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EMB-135BJ > Aircraft General > Flashcards

Aircraft General Flashcards

0
Q

The crank handle for adjusting the height of the pilot seats is located in where?

A

Under the pilot seats

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1
Q

The Captain and First Officer’s seats can be adjusted up and down how:

A

Electrically or Mechanically

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2
Q

The Rudder pedals are adjusted fore and aft how?

A

Electrically with the toggle switch.

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3
Q

The Embraer Legacy is powered by two rear mounted _________.

A

Rolls-Royce AE3007A2 (or A1P or A1E) Turbo Fan Engines

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4
Q

If the cockpit direct vision windows are not properly locked, the indication to the pilot is __________

A

A protruding yellow pin.

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5
Q

The EMB-135BJ Maximum Structural TO weight is?

A

Legacy 600 ……………. 49,604 LBS

Legacy 650 ……………. 53,572 LBS

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6
Q

What is the EMB-135BJ Maximum Structural Ramp Weight?

A

Legacy 600 ………………… 49,758 lbs

Legacy 650 ………………… 53,726 lbs

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7
Q

What is the EMB-135BJ Maximum Structural Landing Wight

A

Legacy 600 …………………. 40,786 lbs

Legacy 650 …………………. 44,092 lbs

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8
Q

What is the EMB-135BJ Maximum Structural Zero Fuel Weight?

A

Legacy 600 …………………. 35,274 lbs

Legacy 650 …………………. 36,155 lbs

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9
Q

The Galley Emergency Light switch will be __________ when selected to the normal flight position

A

Amber

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10
Q

The Galley pocket door is required to be fully _______ for take off and landing.

A

Open

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11
Q

The airstair light switch is located?

A

In front of the flight attendant’s seat

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12
Q

The Captain’s Flashlight is Located?

A

on the wall behind the captains seat above the PBE.

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13
Q

In normal conditions the main cabin door is raised by the ________ hydraulic system.

A

Number 1

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14
Q

If the aircraft is unpowered, the hydraulic accumulator still provides for ________ complete operations of the main cabin door

A

3

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15
Q

Hydraulic system pressure remaining in the line after raising the main cabin door is indicated by a “_________” indication on the Entrance control panel

A

Door Blocked

16
Q

If the Main cabin door becomes blocked by hydraulic system pressure:

A

The emergency valve on the cockpit floor can be turned and held for 2 minutes to release presure

17
Q

The Main Cabin Door is Lowered through ____________

A

Hydraulic dampening

18
Q

The waste service panel is located on the _________ of the airplane (w/o forward lav)

A

Lower R/H aft side

19
Q

Which door associated with the “ACCESS DOORS” EICAS caption is located in the unpressurized part of the aircraft?

A

Forward Electronic Compartment Hatch

20
Q

The forward electronic compartment access hatch is located inside the?

A

Nose Wheel Well.

21
Q

What are the 3 doors associated with the EICAS caution message “ACCESS DOOR OPEN”?

A

Rear Electronic Compartment Hatch
Forward Electronic Compartment Hatch
Under cockpit access hatch

22
Q

The EMB-135BJ Should have no more than ___ people on the airstairs at the same time

A

3

23
Q

The refueling panel is located on the Forward _______ side of the aircraft

A

Right

24
Q

The steering handwheel allow for a maximum of ________ deflection. The rudder pedals allow for ______ degrees of deflection. The total steering deflection using handwheel and rudders is _______ degrees.

A

71º, 5º, 76º

25
Q

The “Main Door Opn” warning message is inhibited on the ground with the _______ engine shutdown.

A

Left or #1

26
Q

The nose gear taxi and landing lights are powered by the _______ buses.

A

Shed

27
Q

The taxi and nose gear landing lights are illuminated when the respective switch is _____, and the landing gear is _______ and locked.

A

On, down

28
Q

The cockpit voice recorder begins recording when?

A

When the batteries are turned on.

29
Q

The Digital Flight Data Recorder (DFDR) begins recording:

A

When the red beacon is turned on.

30
Q

If the digital flight data recorder is not activated through normal procedures it is automatically turned on:

A

When the aircraft is off the ground.

31
Q

The PC power system is available on the ground with the APU powering the electrical system with the ______________

A

Shed buss switched to override.

32
Q

In normal conditions, the illuminated stripe in the push button on the overhead panel, forward panel or center pedestal means that the button is no in the normal position for _________.

A

Flight

33
Q

Four __________ are installed on the leading edge of each wing to prevent span-wise airflow separation at high angles of attack.

A

vortilons

34
Q

Twelve ________ are installed on the top of each wing for the aerodynamic purpose of preventing airflow separations over the top of the wing surface at high airspeeds.

A

Vortex Generators

EMB-135BJ (32 decks)

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