Trying to figure these out....There is a limitation that says, "If both engines are to be started using the APU bleed air, then the operating engine thrust must not exeed 70%N2." Why can't the operating engine exeed 70%?
Also, in flight, why is APU bleed air extraction not permitted for an engine start during single engine operations?
Thanks for any help...
Also, in flight, why is APU bleed air extraction not permitted for an engine start during single engine operations?
Thanks for any help...