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EFIS Equipment-Database Compatibility Matrix

REVISION HISTORY FOLLOWS ON PAGE 2.

WARNING: A printed copy of this document may not be the latest revision. It is the responsibility of the user to ensure that the latest

revision is used. The latest revision of this document may be printed from the Genesys Aerosystems, Inc. electronic document repository.

THIS DOCUMENT CONTAINS PROPRIETARY INFORMATION OF GENESYS AEROSYSTEMS, INC., A GENESYS AERSYSTEMS GROUP COMPANY, NEITHER

RECEIPT, NOR POSSESSION THEREOF, CONFERS ANY RIGHT TO REPRODUCE OR USE, OR DISCLOSE, IN WHOLE OR IN PART, ANY SUCH INFORMATION

WITHOUT WRITTEN AUTHORIZATION FROM GENESYS AEROSYSTEMS, INC.

APPROVAL NAME

PURPOSE: This document identifies the EFIS equipment that utilizes navigation and obstacle databases, and specifies compatibility of equipment to database version.

AUTHOR Dirk ter Veer

CHECK Dean Boston

QUALITY Michael Johnston

COGNIZANT Rick Price

COGNIZANT Stacie Burkhardt

COGNIZANT

RELEASE DATE: 18 May 2016 DOCUMENT NUMBER

01-000062

REV

D STATUS

Released

Typed signatures indicate approval. Handwritten, or electronic signature approval of this document is on file at Genesys Aerosystems, Inc., Anchorage, Alaska.

01-000062 Genesys Aerosystems, Inc. – Confidential of 22

REVISION RECORD

Rev Notes Date Author

D 1. Add §4.3 to describe obstruction database for part numbers in §5 that include the obstruction database. Add obstruction database documents to §2.1.1.

2. Update §2.1.2 with new Pilot Guides..

3. §5 Compatibility Matrix changes:

a. Added §5.1 to define database part number.

b. Split compatibility matrix into §5.2 and §5.3. §5.2 defines the EFIS software versions for all equipment and §5.3 defines the compatible navigation database part numbers for each EFIS software version.

c. Added experimental equipment to §5.2 to assist customer support and Jeppesen.

4. Add Appendix 1 to assist in identifying EFIS equipment, hardware part numbers, and EFIS software revisions.

See cover page

D. Boston

C 1. Rebranding document update from Chelton Flight Systems to Genesys Aerosystems, Inc.

2. §5 Compatibility Matrix Changes:

IDU-IV IDU-450 42-024001-0001 / -00002

8.0D (pending) ~ Current Pending Version

IDU-IV IDU-680P 42-006001-0001

8.0C (pending) ~ Current Pending Version

11/05/2014 M. Johnston

B 1. Correct formatting for PDF version.

2. Sec 1.2: Add reference to DQR document, 20-000076.

3. Sec 2.1: Add 20-000076. Update reference documents.

4. Sec 5: Update pending software versions.

09/12/2013 D. Boston

A Original Version 07/24/2013 D. Boston


TABLE OF CONTENTS

1 SCOPE .......................................................................................................................................................... 4

1.1 DOCUMENT IDENTIFICATION AND OVERVIEW ............................................................................................ 4 1.2 RELATIONSHIP TO OTHER DOCUMENTS .................................................................................................... 4

2 REFERENCED DOCUMENTS .................................................................................................................... 5

2.1 GENESYS AEROSYSTEMS, INC. DOCUMENTS ........................................................................................... 5 2.1.1 Database Process Documents ...................................................................................................................... 5 2.1.2 Installation Manuals and Pilot’s Guides ..................................................................................................... 6

2.2 INDUSTRY DOCUMENTS ........................................................................................................................... 7

3 LIST OF ACRONYMS .................................................................................................................................. 8

4 SYSTEM OVERVIEW ................................................................................................................................ 10

4.1 EFIS SYSTEM ....................................................................................................................................... 10 4.2 IDU NAVIGATION DATABASE .................................................................................................................. 11 4.3 IDU OBSTRUCTION DATABASE .............................................................................................................. 12

5 COMPATIBILITY MATRIX ......................................................................................................................... 13

5.1 DATABASE PART NUMBER ..................................................................................................................... 13 5.2 EFIS SOFTWARE REVISIONS ................................................................................................................. 15 5.3 NAVIGATION DATABASE COMPATIBILITY BY SOFTWARE REVISION .......................................................... 17

APPENDIX 1: EQUIPMENT IDENTIFICATION ................................................................................................ 19


1 SCOPE

1.1 DOCUMENT IDENTIFICATION AND OVERVIEW

This document identifies the EFIS equipment types that utilize navigation databases, and

specifies compatibility of equipment to database version. This document addresses FAA

Advisory Circular (AC) 20-153A, Appendix A Objective 3-2.

