(Refer to figure 4.3.6)
Given:
Distance to Alternate: 450 NM
Landing mass at Alternate: 45 000 kg
Tailwind component: 50 kt
The Alternate fuel required is:
2900 kg
2750 kg
3050 kg
2500 kg
(Refer to figure 4.3.6)
Given:
Distance to Alternate: 450 NM
Landing mass at Alternate: 45 000 kg
Tailwind component: 50 kt
The Alternate fuel required is: