Beech 1900-prop
- 1.
The flight Idle prop blade angle is____degrees
- A.
-3
- B.
13
- C.
7
- D.
0
Correct Answer
B. 13 -
- 2.
During cruise flight (torque=2800, prop 1550rpm), if the primary governor should fail:
- 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
Correct Answer
A. The hydraulic overspeed would limit the prop to 1768rpm -
- 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
Correct Answer
A. The left prop will govern at 1768 rpm -
- 4.
The normal operating range of the BE1900 propeller is:
- A.
1400-1700rpm
- B.
1550-1700rpm
- C.
1200-1700rpm
- D.
900-1700rpm
Correct Answer
A. 1400-1700rpm -
- 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
Correct Answer
C. Both ground and flight low pitch stops are set by the beta valve -
- 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
Correct Answer
C. 96 -
- 7.
The prop sync system uses the left engine as the master
- A.
True
- B.
False
Correct Answer
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
Correct Answer
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
Correct Answer
A. 40 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
Correct Answer
C. 1520-1610 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
Correct Answer
B. The overspeed governor is stuck in the test position -
- 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
Correct Answer
A. Provides protection against power turbine overspeed -
- 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
Correct Answer
D. None of the above are correct -
- 14.
The maximum allowable propeller rpm is:
- A.
1700
- B.
1768
- C.
1802
- D.
1870
Correct Answer
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
Correct Answer
B. The propeller may be feathered using the autofeather system -
- 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
Correct Answer
A. Propeller blade angle increases -
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Current Version
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Dec 27, 2012Quiz Edited by
ProProfs Editorial Team -
Dec 27, 2012Quiz Created by
Highskyflyn
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