LIMITATIONS Flashcards

1
Q

Min Crew:

A

2

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2
Q

Max number of occupants:

A

17

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3
Q

When not in use, the third crewmember seat must be:

A

Folden and Stowed

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4
Q

MMO with the ventral tank empty:

A

0.80 IMN

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5
Q

Maximum air temperature for flight:

A

ISA +35°C

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6
Q

Minimum temperature for takeoff or landing:

A

-40°C

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7
Q

Minimum temperature for route:

A

-75°C

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8
Q

Max tailwind component for takeoff or landing:

A

10 Kts

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9
Q

Max runway slope for takeoff or landing:

A

2% uphill and 2% downhill

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10
Q

Max/Min field pressure altitudes for takeoff or landing:

A

9000 ft and -2000 ft

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11
Q

Maximum altitude for takeoff or landing with the use of a Cabin High Datum Switch:

A

800A: 10,000 ft
800XP: 13,000 ft

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12
Q

In air transport operations, is smoking in the lavatory permitted?

A

No

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13
Q

Maximum battery charge rated immediately before takeoff shall not be greater than:

A

20 Amp

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14
Q

Minimum oil pressure for idle

A

25 PSI

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15
Q

Before taking off with the ventral tank full, each wing must contain at least how many pounds of fuel?

A

3,450 lbs

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16
Q

The maximum difference in weight of the fuel in the wing tanks is:

A

500 lbs

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17
Q

If the ventral tank contains fuel, commence transfer to the wings when the contents indicated for each wing has reduced to:

A

3300 lbs

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18
Q

Minimum required brake cooling time after one rejected takeoff

A

25 minutes

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19
Q

Minimum required brake cooling time after two rejected takeoff

A

45 minutes

20
Q

Is the rudder bias system a no-go item?

A

Yes

21
Q

May lift dump be used in flight?

A

No

22
Q

May flaps and airbrakes be used in flight?

A

No

23
Q

Maximum flap extension speeds

A

FLAPS 15° - 220 kts
FLAPS 25° - 175 kts
FLAPS 45° - 165 kts

24
Q

Maximum altitude for procedural use of flaps for descent or holding

A

15000 ft

25
Q

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.

A

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.

26
Q

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.

A

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.

27
Q

Maximum ramp weight:

A

Hawker 800: 27,520 lbs
Hawker 800XP: 28,120 lbs

28
Q

Maximum takeoff weight:

A

Hawker 800: 27,400 lbs
Hawker 800XP: 28,000 LBS

29
Q

Maximum landing weight:

A

23,350 lbs

30
Q

Maximum zero fuel weight:

A

Hawker 800: 17,520 lbs
Hawker 800XP: 18,450 lbs

31
Q

Where can the maximum weight that may be carried in the baggage compartments be determined?

A

The weight and balance manual and limitation placards on the baggage
Compartments

32
Q

VMO when the ventral tank contains fuel

A

280 KIAS

33
Q

VMO when the ventral tank is empty

A

335 KIAS

34
Q

Maximum Mach Operating Speed (Mmo)

A

0.80 IMN

35
Q

Rough Air Speed (VRA/MRA)

A

230 KIAS/0.7 IMN

36
Q

Maneuvering Speed (VA)

A

196 KIAS

37
Q

VLO/VLE

A

220 KIAS

38
Q

Bird Strike Speed up to 8000 Ft

A

280 KIAS

39
Q

Maximum permissible Altitude for flight

A

41,000 FT

40
Q

Maximum altitude for takeoff or landing

A

9,000 ft if not Cabin Hi Datum Equipped

41
Q

Minimum altitude for takeoff or landing

A

-2000 ft

42
Q

Maximum tailwind for takeoff or landing

A

10 Knots

43
Q

Maximum generator load

A

300 Amps

44
Q

When icing conditions do not exist, the engine inlet anti-icing should not be used for more than __ seconds at temperatures above __°C.

A

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.

45
Q

Hawker 800XP
Maximum ITT for Normal Takeoff, Starting, Relight
Maximum ITT for Takeoff with APR operating
Maximum Continuous ITT

A

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

46
Q

Hawker 800
Maximum ITT for Normal Takeoff, Starting, Relight
Maximum ITT for Takeoff with APR operating
Maximum Continuous ITT

A

Maximum ITT for Normal Takeoff, Starting, Relight
…………………………………………………………………..952°C

Maximum ITT for Takeoff with APR operating
………………………………………………………………….974°C
Maximum Continuous ITT…………………………..924°C