1.2 RELATIONSHIP TO OTHER DOCUMENTS

This document is part of the Type 2 Letter of Authorization (LOA) process definition to

meet the requirements of RTCA/DO-200A and FAA AC 20-153A for navigation databases

used in the Integrated Display Unit (IDU) Electronic Flight Instrument System (EFIS).

Other associated documents are listed in § 2.1.

The intended functions for the navigation database as utilized in the EFIS equipment are

described in the Navigation Database – Data Quality Requirements, document 20-

000076.

Refer to the Installation Manual appropriate for the EFIS equipment and software version

for additional information on installation of the equipment and the database. Refer to the

Pilot’s Guide appropriate for the installed EFIS equipment and software version for

additional information on using the equipment functions which utilize the database. See §

2.1.2 for the list of these documents.


2 REFERENCED DOCUMENTS

2.1 GENESYS AEROSYSTEMS, INC. DOCUMENTS

2.1.1 Database Process Documents

The following Genesys Aerosystems, Inc. documents may be referenced. Unless

otherwise noted the reference is to the latest approved document revision level.

Document Number Document Title

00-000026 TSO Major-Minor Change Evaluation Procedure

01-000021 IDU-680P System Requirements Document (SYRD)

01-000033-XXXX IDU GPS/SBAS Requirements

01-000044 IDU-III System Requirements Document (SYRD)

01-000045 IDU-450/EICAS-450 System Requirements Document (SYRD)

20-000037 Software Process Manual

20-000054 Navigation Database Conversion – Qualification Plan

20-000058 Navigation Database Conversion – Software Requirements

20-000060 Navigation Database Conversion – Compliance Plan

20-000076 Navigation Database – Data Quality Requirements (DQRs)

21-000005 Obstruction Database Conversion - Software Requirements

23-000026 Obstruction Database Conversion - Test Plan

23-000027 Obstruction Database Conversion - Test Results

23-000037 Navigation Database Conversion – Test Plan

23-000038 Navigation Database Conversion – Test Results

43-000233 IDU-450 7.0D TSO C146c Gamma III GPS/SBAS Test Results

43-000253 IDU-III 7.0E TSO-C146c (Gamma III GPS/SBAS) Test Results

60-000001 Quality Assurance Manual

61-000010 Supplier Approval and Monitoring

61-000037 Customer Complaints Handling Procedure

61-000049 Quality Management System Procedure

61-000077 Service Bulletin, Installation Bulletin, Service Information Letter Procedures

61-000083 Customer Service Procedure

61-000091 Obstruction Database Conversion – Work Instruction

61-000097 Jeppesen NavData & Obstruction Data Release Procedure

61-000098 Jeppesen NavData & Obstruction Data Release Template

61-000098-XXXX Jeppesen NavData & Obstruction Data – Cycle XXXX

61-000110 Navigation Database Conversion – Work Instruction


2.1.2 Installation Manuals and Pilot’s Guides

The following Genesys Aerosystems, Inc. documents may be referenced. Unless

otherwise noted the reference is to the latest approved document revision level.


150-045264 IDU-3 System Installation Manual (6.0B and Earlier)

64-000061 IDU-3 System Installation Manual (7.0E and Higher)

64-000048 IDU-450 Installation Manual

64-000022 IDU-680P Installation Manual

150-045240 Pilot’s Operating Guide and Reference [1]

64-000054-070A IDU-450 Pilot’s Guide [2]

64-000054-070B IDU-450 Pilot’s Guide 7.0B

64-000054-070D IDU-450 Pilot’s Guide 7.0D

64-000054-070E EFIS Pilot’s Guide 7.0E (with LPV) [3]

