General Info

Question 1

Fuel Tank gal/lbs

Answer 1

143 gallons/ 540 litres

(939 lbs/ 426 kg)

100% = 143 g

75% = 107.25 g

50% = 71.5 g

25% = 35.75 g

15% = 21.45 g

Question 2

Range full fuel

Answer 2

362 NM

(417 SM)

(670KM)

Question 3

Range – nm (km) without reserve at recommended cruise

Answer 3

360 nm (666 km)

Question 4

Endurance full fuel, no Reserves

Answer 4

143 gallons/48 gal per hr = 2.9 hours

Question 5

Fuel burn

Answer 5

40 gal for 50 min flight + refuel + pax reload

143 gallons/48 gal per hr = 2.9 hours

Question 6

Empty weight (standard configuration)

Answer 6

2,690 lbs/ 1,220 kg

Baseline empty weight includes oil and unusable fuel.

Question 7

Aircraft weight (w/fuel; w/o persons)

Answer 7

2SA with 45% fuel = 3468.30

Pilot + Pax weight ≤ 1,492.7 lbs max

Question 8

T/O Power

Answer 8

732 shp

(546 kw)

Question 9

Max Continuous Power

Answer 9

625 shp

(466 kw)

Question 10

Hover IGE

Answer 10

ISA: 9,850’ (3,000m)

ISA +20C: 7,050’ (2,150m)

Question 11

Hover OGE

Answer 11

ISA: 7,550’ (2,300m)

ISA +20C: 4,250’ (1,300m)

Question 12

Service ceiling at 200 fpm (1 mps) rate of climb

Answer 12

15,100’

(4,600m)

Question 13

Rate of climb at SL

Answer 13

1,675 ft/min/ 8.5 m/sec

Question 14

Ng at 100%

Answer 14

51,800 RPM

Question 15

Ng Test

Answer 15

”- - - “if the temperature probe is operative “LL” when the probe is short-circuited “LH” when the probe is open circuit

Question 16

Nf constant RPM

Answer 16

39,800 RPM

Question 17

CG

Answer 17

Longitudinal Datum = 133.8” forward of the center of the MR Mast

Lateral Datum - perpendicular to cabin floor.

Left hand (-) limit - 7.08” (negative side)

Right hand (+) limit - 5.51” (positive side)

Horizontal Plane 102.3” above the cabin floor datum

Question 18

Starting in strong wind

Answer 18

Apply a little forwrd cyclic

Accelerate the engine up to approximately 320 Nr as fast as compatible with T4 limitations

Then follow normal procedure.