C208B

Question 1

VMO C208

Answer 1

175 KIAS

Question 2

PMD C208B

Answer 2

3969 kg

Question 3

Total fuel capacity C208B

Answer 3

335 U.S. Gallons

1268 L

Question 4

Total capacity each tank C208B

Answer 4

167 lbs

632 L

Question 5

Total usable fuel C208B

Answer 5

332 U.S. Gallons
1256 L
2224 lb

Question 6

MTOW C208b

Answer 6

8750 lbs

Question 7

Fuel flow (L)

Answer 7

200 L

Question 8

Endurance

Answer 8

6 no reserve

Question 9

Limite de ITT

Answer 9

1090

Question 10

Limite

Answer 10

765

740

Question 11

L para kg

Answer 11

X 0,8

Question 12

Lbs p L

Answer 12

X 3,78

Question 13

Engine failure during takeoff roll

Answer 13

1. Power lever …………BETA

2. Brakes ……….. apply

Question 14

Engine failure immediately after takeoff

Answer 14

1. Airspeed ….. 85 KIAS
2. CHECKLIST
3. RPM …. feather
4. Flaps …. (as required. Ideal 20°)
5. Fuel shutoff
6. Fuel tanks … off
7. Battery … off

Question 15

Engine failure during flight

Answer 15

1. Airspeed …. 95 kias
2. Power lever … IDLE
3. Prop RPM … FEATHER
4. Fuel condition lever … CUTOFF
5. Checklist

Question 16

ENGINE FLAMEOUT DURING FLIGHT

Answer 16

IF GAS GENERATOR SPEED (NG) IS ABOVE 50%:
1. POWERLever ……………………..IDLE
2. IGNITIONSwitch ……………………ON
Checklist

IF GAS GENERATOR SPEED (NG) IS BELLOW 50%:
5. Fuel condition lever …. CUTOFF

AIRSTART CHECKLIST