Eurocopter AS 350 83 Flight Manual page 74

FLIGHT MANUAL.
-TEST LIGHT push-button (on interseat console)- engaged
.Warning lights on Caution Advisory Panel
and instrument panel lit ~
.Target and software identification number displayed on both screens , ,
-TEST FIRE push-button (on interseat console) -engaged
.Ignition of ENG FIRE warning light
-On VEMD
.Engine oil temperature and pressure displayed
.Fuel gauge quantity
-Hydraulic pressure ON
-Heating system*, demister, air
conditioner* OFF
-Gyroscopic instruments ON
4 STARTING
~ed and amber) warning lights OUT ...
-Switch on the booster pump On console
.Check that the blue indicator light is on (on the instrument panel).
-Starting selector ON
(for outside air temperatures below -20'C, refer to SUP.04).
.Check that Ng increases.
.Check that t4 remains below its limit.
.Check that the rotor is turning.
.Check that the engine oil pressure increases.
.Check that the following Warning Caution Advisory Panel
lights go out:
-P MOT (ENG.P) (should be out at 70 % Ng)
-P BTP (MGB.P)
-HYDR.
~ : On the ground, to obtain zero thrust at the tail rotor, it is R
necessary to push the LH pedal over 2 cm approx. (0.8 in). R
. -Engage the horn, the HORN light should extinguish.
.Check aural warning operates at approximately 360 rpm
.Check that NR is in the green zone of the indicator, near
the lower limit.
-Lower the switch guard on the starter switch.
-Position the rotor brake safety device.
-Disconnect external power, if used
.Check: Warning-Caution-Advisory Panel GEN and BAT
lights off.
-Switch on PITOT heating on pedestal panel.
.Check that the PITOT light go out
.
* optional
R
DGAC Approved: 350 B3 4.1
II
I~J:::Q:Jn:Q:
ill 98-36 Page 4