64-000076-080A IDU-680 Pilot’s Guide 8.0A

64-000076-080B IDU-680 Pilot’s Guide 8.0B, Sikorsky S-61T

64-000093-080C IDU-680 Pilot’s Guide 8.0C, Fixed Wing (Half Page)

64-000099-080D IDU-680 8.0D Fixed Wing, Pilot Guide

64-000098-080E IDU-680 8.0E Rotorcraft, Pilot Guide [4]

64-000099-080E IDU-680 8.0E Fixed Wing, Pilot Guide [4]

64-000098-080F IDU-680 8.0F Rotorcraft, Pilot Guide [4]

64-000099-080F IDU-680 8.0F Fixed Wing, Pilot Guide [4]

Notes: [1] For IDU-III, software revision 5.0C to 6.0B.

[2] For software revision 7.0A.

[3] For IDU-III and IDU-450.

[4] Pending TSOA and software release.


2.2 INDUSTRY DOCUMENTS

The following industry and regulatory documents may be referenced.


ARINC-424 Navigation System Database

FAA AC 20-153A Acceptance of Aeronautical Data Processes and Associated Databases

FAA AC 90-100A U.S. Terminal and En Route Area Navigation (RNAV) Operations

FAA Order 8110.55 How to Evaluate and Accept Processes for Aeronautical Database Suppliers

RTCA/DO-178B Software Considerations in Airborne Systems and Equipment Certification

RTCA/DO-200A Standards for Processing Aeronautical Data

RTCA/DO-201A Standards for Aeronautical Information

RTCA/DO-229D Minimum Operational Performance Standards for Global Positioning System System/Wide Area Augmentation System Airborne Equipment

TSO-C146c Stand-Alone Airborne Navigation Equipment Using the Global Positioning System Augmented by the Satellite Based Augmentation System


3 LIST OF ACRONYMS

The following acronyms may appear in this document:

AC Advisory Circular AD Airworthiness Directive ADF Automatic Direction Finder A-D Analog to Digital (converter) ADAHRS Air Data Attitude Heading Reference System ADC Air Data Computer ADS-B Automatic Dependent Surveillance-Broadcast AFM Aircraft Flight Manual AGL Above Ground Level AHRS Attitude Heading Reference System AIRMET Airmen’s Meteorological Information AMLCD Active Matrix Liquid Crystal Display ANSI American National Standards Institute APV Approach with Vertical Guidance ARINC Aeronautical Radio, Inc. ARP SAE Aerospace Recommended Practice AS SAE Aerospace Standard ATA AT Attachment (hard disk storage interface) ATC Air Traffic Control CDI Course Deviation Indicator CDTI Cockpit Display of Traffic Information CDR Critical Design Review CFS Genesys Aerosystems, Inc. CM Configuration Management COM Communication CPM Company Project Manager CPU Central Processing Unit CR Change Request CRC Cyclic Redundancy Check DA Decision Altitude D-A Digital to Analog (converter) DAICD Digital Aeronautical Information CD DAR Designated Airworthiness Representative DCN Document Change Notice DEM Digital Elevation Model DER Designated Engineer Representative DH Decision Height DL Data Link DME Distance Measuring Equipment DMIR Designated Manufacturing Inspection

Representative DO RTCA Document DOD Department of Defense DOF Digital Obstruction File DP Departure Procedure DQR Data Quality Requirement DR Dead Reckoning or Defect Report DSP Digital Signal Processing EFIS Electronic Flight Instrument System EGPWS Enhanced Ground Proximity Warning System EIA Electronics Industry Association EICAS Engine Instrument and Crew Alerting System ETA Estimated Time of Arrival ETE Estimated Time Enroute FAA Federal Aviation Administration FAF Final Approach Fix FAR Federal Aviation Regulation FAWP Final Approach Waypoint - same as FAF FDE Fault Detection and Exclusion FHA Functional Hazard Analysis FIFO "First in, First out" FIS Flight Information Service FIS-B Flight Information Service-Broadcast FL Flight Level FLTA Forward Looking Terrain Awareness

