T B M
PILOT’S INFORMATION MANUAL 700
SECTION 3
EMERGENCY PROCEDURES
D.G.A.C. Approved
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Page 3.12.4
Rev. 2
3.12 – DEICING SYSTEM
AMBER WARNING LIGHT
PITOT 1
PITOT 2
OR
STALL HTR
ON
Indicates a heating failure of the corresponding probe
Icing conditions may alter airspeed indications on the
airspeed indicator
1 – AVOID icing conditions
If it is not possible :
2 – Perform moderate descent or climb attitudes
V
MO
overshooting and stall warning lights are always operating
V
MO
overshoot warning may be altered by icing
conditions
Monitor maximum airspeed 3 266 KIAS. . . . . . . . . . . . . . . . . . . . . .
Correct operation of the aural stall warning may be
altered by severe or prolonged icing
MONITOR and MAINTAIN minimum airspeed according to
airplane configuration and icing conditions
PITOT 1
PITOT 2
STALL HTR
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