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Daher TBM 960 - Section 5; Performance

Daher TBM 960
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Section 5
Performance
T
able of Contents
5.1
-
General
...................................................................................... 5.1.1
5.2 - Noise Level ................................................................................ 5.2.1
5.3 - Airspeed Calibration .................................................................. 5.3.1
5.4 - Cabin Pressurization Envelope ................................................. 5.4.1
5.5 - SAT - OAT Conversions ............................................................ 5.5.1
5.6 - Stall Speeds .............................................................................. 5.6.1
5.7 - Wind Components ..................................................................... 5.7.1
5.8 - Engine Operation ...................................................................... 5.8.1
Maximum Climb Power – 124 KIAS ..................................... 5.8.2
Maximum Climb Power – 170 KIAS / M 0.40 ....................... 5.8.19
Maximum Cruise Power ........................................................ 5.8.36
5.9 - Takeoff Distances ...................................................................... 5.9.1
Weight 5,512 lbs (2,500 kg) .................................................. 5.9.3
Weight 5,512 lbs (2,500 kg) – INERT SEP ........................... 5.9.4
Weight 6,579 lbs (2,984 kg) .................................................. 5.9.5
Weight 6,579 lbs (2,984 kg) – INERT SEP ........................... 5.9.6
Weight 7,394 lbs (3,354 kg) .................................................. 5.9.7
Weight 7,394 lbs (3,354 kg) – INERT SEP ........................... 5.9.8
Weight 7,615 lbs (3,454 kg) .................................................. 5.9.9
Weight 7,615 lbs (3,454 kg) – INERT SEP ........................... 5.9.10
5.10 - Climb Performance .................................................................... 5.10.1
MXCL – Vertical Speeds (IAS = 124 KIAS) .......................... 5.10.2
MXCL – Vertical Speeds (IAS = 170 KIAS / M 0.40) ............ 5.10.3
MXCL – Time, Consumption and Climb Distance ................ 5.10.4
Climb Performance after Go-Around .................................... 5.10.11
Climb Performance – Flaps TO ............................................ 5.10.12
5.11 - Cruise Performance .................................................................. 5.11.1
Maximum Cruise ................................................................... 5.11.1
Section 5
Performance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 02
Page 5.0.1
PIM - DO NOT USE FOR FLIGHT OPERATIONS

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