Daher TBM 930 - Climb

Pilot's Operating Handbook
Section 4
Normal procedures
EASA Approved
Edition 1 - January 15, 2018
Rev. 2
Page 4.4.52
Climb 1/2
1 - ALT SEL Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2 - Altimeters setting As required. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3 - Autopilot Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Autopilot status and yaw damper ON
▲ CAUTION ▲
Observe TRQ / Ng / Np / ITT / OIL T° and PSI limitations.
Use optimum torque and / or refer to tables in chapter 5.8.
▲
4 - TRQ adjustment / ITT / Ng Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
● NOTE ●
Torque setting during climb must be adjusted according to engine operation
tables in chapter 5.8. These tables give the max. climb power torque setting
(MXCL). For each engine, when torque is reduced below 100 % at high altitude
according to the tables, during the final climb, reaching the maximum permitted
Ng (104 %) is possible and the ITT will be approximately constant, giving a
particular value of ITT.
For a simplified engine operation during climb, power may be set first of all by
torque, using 100 %, then, when the ITT typical value for climb is reached, by
indicated ITT, using this particular value. The margin between this indicated ITT
and 790°C (recommended ITT limit during continuous operation) will gradually
reduce as flight time is performed.
●
5 - Climb airspeed 124 KIAS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Performance tables concerning climb at 124 KIAS and 170 KIAS / M 0.40
are given in chapter 5.10
6 - EIS Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7 - CAS display Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
8 - Weather radar As required. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
9 - Pressurization Check. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
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PIM - DO NOT USE FOR FLIGHT OPERATIONS