QAVION
8th Sep 2001, 07:40
Yet another question relating to overweight gliders.... :D
Assuming dry fuel tanks at 35,000'... engine flameout and a gliding 747-400... Would the "Range To Altitude Arc" on the Nav Display still be displayed? I have this feeling that the APFD Mode Control Panel is not powered by the Standby Busses... and that the Sel Altitude readout would remain locked at the last selected altitude. If you lost power to the MCP before you had dialled in the altitude of the airport you were intending to divert to, would the Range To Altitude Arc no longer be of any assistance?
Unfortunately, I can't remember what generates the arc.... and I have no access to a sim. I'd guess that the IRS's provide IVS (descent rate) and that the ADCs and MCP provide the altitude differential, but what does the calculation... the EIU's, the FCC's, the FMC's? Does the aircraft remember the last Sel Alt setting if power is lost to the MCP?
Thanks.
Q.
Assuming dry fuel tanks at 35,000'... engine flameout and a gliding 747-400... Would the "Range To Altitude Arc" on the Nav Display still be displayed? I have this feeling that the APFD Mode Control Panel is not powered by the Standby Busses... and that the Sel Altitude readout would remain locked at the last selected altitude. If you lost power to the MCP before you had dialled in the altitude of the airport you were intending to divert to, would the Range To Altitude Arc no longer be of any assistance?
Unfortunately, I can't remember what generates the arc.... and I have no access to a sim. I'd guess that the IRS's provide IVS (descent rate) and that the ADCs and MCP provide the altitude differential, but what does the calculation... the EIU's, the FCC's, the FMC's? Does the aircraft remember the last Sel Alt setting if power is lost to the MCP?
Thanks.
Q.