At least a single cycle aural and visual master warning to signal that the autopilot is

A unique autopilot disconnect aural warning and a visual warning for a limited period of

A continuous aural and visual master warning highlighting to the pilot that he/she must put

A continuous aural and visual master warning sounding until the pilot presses the autopilot

(1) unforeseen or unpredictable factors: (2) alternate

(1) all known predictable factors; (2) alternate

(1) unforeseen or unpredictable factors; (2) destination

(1) all known predictable factors: (2) destination

ADIRU is an Air Data Computer which is integrated with an Inertial Navigation System

ADIRU is an Air Data Computer which is integrated with an Inertial Unit and GPS

ADIRU is an Air Data Computer which is integrated with an Inertial Reference Unit

ADIRU is an Attitude Director Indicator which is integrated with an Inertial Reference Unit

5min

20min

10min

2min

heading.

attitude and heading

attitude and ground speed

position and attitude.

can only operate when interfacing with the radionavigation equipment.

can operate as stand alone equipment without any interface with other navigation equipment.

can only operate when interfacing with the GPS equipment

can only operate when communicating with ground installations.

By setting the INS mode selector to "ALIGN" and waiting for the required time.

By setting the INS mode selector to "ALIGN" and then flying straight and level with NO airspeed variations for

It can NOT, the aircraft must be stationary on the ground for alignment to be performed.

By setting the INS mode selector to "GPS" and realigning the INSARS through the GPS.

1 and 4

2 and 3

2 and 4

1 and 3

increasing RPM and concentrating the mass on the periphery of the rotor.

decreasing RPM and concentrating the mass at the hub of the rotor.

decreasing RPM and concentrating the mass on the periphery of the rotor.

increasing RPM and concentrating the mass at the hub of the rotor.