosswind limit for static takeoff?

A

30 kts

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15
Q

Max demonstrated crosswind for
takeoff and landing?

A

G500: 33 kts
G600: 30 kts

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16
Q

Max tailwind component for
landing with flaps 10° or less?

A

0 kts

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17
Q

Use of autopilot during
single engine go-around?

A

Prohibited

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18
Q

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

A

Prohibited

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19
Q

Turbulent air penetration speed?

A

≥ 10,000 ft: 270 KCAS/.85 MT
< 10,000 ft: 240 KCAS

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20
Q

Max operating speed?

A

0.925 M

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21
Q

Don’t operate weather radar within ____ ft. of refueling ops or within ___ ft. of ground personnel?

A

50

11

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22
Q

Autopilot minimum engage height?

A

200 ft AGL

1

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23
Q

Autopilot minimum disengage
height from ILS or LPV approach?

A

G500: Flaps 39: 90 ft AGL
Flaps 0/10/20: 130 ft AGL

G600: 90 ft AGL for all flap settings

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24
Q

Autopilot minimum disengage
height for all other operations?

A

200 ft AGL

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25
Q

Autopilot minimum disengage
height from ILS or LPV approach?

A

G500: Flaps 39: 90 ft AGL
Flaps 0/10/20: 130 ft AGL

G600: 90 ft AGL for all flap settings

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26
Q

Max demonstrated altitude
loss for coupled go-around?

A

50 ft

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27
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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28
Q

When should Terrain be inhibited?

A

For airports not contained in EGPWS database

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29
Q

Use of SFD declutter mode?

A

Prohibited

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30
Q

Starting APU using external DC power source?

A

Prohibited

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31
Q

Max Flap Extended speed—VFE

10° flaps?
20° flaps?
Flaps down?

A

G500 G600
Takeoff (10) 250 KCAS
T/O APP (20) 220 KCAS
Down (39) 180 KCAS

32
Q

Max operating altitude for extension/flight
with flaps extended to 10 or 20°?

A

25,000 ft MSL

33
Q

Max operating altitude for extension/flight

with flaps down?

A

20,000 ft MSL

34
Q

Restrictions when operating in other than normal mode?

A
  1. MAX Speed - 285 KCAS / .90M
  2. Crosswind for landing - 10 kts
  3. Flight into known icing conditions is prohibited
35
Q

Maneuvering Speed (VA)?

A

206 KCAS

36
Q

Max speed if primary flight control surface (other
than rudder) or spoiler panel is failed, caused by
either component malfunction(s) or hydraulic sys-
tem failure.

A

≤ 285 KCAS / 0.90M

37
Q

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

A

20,000 ft MSL

38
Q

Max speed for extending or retracting landing gear?

A

Vlo = 225 KCAS

39
Q

Max speed for flying with landing gear

extended?

A

Vle = 250 KCAS

40
Q

Max speed for flying with landing gear
extended after alternate extension?

A

225 KCAS

41
Q

Max nose wheel and pedal steering

authority?

A

Nose ± 82°
Pedal ± 40°

42
Q

Max cabin pressure differential
permitted for taxi, takeoff or landing?

A

0.30 psi

43
Q

Max normal differential pressure?

A

10.69 psi

44
Q

ECS duct temperature limit during manual
zone temperature control?

A

< 200°F

45
Q

FAR 91.211
Supplemental oxygen.Requirements for donning and
using supplemental oxygen? Pressurized aircraft

A

> 41,000 ft: one pilot must mask

> 35,000 ft: pilot must mask if other pilot leaves

cockpit

46
Q

FAR 135.89
Supplemental Oxygen
Pilot requirements: Use of oxygen.
Pressurized aircraft

A

> 35,000 ft: one pilot must mask

> 25,000 ft: pilot must mask if other pilot leaves

cockpit

47
Q

APU starter duty cycle?

A

Limited to max of 3 consecutive startattempts with
a one minute cool downperiod between attempts.

After three start attempts,
observe a 1-hour cool down period
before attempting another start.

48
Q

APU max start altitude?

A

37,000 ft

49
Q

APU max operating altitude?

A

45,000 ft

50
Q

Max altitude at which APU can provide
starter-assist for main engine start?

A

30,000 ft

51
Q

When is takeoff with APU operating prohibited?

A

OAT > 45°C

52
Q

Max TAT for APU inflight operation?

A

47°C

53
Q

Engine starter duty
cycle?

A

Three start attempts of up to 3 min, with 15 sec
between start cycles, followed by 10 min cooling

period.

54
Q

Max crosswind component and tailwind
component for engine ground start?

A

40 kt crosswind
25 kt tailwind

55
Q

Min oil temp for ground start?

A

-40°C

56
Q

Max start TGT?

A

975°C

57
Q

Use of takeoff thrust?

A

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

58
Q

Max takeoff TGT?

A

965°C for 5 min

59
Q

Max continuous TGT?

A

956°C

60
Q

Speed for cancelling reverse thrust?

A

Initiate to be at reverse idle by 60 KCAS

61
Q

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

A

Record and report for maintenance action

62
Q

Use of thrust reversers for
power back?

A

Not approved

63
Q

When is use of both
thrust reversers prohibited?

A

< 10 kts

64
Q

Limit for engine operation below zero G?

A

7 seconds

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 surfaces,
engine inlets, or other critical surfaces.

67
Q

What altitude does automatic anti-ice feature work?

A

Between 400 ft AGL and 35,000 ft

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

Minimum speed for 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

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 - 1000 lbs
Inflight - 2000 lbs