Daher TBM 850, Pilot'S Information Manual

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SECTION 5
PERFORMANCE
T B M
850 PILOT’S OPERATING HANDBOOK
Page 5.8.1A Edition 1 -- June 22, 2007
Rev. 14
POST--GARMIN SOFTWARE VERSION 9.14 or ANY LATER
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 0719.06 or later.
This information is displayed on the MFD Power--up page upon
system start.
The following conditions are given :
-- Np = 2000 RPM,
-- BLEED switch on AUTO.
The torque must be set at or below the value corresponding to the local
conditions of flight level and temperature.
NOTE :
Inertial separator must be OFF and BLEED HI msg OFF.
Example : for FL = 260 and OAT = -- 22
°
C, the following tables give the
maximum torque to be set.
Maximum climb power : TRQ = 92 % for IAS = 130 KIAS
(Add 1 % of TRQ for each additional
10 KIAS on climb airspeed)
(cf. tables Figures 5.8.1 and 5.8.1A)
Climb at 700 SHP power : TRQ = 92 % for IAS = 130 KIAS
(Add 1 % of TRQ for each additional
10 KIAS on climb airspeed)
(cf. tables Figures 5.8.2 and 5.8.2A)
Maximum cruise power : TRQ = 108 %
(cf. tables Figures 5.8.3 and 5.8.3A)
Recommended cruise power : TRQ = 103 %
(cf. tables Figures 5.8.4 and 5.8.4A)
PIM - DO NOT USE FOR FLIGHT OPERATIONS