G500_600 Memory Flash Cards Flashcards by Michael Jessup

Length, height & wingspan G600

L: 96’ 1” H: 25’ 3” S: 95’ 0”

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Maximum Weights?
Ramp
Takeoff
Landing
Zero fuel

Aircraft G600

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

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Max approved wt. in baggage comp

G600: 2500lbs

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Max passengers

19 Depending on floor plan

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Min taxi strip for 180° turn

G600: 65’

135’ no tiller

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Cruising Altitudes

Initial

Max

Initial: FL430
Max: FL510

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High speed cruise

0.90M

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Internal baggage door altitude restriction

Shall remain closed > 45,000’

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Max fuel weight

G600: 41,500lbs

33,500 over wing

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Max approved pressure alt for T/O & Landing

15,000’

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Max runway slope for T/O & Landing

+/- 2%

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Max tailwind component for T/O & Landing

10kts

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Xwind limit for static Takeoff

30kts

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Max demonstrated xwind for T/O & Landing

G600: 30kts

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Max tailwind component for landing flaps 10° or less

0kts

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Max wind speed for landing (including gusts)

15kts

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Max wind gust for landing

5kts

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Use of autopilot during single engine go-around

Prohibited

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Use of autothrottles for approach & landing

Required during normal ops

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

Prohibited

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Turbulent air penetration speed

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

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Max operating speed

0.925M

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

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Autopilot minimum engage height

200’ AGL

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Autopilot minimum disengage height from ILS or LPV approach

G600: 90’ AGL

Autopilot minimum disengage height for all other ops

200’ AGL

Max demonstrated altitude loss for coupled go-around

50’

Use of VOR Approach (VORAP) mode

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

When should Terrain be inhibited

For all airports not contained in EGPWS database

Use of SDF declutter mode

Prohibited

Starting APU with external DC power source

Prohibited

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

250 KCAS 220 KCAS 180 KCAS

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

25,000’ MSL

Max operating altitude for extension/flight with flaps down

20,000’ MSL

When is use of Speed breaks prohibited on G500

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

Restrictions when operating in other than normal mode

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

Maneuvering speed (VA)

206 KCAS

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

= 285 KCAS/.90M

Flight attitudes Negative & zero “g” ops limited to

7 sec of operation

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

20,000’ MSL

Max speed for extending or retracting landing gear

Vlo = 225 KCAS

Max speed for flying with Landing gear extended

Vle = 250 KCAS

Max nose wheel and pedal steering authority

Nose +- 82° Pedal +- 40°

Max cabin pressure differential permitted for taxi, takeoff or landing

0.30psi

Max normal differential pressure

10.69psi

ECS duct temperature limit during manual zone temperature control

< 200°F

FAR 91.211 Supplemental O2 Requirements for donning & using O2

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

APU starter duty cycle

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

APU max start altitude

37,000’

APU Max operating altitude

45,000’

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

30,000’

When is takeoff with APU operating prohibited

OAT > 45°C

Max TAT for APU inflight operation

47°C

Engine starter duty cycle

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

Max crosswind component and tailwind component for engine ground start

40 kt crosswind 25 kt tailwind

Minimum oil temp for ground start

-40°C

Max start TGT

975°C

Use of takeoff thrust

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

Max takeoff TGT

965°C for 5 min

Max continuous TGT

956°C

Speed for canceling reverse thrust

Initiate to be at reverse Idle by 60 KCAS

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

Record and report for maintenance action

Use of thrust reversers for power back

Not approved

When is use of both thrust reversers prohibited

< 10 kts

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

+10°C

When is Takeoff prohibited

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

Where does automatic anti-ice feature work

Between 400’ AGL and 35,000’

Use of wing and cowl anti-ice

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

Flight with flaps or landing gear extended in icing conditions

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

Use of flaps in icing > 10 minutes

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

Extended operations in icing conditions

Limited to flaps up configuration

Operation in forecast or reported severe icing

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

Ops with WAI on in flaps up configuration

Maintain minimum of 200 KCAS until ready to configure for landing

When select WAI to on if required for takeoff

At least 4 minutes prior to setting takeoff power 20 minutes max cumulative

Boost pump operation

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

Max fuel imbalance - Takeoff - Inflight

Takeoff - 1000lbs Inflight - 2000lbs

Max Altitude with single bleed source and anti-ice on

32,000’

Engine Type

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

Minimum Tire Pressure

185psi Cyan CAS 101psi Amber CAS

Capacity of hopper tank

1170 lbs