General

Question 1

The Captain’s seat, but not the First Officer’s seat, can be adjusted up and down by an electric actuator.

a) True
b) False

Answer 1

b) False

Question 2

There is no mechanical means of adjusting the height of the pilot seats.

a) True
b) False

Answer 2

b) False

Question 3

The rudder pedals can be adjusted fore and aft electrically.

a) True
b) False

Answer 3

a) True

Question 4

What is the EMB-145 Maximum Structural Takeoff Weight?

a) 40,785 lbs.
b) 42,549 lbs.
c) 48,722 lbs.
d) 49,823 lbs.

Answer 4

d) 49, 823 lbs.

Question 5

When the Cockpit Direct Vision (DV) Windows (side windows) are not properly locked in the closed position, which of the following indications will be present?

a) Single caution chime
b) Message (MSG) on the EICAS display
c) A yellow pin protruding form the flat plate linkage near opening handle
d) Both A and B

Answer 5

c) A yellow pin protruding form flat plate linkage near opening handle

Question 6

The Emergency Locater Transmitter (ELT) is located above the toilet.

a) True
b) False

Answer 6

a) True

Question 7

The lavatory toilet is flushed by a pump with is powered:

a) Electrically
b) Hydraulically
c) Pneumatically
d) Mechanically

Answer 7

a) Electrically

Question 8

The Waste Service Panel and the Potable Water Service Panel are located on the lower aft ______ side of the airplane.

Answer 8

Right

Question 9

What are the exterior dimensions (in feet) of the EMB-140 and 145 respectively?

a) 105 x 67 x 23, 98 x 67 x 23
b) 94 x 66 x 22, 98 x 66 x 22
c) 100 x 66 x 22, 97 x 66 x 22
d) 98 x 67 x 22, 96 x 67 x 22

Answer 9

b) 94 x 66 x 22, 98 x 66 x 22

Question 10

The Galley Service Door is hydraulically operated.

a) True
b) False

Answer 10

b) False

Question 11

To block the baggage door the handle must be turned

a) Clockwise
b) Counter-clockwise

Answer 11

a) Clockwise

Question 12

Name the three compartment hatches that share the amber EICAS “ACCESS DOOR OPEN” caution MSG.

Answer 12

Forward Electronics Compartment
Rear Electronic Compartment
Under cockpit access (rigging) hatch

Question 13

The status of the doors and hatches can be found on the Doors section of the _______ page on the ________.

Answer 13

Takeoff System, MFD

Question 14

In the event of a landing below -40°C, the airplane may not take off without further maintenance inspection.

a) True
b) False

Answer 14

a) True

Question 15

The minimum operation temperature for takeoff and lading is __°C and the maximum at -1,000 ft. PA is ___°C

Answer 15

-40°C SAT, 52°C SAT

Question 16

Vlor is ___ KIAS, Vloe is ____ KIAS and Vle is ____ KIAS

Answer 16

200, 250, 250

Question 17

Mmo is ____, and Vmo is ___ at and above 10,000 ft. is ___ KIAS

Answer 17

.78M, 320

Question 18

What is the EMB-145 Maximum Structural Landing Weight?

a) 43,651 lbs.
b) 40,785 lbs.
c) 44,092 lbs.
d) 44,312 lbs.

Answer 18

a) 43,651 lbs.

Question 19

Va is ___ KIAS.

Answer 19

200

Question 20

Vfe for flaps 9° is __ KIAS, for flaps 22° is __ KIAS, and for flaps 45° is __ KIAS.

Answer 20

250, 200, 145

Question 21

The maximum takeoff and landing tailwind component is __ KIAS.

Answer 21

10

Question 22

The runway slope limitation is a negative __% and a positive __%.

Answer 22

-2, +2

Question 23

The minimum temperature for (manual) Anti-icing Operation is __°C and maximum is __°C.

Answer 23

-40°C, 10°C

Question 24

The holding configuration while in icing conditions are Landing Gear ___, Flaps ___°, and a minimum airspeed of ___ KIAS.

Answer 24

Up, 0°, 200 KIAS

Question 25

What is the Maximum recommended holding airspeed?

Answer 25

200 KIAS

Question 26

The maximum load on the engine generator and the APU generator is ___ amps.

Answer 26

400

Question 27

The maximum battery temperature is __°C and the minimum battery temperature for and APU start is ___°C.

Answer 27

70°C, -20°C

Question 28

The maximum altitude for flap extension is ____ ft.

Answer 28

20,000 ft. MSL

Question 29

Minimum altitude with Autopilot engaged during and ILS approach is ___.

Answer 29

MDA/DA/DH

Question 30

What is the EMB-140 Maximum Structural Landing Weight?

a) 41,226 lbs.
b) 42,549 lbs.
c) 40,785 lbs.
d) 43,001 lbs.

Answer 30

a) 41,226 lbs.

Question 31

Minimum Engagement Height for the Autopilot is ____ ft.

Answer 31

500 ft.

Question 32

What is the EMB-145 Maximum Structural Zero Fuel Weight?

a) 35,274 lbs.
b) 40,564 lbs.
c) 39,462 lbs.
d) 38,762 lbs.

Answer 32

b) 40,564 lbs.

Question 33

Descent to 50 ft. below the MDA on a non-precision approach with the Autopilot engaged is allowed.

a) True
b) False

Answer 33

b) False

Question 34

Approach mode selection during localizer capture with the autopilot engaged is allowed only when airplane is ____.

Answer 34

Inbound

Question 35

What is the minimum pavement width for a 180° turn for the EMB-140/145 respectively?

a) 60 ft., 65 ft.
b) 66 ft., 70 ft.
c) 80 ft., 82 ft.
d) 83 ft., 90 ft.

Answer 35

b) 66 ft., 70 ft.

Question 36

What is the maximum section capacity of the EMB-140/145 respectively?

a) 44 pax, 50 pax and 4 crew
b) 46 pax, 50 pax and 4 crew
c) 40 pax, 50 pax and 4 crew
d) 45 pax, 50 pax and 4 crew

Answer 36

a) 44 pax, 50 pax and 4 crew

Question 37

The minimum EMB-140/145 operation envelope temperature in flight is:

a) -54°C Static Air Temperature (SAT)
b) -65°C Outside Air Temperature (OAT)
c) -65°C Total Air Temperature (TAT)
d) -65°C SAT

Answer 37

d) -65°C SAT

Question 38

No Aircraft Maintenance Log (AML) entry is required for and overweight landing conducted at 300 fpm or less.

a) True
b) False

Answer 38

b) False

Question 39

The DV windows may be used:

a) To pass required paperwork from the aircraft to the departure station.
b) Cockpit Evacuation.
c) To signal ramp personnel we are cleared for pushback.
d) All of the above.

Answer 39

b) Cockpit Evacuation