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Primary Radar is. (Level 1)

• for ground use only.
• reflected signal from aircraft's own radar.
• interrogation of aircraft's transponder.

In a Central Air Data Computer (CADC) system, True Air Speed (TAS) is derived from the Mach information and. (Level 1)

• Static Air Pressure.
• Pitot Air Pressure.
• Total Air Temperature.

An aircraft with autoland is fitted with a CM (Level 1)

• It records all faults in non-volatile memory.
• All memory is erased when aircraft lands.
• It records all faults in volatile memory.

With on-board maintenance (OBM) systems, the purpose of central maintenance function (CMF) is to. (Level 3)

• log relevant maintenance dat
• provides detaILS of defect action.
• transmits to the CM

When an autopilot is Fail Passive,. (Level 1)

• the aircraft reverts to fail operational autopilot.
• the pilot must resume control and land the aircraft.
• the autoland can continue.

On an aircraft fitted with a CMC, how do you get to the system pages?. (Level 2)

• Through the Existing faults function.
• Through the Present Leg faults function.
• Through the ground test function.

A modern aircraft CMC uses. (Level 2)

• a CRT screen.
• a magnetic fault indicator.
• an LED display.

With on-board maintenance (OBM) systems, the purpose of central maintenance function (CMF) is to. (Level 2)

• log relevant maintenance dat
• provides detaILS of defect action.
• transmits to the AM

On an aircraft fitted with a CMC, how do you get to the system pages?. (Level 2)

• Existing faults function.
• Through the Present Leg faults function.
• Through the ground test function.

A modern aircraft CMC uses. (Level 2)

• a CRT screen.
• a magnetic fault indicator.
• transmits to the CM