Daher-Socata TBM 900 Pilot's Information Manual page 557

PILOT'S OPERATING HANDBOOK
5.8 - ENGINE OPERATION
The following tables or/and the optimum torque indicator must be used during normal operation of the airplane.
IMPORTANT : It is the responsibility of the Operator to make sure that the required version of Garmin
System Software is installed prior to using the hereafter Engine Operation tables.
The Garmin System Software required for this revision of the Engine Operation tables
is the version 0719.10 or later.
This information is displayed on the MFD Power-up page upon system start.
The following conditions are given :
- BLEED AUTO.
The torque must be set at or below the value corresponding to the local conditions of flight level and temperature.
Example : for FL = 260 and OAT = - 22°C, the following tables give the maximum torque to be set.
Maximum climb power :
TRQ = 82 % for IAS = 124 KIAS (Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed)
(cf. tables Figures 5.8.1 and 5.8.1A)
Maximum cruise power :
TRQ = 96 % (cf. tables Figures 5.8.2 and 5.8.2A)
Recommended cruise power :
TRQ = 91 % (cf. tables Figures 5.8.3 and 5.8.3A)
REMARK : The engine ITT limit at 840°C during continuous operation may be used in case of
operational need.
Edition 0 -- October 31, 2013
Rev. 1
Inertial separator must be OFF and "BLEED HI" MSG OFF.
THE TRQ SETTING MUST NEVER EXCEED 100 %.
WHEN SETTING TRQ, NG MUST NEVER EXCEED 104 %
NOTE
CAUTION
SUPPLEMENT 58
FIVE--BLADED PROPELLER
Page 9.58.7