1-4
Descriptive Data
1-4-1
Engine
Number of Engines
1
Engine Manufacturer
Pratt & Whitney Canada
Engine Model Number
PT6E-67XP
Engine Type
This airplane incorporates a twin shaft
turboprop engine with 4 axial and 1 centrifugal
compressor stages, an annular combustion
chamber, and a 3 stage turbine where one
stage drives the compressor and two stages
power the propeller.
Horsepower Rating and Engine Speed:
Takeoff Power
1,200 shp
Maximum Climb/Cruise Power
1,200 shp
Compressor Turbine (N
g
) Speed (104%)
38,967 rpm
Propeller Speed (N
p
)
1,700 rpm
Prop Low Speed Mode (optional)
1,550 rpm
1-4-2
5-Bladed Propeller
Number of Propellers
1
Propeller Manufacturer
Hartzell
Propeller Model Number
HC-E5A-31A/NC10245B
Number of Blades
5
Propeller Diameter
105" (2.67 m)
Propeller Type
The propeller assembly consists of a hub unit
and five composite blades, and is a
hydraulically actuated, constant speed, full
feathering and reversible type.
1-4-3
Fuel
Approved Fuels
Any fuel which complies with Section 2, Limitations,
, of this POH.
Total Capacity
−
406.8 US gal, 2,736.5 lb (1,540 liters, 1,241.3 kg).
Usable Fuel
−
402 US gal, 2,703.6 lb (1,521.5 liters, 1,226.4 kg).
Anti-Icing Additive
If anti-icing additive is to be used, then use anti-icing additives in compliance with Section 2,
Limitations,
, of this POH.
Section 1 - General
Descriptive Data
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 1-4-1
12-C-A15-00-0104-00A-030A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY