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Exam (elaborations)

GulfStream G600 limitations || with 100% Verified Solutions.

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  • Course
  • GulfStream G600
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  • GulfStream G600

Wing Span correct answers 95' Length of the G600 correct answers 96' 1" Height of the tail of the 600 correct answers 25' 3" Max Ramp Weight correct answers 95,000 pounds Max take off weight correct answers 94,600 pounds Max landing weight correct answers 76,800 pounds Max Zero Fu...

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  • October 13, 2024
  • 5
  • 2024/2025
  • Exam (elaborations)
  • Questions & answers
  • GulfStream G600
  • GulfStream G600
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FullyFocus
GulfStream G600 limitations || with 100% Verified
Solutions.
Wing Span correct answers 95'

Length of the G600 correct answers 96' 1"

Height of the tail of the 600 correct answers 25' 3"

Max Ramp Weight correct answers 95,000 pounds

Max take off weight correct answers 94,600 pounds

Max landing weight correct answers 76,800 pounds

Max Zero Fuel Weight (MZFW) correct answers 57,440 pounds

Max approved weight in baggage compartment? correct answers 2500 pounds

Maximum number of passengers? correct answers 19 depending on floor plan.

Minimum width of taxi strip for a 180° turn correct answers 65'

Flight, cruising altitude correct answers Initial flight level 43,000 maximum flight level 51,000.

High speed cruise correct answers 0.90 Mach

Internal baggage door, altitude restriction correct answers Door shall remain closed above 45,000
feet

Maximum Fuel Weight correct answers 41,500 pounds

Maximum approved Airport pressure altitude for takeoff and landing? correct answers 15,000
feet

Maximum runway slope for takeoff and landing operations? correct answers +/- 2 %

Maximum tailwind component for takeoff and landing correct answers 10 knots

Crosswind limit for static take off? correct answers 30 knots

Maximum demonstrated crosswind for takeoff and landing? correct answers 30 Knots.

Maximum tailwind component for landing with flaps 10° or less? correct answers 0 Knots.

, Use of auto pilot during single engine go around? correct answers Is Prohibited.

Use of auto throttle's during single engine, approach or approach and landing with flaps 10° or
flaps 0? correct answers Is prohibited.

Turbulent Air Penetration Speed correct answers Equal to or greater than 10,000 feet, 270
KCAS/ .85 MT
Less than 10,000 feet 240 KCAS

Maximum operating speed? correct answers 0.925 Mach.

Do not operate weather radar within ——- feet of refueling operations or within——-feet of
ground personal? correct answers 50' and 11'

Auto pilot minimum engage height? correct answers 200 feet AGL.

Auto pilot minimum disengage height from ILS or LPV approach? correct answers 90 feet AGL
for all flap settings.

Auto pilot minimum disengage height for all other operations excluding ILS or LPV? correct
answers 200 foot AGL.

Maximum demonstrated altitude loss for coupled, go- around? correct answers 50 feet

Use of VOR approach (VORAP) mode? correct answers Prohibited if VOR station over flight is
required during any portion of intermediate or final approach segments, excluding the missed
approach point.

When should terrain be inhibited? correct answers For airports not contained in EGPWS
database.

Use of SFD declutter mode? correct answers Is prohibited.

Starting APU using external DC power source? correct answers Is prohibited.

Maximum Flap Extended Speed (Vfe) 10 degrees correct answers 250 kn

Maximum Flap Extended Speed (Vfe) 20° correct answers 220 kn

Maximum Flap Extended Speed (Vfe) flaps down full? correct answers 180 kn

Maximum operating altitude for extension/flight with flaps extended to 10 or 20° correct answers
25,000 feet MSL

Maximum operating altitude for extension/flight with flaps down full? correct answers 20,000
feet MSL

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