FMEA Fault Mode and Effects Analysis FMS Flight Management System FPE Floating Point Emulation FPM Feet per Minute FSD Full Scale Deflection FTE Flight Technical Error GLS GNSS Landing System GND Ground (potential) GNSS Global Navigation Satellite System GPH Gallons per Hour GPS Global Positioning System GPWS Ground Proximity Warning System HAL Horizontal Alert Limit HAT Height Above Threshold HFOM Horizontal Figure of Merit HPL Horizontal Protection Level HSI Horizontal Situation Indicator HUL Horizontal Uncertainty Limit IAP Instrument Approach Procedure, also Initial

Approach Point IAS Indicated Airspeed IAWP Initial Approach Waypoint - same as IAP IC Integrated Circuit ICAO International Civil Aviation Organization ICD Interface Control Document ID Identity or Identification IDU Integrated Display Unit IFR Instrument Flight Rules ILS Instrument Landing System IM Inner Marker IO Input/Output IPV Instrument Procedure with Vertical Guidance ISR Interrupt Service Routine JAD Jeppesen Aviation Database JTAG Joint Test Action Group (IEEE 1149.1 Standard) K Kilo=1000 KB Kilobyte KIAS Knots Indicated Airspeed KT Knot - Nautical Mile per Hour KTAS Knots True Airspeed LDA Localizer-type Directional Aid LED Light Emitting Diode LNAV Lateral Navigation LOA Letter of Authorization LOC Localizer LRU Line Replaceable Unit LSB Least Significant Bit or Byte MAHP Missed Approach Holding Point MAHWP Missed Approach Holding Waypoint - same as

MAHP MAP Missed Approach Point MASPS Minimum Aviation System Performance Standard MAWP Missed Approach Waypoint - same as MAP MB Megabyte MDA Minimum Descent Altitude MEMS Micro Electro Mechanical System MFD Multifunction Display (an IDU with software for

showing multiple display screens) MM Middle Marker MOPS Minimum Operational Performance Standard MOT Mark On Target MSB Most Significant Bit or Byte MSL Mean Sea Level MSU Magnetic Sensor Unit MTBF Mean Time Between Failures


NACO National Aeronautical Charting Office NAS U.S. National Airspace System NASA National Aeronautics and Space Administration NED National Elevation Dataset NIMA National Imagery and Mapping Agency ND Navigation Display NDB Nondirectional Beacon NM Nautical Mile NPA Non-Precision Approach OAT Outside Air Temperature OBS Omnibearing Selector OM Outer Marker OT Other Traffic (Traffic Function) PA Proximate Advisory (Traffic Function) PDA Premature Descent Alert PDR Preliminary Design Review PFD Primary Flight Display (the display screen showing

primary instrumentation -- can also refer to the primary IDU with software that only shows primary instrumentation)

PFDE Predictive Fault Detection and Exclusion PIC Peripheral Interface Controller PLI Pitch Limit Indicator PN Part Number PRAIM Predictive Receiver Autonomous Integrity Monitoring PSAC Plan for Software Aspects of Certification PSCP Project Specific Certification Plan PSP Partnership for Safety Plan PTN Problem Tracking Number QA Quality Assurance QFE Altimeter setting that provides height above

reference point. QM Quality Management QNE Altimeter setting that provides pressure altitude

readout QNH Altimeter setting that provides MSL altitude at a

reporting point RA Resolution Advisory (Traffic Function) RAM Random Access Memory RBP Remote Bug Panel RMI Radio Magnetic Indicator RNAV Area Navigation RNP Required Navigation Performance RS EIA Recommended Standard RTC Real Time Computing RTCA Radio Telephone Commission for Aeronautics RTD Resistive Thermal Detector RTL Run Time Library Rx Receive SA Selective Availability SAE Society of Automotive Engineers SAS Software Accomplishment Summary SBAS Satellite Based Augmentation System SCI Software Configuration Index SCMP Software Configuration Management Plan SCR Software Conformity Review SCS Software Coding Standards SDD Software Design Document SDP Software Development Plan SDS Software Design Standards SECI Software Environment Configuration Index SIGMET Significant Meteorological Advisory SMA Sub-Miniature version A connector SN Serial Number SNI Serial Number Information SOI Stage of Involvement (FAA software audit) SPR Software Problem Report SQA Software Quality Assurance SQAP Software Quality Assurance Plan SQAR Software Quality Assurance Representative

