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Thommen AD20 User Manual

Thommen AD20
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REVT.ETHOMMENAG
CH-4437
Waldenburg
07-Sep-2009
AD20 Standby Altimeter
p
age 1
or
72
Document No: AD-l NSOP-800
Revision: 1.6
TITLE:
INSTALLATION
AND
OPERATION
MANUAL
AD20 Standby
Altimeter
DOCUMENT
NO.:
AD-INSOP-8O0
REVISION:
PRCJECT:
1.6
Solid
State Flight
lnstrument
Family
MANUFACTURER:
REVUETHOMMENAG
CH-4437 Waldenburg
Switzerland
ISSUING OFFICE:
Development Department
Näme
Si,gnature
Date
Author:
M.Baumann
/n9"tfto-^*
07-Sep-2009
Project Management: R.
Wehrli
/.ü/u{
22-Sep-2009
Development M anagement: R.
Wehrli
/.ü/u{
22-Sep-2009
Quality
Management: O.
Thommen
en^ zg"
?
äf
@ Copyright
by REVUE THOMMEN
AG,
CH-4437
Waldenburg
Switzerland

Table of Contents

Questions and Answers:

Thommen AD20 Specifications

General IconGeneral
BrandThommen
ModelAD20
CategoryMeasuring Instruments
LanguageEnglish

Summary

1 SECTION I

1.1 Introduction

Overview of the AD20 Standby Altimeter manual's purpose, scope, and target audience.

1.1.1 Purpose of the manual

Explains the manual's objective, content, and user qualifications for the AD20 Altimeter.

1.1.2 Equipment Specification

Details the technical specifications and requirements for the AD20 Standby Altimeter.

1.1.2.1 Applicable Documents

Lists relevant documents forming the basis of approvals for the AD20 Standby Altimeter.

1.1.2.2 Identification

Provides identification details for the AD20 Standby Altimeter, including drawings and plates.

1.1.2.2.1 Type Identification Drawing

Shows the type identification drawing and specifications for the AD20 Standby Altimeter.

1.1.2.2.2 Identification/Name Plate

Illustrates the identification and name plate details for the AD20 Standby Altimeter.

1.1.2.3 Installation Kit

Lists the necessary components included in the installation kit for the AD20 Standby Altimeter.

1.1.3 Technical Specification

Outlines the key technical specifications and performance parameters of the AD20 Standby Altimeter.

1.1.4 Equipment Dimensions

Details the physical dimensions and measurements of the AD20 Standby Altimeter unit.

1.1.5 Pneumatic Pressure Port

Describes the specifications and characteristics of the pneumatic pressure port on the AD20 Altimeter.

1.1.6 Interface Block diagram

Presents a block diagram illustrating the interface connections of the AD20 Standby Altimeter.

2 SECTION II

2.1 General Information

Provides general information and an overview of the AD20 Standby Altimeter unit.

2.2 Description

Describes the AD20 Standby Altimeter, its components, and overall design.

2.2.1 Instrument Description

Details the AD20 Standby Altimeter's measured altitude, display, and operational features.

2.2.2 Functional Description

Explains the functional aspects and operation of the AD20 Standby Altimeter.

2.2.2.1 Display

Details the digital altitude display, altitude pointer, and scale settings of the AD20 Altimeter.

2.2.2.2 Controls

Explains the controls of the AD20 Standby Altimeter, including knobs and buttons.

2.3 Operations

2.3.1 Theory of Operation

Explains the underlying theory of operation for the AD20 Standby Altimeter.

2.4 TESTING

2.4.1 Startup BIT Sequence

Describes the sequence of tests performed when the AD20 Standby Altimeter powers on.

2.4.2 Built-in-Test

Details the different types of Built-in-Test (BIT) functions for the AD20 Standby Altimeter.

2.4.3 Failure Modes

Explains the different failure modes and how the AD20 Standby Altimeter handles them.

3 SECTION III

3.1 Approvals

Details the approvals and certifications met by the AD20 Standby Altimeter.

3.1.1 General

General statement regarding the approval status and compliance of the AD20 Standby Altimeter.

3.1.2 Instructions for Continued Airworthiness

Provides instructions for maintaining the AD20 Standby Altimeter's airworthiness and required tasks.

3.1.3 Environmental Qualification

Outlines the environmental conditions and qualification standards the AD20 Standby Altimeter meets.

3.1.3.1 Electromagnetic Environment (EME)

Describes the design, analysis, installation, and testing for aircraft electromagnetic environment.

3.1.3.2 Electromagnetic compatibility (EMC)

Proves electromagnetic compatibility, ensuring no degradation due to EMI with other systems.

3.1.3.3 Electromagnetic interference (EMI)

Controls EMI generation and susceptibility according to RTCA/DO-160D.

3.1.3.4 Pointer position error

Specifies the maximum allowable pointer position error for the AD20 Standby Altimeter.

3.1.3.5 Scale error

Defines scale error tolerances as specified in Section II Part 3 Para A.8.

3.1.3.6 Hysteresis

Limits apparent hysteresis for stability of the AD20 Standby Altimeter display.

4 SECTION IV

4.1 Installation

Covers the installation process, including checks, interface, and diagrams for the AD20 Altimeter.

4.1.1 General

Introduces the installation section, covering pre-installation checks and interface data.

4.1.2 Unpacking and Inspecting

Guides on how to unpack and visually inspect the AD20 Standby Altimeter for shipping damage.

