Twistgrip in CUTOFF position.
Actuate starter.
After N
1
reaches steady level (18 to 22%) and TOT is 150°C or be-
low, advance twistgrip to GROUND IDLE.
Open throttle to 91% N
2
MALFUNCTIONS
3-14. CAUTION AND WARNING LIGHTS
The light panel is located at the top of the instrument panel (Fig.
3-1).
The lights will illuminate when a condition other than normal exists.
The lights will also illuminate when the PUSH TO TEST switch
button is depressed, to test the individual bulbs.
The fire detection system is automatically tested when the PUSH TO
TEST switch button is depressed.
RED WARNING LIGHTS
ENG OUT/LO ROTOR:
Refer to Para 3-1 and Fig. 3-1.
Red light.
Pulsating sound from warning horn and in headset, if installed.
ENG FIRE (Engine Fire):
Refer to Fig. 3-1.
Red light.
Land as soon as possible.
Emergency Procedures
Schweizer RSG, LLC.
Model 269D Helicopter
Pilot's Flight Manual
Reissued: 16 Jan 2019
3-11
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FAA Approved
Book 3.indd 79 8/4/19 1:25 PM