AlliedSignal KAP 140 Manual de instalación descargar pdf (Pagina 8)

BENDIX/KING

KAP 140

Page 1--2

Revision 6, Oct 2002

CS:00991I06.IDU

1.2 EQUIPMENT DESCRIPTION

The system modes for the KAP 140 Flight Control System is as follows:

Pitch Modes:

Vertical Speed (Default) (--5001 & up) A

Altitude Hold (--5001 & up) A

Glideslope (--5001 & up) A

Altitude Select Capture (--7501 & up) A

Roll Modes : Wings Level (Default)

Heading Select (--2501 & up) A

Nav (--2501 & up) A

Approach (--2501 & up) A

Reverse Localizer (--2501 & up) A

Other: Manual Trim

Automatic Trim (--5001 & up) A

Self Test

Control Wheel Steering

The KAP 140 Flight Control System for a two axis with trim configuration consists of the following

units:

UNIT

DESCRIPTION

KC 140 Flight Computer

KCM 100 Configuration Module

KS 270C Pitch Axis Servo Actuator

KS 271C Roll Axis Servo Actuator

KS 272C Elevator Trim Servo Actuator

Supplied by Mid Continent Rate Gyro

Supplied by SIGMA--TEK DG

KM 275 or KM 277 (Total of 3 Required) Servo Mount

A Number refers to flight computer version number

1 2 3 4 5 6 7 8 9 10 11 12 13 ... 93 94

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AlliedSignal KAP 140 Manual de instalación Pagina 8