Beech 1900-prop
Settings
- 1.The flight Idle prop blade angle is____degrees
- A.
-3
- B.
13
- C.
7
- D.
0
- 2.
- A.
The hydraulic overspeed would limit the prop to 1768rpm
- B.
The prop will feather
- C.
The fuel-topping governor will limit the prop to 106% of selected rpm
- D.
The prop will stay on speed and in sync
- 3.During the takeoff roll the left primary governor fails:
- A.
The left prop will govern at 1768 rpm
- B.
The left prop will govern at 96% of selected rpm
- C.
The left prop will feather
- D.
The prop will move to idle position
- 4.The normal operating range of the BE1900 propeller is:
- A.
1400-1700rpm
- B.
1550-1700rpm
- C.
1200-1700rpm
- D.
900-1700rpm
- 5.Which of the following is a true statement?
- A.
The position of the pitch stop is controlled in the cockpit by the prop lever
- B.
To enter the Beta range, the prop lever must be in the full forward position
- C.
Both ground and flight low pitch stops are set by the beta valve
- D.
Is is advisable to place the power levers in the reverse position while the props are feathered
- 6.The fuel topping governor is set to what % of the primary governor when the power levers are in reverse
- A.
104
- B.
106
- C.
96
- D.
94
- 7.The prop sync system uses the left engine as the master
- A.
True
- B.
False
- 8.For which type of landing should the propellers be in the forward position
- A.
Full stop landings
- B.
Maximum reverse thrust landings
- C.
Short field landings
- D.
All of the above are correct
- 9.The propellers should not be in reverse below:
- A.
40 knots
- B.
50 knots
- C.
60 knots
- D.
70 knots
- 10.For testing, the hydraulic overspeed governor should read between:
- A.
1643-1802 rpm
- B.
1700-1768 rpm
- C.
1520-1610 rpm
- D.
1400-1550 rpm
- 11.A propeller rpm of 1565 on takeoff would indicate:
- A.
The primary governor has failed
- B.
The overspeed governor is stuck in the test position
- C.
The low pitch solenoid has not reset
- D.
Is is acceptable since the propeller is still indicating in the green arc
- 12.The fuel topping governor:
- A.
Provides protection against power turbine overspeed
- B.
Limits power turbine speed (N2) to 36000 rpm
- C.
Is set to a higher value for reversing
- D.
None of the above are correct
- 13.If the low pitch solenoid is inoperative:
- A.
The propellers will not attain 1700 RPM
- B.
The propellers will not go into reverse
- C.
The propeller can not be feathered
- D.
None of the above are correct
- 14.The maximum allowable propeller rpm is:
- A.
1700
- B.
1768
- C.
1802
- D.
1870
- 15.If the propeller doesnt manually feather during an inflight engine failure:
- A.
The propeller cant be feathered any other way
- B.
The propeller may be feathered using the autofeather system
- C.
The propeller will go to an overspeed condition
- D.
None of the above are correct
- 16.As oil leaves the propeller dome:
- A.
Propeller blade angle increases
- B.
Propeller blade angle decreases
- C.
Propeller pitch decreases
- D.
Propeller rpm increases
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