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CS ACNS.E.TAWS.010 Required Functions and Interfaces

ED Decision 2013/031/R

(See AMC1 ACNS.E.TAWS.010, AMC2 ACNS.E.TAWS.010)

TAWS Class A or Class B provides suitable alerting and warning capabilities and other system interfaces to support the following functions:

 

TAWS System Function

Class A TAWS

Class B TAWS

Alerting

Imminent contact with ground indications (GPWS functions) including:

(19)      excessive Rates of Descent;

(20)      negative Climb Rate or Altitude Loss After Take-Off or Go-around.

A Voice callout when descending through a predefined altitude above the terrain or nearest runway elevation.

X

With a 500 ft call out

x

With a 500 ft call out

 

A forward Looking Terrain Avoidance (FLTA) function, including:

·            a Reduced Required Terrain Clearance (RTC) function;

·            an Imminent Terrain Impact function;

·            a FLTA Turning Flight function.

x

x

 

A Premature Descent Alert (PDA) function, including detection and alerting for Premature Descents Along the Final Approach Segment

x

x

 

Excessive Closure Rate to Terrain

x

 

 

Flight Into Terrain When not in Landing Configuration

x

 

 

Excessive Downward Deviation from a glide slope or glide path

x

 

 

TAWS and sensor failure monitoring and annunciation function

x

x

 

Capability to initiate the TAWS self-test function on the ground and where feasible in the air

x

x

 

TAWS System Interfaces

Class A TAWS

Class B TAWS

 

A terrain display capability

x

 

 

Capability to drive a terrain display

 

x

 

The use of position source input

x

x

 

The use of landing guidance deviation input

x

 

 

The use of radio altimeter sensor input

x

 

 

The use of Terrain and Airport information

x

x

 

Interface with the flight recording system to record TAWS alerts and inhibition of the FLTA or PDA functions

x

x

 

The use of landing gear and flaps position

x

 

 

The use of roll attitude input

x

 

 

The interface with flight deck audio systems

x