Quantcast Flight Management System

 

Click here to make tpub.com your Home Page

Page Title: Flight Management System
Back | Up | Next

Click here for thousands of PDF manuals

Google


Web
www.tpub.com

Home

   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
   
   

 



CHAPTER TEN
STUDENT GUIDE FOR T-1A AIRCRAFT SYSTEMS
Attitude Heading Computer
Two AHCs, mounted in the avionics rack, provide pitch, roll, and stabilized magnetic heading
data to:
1.
DPU number one and two
2.
MFD
3.
FCS
4.
GPWS and TCAS (number one AHC only)
5.
Flight Data Recorder (FDR) via the Data Acquisition Unit (DAU)
Flux Detector Unit
Two FDUs, one located in each wingtip, are two-axis sensors that sense the horizontal
component of the earth's magnetic field. The FDUs provide flux sense outputs to the AHCs.
The outputs are used to compute the aircraft magnetic heading angle.
AHRS Standby Battery
The AHRS standby battery, located in the avionics rack, provides power in the event of primary
power loss. The battery provides approximately 11 minutes of operating power to AHC number
one and two.
1010. FLIGHT MANAGEMENT SYSTEM
The FMS consists of:
1.
A CDU located on the pedestal
2.
A flight management computer
3.
A Database Unit (DBU) located on the avionics rack
CDU
The CDU provides a means of entering radio frequencies and transponder codes as secondary to
the RTU. The CDU is a high resolution seven color LCD containing:
1.
A display
2.
Keys
10-10
AVIONICS


Privacy Statement - Press Release - Copyright Information. - Contact Us

Integrated Publishing, Inc.