Eurocopter AS 350 83 Flight Manual page 331

C~PLEMENTARY FLIGHT MANUAL
Structure .
-Remove the cabin cover once the inspection is completed.
-Make sure that the windshield wiper has not remained stuck on the
canopy.
FliQht controls -EnQine controls
-8efore operating the controls, it is recommended to heat-up the inside
of the cabin.
-Operate the controls progressively, then operate the rotor brake
controls, fuel flow control and collective pitch control over their
c~lete travel.
!!,~S re~ommend~d got to oerform extensive travel of the cvclic and
.
tail rotor controls.
Fuel svsten bleedino
Do not bleed the fuel system under a te..,erature equal to or lower than
-10 .C where valve seals prove inefficient.
3.6 Check after Last Fliaht of the Day
The operations described in SEGION 8.4.1 are to be c~leted by the
following actions.
-Inspection of the engine magnetic plugs should be performed within
30 min after the rotor has stopped rotating, in order to avoid seal
damaging.
-Care must be taken not to leave doors open.
-Install the air intake cover and exhaust nozzle blank.
-When the aircraft is parked in an unsheltered area it is reconmended to
apply anti-icing materials and to carry out the aircraft parking and
mooring.
NOTE: ANTI-ICING MATERIALS
--Anti-icing fluid -isopropyl alcohol as per AIR 3660 or deicing
as per AIR 356S (MIL-A-6091).
-Anti-icing sealing co..,ound 8.437.
-Anti-icing co..,ound E. 57.
. -Anti-rain material S.P.R. G7.
-Anti-icing material to be applied on blades: Kilfrost ABC or
Kilfrost DF.
CAUTION: -REFER TO GENERAL INSTRUmONS FOR THE USE OF
-ANTI-ICING MATERIALS.
-ANTI-ICING MATERIALS CAN DAMAGE THE HELICDPTER
C~PONENTS.
-USE RECOMMENDED AND APPROVED ANTI-ICING MATERIALS
ONLY.
350 83 8.4 .
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