Limitations Flashcards
G500
Ramp Wt.
Takeoff Wt.
Landing Wt.
Zero Fuel Wt.
80,000 lbs.
79,600 lbs.
64,350 lbs.
52,100 lbs.
Length, height and wingspan?
G500 / G600
G500 92x88x26
G600 97x95x26
G600
Max Ramp Wt.
Max Takeoff Wt.
Max Landing Wt.
Max Zero Fuel Wt.
95,000 lbs.
94,600 lbs.
76,800 lbs.
57,440 lbs.
Max approved weight in baggage compartment?
G500: 2250 lbs
G600: 2500 lbs
Max passengers?
19
(depending on floor plan)
Min taxi strip for 180° turn?
G500: 57 ft
G600: 60 ft
Cruising altitudes?
Initial
Max
Initial FL430
Max FL510
High speed cruise?
0.90 M
Internal baggage door altitude
restriction?
Shall remain closed > 45,000 ft
Max fuel weight?
G500
G600
G500: 30,250 lbs
G600: 41,500 lbs
Max approved airport pressure altitude for takeoff
and landing?
15,000 ft
Max runway slope for takeoff
and landing operations?
± 2%
Max tailwind component for takeoff
and landing?
10 kts
Crosswind limit for static takeoff?
30 kts
Max demonstrated crosswind for
takeoff and landing?
G500: 33 kts
G600: 30 kts
Max tailwind component for
landing with flaps 10° or less?
0 kts
Use of autopilot during
single engine go-around?
Prohibited
Use of autothrottles during
single engine approach,
or approach and landing with
flaps 10° or flaps 0°?
Prohibited
Turbulent air penetration speed?
≥ 10,000 ft: 270 KCAS/.85 MT
< 10,000 ft: 240 KCAS
Max operating speed?
0.925 M
Don’t operate weather radar within ____ ft. of refueling ops or within ___ ft. of ground personnel?
50
11
Autopilot minimum engage height?
200 ft AGL
1
Autopilot minimum disengage
height from ILS or LPV approach?
G500: Flaps 39: 90 ft AGL
Flaps 0/10/20: 130 ft AGL
G600: 90 ft AGL for all flap settings
Autopilot minimum disengage
height for all other operations?
200 ft AGL
Autopilot minimum disengage
height from ILS or LPV approach?
G500: Flaps 39: 90 ft AGL
Flaps 0/10/20: 130 ft AGL
G600: 90 ft AGL for all flap settings
Max demonstrated altitude
loss for coupled go-around?
50 ft
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 airports not contained in EGPWS database
Use of SFD declutter mode?
Prohibited
Starting APU using external DC power source?
Prohibited
Max Flap Extended speed—VFE
10° flaps?
20° flaps?
Flaps down?
G500 G600
Takeoff (10) 250 KCAS
T/O APP (20) 220 KCAS
Down (39) 180 KCAS
Max operating altitude for extension/flight
with flaps extended to 10 or 20°?
25,000 ft MSL
Max operating altitude for extension/flight
with flaps down?
20,000 ft MSL
Restrictions when operating in other than normal mode?
- MAX Speed - 285 KCAS / .90M
- Crosswind for landing - 10 kts
- Flight into known icing conditions is prohibited
Maneuvering Speed (VA)?
206 KCAS
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.
≤ 285 KCAS / 0.90M
Max operating altitude for extending landing gear
or flying with landing gear extended?
20,000 ft MSL
Max speed for extending or retracting landing gear?
Vlo = 225 KCAS
Max speed for flying with landing gear
extended?
Vle = 250 KCAS
Max speed for flying with landing gear
extended after alternate extension?
225 KCAS
Max nose wheel and pedal steering
authority?
Nose ± 82°
Pedal ± 40°
Max cabin pressure differential
permitted for taxi, takeoff or landing?
0.30 psi
Max normal differential pressure?
10.69 psi
ECS duct temperature limit during manual
zone temperature control?
< 200°F
FAR 91.211
Supplemental oxygen.Requirements for donning and
using supplemental oxygen? Pressurized aircraft
> 41,000 ft: one pilot must mask
> 35,000 ft: pilot must mask if other pilot leaves
cockpit
FAR 135.89
Supplemental Oxygen
Pilot requirements: Use of oxygen.
Pressurized aircraft
> 35,000 ft: one pilot must mask
> 25,000 ft: pilot must mask if other pilot leaves
cockpit
APU starter duty cycle?
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.
APU max start altitude?
37,000 ft
APU max operating altitude?
45,000 ft
Max altitude at which APU can provide
starter-assist for main engine start?
30,000 ft
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 3 min, with 15 sec
between start cycles, followed by 10 min cooling
period.
Max crosswind component and tailwind
component for engine ground start?
40 kt crosswind
25 kt tailwind
Min oil temp for ground start?
-40°C
Max start TGT?
975°C
Use of takeoff thrust?
Limited to 5 min with all engines operating or
10 min for one engine in event of engine failure
Max takeoff TGT?
965°C for 5 min
Max continuous TGT?
956°C
Speed for cancelling 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
Limit for engine operation below zero G?
7 seconds
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 surfaces,
engine inlets, or other critical surfaces.
What altitude does automatic anti-ice feature work?
Between 400 ft AGL and 35,000 ft
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.
Minimum speed for 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
Boost pump operation?
All boost pumps should be ON for all
phases of flight unless balancing fuel.
Max fuel imbalance?
- Takeoff
- Inflight
Takeoff - 1000 lbs
Inflight - 2000 lbs
