2-45.
Canopy actuator field windings--
open.
1. A
2. B
3. C
4. F
2-46.
Canopy actuator brake winding.
1. D
2. C
3. B
4. A
2-47.
Canopy actuator thermal protection
device.
1. D
2. E
3. F
4. G
2-48.
Canopy up-travel-limit switch--not up
contact.
1. B
2. C
3. D
4. E
2-49.
Canopy actuator field windings--
close.
1. A
2. B
3. C
4. G
2-50.
How many systems and components are
related to the electrical canopy
system?
1.
Seven
2.
Nine
3.
Three
4.
Four
2-51.
Unlike the external canopy control
switch, the internal canopy control
switch has only two positions, open
and close.
1.
True
2.
False
IN ANSWERING QUESTION 2-52, REFER TO FIGURE
12-9 IN THE TEXT.
2-52.
Which of the following switches
is/are a double pole double throw
switch(es)?
1.
Canopy position switch
2.
Internal canopy control switch
3.
External canopy control switch
4.
Both 2 and 3 above
2-53.
Explosive stimulus produced by the
initiator is transferred through the
SMDC to what component?
1.
Canopy unlatch thruster
2.
Emergency escape disconnect
3.
Flexible confined detonating
cord
4.
Rocket motors
2-54.
What component prevents explosive
stimulus from continuing toward the
ejection seat components during
internal canopy jettison?
1.
FCDC
2.
Canopy unlatch thruster
3.
Emergency escape disconnect
4.
One way transfer valve
2-55.
What action does each rocket motor
produce to separate the canopy from
the aircraft?
1.
Thrust aft and up
2.
Sufficient burn time
3.
Vertical thrust
4.
Horizontal thrust
14
