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BJM 800 > Self Check 1 > Flashcards

Self Check 1 Flashcards

1
Q

The Minimum Crew for 800/800XP/850XP is?

A

Two

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2
Q

The Maximum Number of Occupants is?

A

17

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3
Q

The third crew member seat must be ______ when in use and when not in use, folded and _____.

A

Locked, stowed.

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4
Q

The maximum takeoff for 800/800XP/850XP is.

A

27,400 / 28,000 / 29000 lbs

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5
Q

The maximum landing weight except in emergency is:

A

23,350 lbs

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6
Q

MMO is:

A

.80 IMN

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7
Q

VMO if the ventral tank is not empty is:

A

280 KTS

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8
Q

The maximum air temperature in which to operate is:

A

ISA +35° C

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9
Q

The minimum temperature for takeoff and landing is:

A

-40° C

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10
Q

The minimum temperature enroute is:

A

-75° C

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11
Q

The maximum tailwind component for takeoff and landing is:

A

10 Knots

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12
Q

The maximum demonstrated crosswind component for takeoff or landing is:

A

30 Knots

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13
Q

The maximum runway slope for takeoff or landing is:

A

2% up and 2% down

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14
Q

What is the bird strike speed up to 8,000 ft:

A

280 Knots

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15
Q

The maximum permissible altitude for flight is:

A

41,000 ft

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16
Q

Maneuvering speed (VA) is:

A

196 Knots

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17
Q

The ENT DOOR UNLOCKED annunciator extinguishes when:

A

The door closed and the door locked microswitches are both depressed.

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18
Q

What is the maximum and minimum altitude for takeoff and landing:

A

Max 9,000 ft and minimum -2,000 ft

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19
Q

With the cabin high datum switch (if installed) selected, the airplane may be operated into and out of airports as high as:

A

13,000 ft

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20
Q

The outward opening, entry door is counterbalanced by:

A

A spring loaded tensator motor (with four constant force springs.

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21
Q

Is smoking allowed in air transport operations:

A

No

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22
Q

The emergency exit is located:

A

On the right side of the airplane above the right wing.

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23
Q

A PBE (Portable Breathing Equipment) must be carried on board! True or False?

A

True

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24
Q

The rudder gust lock may be used to operate the hand pump for emergency landing gear extension: True or False?

A

True

25
Q

The aileron/elevator gust lock is located under the left writing pad, swings out to lock the left side rams horn yoke and will prevent full operation of one power lever when installed. True or False?

A

True

26
Q

Where is the crash ax stowed?

A

Behind the pilot’s seat on the bulkhead below the stall diagnostic panel.

27
Q

Each pilot station is equipped with a flashlight, oxygen mask, and goggles (or full mask). A fire extinguisher is required to be in the cockpit. True or False?

A

True

28
Q

Lead-acid batteries are used and provide 24 V with either 25 or 28 Amp-hours. True or False?

A

True

29
Q

What is the maximum continuous generator load?

A

300 Amp’s

30
Q

How can a generator be manually disconnected from it’s PS Bus?

A

Select the generator switch to TRIP the release.

31
Q

How can the battery charge rate be monitored?

A

Depress the ammeter BATT push button.

32
Q

When the AMP BATT switch is depressed the charge rate of the batteries, expressed in Amps is displayed on the ammeters. When the 0-40 button is then pressed with the AMP BATT switch held, the ammeter scale changes from 0 to 400 Amps and becomes 0 to 40 Amps. True or False?

A

True

33
Q

The ground power receptacle is located…

A

Right rear fuselage

34
Q

The initial selection of the battery switch to ON does what?

A

Connects No. 1 and No. 2 batteries to PE bus bar via the emergency contactors.

35
Q

How do you confirm that batteries are being charged from a ground power unit:

A

By pushing the AMP BATT push button on the overhead panel and confirm the reading.

36
Q

In the Hawker 800 a battery capacity check is recommended prior to an engine start using ground power source. True or False?

A

True

37
Q

What do you do after you start both engines using an external power source?

A

START PWER switch OFF; EXT POWER switch - OFF Disconnect External and check batteries charging.

38
Q

After an external ground power engine start, the GEN FAIL, annunciator light is extinguished indicating the generator is on line

a. When the START PWR switch is selected off
b. Automatically when the EXT POWER switch is selected off
c. Automatically when the generator voltage is greater than the battery voltage

A

b. Automatically when the EXT POWER switch is selected off

39
Q

When using external ground power, the bus bar system is energized ___

a. Only when the EXT PWR and BATT switches are ON
b. When EXT PWR switch is ON, regardless of battery switch position
c. Only when ground power voltage is between 24.5 and 29.5 volts

A

b. When EXT PWR switch is ON, regardless of battery switch position

40
Q

The maximum battery charge rate immediately before takeoff shall not be greater than:

A

20 Amps

41
Q

What is maximum generator load in flight?

