Beech 1900-Prop

1. For which type of landing should the propellers be in the forward position

Full stop landings

Maximum reverse thrust landings

Short field landings

All of the above are correct

2. During the takeoff roll the left primary governor fails:

The left prop will govern at 1768 rpm

The left prop will govern at 96% of selected rpm

The left prop will feather

The prop will move to idle position

3. If the propeller doesnt manually feather during an inflight engine failure:

The propeller cant be feathered any other way

The propeller may be feathered using the autofeather system

The propeller will go to an overspeed condition

None of the above are correct

4. As oil leaves the propeller dome:

Propeller blade angle increases

Propeller blade angle decreases

Propeller pitch decreases

Propeller rpm increases

5. The prop sync system uses the left engine as the master

True

False

6. The propellers should not be in reverse below:

40 knots

50 knots

60 knots

70 knots

7. The flight Idle prop blade angle is____degrees

-3

13

7

0

8. The normal operating range of the BE1900 propeller is:

1400-1700rpm

1550-1700rpm

1200-1700rpm

900-1700rpm

9. During cruise flight (torque=2800, prop 1550rpm), if the primary governor should fail:

The hydraulic overspeed would limit the prop to 1768rpm

The prop will feather

The fuel-topping governor will limit the prop to 106% of selected rpm

The prop will stay on speed and in sync

10. Which of the following is a true statement?

The position of the pitch stop is controlled in the cockpit by the prop lever

To enter the Beta range, the prop lever must be in the full forward position

Both ground and flight low pitch stops are set by the beta valve

Is is advisable to place the power levers in the reverse position while the props are feathered

11. A propeller rpm of 1565 on takeoff would indicate:

The primary governor has failed

The overspeed governor is stuck in the test position

The low pitch solenoid has not reset

Is is acceptable since the propeller is still indicating in the green arc

12. The fuel topping governor:

Provides protection against power turbine overspeed

Limits power turbine speed (N2) to 36000 rpm

Is set to a higher value for reversing

None of the above are correct

13. The fuel topping governor is set to what % of the primary governor when the power levers are in reverse

104

106

96

94

14. For testing, the hydraulic overspeed governor should read between:

1643-1802 rpm

1700-1768 rpm

1520-1610 rpm

1400-1550 rpm

15. If the low pitch solenoid is inoperative:

The propellers will not attain 1700 RPM

The propellers will not go into reverse

The propeller can not be feathered

None of the above are correct

16. The maximum allowable propeller rpm is:

1700

1768

1802

1870

Beech 1900-prop

1. For which type of landing should the propellers be in the forward position

2.

What first name or nickname would you like us to use?

2. During the takeoff roll the left primary governor fails:

3. If the propeller doesnt manually feather during an inflight engine failure:

4. As oil leaves the propeller dome:

5. The prop sync system uses the left engine as the master

6. The propellers should not be in reverse below:

7. The flight Idle prop blade angle is____degrees

8. The normal operating range of the BE1900 propeller is:

9. During cruise flight (torque=2800, prop 1550rpm), if the primary governor should fail:

10. Which of the following is a true statement?

11. A propeller rpm of 1565 on takeoff would indicate:

12. The fuel topping governor:

13. The fuel topping governor is set to what % of the primary governor when the power levers are in reverse

14. For testing, the hydraulic overspeed governor should read between:

15. If the low pitch solenoid is inoperative:

16. The maximum allowable propeller rpm is: