1
Q
VMO C208
A
175 KIAS
2
Q
PMD C208B
A
3969 kg
3
Q
Total fuel capacity C208B
A
335 U.S. Gallons
1268 L
4
Q
Total capacity each tank C208B
A
167 lbs
632 L
5
Q
Total usable fuel C208B
A
332 U.S. Gallons
1256 L
2224 lb
6
Q
MTOW C208b
A
8750 lbs
7
Q
Fuel flow (L)
A
200 L
8
Q
Endurance
A
6 no reserve
9
Q
Limite de ITT
A
1090
10
Q
Limite
A
765
740
11
Q
L para kg
A
X 0,8
12
Q
Lbs p L
A
X 3,78
13
Q
Engine failure during takeoff roll
A
- Power lever …………BETA
2. Brakes ……….. apply
14
Q
Engine failure immediately after takeoff
A
- Airspeed ….. 85 KIAS
- CHECKLIST
- RPM …. feather
- Flaps …. (as required. Ideal 20°)
- Fuel shutoff
- Fuel tanks … off
- Battery … off
15
Q
Engine failure during flight
A
- Airspeed …. 95 kias
- Power lever … IDLE
- Prop RPM … FEATHER
- Fuel condition lever … CUTOFF
- Checklist
16
Q
ENGINE FLAMEOUT DURING FLIGHT
A
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