SRD Software Requirements Document SRS Software Requirements Standards SRTM Shuttle Radar Topographical Mission SSA System Safety Assessment STAR Standard Terminal Arrival Routes STC Supplemental Type Certificate STP Software Test Protocol STS Software Test Specification SUA Special Use Airspace SV Service Vehicle SVCP Software Verification Cases and Procedures SVP Software Verification Plan SVR Software Verification Results SYRD System Requirements Document TA Traffic Advisory (Traffic Function) TAFs Terminal Aerodrome Forecasts TAS Traffic Advisory System TAWS Terrain Awareness and Warning System TCAD Traffic Collision Alert Device TCAS Traffic Collision Alert System TERPS Terminal Instrument Procedures TCH Threshold Crossing Height TD Traffic Display TFR Temporary Flight Restriction TIS Traffic Information Service TIS-B Traffic information Service-Broadcast TMS Texas Instruments family of DSP processors TQP Tool Qualification Plan TSO Technical Standard Order Tx Transmit UART Universal Asynchronous Receiver-Transmitter USGS United States Geological Survey UTC Universal Time Coordinated VAL Vertical Alert Limit VFOM Vertical Figure of Merit VFR Visual Flight Rules VHF Very High Frequency VNAV Vertical Navigation VOR VHF Omnidirectional Radio VPL Vertical Protection Level VSI Vertical Speed Indicator VTF Vectors to Final VUL Vertical Uncertainty Limit SBAS Wide Area Augmentation System WGS84 World Geodetic System 1984


4 SYSTEM OVERVIEW

4.1 EFIS SYSTEM

The EFIS is a complete flight and navigation instrumentation system that intuitively

provides information to a pilot via computer generated screen displays on IDUs. The

screen displays are a three-dimensional, enhanced situational awareness PFD and an

MFD that can be configured to show a moving map, an HSI, traffic, terrain or weather

displays.

Generally, IDUs are part of a complete flight and navigation instrumentation system that

intuitively provides information to a pilot via computer generated screen displays. The

IDUs may be configured as a PFD (a three-dimensional, enhanced situational awareness

Primary Flight Display) or an MFD (Multi-Function Display that can be configured to show

a moving map, an HSI, traffic, terrain or weather displays). A system consists of various

discrete digital sensor modules that communicate with IDUs via RS-232, RS-422 or

ARINC 429 serial data. Each IDU incorporates a high-brightness AMLCD screen, bezel

keys, a screen and keyboard lighting intensity control, rotary selector and enter switches,

a central processing unit, numerous RS-232, RS-422 and ARINC 429 receive and

transmit ports, and discrete IO ports. Because the receive ports of the IDUs are

connected to the digital sensor modules in parallel, each IDU is independent from all

other IDUs. The following is a typical system diagram.


Pilot Co-Pilot

IDU #1

*IDU #2

*IDU #3

*IDU #4

GPS #1

*GPS #2

ADC #1

*ADC #2

AHRS #1

*AHRS #2

*Datalink/

ADS-B

*WX-500

IDU #1

*IDU #2

*IDU #3

*IDU #4

*Analog

Interface

*Traffic

Sensor

*Remote

Tune Radios

*Video

*Remote

Bugs Panel

*Digital

Autopilot

*Airframe/

Engine Data

*Weather

Radar

*Mode S

Transponder

*Fuel Flow/

Quantity

Note: * = Optional

Synch Synch

Crosslink

4.2 IDU NAVIGATION DATABASE

The navigation database provides information relating to navigation aids, procedures and

communications. Database elements to support TSO-C146c Class Gamma-3 include:

Airports

Navigation Aids (VORs, DMEs, VOR/DMEs, VORTACs and NDBs)

Named Waypoints and Intersections

RNAV DPs

RNAV STARs

LNAV, LNAV/VNAV and LPV Approach Procedures and Levels of Service

FAS Data Blocks with embedded CRC-32s

Approach Levels of Service

Approach HALs and VALs


Additional database elements to support flight planning features and moving map

depictions include:

Airspace

Airways

Enroute and airport communications

Navigation data elements are obtained by electronic data transfer from the Jeppesen

Aviation Database (JAD, Jeppesen Sanderson Inc.) on a 28-day update cycle. Required

data elements are extracted from the ARINC-424 format JAD and reformatted without

modification to meet IDU requirements. Data elements selected for processing vary with

the area of coverage selected by the end-user. A detailed description of the packing tool

design requirements are presented in the Navigation Database Conversion – Software

Requirements (Doc. No. 20-000058).

