Quantcast Unit Three Review Questions

 

Click here to make tpub.com your Home Page

Page Title: Unit Three Review Questions
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
   
   

 



STUDENT GUIDE T-39N/G NATOPS
UNIT THREE REVIEW QUESTIONS
1.
External power requirements are:
Utility: ____ volts ________ amps
Start:
____ volts ________ amps
2.
The battery bus is connected to two __________ volt batteries through __________.
3.  The Starter bus is powered either by _______________ connected in (series/parallel) or by
_______________
4.  The Starter bus supplies power to the starter-generators and engine instruments necessary
to monitor the start. (TRUE/FALSE)
5.  The Paralleling bus is powered by the _______________ bus, the __________ or
__________.
6.  The DC Essential bus is normally powered by the _______________ bus; in the event of
a dual generator failure in flight, it receives power directly from the__________________
bus.
7.
The ESS position of the battery switch should be selected only if _______________.
8.  With a single generator failure, Mission DC bus(es) will be shed.  Mission
bus(es) may be regained by placing the mission bus switch to EMER. (TRUE/FALSE)
9.  On deck, with a single generator operating, the Secondary bus will remain unpowered.
(TRUE/FALSE)
10. Aircraft AC power is supplied by two volt-amp inverters or one _______________ volt-
amp inverter, which in turn receive DC power from the _______________ bus.
11.  If both the MAIN and STANDBY inverters fail, AC power is available from the
_______________ inverter to the _______________ bus only.
12. AC power from the MAIN or STANDBY inverters power the AC _______________ bus,
which in turn powers the _______________ bus, one 26 VAC bus and four 5 VAC buses.
13. In the event of a loss of all AC power, the _______________ caution light will
illuminate.
14. Mission AC inverters are powered by Mission DC bus. (TRUE/FALSE)
3-6
ELECTRICAL SYSTEM


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

Integrated Publishing, Inc.