Limitations Flashcards

1
Q

Max Takeoff Weight -800?

A

27,400 lbs.

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2
Q

Mmo with the ventral tank empty is?

A

.80 Mach

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3
Q

Vmo when the ventral tank is empty?

A

-335 kts.

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4
Q

Vmo when the ventral tank contains fuel?

A

-280 kts.

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5
Q

What is max temperature for flight?

A

-ISA +35°C

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6
Q

Minimum temp for takeoff and landing?

A

-40°C

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7
Q

Minimum temperature en-route?

A

-75°C

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8
Q

The maximum demonstrated crosswind component for takeoff or landing is?

A

30 kts.

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9
Q

The maximum runway slope for takeoff or landing is?

A

+ or - 2%

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10
Q

The bird strike speed up to 8 000 feet is?

A

-280 kts.

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11
Q

Maneuvering Speed Va is?

A

-196 kts.

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12
Q

The maximum and minimum altitudes for takeoff or landing without the use of a Cabin High is?

A

+9,000 feet to -2,000 feet.

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13
Q

How is the main cabin door counterbalanced?

A

-With a spring-loaded Tensator Motor.

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14
Q

What is the maximum continuous generator load limit?

A
  • 300 Amps
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15
Q

What are the BJM -800’s batteries rated at?

A
  • 24 Volts and 28 Amp hours.
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16
Q

What voltage range is required for the GPU to energize the bus bar system on the -800?

A
  • 24.5 to 29.5 Volts.
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17
Q

What is the max charging rate immediately before takeoff?

A
  • 20 Amps
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18
Q

What are the limitations that need to be met to hook up and use a GPU?

A
  • 28 Volts
  • 1,100 Amp current limiter
  • 1,500 Amp short term capacity
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19
Q

How many Volts does the APU generator produce?

A
  • 25 Volt DC
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20
Q

What kind of engines are installed on BJM’s -800?

A
  • Honeywell TFE-731-5R-1H
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21
Q

What is the minimum oil pressure for idle?

A
  • 25 PSI
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22
Q

How many fire extinguisher bottles are in the rear bay?

A
  • Three
23
Q

Before filling the ventral tank, the wings must contain how much fuel in each side?

A
  • 1,000 pounds
24
Q

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

A
  • 3,450 lbs
25
Q

The maximum allowable refuel pressure from the truck is:

A
  • 50 PSI
26
Q

The maximum allowable de-fuel suction is:

A
  • 11 PSI
27
Q

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

A
  • 500 lbs
28
Q

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

A
  • 3,300 lbs
29
Q

How long does the transfer of fuel from the ventral tank to the wing tanks take?

A
  • Approx. 12 minutes
30
Q

If the Ventral (Auxiliary) tank contains fuel, the VMO horn will sound whenever the aircraft speed exceeds:

A
  • 280 Kts
31
Q

Fuel is supplied to the fuel control units by two:

A
  • 28 VDC fuel pumps
32
Q

If the fuel quantity is less than ______ pounds, a go-around should not be attempted.

A
  • 400 lbs
33
Q

The main hydraulic accumulator is charged to how many PSI when empty?

A
  • 1,000 PSI
34
Q

The Emergency Brake hydraulic accumulator is charged to how many PSI when empty?

A
  • 1,000 PSI
35
Q

The purpose of the Pressure Maintaining Valve (PMV) is to trap how many PSI for normal braking with anti-skid?

A
  • 2,300 PSI
36
Q

What s normal hydraulic pressure?

A
  • 3,000 PSI
37
Q

In order to ensure adequate braking before engine start, there should be a minimum of how many PSI displayed on the emergency brake accumulator gauge?

A
  • 1,750 PSI
38
Q

The maximum published turning range of the nose wheel steering system is how many degrees left and right of center?

A
  • 45°
39
Q

If either throttle is retarded to less than 65% N1 the landing gear warning horn will sound when speed is less than how many knots?

A
  • 150 Kts
40
Q

The maximum speed for extension or retraction of the landing gear is:

A
  • 220 Kts
41
Q

The minimum required brake cooling time after one rejected takeoff is?

A
  • 25 minutes
42
Q

The minimum required brake cooling time after two rejected takeoffs is:

A
  • 45 minutes
43
Q

The maximum flap extension speeds are:

A
  • Flaps 15 degrees ─ 220 Kts
  • Flaps 25 degrees ─ 175 Kts
  • Flaps 45 degrees ─ 165 Kts
44
Q

Single engine flap retraction speed following engine failure on takeoff is:

A
  • V2 + 9 Kts
45
Q

Engine ANTICE should be used when in visible moisture and at or below a temperature of?

A
  • 10°C
46
Q

Wing/Tail ANTICE should not be used in flight when the temperature is below how many degrees?

A
  • -28°C
47
Q

Windshield heat must be ON prior to takeoff for at least ____ minutes in ambient temperatures below -10°C or ____ minutes in ambient temperatures below -20° C for maximum birds strike protection

A
  • 5 minutes
  • 15 minutes
48
Q

If it is not possible 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 ____ feet is reached

A
  • 257 Kts
  • 8,000 feet
49
Q

The pressurization system normal maximum differential pressure is ______PSI

A
  • 8.55 PSI
50
Q

At what altitude will the red CABIN ALT annunciator illuminate?

A
  • 9,300 feet +/- 300 feet
51
Q

The barometric valve will automatically cause the passenger masks to drop when the cabin altitude exceeds what altitude?

A
  • 12,000 feet ±500 feet
52
Q

What is the maximum ramp weight?

A
  • Hawker 800: 27,520 pounds
53
Q

What is the maximum landing weight?

A
  • 23,350 pounds
54
Q

What is the maximum zero fuel weight?

A
  • Hawker 800: 17,520 pounds