ATPL Navaids P3

The flashing of the airspeed tape and an aural warning of "stall"

The stick shaker and the appearance of the PLIs on the ADI/PFD

The speed tape changes to red and the PLIs flash red

The stall warning horn sounds and the stick pusher activates

required attitudes for a 2000ft/min go around

required pitch attitude to maintain the glideslop

required pitch attitude to maintain the current altitude

pitch attitude at which the stick shaker will occur.

(a) and (e)

(b) and (d)

(a), (b), (e), (f), and (g)

all of them

Mature

Dissipating

Heavy

Developing

Fire warning bell, master warning light

Windshear, engine failure, pull up (terrain)

It warns crew of the aircrafts approach to and deviation form the assigned (MCP set) altitude

It activates within 900ft when approaching the altitude selected on the MCP

The altitude alerter will warn crew if the aircraft deviates more than 200ft from the altitude set on the MCP

The altitude alerter automatically adjusts the target altitude based on the aircraft’s rate of climb or descent

It determines the aircrafts height above the ground by comparing the frequency of the outgoing and incoming signals

To give a measurable frequency difference at very low altitudes a wide sweep of frequencies is used

In order to avoid the risk of height ambiguity in a radar altimeter, a low rate of modulation of the sweep band frequencies must be used.

The radio altimeter operates in a height range of 0 to 2500ft AGL

Glideslope

Minimum Fuel

Decision Height (DH)

Minimum Decision Height (MDH)

ADF receiver, brake temperature sensors, and cabin pressure controller.

Radio altimeter, ILS receiver, air data computer, flap position, and landing gear position.

Radar weather receiver, air conditioning pack status, and transponder mode.

Flight control surface deflection sensors, fuel temperature probes, and autopilot status.