ICE AND RAIN PROTECTION
Operation
Aircraft Operations Manual
11.2
PAGE
3
Jun 01/19
CONDITIONS
NORMAL PROCEDURES
(Cont’d)
Takeoff on RWY with standing water, slush, wet or dry snow
When taking off in this condition there is a risk of spray ingestion into the en-
gines. Switch on engine anti
−
ice when ambient temperature is +5
C (+10
C ac-
cording to FAA AD 96
−
01
−
04 R1 and 2008
−
06
−
11) and below (operation may
be restricted by national rules).
For a/c with Mod.no 3529 for 340B / 3530 for 340WT
Departure when icing conditions on ground and expected icing after lift
−
off
−
When engine anti
−
ice is selected, before take
−
off, L/R ENG ANTI
−
ICE lights
on the Flight Status Panel will come on. Use these lights, also as
Ice Speed
“armed” lights
. This is the indication that the stall warning will change (in-
crease) the stall warning triggering airspeeds after 6 minutes from lift
−
off. (
See also FLIGHT PROCEDURES 25/3 and 25/10 Takeoff briefing and Call
−
outs).
Ice formation discovery during darkness
When operationally feasible, switching on the cockpit dome light will increase
the possibility of discovering unexpected ice, for example on the wipers.
Using the strobe
−
lights or switching on the landing lights now and then will in-
crease the possibility of identifying unexpected icing conditions.
The air inlet can be inspected from the cockpit by use of a flashlight.
Operation in and after certain icing conditions
During flight through heavy snow, heavy sleet or ice crystals, substantial
amounts of ice may be collected on parts of the bird catcher even with a fully
functioning engine anti
−
ice system. This is no problem as long as a positive air-
flow through the birdcatcher is assured. However, REVERSE POWER OP-
ERATION BELOW 50 KTS (EVEN WITH A FULLY OPEN EXHAUST
NOZZLE) AND DURING PROPELLER BRAKE OPERATION WITH A MORE
THAN 30 PERCENT ICED
−
UP (BLOCKED) NOZZLE THE AIRFLOW IS RE-
VERSED THROUGH THE BIRDCATCHER.
Such conditions are potentials for ice being sucked into the engine. After en-
countering such conditions, keep the engine anti
−
ice system ON for the dura-
tion of flight at temperature below +5
C if operationally feasible.
Engine anti
−
ice ON during ground operation after landing will assure that both
the air and the walls in the birdcatcher is warmed up. This will expedite the melt-
ing of possible ice collected in the birdcatcher. However, if the prevailing tem-
perature is below the freezing point, de
−
icing of the birdcatcher might be neces-
sary. An inspection of the air intake/birdcatcher for possible residual ice/snow
will determine the need for de
−
icing of the birdcatcher.
(Cont’d)
Содержание 340B
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