Quantcast Propeller autofeathering system and propeller unfeathering

 

Click here to make tpub.com your Home Page

Page Title: Propeller autofeathering system and propeller unfeathering
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
FWD VENT BLOWER switch
Up
TM-1-1510-223-MTF Maintenance Test Flight Manual Army Model RC-12
Next
Engine cleanup - TM-1-1510-223-MTF0083
TM 1-1510-223-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
LOW SPEED SYSTEMS CHECK (CONT)
(11) CONDITION lever - LOW IDLE.
(12) ENG START switch - OFF after TGT
peaks.
(13) CONDITION lever - HIGH IDLE.
(14) PROP lever - As required.
(15) POWER lever - As required.
switch - RESET, then
ON.
(17) Engine AUTO IGNITION -As required.
(18) PROP SYNC switch - As required.
(19) Electrical equipment - As required.
h.
Repeat step g for opposite engine if
required.
*12. Propeller autofeathering system and
propeller unfeathering - Check as follows:
a. AUTOFEATHER switch - ARM.
b. Airspeed - 120 KIAS.
c. PROP levers - Set 1700 RPM.
d. POWER levers - Set as required to arm auto
feather system.
e. CONDITION lever (engine to be feathered) -
IDLE CUTOFF.
*f.
Record the time from fuel cutoff until
propeller is feathered.
(Propeller is
considered to be feathered
2-70

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

Integrated Publishing, Inc.