Daher TBM 960 - Descriptive Data; Engine; Propeller; Fuel

1.3 -
Descriptive Data
Engine
Number of engines: 1
Engine manufacturer: Pratt & Whitney Canada
Engine model number: PT6E-66XT
Engine type: Free turbine, reverse flow and two turbine sections
-
Compressor type: four axial stages, one centrifugal stage
-
Combustion chamber type: annular
-
Turbine type: one gas generator turbine stage, two power turbine stages
Horsepower rating and propeller speed: 895 SHP (667 kW) at 1,925 RPM
The engine is electronically controlled by a Full Authority Digital Engine Control
(FADEC) system.
Propeller
Number of propellers: 1
Propeller manufacturer: Hartzell
Propeller model number: 5D31-NK366B1 / 86DB01B
Number of blades: 5
Propeller diameter: 91 in (2.311 m)
Propeller type: Adjustable constant speed, with feathering and hydraulic control
reverse
Propeller blade setting at 30-inch station:
- Low pitch: 19.5°
- Feathering: 86.1°
- Maximum reverse: - 9.3°
The electro-hydro-mechanical Propeller Control Unit (PCU) modulates the blade
angle.
Fuel
Total capacity: 301 USG (1,140 liters)
Total capacity, each tank: 150.5 USG (570 liters)
Section 1
General
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 00
Page 1.3.1
PIM - DO NOT USE FOR FLIGHT OPERATIONS