ENVOY EMB 145 STUDY QUESTIONS || with
Authenticated Answers.
AIRCRAFT GENERAL correct answers AIRCRAFT GENERAL
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 correct answers b) False
2. There is no mechanical means of adjusting the height of the pilot seats.
a) True
b) False correct answers b) False
3. The rudder pedals can be adjusted fore and aft electrically.
a) True
b) False correct answers a) True
4. What is the EMB-145 Maximum Structural Takeoff Weight?
a) 40,785 lbs.
b) 42,549 lbs.
c) 48,501 lbs.
d) 49,823 lbs. correct answers d) 49,823 lbs.
5. When the Cockpit Direct Vision 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 on EICAS
c) A yellow pin protruding from flat plate linkage near opening handle
d) Both A and B correct answers c) A yellow pin protruding from flat plate linkage near opening
handle
6. The ELT is located above the toilet.
a) True
b) False correct answers a) True
7. The lavatory toilet is flushed by a pump which is powered:
a) Electrically
b) Hydraulically
c) Pneumatically
d) Mechanically correct answers a) Electrically
8. The Waste Service Panel and the Potable Water Service Panel are located on the lower aft
_________ side of the airplane. correct answers Right
,9. What are the exterior dimensions (in feet) of the EMB-145 and 140 respectively?
a) 105 x 67 x 23, 98 x 67 x 23
b) 98 x 66 x 22, 94 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 correct answers b) 98 x 66 x 22, 94 x 66 x 22
10. The Galley Service door is hydraulically operated.
a) True
b) False correct answers b) False
11. To unlock the baggage door the handle must be turned
a) Clockwise
b) Counter-clockwise correct answers a) Clockwise
12. Name the three compartment hatches that share the EICAS Caution MSG
"ACCESS DOOR OPEN."
a) ________________________________
b) ________________________________
c) ________________________________ correct answers a) Foreward Electronic hatch
b) Rear electronic hatch
c) Under cockpit hatch
13. The status of the doors and hatches can be found on the Doors section of the
__________________ page on the ________________. correct answers TAKEOFF SYSTEMS
page on the MFD
14. In the event of a landing below - 40 °C, the airplane may not take off without further
maintenance inspection.
a) True
b) False correct answers a) True
15. The minimum operational temperature for takeoff and landing is __________ and the
maximum at -1,000 ft. PA is _____________. correct answers -42°C, +52°C
16. VLOR is _________ kts.
VLOE is _________ kts.
VLE is ________ kts. correct answers 200
250
250
17. MMO is _______, and VMO at and above 10,000 ft. is ________ KIAS. correct answers
0.78 MACH, 320 KIAS
18. What is the EMB-145 Maximum Structural Landing Weight?
a) 42,549 lbs.
b) 40,785 lbs.
,c) 44,092 lbs.
d) 43,651 lbs. correct answers d) 43,651 lbs.
19. VA is __________ kts. correct answers 200
20. VFE for flaps 9 is _________ kts., for flaps 22 is __________ kts. and for flaps 45 is
_________ kts. correct answers 250, 200, 145
21. The maximum takeoff and landing tailwind component is ______ kts. correct answers 10
22. The runway slope limitation is a negative ____% and a positive ____%. correct answers -2
TO +2%
23. The minimum temperature for (manual) Anti-icing Operations is ______ and maximum is
________. correct answers -40°C, 10°C
24. The holding configuration while in icing conditions is Landing Gear ______, Flaps ______,
and a minimum airspeed of ______ kts. correct answers UP, UP, 200
25. What is the maximum recommended holding airspeed (FM - Part 1/AIM) above 14,000 ft.?
_______________. correct answers 265
26. The maximum load on the engine generators and the APU generator is _______ amps.
correct answers 400
27. Maximum battery temperature is _______ and the minimum battery temperature for APU
start is _________. correct answers 70°C, -20°C
28. The maximum altitude for flap extension is _________ ft. correct answers FL200
29. Minimum altitude with Autopilot engaged during an ILS approach is __________. correct
answers MINIMUMS
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. correct answers a) 41,226 lbs.
31. Minimum engagement height for the Autopilot is ________ ft. correct answers 500
32. What is the EMB-145 Maximum Structural Zero Fuel Weight?
a) 35,274 lbs.
b) 40,785 lbs.
c) 40,564 lbs.
d) 38,762 lbs. correct answers c) 40,564 lbs
, 33. Descent to 50 ft. below the MDA on a non-precision approach with the Autopilot engaged is
allowed.
a) True
b) False correct answers b) False
34. Approach mode selection during localizer capture with the autopilot engaged is allowed only
when airplane is _________. correct answers INBOUND
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. correct answers b) 66 ft., 70 ft.
36. What is the maximum seating 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. correct answers a) 44 pax, 50 pax, and 4 crew.
37. The minimum EMB operational envelope temperature in flight is:
a) -54 °C SAT
b) -65 °C OAT
c) -65 °C TAT
d) -65 °C SAT correct answers d) -65 °C SAT
38. No AML entry is required for an overweight landing conducted at 300 fpm or less.
a) True
b) False correct answers b) False
39. 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. correct answers b) Cockpit Evacuation.
MISCELLANEOUS correct answers MISCELLANEOUS
1. The oxygen system is divided into two different and separate systems.
Name them.
a) _____________________ for crewmembers.
b) _____________________ for passengers and Flight Attendant. correct answers COCKPIT
GASEOUS
CABIN CHEMICAL
Authenticated Answers.
