Quantcast SECOND ENGINE START (BATTERY START) - TM-1-1510-223-MTF0047

 

Click here to make tpub.com your Home Page

Page Title: SECOND ENGINE START (BATTERY START)
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
   
   

 

Share on Google+Share on FacebookShare on LinkedInShare on TwitterShare on DiggShare on Stumble Upon
Back
CONDITION lever (after N1 RPM passes 13% minimum)
Up
TM-1-1510-223-MTF Maintenance Test Flight Manual Army Model RC-12
Next
ABORT START PROCEDURE
TM 1-1510-223-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
SECOND ENGINE START (BATTERY START)
1.
# 2 generator load - Verify less than 50%.
2.
Propeller area - Clear.
3.
# 1 ENG START switch - START-IGNITION.
# 1 IGN ON annunciator should illuminate and # 1
FUEL PRESS annunciator should extinguish.
4.
CONDITION lever (after N1 RPM passes13%
minimum - LOW IDLE.
5.
TGT and N1 - Monitor (TGT 1000 maximum).
C
6.
Oil pressure - Check (60 PSI minimum).
7.
# 1 ENG START switch - OFF after TGT peaks.
8.
CONDITION levers - HIGH IDLE. Monitor TGT as
CONDITION lever is advanced.
9.
POWER levers - GROUND FINE.
10. PROP levers - Retard to FEATHER detent.
11. BATTERY CHARGE annunciator - Check on.
BATTERY CHARGE annunciator should extinguish
within 5 minutes following a normal engine start on
battery.
12. # 1 and # 2 INVERTER switches - ON, check
INVERTER annunciators off.
13. # 1 GENERATOR switch - RESET, then ON.
2-35

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

Integrated Publishing, Inc.