AVS1230_Lab3_flight controls 2023

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School

Western Michigan University *

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Course

1230

Subject

Mechanical Engineering

Date

Dec 6, 2023

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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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