General

Question 1

Lenght: _________
Width: _________
Height: _________

Answer 1

Lenght: 29.6ft / 9.92M
Width: 43ft / 13.11M
Height: 11.3ft / 3.44M

Question 2

Dihedral: ____________

Fuselage Width: ______

Answer 2

Dihedral: 4.5˚

Fuselage Width: 4.58ft / 1.39M

Question 3

Engine: ____________________________

Engine Type: _______________________

Answer 3

Engine: Pratt & Whitney Canada PT6A-42A
Engine Type: Free shaft turboprop with 3 axial and 1 centrifugal compressor stages, an annular combustion chamber, and a 3 stage turbine where one stage drives the compressor and a dual stage powers the propeller

Question 4

T/O PWR + Max Continues: ___________
Compressor Turbine Speed Ng: _______
Propeller Speed Np: _________________

Answer 4

T/O PWR + Max Continues: 500 SHP
Compressor Turbine Speed Ng: 38.100 RPM (101,7%)
Propeller Speed Np: 2.000 RPM

Question 5

Propeller: __________

Propeller Type: _____

Answer 5

Propeller: Hartzell 5 blade
Propeller Type: The propeller assembly consists og a hub unit and five metal blades, and is a hydraulically actuated, constant speed, full feathering and reversible type.

Question 6

Fuel: ______________
Fuel Capacity: ______
Unuseable Fuel: ____

Answer 6

Fuel: Jet A, Jet A-1
Fuel Capacity: 1160LBS / 173 USG
Unuseable Fuel: 20LBS / 3 USG

Question 7

Weight:
MRW:  \_\_\_\_\_\_\_\_\_\_\_\_\_\_
MTOW: \_\_\_\_\_\_\_\_\_\_\_\_\_
MLW:  \_\_\_\_\_\_\_\_\_\_\_\_\_\_
MZFW: \_\_\_\_\_\_\_\_\_\_\_\_\_
Max. Weight Bag.: \_\_\_\_

Answer 7

Weight:
MRW:  5134 LBS (2328,7 Kg)
MTOW: 5092 LBS (2309,7 Kg)
MLW:  4850 LBS (2199,9 Kg)
MZFW: 4850 LBS (2199,9 Kg)
Max. Weight Bag.: 100 LBS (45,3 Kg)