Daher-Socata TBM 900 Pilot's Information Manual page 213

SECTION 4
NORMAL PROCEDURES
EASA Approved
AFTER STARTING ENGINE (3/3)
This light may remain OFF, if cabin temperature is very high, for example after a prolonged parking in hot
conditions (see Chapter 7.13 for operational principle).
- "WINDSHIELD" switch
Increase power so as to get Ng ≥ 80% to check AIRFRAME DE ICE.
Theoretically, necessary air bleed to inflate wing and empennage leading edges, as well as depression
necessary to their deflation are sufficient when throttle is positioned on Flight IDLE. However, it is advised
for check to choose a Ng power ≥ 80 % in order to obtain operation design pressure, which enables
illuminating surely the two green lights and avoiding
- "AIRFRAME DE ICE" switch
The cycle lasts 67 seconds. Check both inflation impulses, and illumination of each corresponding green
light :
- the first impulse inflates the external and middle wing boots,
- the second impulse inflates the leading edge boots of empennages and inner wing.
- "AIRFRAME DE ICE" switch
- "INERT SEP" switch
WARNING CAS MESSAGE
14 - "INERT SEP" switch is kept ON while taxiing in order to avoid ingestion of particles by the engine.
Page 4.4.22
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Visually check functioning of deicer boots during 1 total cycle
and illumination of the two green lights located above the switch
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"INERT SEP ON"
PILOT'S OPERATING HANDBOOK
"VACUUM LOW"
untimely alarms.
. . . . . . . . . . . . . .
full deflection takes
about 30 seconds
Edition 0 -- October 31, 2013
OFF
ON
OFF
ON
ON
Rev. 1