(Refer to CAP 698 figure 4.23)
Find the maximum mass at which a net level-off altitude of 17000 ft can be maintained in case of engine failure (ISA+15° C, A/C AUTO):
48500 Kg
51000 Kg
53200 Kg
50700 Kg
(Refer to CAP 698 figure 4.23)
Find the maximum mass at which a net level-off altitude of 17000 ft can be maintained in case of engine failure (ISA+15° C, A/C AUTO):