4.1.3 Pre and Post Installation Check

Details pre and post installation checks to ensure the AD20 Altimeter meets performance specs.

4.1.4 Electrical Interface

Describes the electrical interfaces of the AD20 Standby Altimeter, including power and data.

4.1.4.1 Overview of electrical interface

Lists the electrical interfaces for the AD20 Standby Altimeter: power, lighting, and data.

4.1.4.2 Power Control (DC Primary)

Details the 28 VDC power supply requirements for the AD20 Standby Altimeter.

4.1.4.3 Power Consumption

Shows values of power consumed by the AD20 Standby Altimeter at different operating stages.

4.1.4.4 Power Failure indication

Explains the indication for power supply failure or switching off the instrument.

4.1.4.5 Groundings and Shielding

Provides guidelines for grounding and shielding to prevent interference and ensure safety.

4.1.4.5.1 Harness with shielded power wires, RF Susceptibility Cat. [YY]

Details requirements for shielded power wire harnesses to meet RF susceptibility.

4.1.4.5.2 Harness with unshielded power wires, RF Susceptibility Cat. [WW]

Details requirements for unshielded power wire harnesses to meet RF susceptibility.

4.1.5 Electrical connector

Details the electrical connector type and pin assignments for the AD20 Standby Altimeter.

4.1.5.1 Pin Assignments

Provides the specific pin assignments for the MS3112E-14-19P connector.

4.1.5.2 Wiring Diagram (shielded power wires, RF Susc. Cat. [YY])

Illustrates the wiring diagram for shielded power wires relevant to RF Susceptibility.

4.1.5.3 Wiring Diagram (unshielded power wires, RF Susc. Cat. [WW])

Illustrates the wiring diagram for unshielded power wires relevant to RF Susceptibility.

4.1.6 Digital Data Interface

Describes the digital data interfaces for the AD20 Standby Altimeter, including ARINC 429.

4.1.6.1 ARINC 429 (optional)

Details the ARINC 429 data bus interface, including speed and label formats.

4.1.6.1.1 ARINC 429 Data bus Interface

Specifies digital data standards for ARINC 429 Mark 33 DITS and ARINC 706 ADS.

4.1.6.1.2 ARINC 429 BIT Rate

Defines the ARINC 429 data bus speed options: High Speed and Low Speed.

4.1.6.1.3 ARINC Label Formats

Specifies label formats according to ARINC 429 Mark 33 DITS, equipment ID 006.

4.1.6.1.4 Label 203 (Pressure Altitude)

Details the format and data for ARINC Label 203, representing Pressure Altitude.

4.1.6.1.5 Label 204 (Baro corrected altitude #1)

Details the format and data for ARINC Label 204, representing Baro corrected altitude.

4.1.6.1.6 Label 217 (Static Pressure)

Details the format and data for ARINC Label 217, representing Static Pressure.

4.1.6.1.7 Label 234 (Baro correction hPa #1)

Details the format and data for ARINC Label 234, representing Baro correction in hPa.

4.1.6.1.8 Label 235 (Baro correction inHg #1)

Details the format and data for ARINC Label 235, representing Baro correction in inHg.

4.1.6.1.9 Label 270 (Discrete word #1)

Details the format and data for ARINC Label 270, representing Discrete Word #1.

4.1.6.1.10 Label 350 (Maintenance word #1) (Provision)

Details the format and data for ARINC Label 350 (Maintenance word #1), content to be defined.

4.1.6.2 Discrete I/O's

Details the discrete inputs and outputs and their functions on the AD20 Standby Altimeter.

4.1.6.2.1 Discrete Inputs

Details the voltage levels for the five discrete inputs available on the AD20 Altimeter.

4.1.6.2.2 Discrete Input Functions

Describes the functions assigned to the discrete input pins by parameterization.

4.1.6.2.3 Aircraft Type Selection

Explains how aircraft type is detected via pin strapping and assigned parameters.

4.1.6.2.4 Discrete Outputs

Details the discrete outputs available for warning flags and battery status.

4.1.6.3 RS232 Serial Interface

Describes the RS232 interface for maintenance and calibration purposes only.

5 SECTION V

5.1 Trouble shooting

Provides information and remedies for troubleshooting common malfunctions of the AD20 Standby Altimeter.

5.2 Maintenance

Summarizes the maintenance modes available for the AD20 Standby Altimeter.

5.3 Manual Maintenance Mode

Details the manual maintenance mode for accessing internal settings and maintenance functions.

5.3.1 Entering Manual Maintenance Mode

Explains how to enter the manual maintenance mode via the UNIT button.

5.3.2 Display 1: Battery Capacity Test (provision)

Details the procedure for determining the current capacity of the instrument's battery.

5.3.3 Display 2: High Resolution Altitude

Describes the high resolution display indicating baro corrected altitude in 1 foot resolution.

5.3.4 Display 3: Lighting Curve Selection

Explains how to select and configure lighting curves for different aircraft types.

5.3.5 Display 4: Lighting Curve Adjustment

Details how to adjust the instrument's lighting characteristics for each dim step.

6 APPENDICES

6.1 APPENDIX I: Function Overview

Provides an overview of the standard and optional features of the AD20 Standby Altimeter.

6.2 APPENDIX II: Failure Codes

Lists and describes failure codes associated with the AD20 Standby Altimeter.

6.3 APPENDIX III: Altimeter Calibration Table

Presents the calibration table for the AD20 Standby Altimeter, showing tolerances.

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