G550 Limitations Flashcards
Maximum runway slope for takeoff and landing operations
+/- 2%
Maximum tailwind component approved for takeoff and landing
10 knots
Maximum approved airport pressure altitude for takeoff and landing
14,500 normal
12,000 early models without mod
15,000 later models with high alt mod
Maximum operating altitude
51,000 feet
Maximum altitude with a single air conditioning pack operating
48,000 feet
Maximum operating altitude with the yaw damper inop
45,000 feet
Maximum landing gear extension altitude
20,000 feet
Maximum altitude for extending flaps 39
20,000 feet
Maximum altitude for extending flaps 10 or 20
25,000 feet
Minimum control speed, air
112 KCAS
Minimum control speed, landing
110 KCAS
Minimum control speed, ground
107 KCAS (Sea Level) 86 KCAS (15,000 ft)
Maneuvering speed (Va)
206 KCAS
Flaps extended speed (Vfe/Mfe)
Takeoff (10): 250 KCAS/0.60M
T/O APP (20): 220 KCAS/0.60M
DOWN (39): 170 KCAS/0.60M
Landing gear extended speed (Vle/Mle)
250 KCAS/0.70M (gear doors open or closed)
Landing gear operation speeds (Vlo/Mlo)
225 KCAS/0.70M (normal ops) 175 KCAS (alternate ops)
Maximum speeds with yaw damper inop
210 knots above 20,000 ft
Use ref table below 20,000 ft
Maximum speed with Mach Trim or electric elevator trim inop
0.80M
Turbulence penetration speeds
270KCAS/0.80M above 10,000 ft
240 KCAS below 10,000 ft
Maximum tire speed
195 knots
Maximum speed with emergency stab trim armed, autopilot engaged and a jammed elevator
270 KCAS / 0.80M
Maximum zero fuel weight
54,500 lbs
Maximum ramp weight
91,400 lbs
Maximum takeoff weight
91,000 lbs
Maximum landing weight
75,300 lbs
Maximum fuel imbalance in flight
2,000 lbs
Proceed with fuel balancing before the fuel imbalance exceeds:
1,000 lbs
Maximum cabin pressure differentials:
- 48 psi
0. 3 psi for taxi, takeoff and landing
Internal baggage door shall remain closed above:
40,000 feet (limited to 5 mins open)
Is a single engine autopilot-coupled go-around approved?
No
Minimum autopilot engage height
200 feet
Minimum autopilot disengage height
60’ below DH on ILS
50’ below MDA from LNAV/VNAV
Are autothrottles allowed for single-engine approaches?
No
Use of speedbrakes with the HMG in operation:
Slow operation (3 seconds for full range of movement)
Speedbrakes not approved for extension in flight when:
Flaps 39 or Landing Gear Extended
Takeoff permitted with automatic ground spoilers inoperative provided:
Anti-skid is operative
20 Flaps used
Cowl and Wing anti-ice systems are not used
Usable fuel capacity:
41,300 lbs
Wing anti-icing must be turned on:
If icing conditions are imminent, or immediately upon detection of ice formation on wings, winglets or windshield edges
Cowl anti-icing is required on the ground:
When the SAT is +10C or below and visible moisture, precipitation, or wet runways are present
Cowl anti-icing is required in flight:
As indicated in the cowl anti-icing table, when visible moisture or precipitation is present or when signs of icing are observed
Procedure to shed engine ice in flight:
Quickly retard one engine at a time to idle, hold for 5 seconds and then accelerate engine to 90% LP RPM.
The power lever may then be returned to its original position
Use of flaps while holding in icing conditions:
Not permitted
Takeoff is permitted with anti-skid inoperative, provided:
Runway is dry
Ground spoilers are operative
20 Flaps used
Cowl and wing anti-ice systems are not used
Do not operate weather radar on the ground:
During refueling
Within 300 feet of fueling ops
Within 49 feet of ground personnel
A current FMS database is required for:
GPS approaches
Localizer based approaches must be flown using the following displayed / coupled navigation source:
NAV (“Green” data)
What approaches may be flown using FMS as the displayed/coupled source?
RNAV(GPS)
VOR, VOR/DME, VOR/DME RNAV
NDB
GPS
TCAS operation with one engine inoperative:
TA ONLY
Maximum speed for RVSM operations
0.87 M
Crew and passenger masks are not approved for use above:
25,000 for passenger masks
40,000 for crew masks
45,000 if a/c has Scott EROS crew masks
General EICAS range markings colors:
Normal range values - green or white
Caution range values - Amber
Warning range values - Red
APU starting limits (battery power):
3 consecutive start attempts, followed by 1 hour cooldown
APU starting limits (external DC power):
3 start attempts, 15 minute cooldown between each attempt
Maximum APU operating altitude
45,000 feet
APU generator electrical load limit:
100% (40kVA) sea level to 45,000 feet
Maximum engine TGT prior to ground start:
150 C
Maximum takeoff TGT:
900 C
5 minutes with both engines
10 minutes on one engine
Maximum continuous TGT:
860 C - no time limit
Maximum crosswind component for engine start:
30 knots
Maximum tailwind component for engine start:
20 knots
Stabilized engine operation on the ground (static) is prohibited between what power settings?
66% - 80% LP RPM
The preferred method of engine airstart is:
Automatic
