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Front Back
1.) How are the primary flight controls operated? 8-1
Mechanically
2.) How are the Trims operated? 8-1
Electrically
3.) How are the Flaps operated? 8-1
Hydraulically
4.) What joins the ailerons together? 8-1
Aileron Interconnect unit
5.) Which side aileron trim is operated when the main trim is used? 8-1
Left side
6.) Which side aileron trim is operated if the Standby trim is used? 8-1
Right side
7.) What makes up the Interconnect unit? 8-2
A friction device to hold the two ailerons together
8.) How can the ailerons be reconnected after the roll disconnect has been pulled? 8-2
Only by maintenance on the ground
9.) How are the two elevators joined together? 8-2
Elevator Interconnect unit
10.) Which elevator trim moves when the yoke mounted trim switch is moved? 8-4
Both main and standby when PITCH TRIM is synched
11.) What allows the main and standby trims to operate together? 8-4
The pitch trim synchronizer
12.) How are the Main and Standby trims separated from each other? 8-4
By operating the Standby trim switch
13.) How are the main and Standby trims tied together? 8-4
Pitch trim synchronizer
14.) If the left control wheel trim switch is operated and the right wheel switch operated in the other direction how do the trims respond? 8-5
The Captain’s trim will override the FO’s trim
15.) When would you get a CONFIG CWP light? 8-6
(Also Warning Systems) During T/O when: Pitch trims are out of takeoff range, “green arc” Condition levers not at Max Flaps are beyond 15º When attempting to start the #1 engine and the FI Stop Override switch is pulled.
16.) If takeoff is attempted with the trims outside of the green arc what happens? 8-6
Master Warning, CONFIG CWP, and Intermittent Horn
17.) A stall warning is provided by what simultaneous indications? 8-6
An Aural Clacker A Stick Shaker
18.) At Stall Threshold what happens? 8-6
The Stick Pusher activates
19.) How much pressure does the Stick Pusher generate? 8-6
80 pounds of force
20.) What lights will illuminate as the Stick Pusher activates? 8-6
PUSH 1 and PUSH 2 on both sides of the panel
21.) How is the Stick Pusher Overridden? 8-6
By overpowering the 80lbs of force
22.) What are the 3 warning signs of a stall? 8-6
Stick shaker, clacker, and push lights
23.) How is the Stick Pusher deactivated? 8-7
Reduce the Angle of Attack Pressing the PUSHER DISARM button
24.) What is being checked when the stall test switches are both pushed down? 8-7
The .5g sensor is functioning properly, and the pusher does not activate
25.) When testing the stall system what is being checked? 8-7
Associated PUSH light illuminates Aural alert (clacker) Stick shaker With both switches up stick pusher activates along with PUSH 1 and PUSH 2 With both switches down pusher does not activate with PUSH 1 and PUSH 2
26.) How can the Pusher System be reset after deactivation? 8-7
Only by maintenance
27.) When is the Stick Pusher inhibited? 8-7
While on the ground After takeoff for 7 seconds Anytime load factor is less than .5g
28.) What angle does the Stick Pusher move the elevator to? 8-7
4º nose down
29.) How long is the Stick Pusher sustained for? 8-7
As long as the excessive AOA exist Load factor less than .5g
30.) What does a STALL FAIL CWP light indicate? 8-8
A fault detected in a stall warning/ident computer
31.) What is the purpose of the Rudder Limiter? 8-11
To limit rudder travel at high airspeeds
32.) What are the speed and travel limits of the Rudder Limit system? 8-11
Full travel (up to 30º) at speeds up to 150 knots Intermediate travel (up to 15º) at speeds between 150-200 Knots Minimum travel (up to 5.7º) at speeds above 200 Knots
33.) What does a RUDDER LIMIT CWP light indicate? 8-11
Discrepancies between monitored Airspeeds or an improperly positioned limiting mechanism
34.) What is the Purpose of the RUD LIM switch? 8-11
In OVRD, allows full rudder travel by retracting rudder limiting mechanism
35.) What kind of flaps does the Saab 340 have? 8-13
Single panel Fowler flaps
36.) Are the flaps operated as a single unit? 8-13
No they are 2 individual flaps operated by a single HYDR. actuator for each flap
37.) What keeps the flaps from a split flap condition? 8-13
A mechanical Interconnection
38.) What are the flap detent settings? 8-14
0, 7, 15, 20, and 35 degrees
39.) What is indicated by an illuminated FLAPS CWP light? 8-14
Failure of the flap controller Disagreement between Flap handle selection and left Flap position
40.) Does a split flap automatically trigger a FLAPS CWP light? 8-14
No, if the left flap agrees then no light
41.) If the flap controller fails what are the indications? 8-14
FLAPS CWP light Master Caution Flaps become locked in position without further control
42.) With a flap controller failure how could the crew verify flap position? 8-14
By use of the flap angle marks on the flap
43.) At what settings are the gates located during flap retraction? 8-14
7 and 20 degrees
44.) What position do the Gust locks fail to? 8-18
Unlocked
45.) How do the GUST LOCKS prohibit Takeoff while engaged? 8-18
Power lever movement is limited
46.) When would you get a GUST LOCK CWP light? 8-18
When the Gust Lock is released and the rudder fails to unlock
47.) Are the aileron and elevator gust locks electric or mechanical? 8-18
Mechanical
48.) Is the Rudder gust lock electric or mechanical? 8-18
Electrical
49.) How are the trim switches operated?
Both switches must be moved together
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