T B M
PILOT’S INFORMATION MANUAL 700
SECTION 3
EMERGENCY PROCEDURES
D.G.A.C. Approved
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Page 3.3.10
Rev. 8
3.3 – ENGINE FAILURES
RED WARNING LIGHT ”ITT” ON (Cont’d)
3 – Record the engine parameters read in case of overtemperature, as
well as ground conditions.
4 – Inform maintenance department.
During flight
1 – ITT indicator CHECK. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2 – Reduce power and correct display according to ”Engine Operation”
tables – Chapter 5.7
If ITT remains > 800°C :
3 – Reduce power to maintain ITT < 800°C.
4 – Shorten the flight.
5 – Record the airplane and engine parameters read in case of
overtemperature.
6 – Inform maintenance department at the end of the flight.
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