IN ANSWERING QUESTIONS 3-35 THROUGH 3-38,
SELECT THE COMPONENT FROM COLUMN B THAT
MATCHES THE PURPOSE OF THE ROTARY
RETRACTION ENGINE COMPONENT LISTED IN
COLUMN A.
3-35.
3-36.
3-37.
3-38.
A. PURPOSES
Guides the cables
between the engine
and the grab
Prevents the
cables from
becoming crossed
and tangled on
the drum
Operates
hydraulically
to keep the
retraction engine
cables tight
Provides a means
of transmitting the
force developed by
the tensioner to
the cable
B. COMPONENTS
1. Cable
tensioner
assembly
2. Screw and
traverse
carriage
assembly
3. Lead sheave
assembly
4.
Cable
tensioner
sheave
assembly
3-39.
What is the function of the rotary
retraction engine maneuvering
valve?
1.
To protect the engine from
damage in the event of a
malfunction
2.
To control the bridle tensioner
control valve
3.
To control the speed of the
grab after advance or retract
stroke braking has been
completed
4.
To initiate the advance and
retract stroke braking
3-40.
The bridle tensioner fully aft
limit switch is part of two
catapult electrical circuits.
One
is the retract permissive circuit.
What is the other one?
1.
The maneuver forward
2.
The maneuver aft
3.
The military power
4.
The suspend circuit
3-41.
The C-7 and C-11 catapult control
systems differ from the C-13
control system in which of the
following ways?
1.
They have various circuit
breakers, fuses, and panel
lights
2.
They have control units that
utilize only solenoids and
relays
3.
They have control consoles
located below the flight deck
4.
They have cam operated pilot
valves used in conjunction with
the electrical components
3-42.
A total of how many positions are
indicated on the C-7/C-11 catapult
control console sequence indicator
dial?
1.
Five
2.
Six
3.
Seven
4.
Eight
IN ANSWERING QUESTIONS 3-43 THROUGH 3-45,
SELECT FROM COLUMN B THE COMPONENT OF THE
CAM CONTROL UNIT THAT PERFORMS THE
FUNCTION LISTED IN COLUMN A.
A. FUNCTIONS
B. COMPONENTS
3-43.
Drives the main-
1. DC shaft
drive indicator
on the sequence
2. DK shaft
indicator dial
3.
Fire
3-44.
Controls the
solenoid
camshafts and
the cam control
4. Handcrank
unit
3-45.
Actuates the
launch valve
pilot valve
3-46.
Which of the following controls is
NOT a momentary contact push
button?
1.
Fire
2.
Maneuver aft
3.
Lube
4.
Maneuver forward
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