AVS1230_Lab3_flight controls 2023
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Western Michigan University *
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Course
1230
Subject
Mechanical Engineering
Date
Dec 6, 2023
Type
docx
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3
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AVS 1230
Lab 3: Aircraft Flight Controls 2023
Name_________________________I certify this is my own work. Date__________
Purpose:
Identify primary and secondary flight controls and apply their effect on aircraft flight.
Categorize the planform of several aircraft.
Reference:
Aircraft Manuals
Internet
Interactive 3D content
Activities: (50 points total)
Part 1:
1. 40 points.
Explore the Interactive SR20 3D Model with interactive fight controls and then
answer the following questions, then take the quiz and attach your completion certificate
(screen shot).
aileronshey have now removed the rudder aileron connect in our WMU SR20s.
https://elevate.wmich.edu/aviation/modules/cirrus-flight-controls
Note: they have now
removed the rudder aileron connect in our SR20s.
Use Chrome or Edge on a PC *Does not work on phone or tablet devices.
Part 2: Research using the
SR20 manual.
41. What type of flap is installed on the Cirrus SR20?
1
A. Single-Slotted
B. Fowler
C. Plain
D. Split
42. Which flight controls on the Cirrus SR20 have ground adjustable trim tabs?
A.
________ _________________________
B.
__________ ______________________
C.
___________ ______________________
43. The Cirrus SR20 has electric trim to control _______ _________ and _______ _________.
44. If the control stick is rotated to the left, what direction do the left and right ailerons move?
45. The flight controls on the Cirrus SR20 are ___________________ design.
A. Hydraulically
B. Electrically
C. Cable
D. Conventional
Part 3: Textbook Questions (1 points each)
https://www.faa.gov/regulations_policies/handbooks_manuals/aviation/FAA-H-8083-
31B_Aviation_Maintenance_Technician_Handbook.pdf
46. A stabilator controls ___ about the _____________ axis.
47. An elevator controls _______ ___________ about the ______ ________ axis.
48. On a servo tab control system, the tab is actuated for what reason?
A.
To control level flight in turbulence
B.
To assist in the movement of the
control surface
C.
To provide a negative feedback to the pilot
D.
To provide a nose up attitude during landing
49. Leading edge flaps help controllability at _______________ airspeeds and
_______________ angles of attack.
A.
Low, High
B.
High, Low
C.
High, High
D.
Low, Low
2
50.
Ailerons control _______ ___________ about the ____ _____________ axis.
3
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