General Flashcards
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
b) False
There is no mechanical means of adjusting the height of the pilot seats.
a) True
b) False
b) False
The rudder pedals can be adjusted fore and aft electrically.
a) True
b) False
a) True
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.
d) 49, 823 lbs.
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
c) A yellow pin protruding form flat plate linkage near opening handle
The Emergency Locater Transmitter (ELT) is located above the toilet.
a) True
b) False
a) True
The lavatory toilet is flushed by a pump with is powered:
a) Electrically
b) Hydraulically
c) Pneumatically
d) Mechanically
a) Electrically
The Waste Service Panel and the Potable Water Service Panel are located on the lower aft ______ side of the airplane.
Right
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
b) 94 x 66 x 22, 98 x 66 x 22
The Galley Service Door is hydraulically operated.
a) True
b) False
b) False
To block the baggage door the handle must be turned
a) Clockwise
b) Counter-clockwise
a) Clockwise
Name the three compartment hatches that share the amber EICAS “ACCESS DOOR OPEN” caution MSG.
Forward Electronics Compartment
Rear Electronic Compartment
Under cockpit access (rigging) hatch
The status of the doors and hatches can be found on the Doors section of the _______ page on the ________.
Takeoff System, MFD
In the event of a landing below -40°C, the airplane may not take off without further maintenance inspection.
a) True
b) False
a) True
The minimum operation temperature for takeoff and lading is __°C and the maximum at -1,000 ft. PA is ___°C
-40°C SAT, 52°C SAT
Vlor is ___ KIAS, Vloe is ____ KIAS and Vle is ____ KIAS
200, 250, 250
Mmo is ____, and Vmo is ___ at and above 10,000 ft. is ___ KIAS
.78M, 320
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.
a) 43,651 lbs.
Va is ___ KIAS.
200
Vfe for flaps 9° is __ KIAS, for flaps 22° is __ KIAS, and for flaps 45° is __ KIAS.
250, 200, 145
The maximum takeoff and landing tailwind component is __ KIAS.
10
The runway slope limitation is a negative __% and a positive __%.
-2, +2
The minimum temperature for (manual) Anti-icing Operation is __°C and maximum is __°C.
-40°C, 10°C
The holding configuration while in icing conditions are Landing Gear ___, Flaps ___°, and a minimum airspeed of ___ KIAS.
Up, 0°, 200 KIAS
What is the Maximum recommended holding airspeed?
200 KIAS
The maximum load on the engine generator and the APU generator is ___ amps.
400
The maximum battery temperature is __°C and the minimum battery temperature for and APU start is ___°C.
70°C, -20°C
The maximum altitude for flap extension is ____ ft.
20,000 ft. MSL
Minimum altitude with Autopilot engaged during and ILS approach is ___.
MDA/DA/DH
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.
a) 41,226 lbs.
Minimum Engagement Height for the Autopilot is ____ ft.
500 ft.
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.
b) 40,564 lbs.
Descent to 50 ft. below the MDA on a non-precision approach with the Autopilot engaged is allowed.
a) True
b) False
b) False
Approach mode selection during localizer capture with the autopilot engaged is allowed only when airplane is ____.
Inbound
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.
b) 66 ft., 70 ft.
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
a) 44 pax, 50 pax and 4 crew
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
d) -65°C SAT
No Aircraft Maintenance Log (AML) entry is required for and overweight landing conducted at 300 fpm or less.
a) True
b) False
b) False
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.
b) Cockpit Evacuation
