AVS1230_lab5_hydraulicsystems 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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6

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AVS1230 Lab 5: Hydraulic Systems 2023 Name____________________________________ Date_____________________________ Resources: Seneca PA34 section 2-7 POH, FAA AMT Handbook , Internet research, 3D interactive model for SR20 (note you will have zoom in the SR20 wheel and brake section to this part of the module. 35 Points- Part 1 . Complete the landing gear module and make sure you are on a PC and n full screen mode attach your completion certificate here (screenshot) https://elevate.wmich.edu/aviation/modules/landing-gear
15 Points -Part 2. Matching the images and components with their definitions and images A. Sphere Accumulator B. Hydraulic Pump C. Reservoir
D. Powerpack E. Filter
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F. Shuttle Valve G. Actuator H Cylinder Accumulator
I Relief Valve 36. _____________________________________ is a small unit that consists of an electric pump, filters, reservoir, valves, and pressure relief valve. 37. ___________________________extends the main landing gear outboard and down from the wheel well and locks the landing gear in the down position using internal locking keys located in the lower end of actuator cylinder. 38. The ____________________________________consist of a cylinder and piston assembly. The internal piston separates the fluid and air/nitrogen chambers. 39. The _______________________ prevents over pressure. 40. _____________________ is a tank in which an adequate supply of fluid for the system is stored. 41. ___________________________are used to move non-compressible fluid through an aircraft hydraulic system. 42. The________________________ keeps the fluid free of contaminates. 43. _________________________________ is constructed in two halves. The top port accepts fittings to connect to the pressurized hydraulic system to the ____________. The bottom port is fitted with a gas servicing valve, such as a Schrader valve. 44. The ___________________ allows pressure in a line to be obtained from alternative sources. PART 3. Using the POH for PA 34 Seneca aircraft (landing gear section 2-7) Identify the components and state their function.
45. 1. _________________Function: 46.2. _________________ Function: 47.3. _________________ Function: 48. 4. _________________ Function: 49. 5. _________________ Function: 50. 6. _________________ Function:
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