Daher TBM 850, Pilot'S Information Manual

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SECTION 5
PERFORMANCE
T B M
850 PILOT’S OPERATING HANDBOOK
Page 5.8.1 Edition 1 -- June 22, 2007
Rev. 14
P RE--GARMIN SOFTWARE VERSION 9.14
5.8 -- ENGINE OPERATION
The following tables or/and the optimum torque indicator must be used during
normal operation of the airplane.
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 = -- 21
°
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 = 106 %
(cf. tables Figures 5.8.3 and 5.8.3A)
Recommended cruise power : TRQ = 101 %
(cf. tables Figures 5.8.4 and 5.8.4A)
CAUTION
THE TRQ SETTING MUST NEVER EXCEED 121.4 % FOR
NP = 2000 RPM.
WHEN SETTING TRQ, NG MUST NEVER EXCEED 104 %
REMARK :
The engine ITT limit at 840
° C during continuous operation may be used in
case of operational need.
PIM - DO NOT USE FOR FLIGHT OPERATIONS