Aircraft General

Question 0

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

Answer 0

Under the pilot seats

Question 1

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

Answer 1

Electrically or Mechanically

Question 2

The Rudder pedals are adjusted fore and aft how?

Answer 2

Electrically with the toggle switch.

Question 3

The Embraer Legacy is powered by two rear mounted _________.

Answer 3

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

Question 4

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

Answer 4

A protruding yellow pin.

Question 5

The EMB-135BJ Maximum Structural TO weight is?

Answer 5

Legacy 600 ……………. 49,604 LBS

Legacy 650 ……………. 53,572 LBS

Question 6

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

Answer 6

Legacy 600 ………………… 49,758 lbs

Legacy 650 ………………… 53,726 lbs

Question 7

What is the EMB-135BJ Maximum Structural Landing Wight

Answer 7

Legacy 600 …………………. 40,786 lbs

Legacy 650 …………………. 44,092 lbs

Question 8

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

Answer 8

Legacy 600 …………………. 35,274 lbs

Legacy 650 …………………. 36,155 lbs

Question 9

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

Answer 9

Amber

Question 10

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

Answer 10

Open

Question 11

The airstair light switch is located?

Answer 11

In front of the flight attendant’s seat

Question 12

The Captain’s Flashlight is Located?

Answer 12

on the wall behind the captains seat above the PBE.

Question 13

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

Answer 13

Number 1

Question 14

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

Answer 14

3

Question 15

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

Answer 15

Door Blocked

Question 16

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

Answer 16

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

Question 17

The Main Cabin Door is Lowered through ____________

Answer 17

Hydraulic dampening

Question 18

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

Answer 18

Lower R/H aft side

Question 19

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

Answer 19

Forward Electronic Compartment Hatch

Question 20

The forward electronic compartment access hatch is located inside the?

Answer 20

Nose Wheel Well.

Question 21

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

Answer 21

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

Question 22

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

Answer 22

3

Question 23

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

Answer 23

Right

Question 24

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.

Answer 24

71º, 5º, 76º

Question 25

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

Answer 25

Left or #1

Question 26

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

Answer 26

Shed

Question 27

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

Answer 27

On, down

Question 28

The cockpit voice recorder begins recording when?

Answer 28

When the batteries are turned on.

Question 29

The Digital Flight Data Recorder (DFDR) begins recording:

Answer 29

When the red beacon is turned on.

Question 30

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

Answer 30

When the aircraft is off the ground.

Question 31

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

Answer 31

Shed buss switched to override.

Question 32

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 _________.

Answer 32

Flight

Question 33

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

Answer 33

vortilons

Question 34

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.

Answer 34

Vortex Generators