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G550 limitations
| Question | Answer |
|---|---|
| Maximum runway slope for takeoff and landing operations | +2% uphill -2% downhill |
| Maximum tailwind component approved for takeoff and landing | 10 knots |
| Maximum approved airport pressure altitude for takeoff or landing | 12,000 ft. ( A/C SN 5001-5059 NOT havingASC040) 14,500ft ( A/C SN 5001-5059 having ASC 040) 14,500ft ( A/C SN 5060-sub) 15,000ft (A/C SN 5323-sub + HLFE PAX oxygen controller) |
| Maximum operating altitude | 51,000 ft |
| Maximum altitude with a single air conditioning pack operating | 48,000ft |
| Maximum operating altitude with the yaw damper inoperative | 45,000ft |
| Maximum landing gear extension altitude | 20,000ft msl |
| Maximum altitude for extending flaps 39degrees | 20,000ft MSL |
| Maximum altitude for extending flaps 10 or 20 degrees | 25,000ft msl |
| Minimum control speed, air | 112 kcas |
| Minimum control speed, landing | 110 kcas |
| Minimum control speed, ground | 107 kcas sea level 86 kcas (15,000ft) |
| Maneuvering speed (va) | 206 kcas |
| Flaps extended speeds (Vfe/Mfe) | Takeoff(10deg): 250 kcas/.60M T/O APP(20 deg):220 kcas/.60M Down(39def):170 kcas/.60M |
| Landing gear extended speed(Vle/Mle) | 250 kcas/.70M ( gear door open or close) |
| Landing gear Operating Speeds (Vlo/Mlo) | 225 kcas/.70M( normal operations) 175 kcas( alternate operation) |
| Maximum speeds with yaw damper Inoperative | 260 Kcas/.80M (above 10,000ft) 250 kcas ( below 10,000ft) |
| Minimum speeds with yaw damper inoperative | 210 (above 20,000ft.) Use reference table below 20,000 ft) |
| Maximum speed with Mach trim or electric elevator trim inoperative | .80M |
| Turbulence penetration speeds | 270 kcas/.80 M above 10,000 ft 240 kcas below 10,000 ft |
| Maximum tire speeds | 195 kts |
| Maximum speed with emergency stabilizer trim armed, autopilot engaged and a jammed elevator | 270kcas/.80M |
| Maximum zero fuel weight | 54,500lb G500 and G550 52,000lb for EASA AIRCRAFT |
| Maximum ramp weight | 91,400 lb g550 85,500 lb g500 |
| Maximum takeoff weight | 91,000 lb g550 85,100 lb g500 |
| Maximum landing weight | 75,300 lb g550 and g500 |
| Maximum fuel Inbalance for flight | 2000 lb |
| Proceed with fuel inbalancing before the fuel imbalance exceeds | 1000 lbs |
| Maximum cabin differential | 10.48 PSI (.3 for taxi takeoff and landing) |
| Internal baggage door shall remain closed above | 40,000 ft ( limit if 5 minutes open) |
| Single engine autopilot coupled to around | NOT APPROVED |
| minimum autopilot engage height | 200ft |
| Minimum autopilot disengage height | 60 feet from an ils approach 50 feet below MDA/DA from an LNAV/VNAV approach) |
| Use of auto throttles on a single engine approach | NOT PERMITTED |
| Use of speed brakes with the HMG in operation | SLOW OPERATION (Approximately 3 seconds for full range of movement) |
| Speed brakes not approved for extension in flight when | FLAPS 39 deg, or LANDING GEAR EXTENDED |
| Takeoff permitted with automatic ground spoilers inoperative provided | -ANTI-SKID IS OPERATIVE -20deg FLAPS ARE USED -COWL AND WING ANTI-ICE SYSTEM ARE NOT USED |
| Usable fuel capacity | 41,300 lb g550 35,200 lb g500 (EXCEEDANCE IS PERMITTED AS LONG AS THE MAX RAMP WEIGHT OR MAX TAKEOFF WEIGHT ARE NOT EXCEEDED, AND THE LOADED AIRCRAFT CG IS WITHIN LIMITS |
| Wing anti-ice 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 +10Deg C, 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 IR PRECIPITATION IS PRESENT OR WHEN SIGNA OF ICING ARE OBSERVED |
| Procedure to shed engine ice in flight is | QUICKLEY Retard one engine at a time to idle hold for five seconds and then accelerate engine to 90% LPRPM the power lever may then be returned to its original position |
| Use of flaps while holding an ice and conditions | Not permitted |
| Takeoff is permitted with anti-skid inoperative, provide | -RUNWAY IS DRY -GROUND SPOILERS ARE INOPERATIVE -20 deg FLAPS ARE USED -COWL AND WING ANTIICE SYSTEMS ARE NOT USED |
| Do not operate weather radar on the ground | -during refueling of the airplane within 300 feet92 m of fueling operations -within 49 feet 15 m 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) |
| The following 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 | Select TA ONLY as the operating mode |
| MAXIMUM SPEED FOR RVSM OPERATIONS | .87M |
| Crew and Passenger oxygen mask or not approved for use above | -25,000 ft cabin altitude for passenger masks -40,000 ft cabin altitude (crew masks) (NOTE: if you have the newer Scott EROS crew mask installed it is approved for use to a cabin altitude to 45,000 feet |
| General EICAS range markings colors | Normal range: GREEN OR WHITE Caution range: AMBER Wrninf range: RED |
| APU starting limits ( battery power) | 3 consecutive starts attempts Followed by 1 hour cool down |
| APU staring limits ( external DC power) | 3 start attempts 15 minute cool down in between each attempt |
| Maximum APU operating altitude | 45,000 ft |
| APU generator electric load limit | 109%( 40 kVA) sea level to 45,000 ft |
| Maximum engine TGT prior to ground start | 150 deg C |
| Maximum takeoff TGT | 900deg C ( 5 minutes with both engines/ 10 minutes w/ one engine) |
| Maximum continuous TGT | 860 deg C ( NO TIME LIMITATION) |
| Maximum crosswind component for engine start | 30 kts |
| Maximum tailwind component for engine start | 20 kts |
| Stabilized engine operation on the ground static is prohibited between | 66% and 80% LP RPM |
| The preferred method of engine airstart is | AUTOMATIC |
Created by:
Caleenc2998