LIMITATIONS Flashcards
Min Crew:
2
Max number of occupants:
17
When not in use, the third crewmember seat must be:
Folden and Stowed
MMO with the ventral tank empty:
0.80 IMN
Maximum air temperature for flight:
ISA +35°C
Minimum temperature for takeoff or landing:
-40°C
Minimum temperature for route:
-75°C
Max tailwind component for takeoff or landing:
10 Kts
Max runway slope for takeoff or landing:
2% uphill and 2% downhill
Max/Min field pressure altitudes for takeoff or landing:
9000 ft and -2000 ft
Maximum altitude for takeoff or landing with the use of a Cabin High Datum Switch:
800A: 10,000 ft
800XP: 13,000 ft
In air transport operations, is smoking in the lavatory permitted?
No
Maximum battery charge rated immediately before takeoff shall not be greater than:
20 Amp
Minimum oil pressure for idle
25 PSI
Before taking off with the ventral tank full, each wing must contain at least how many pounds of fuel?
3,450 lbs
The maximum difference in weight of the fuel in the wing tanks is:
500 lbs
If the ventral tank contains fuel, commence transfer to the wings when the contents indicated for each wing has reduced to:
3300 lbs
Minimum required brake cooling time after one rejected takeoff
25 minutes
Minimum required brake cooling time after two rejected takeoff
45 minutes
Is the rudder bias system a no-go item?
Yes
May lift dump be used in flight?
No
May flaps and airbrakes be used in flight?
No
Maximum flap extension speeds
FLAPS 15° - 220 kts
FLAPS 25° - 175 kts
FLAPS 45° - 165 kts
Maximum altitude for procedural use of flaps for descent or holding
15000 ft
Windshield heat must be ON prior to takeoff for at least
__ minutes in ambient temperature below -10°C or
__ minutes in ambient temperatures below -20°C for
Maximum bird strike protection.
Windshield heat must be ON prior to takeoff for at least
5 minutes in ambient temperature below -10°C or
15 minutes in ambient temperatures below -20°C for
Maximum bird strike protection.
If it is not possible for the windshield for the windshield heat to be on for the prescribed
Period before takeoff, airspeed must be restricted to __ Kts indicated airspeed until an altitude of ______ ft is reached.
If it is not possible for the windshield for the windshield heat to be on for the prescribed
Period before takeoff, airspeed must be restricted to 257 Kts indicated airspeed until an altitude of 8000 ft is reached.
Maximum ramp weight:
Hawker 800: 27,520 lbs
Hawker 800XP: 28,120 lbs
Maximum takeoff weight:
Hawker 800: 27,400 lbs
Hawker 800XP: 28,000 LBS
Maximum landing weight:
23,350 lbs
Maximum zero fuel weight:
Hawker 800: 17,520 lbs
Hawker 800XP: 18,450 lbs
Where can the maximum weight that may be carried in the baggage compartments be determined?
The weight and balance manual and limitation placards on the baggage
Compartments
VMO when the ventral tank contains fuel
280 KIAS
VMO when the ventral tank is empty
335 KIAS
Maximum Mach Operating Speed (Mmo)
0.80 IMN
Rough Air Speed (VRA/MRA)
230 KIAS/0.7 IMN
Maneuvering Speed (VA)
196 KIAS
VLO/VLE
220 KIAS
Bird Strike Speed up to 8000 Ft
280 KIAS
Maximum permissible Altitude for flight
41,000 FT
Maximum altitude for takeoff or landing
9,000 ft if not Cabin Hi Datum Equipped
Minimum altitude for takeoff or landing
-2000 ft
Maximum tailwind for takeoff or landing
10 Knots
Maximum generator load
300 Amps
When icing conditions do not exist, the engine inlet anti-icing should not be used for more than __ seconds at temperatures above __°C.
When icing conditions do not exist, the engine inlet anti-icing should not be used for more than 10 seconds at temperatures above 10°C.
Hawker 800XP
Maximum ITT for Normal Takeoff, Starting, Relight
Maximum ITT for Takeoff with APR operating
Maximum Continuous ITT
Hawker 800XP
Maximum ITT for Normal Takeoff, Starting, Relight
…………………………………………………………………..978°C
Maximum ITT for Takeoff with APR operating
…………………………………………………………………..996°C
Maximum Continuous ITT…………………………..968°C
Hawker 800
Maximum ITT for Normal Takeoff, Starting, Relight
Maximum ITT for Takeoff with APR operating
Maximum Continuous ITT
Maximum ITT for Normal Takeoff, Starting, Relight
…………………………………………………………………..952°C
Maximum ITT for Takeoff with APR operating
………………………………………………………………….974°C
Maximum Continuous ITT…………………………..924°C
