AVS1230_ Lab 1 2023(2)
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Jordy Keurntjes AVS1230
September 19th
AVS 1230
Lab 1
Aircraft Flight Controls
Purpose:
Identify primary and secondary flight controls and apply their effect on aircraft flight. Categorize the planform of several aircraft.
Reference:
Electronic Flight Book - COA
Internet Activities:
Part 1: Aircraft planform
Internet search
Identify the planform of the 11 different types of aircraft according to their wing shapes. List the
aircraft and the type of their planform(wing shape).
Aircraft
Planform
1
Supermarine Spitfire Eliptical Wing
2
Seversky-35
Semi-Elliptical Wing
3
Piper PA 38
Rectengular Wing
4
P-51 Mustang Tapered Wing
5
Mirage 2000
Delta
6
English Electric Canberra Constant Chord with Tapered Outer
7
Lockheed Martin F-22 Raptor
Tapezoidal
8
Aérospatiale-BAC Concorde
Ogive
9
Boeing 787 Dreamliner
Swept Back Wings
10
Suko Su-47 Berkut
Swept Forward Wings
11
General Dynamics F-
111 Aardvark
Variable Sweep Wings
Jordy Keurntjes AVS1230
September 19th
Part 2: WMU Fleet Flight Controls
EFB Toolkit
1.
The primary flight controls on the Cirrus SR20 are ___________________ actuated. (Finals Question)
A. Hydraulically
B. Cable
C. Pneumatic
2.
What type of flap is installed on the Cirrus SR20?
See Cirrus Manual (7-22) EFB Toolkit
A. Plain
B. Split
C.
Single-slotted flaps
D. Fowler
3.
Which flight controls on the Cirrus SR20 have ground adjustable trim tabs?
A. Rudder
B. Elevator C. Aileron 4.
The Cirrus SR20 has electric trim to control Pitch and Roll
SEMINOLE, Hangar 3.
Note: Do not enter the Seminole cockpit without permission.
What is Item A marked on the Seminole in Hangar 3?
What type of Trim tab is Item A.1 (Servo or Anti Servo)
Jordy Keurntjes AVS1230
September 19th
5.
In what position must the flaps be to allow passengers to enter the cabin of the Seminole?
6.
Which flight control is used to control pitch on the Seminole?
7.
The flaps on the Seminole are ___________________ actuated.
A. Manually
B. Electrically
C. Hydraulically
D. Pneumatically
8.
The stabilator trim on the Seminole can be electrically or __________________ operated.
Cessna 172 Lab aircraft located in Hangar 2.
What type of flap does the 172R use?
Single Slotted Flaps What is Item A
Single Slotted Flaps
Item B
Elevator
Item C
Horizontal stabilizers Item D
Elevator trim tab
King Air Hangar 4
Item A
Trim tab for rudder
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Jordy Keurntjes AVS1230
September 19th
Item B
Rudder
Item C
Trim tab for Aileron
Item D
Aileron
1.
Enter the King Air. Make sure the aileron area is clear. If the control yoke is rotated to the left, what direction do the left and right ailerons move? If the yoke is rotated to the left is goes down and when to the right, it goes up this is the opposite for the other side of the wing (Right) Which aileron has the greater travel?
The left aileron has the greater travel Mooney Aircraft, Hangar 4
Item D, Tail assembly-How is the Horizontal Stabilizer trimmed for Flight? This is done with the Trim wheel What part of the tail moves?
Rudder, Tail
Many aircraft have an interconnect system for the aileron and rudder to counteract Adverse yaw. Move the flight controls in the Mooney aircraft in the hangar. Does this aircraft utilize an interconnect system?
Part 3: Questions
Jordy Keurntjes AVS1230
September 19th
1.
Spoilers assist the Ailerons during approaches for landing.(
Finals question) 2.
What is the purpose of a pulley in a cable flight control system?
A.
To assist the cable in turning corners
B.
Route the cable through structures
C.
Keep tension on the cable
D.
Adjustment point for flight control travel
3.
Why do moveable flight control surfaces have large counterweights installed in the leading edge? What happens is that it will limit the gusts loads and as well it will suppress flutter
Reference:
https://aviation.stackexchange.com/questions/35352/why-are-counterweights-used-in-aircraft-
production
4.
When a flight control with a balanced tab is moved, the tab will move in the opposite direction as the flight control.
5.
When a flight control with an anti-servo tab is moved, the tab will move in the Same direction as the flight control.
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Situation 9 - A 6-m long ladder weighing 600 N is shown in the Figure. It is required to determine
the horizontal for P that must be exerted at point C to prevent the ladder from sliding. The
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The jet plane has a mass of 250 Mg and a horizontal
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Consider the difference between tension and compression. We defined
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The 20-g bullet is travelling at 400 m/s when it becomes
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The spring has a stiffness k = 200 N/m and an
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