A

300 Amps

42
Q

The transient excursions of engine generator load up to maximum of 400 Amps are permitted for a maximum of 2 minutes. True/False?

A

True

43
Q

When both generators on line and the bus tie closed, the maximum permissible discrepancy between generator No. 1 and No. 2 ammeter reading is

a. 40 A
b. 10% of average load

A

a. 40 A

44
Q

What is the purpose of the standby inverter in airplanes so equipped is;

A

To power the XE bus providing power for the captain’s flight instruments in the event of loss of power from XS 1 bus.

45
Q

On aircraft equipped with a standby inverter, the stand by inverter ____
a. Is set to ARM for normal flight
b. Immediately comes into operation in the event either main inverter fails weather armed or not
c, Will power both XS-1 and XS-2 bus for a limited period of time
d. Will power the fan operated venturi

A

a. Is set to ARM for normal flight

46
Q

From what four sources may the main batteries be charged?

  1. Left engine____-____
  2. Right engine ____-___
  3. ____Starter-Generator
  4. ____ Power unit
A

From what four sources may the main batteries be charged?

  1. Left engine Starter-Generator
  2. Right engine Starter-Generator
  3. APU Starter-Generator
  4. Ground Power unit
47
Q

When the BATT Switch is selected on, power from the number ___ battery closes both emergency contactors.

A

When the BATT Switch is selected on, power from the number 1 battery closes both emergency contactors.

48
Q
  1. When the BATT switch is in the BATT EMERG position, power from battery number __ and battery number __ closes the emergency contactors and both _____ contactors are forced open.
A

When the BATT switch is in the BATT EMERG position, power from battery number 1 and battery number 2 closes the emergency contactors and both battery contactors are forced open.

49
Q
  1. The battery isolate switch may be used to isolate ____ or __ from it’s charging source.
A

The battery isolate switch may be used to isolate batt 1 or 2 from it’s charging source.

50
Q
  1. For external starts, a ground power unit supplying ___ volts D.C. with a short term capability of ___ AMP’s and fitted with a ____ Apm’s current limiter must be used.
A

For external starts, a ground power unit supplying 28 volts D.C. with a short term capability of 1500 AMP’s and fitted with an 1100 Apm’s current limiter must be used.

51
Q
  1. When charging the aircraft batteries using ground power, the. EXT BATT CHG switch should be selected OFF when the charge current drops to less than __ AMP’s
A

When charging the aircraft batteries using ground power, the. EXT BATT CHG switch should be selected OFF when the charge current drops to less than 5 AMP’s

52
Q
  1. Two ___ Volt AMP’s (VA) or two ____ VA static inverters are fitted in the rear bay and under normal circumstances supply __ volts at ___ Hertz for AC powered aircraft services.
A

Two 1250 Volt AMP’s (VA) or two 1500 VA static inverters are fitted in the rear bay and under normal circumstances supply 115 volts at 400 Hertz for AC powered aircraft services.

53
Q
  1. In Hawker 800 and 800XP aircraft with standby inverters, the standby inverter provides ___ VA at a frequency of ___ Hertz and supplies 115 volts providing power to the XE bus in the event of a loss of power on the XS-1 bus.
A

In Hawker 800 and 800XP aircraft with standby inverters, the standby inverter provides 250 VA at a frequency of 400 Hertz and supplies 115 volts providing power to the XE bus in the event of a loss of power on the XS-1 bus.

54
Q
  1. The APU generator provides __ volts DC power.
A

The APU generator provides 28 volts DC power.

55
Q
  1. When the APU generator comes online it energizes bus bars PS-_ and __ and ____ and connects the number _ battery to its charge circuit.
A

When the APU generator comes on line it energizes bus bars PS-2 and PE and PE2 and connects the number 2 battery to its charge circuit.

56
Q
  1. After the APU comes online which switch must be operated to connect the number one battery to its charge circuit?
A

The Bus Tie.

57
Q
  1. During external battery charging, a bus bar protection unit monitoring bus bar voltage will open both battery contactors to discontinue battery charging if the bus bar voltage is above ____ volts and or below ____volts.
A

During external battery charging, a bus bar protection unit monitoring bus bar voltage will open both battery contactors to discontinue battery charging if the bus bar voltage is above 29.5 volts and or below 24.5 volts.

58
Q
  1. Under normal conditions, the # 1 inverter powers ____ and __ bus bars and the # 2 inverter powers the ____ bus.
A

Under normal conditions, the # 1 inverter powers XS-1 and XE bus bars and the # 2 inverter powers the XS-2 bus.

59
Q
  1. What is the purpose of the bus tie?
A

It ties (or separates) PS-1 to PS-2 bus.

BJM 800 (23 decks)

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