Order this information in Print

Order this information on CD-ROM

Download in PDF Format

     

Click here to make tpub.com your Home Page

Page Title: 2-3. CONTROLS AND INDICATORS
Back | Up | Next

Click here for a printable version

Google


Web
www.tpub.com

Home


   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Combat
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
USMC
   
Products
  Educational CD-ROM's
Printed Manuals
Downloadable Books
   

 

TM 1-4920-458-13&P 2-3. CONTROLS AND INDICATORS a. General.  This section describes and furnishes the operator with sufficient information pertaining to the various controls and indicators provided for the proper operation of the equipment. b. Power Switch (1).  The single pole, double throw, toggle-type power switch, has an OFF position which opens the circuit and shuts off the electrical power supply to the tester.  The ON position is in the circuit to provide electrical current to the tester when the power source is connected. c. Indicator light (2).  The indicator light illuminates when the power circuit in the tester is operating. d. Cartridge fuse (3).  The 28 V dc, 5 amp cartridge fuse provides protection against an excessive flow of current which would damage the electrical system. e. Vacuum Selector Knob (4).  The vacuum selector knob has three positions, and operates a valve which controls the vacuum systems required to test aircraft instruments. f. Pressure Selector Knob (5).  The pressure selector knob has three positions and operates a valve which controls the pressure systems required to test aircraft instruments. g. Pressure Bleed Down Knob (6).  Counterclockwise rotation of pressure bleed down knob opens a needle valve allowing system pressure to bleed off.  ROTATE clockwise for pressure up. h. Pressure Control Knob (7).  Counterclockwise rotation of pressure control knob opens a needle valve allowing pressure in system to increase. i. Vacuum Bleed Knob (8).  Counterclockwise rotation of vacuum bleed  knob permits system vacuum to bleed off. ROTATE clockwise for vacuum up. j. Vacuum Control Knob (9).  Counterclockwise rotation of vacuum control knob opens a needle valve and provides increased vacuum in system. k. Shut-off Valves (10).  Shut-off valves located on the top of the operator panel are provided for testing aircraft instruments and checking the master instruments for leaks. l. Altimeter Indicator (11).  The altimeter indicator measures from -1,000 feet below to 35,000 feet above sea level at a rate of 6,000 feet per minute. 2-3

Privacy Statement - Press Release - Copyright Information. - Contact Us - Support Integrated Publishing

Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business