AIRCRAFT GENERAL correct answers AIRCRAFT GENERAL
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 correct answers b) False
2. There is no mechanical means of adjusting the height of the pilot seats.
a) True
b) False correct answers b) False
3. The rudder pedals can be adjusted fore and aft electrically.
a) True
b) False correct answers a) True
4. What is the EMB-145 Maximum Structural Takeoff Weight?
a) 40,785 lbs.
b) 42,549 lbs.
c) 48,501 lbs.
d) 49,823 lbs. correct answers d) 49,823 lbs.
5. When the Cockpit Direct Vision 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 on EICAS
c) A yellow pin protruding from flat plate linkage near opening handle
d) Both A and B correct answers c) A yellow pin protruding from flat plate linkage near opening
handle
6. The ELT is located above the toilet.
a) True
b) False correct answers a) True
7. The lavatory toilet is flushed by a pump which is powered:
a) Electrically
b) Hydraulically
c) Pneumatically
d) Mechanically correct answers a) Electrically
8. The Waste Service Panel and the Potable Water Service Panel are located on the lower aft
_________ side of the airplane. correct answers Right
,9. What are the exterior dimensions (in feet) of the EMB-145 and 140 respectively?
a) 105 x 67 x 23, 98 x 67 x 23
b) 98 x 66 x 22, 94 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 correct answers b) 98 x 66 x 22, 94 x 66 x 22
10. The Galley Service door is hydraulically operated.
a) True
b) False correct answers b) False
11. To unlock the baggage door the handle must be turned
a) Clockwise
b) Counter-clockwise correct answers a) Clockwise
12. Name the three compartment hatches that share the EICAS Caution MSG
"ACCESS DOOR OPEN."
a) ________________________________
b) ________________________________
c) ________________________________ correct answers a) Foreward Electronic hatch
b) Rear electronic hatch
c) Under cockpit hatch
13. The status of the doors and hatches can be found on the Doors section of the
__________________ page on the ________________. correct answers TAKEOFF SYSTEMS
page on the MFD
14. In the event of a landing below - 40 °C, the airplane may not take off without further
maintenance inspection.
a) True
b) False correct answers a) True
15. The minimum operational temperature for takeoff and landing is __________ and the
maximum at -1,000 ft. PA is _____________. correct answers -42°C, +52°C
16. VLOR is _________ kts.
VLOE is _________ kts.
VLE is ________ kts. correct answers 200
250
250
17. MMO is _______, and VMO at and above 10,000 ft. is ________ KIAS. correct answers
0.78 MACH, 320 KIAS
18. What is the EMB-145 Maximum Structural Landing Weight?
a) 42,549 lbs.
b) 40,785 lbs.
,c) 44,092 lbs.
d) 43,651 lbs. correct answers d) 43,651 lbs.
19. VA is __________ kts. correct answers 200
20. VFE for flaps 9 is _________ kts., for flaps 22 is __________ kts. and for flaps 45 is
_________ kts. correct answers 250, 200, 145
21. The maximum takeoff and landing tailwind component is ______ kts. correct answers 10
22. The runway slope limitation is a negative ____% and a positive ____%. correct answers -2
TO +2%
23. The minimum temperature for (manual) Anti-icing Operations is ______ and maximum is
________. correct answers -40°C, 10°C
24. The holding configuration while in icing conditions is Landing Gear ______, Flaps ______,
and a minimum airspeed of ______ kts. correct answers UP, UP, 200
25. What is the maximum recommended holding airspeed (FM - Part 1/AIM) above 14,000 ft.?
_______________. correct answers 265
26. The maximum load on the engine generators and the APU generator is _______ amps.
correct answers 400
27. Maximum battery temperature is _______ and the minimum battery temperature for APU
start is _________. correct answers 70°C, -20°C
28. The maximum altitude for flap extension is _________ ft. correct answers FL200
29. Minimum altitude with Autopilot engaged during an ILS approach is __________. correct
answers MINIMUMS
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. correct answers a) 41,226 lbs.
31. Minimum engagement height for the Autopilot is ________ ft. correct answers 500
32. What is the EMB-145 Maximum Structural Zero Fuel Weight?
a) 35,274 lbs.
b) 40,785 lbs.
c) 40,564 lbs.
d) 38,762 lbs. correct answers c) 40,564 lbs
, 33. Descent to 50 ft. below the MDA on a non-precision approach with the Autopilot engaged is
allowed.
a) True
b) False correct answers b) False
34. Approach mode selection during localizer capture with the autopilot engaged is allowed only
when airplane is _________. correct answers INBOUND
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. correct answers b) 66 ft., 70 ft.
36. What is the maximum seating 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. correct answers a) 44 pax, 50 pax, and 4 crew.
37. The minimum EMB operational envelope temperature in flight is:
a) -54 °C SAT
b) -65 °C OAT
c) -65 °C TAT
d) -65 °C SAT correct answers d) -65 °C SAT
38. No AML entry is required for an overweight landing conducted at 300 fpm or less.
a) True
b) False correct answers b) False
39. 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. correct answers b) Cockpit Evacuation.
MISCELLANEOUS correct answers MISCELLANEOUS
1. The oxygen system is divided into two different and separate systems.
Name them.
a) _____________________ for crewmembers.
b) _____________________ for passengers and Flight Attendant. correct answers COCKPIT
GASEOUS
CABIN CHEMICAL