4.3 IDU OBSTRUCTION DATABASE

The obstruction database provides information relating to obstructions and hazards to

navigation including:

Arches, balloons, bridges, buildings, building towers, catenaries, control

towers, cooling towers, crane, dams, domes, elevators, monuments, plants,

poles, rigs, refineries, signs, spires, stacks, tanks, transmission line towers,

towers, tramways, and windmills.

Obstruction information is provided for the entire world. Obstruction data elements are

obtained in digital format from Jeppesen Sanderson, Inc. on a 28-day update cycle.

Required data elements are extracted from the supplied digital file and reformatted to

meet IDU requirements. A detailed description of the packing tool design requirements

are presented in the Obstruction Database Conversion – Software Requirements (Doc.

No. 21-000005). The obstruction database is not covered by the Type 2 LOA and is

described here because it may be bundled with the navigation database.


5 COMPATIBILITY MATRIX

5.1 DATABASE PART NUMBER

The IDU navigation database can be delivered stand-alone or bundled with the

obstruction database. The part number of the stand-alone or bundled database product

is encoded as follows:

CS[A][BBB]_[xxxx]_[wwwwwwww]

[A] Description

EFIS Software Revision Database

1 7.0D to 8.0C NavData only

2 7.0C and earlier NavData only

3 7.0D to 8.0C NavData bundled with Obstacles

4 7.0C and earlier NavData bundled with Obstacles

5 8.0D and later NavData only

6 8.0D and later NavData bundled with Obstacles

[BBB] [1]

Coverage

001 World

002 Americas

003 International

CAP Capstone tailored World

REG Rega tailored World

Notes: [1] [BBB] can be any 3-letter identifier to accommodate future tailored database customers.

Field Description

[xxxx] Database cycle number. For example: 1604.

[wwwwwwww] 8-character hexadecimal 32-bit CRC of database file. For example: EE9DB378.

Notes: Database cycle number changes based on a schedule published by Jeppesen: http://ww1.jeppesen.com/support/final/update-schedule.jsp. 8-character CRC value changes with each cycle based on the contents of the database file.

http://ww1.jeppesen.com/support/final/update-schedule.jsp


Database Part Number Decoding Examples:

Database Part Number Description

CS4002_1604_EE9DB378 Part Number Prefix: CS4002

Contents: NavData bundled with Obstacles

EFIS Software Revision: 7.0C and earlier

Coverage: Americas

Cycle: 1604

Filename: CS4002_1604_EE9DB378.zip

CS3REG_1513_7445F065 Part Number Prefix: CS3REG

Contents: NavData bundled with Obstacles

EFIS Software Revision: 7.0D to 8.0C

Coverage: Rega tailored World

Cycle: 1513

Filename: CS3REG_1513_7445F065.zip

CS5001_1608_2E5E0A8A Part Number Prefix: CS5001

Contents: NavData only

EFIS Software Revision: 8.0D and later

Coverage: World

Cycle: 1608

Filename: CS5001_1608_2E5E0A8A.zip


5.2 EFIS SOFTWARE REVISIONS

The EFIS software revision defines the compatible database part numbers. Table 5.1

lists experimental EFIS equipment and the applicable approved and compatible EFIS

software revisions. Table 5.2 lists the certified EFIS equipment (under FAA TSOA) and

the applicable approved and compatible EFIS software revisions. Images of the EFIS

equipment, identifying characteristics, hardware part number locations, and software

revision identification is provided in Appendix 1.

Table 5.1 Experimental EFIS Equipment

Make [3]

Model [3]

Part Number

Software Revision Hardware Software

IDU-I IDU-I

ID-A1

IUA0A.I/P-SI

IUA0B.I/P-SI

IUA0C.I/P-SI

IUA1A.I/P-SI

IUA1B.I/P-SI

IUA1C.I/P-SI

42-023001-0001

42-023001-0002

320-345239-050C

320-345239-060B

5.0C

6.0B-X [2]

IDU-III [1]

IDU-III [1]

EXP-045500-0101

320-345239-050C

320-345239-060B

5.0C

6.0B-X [1]

25-EFIS70E-SW-0003

25-EFIS70E-SW-0006

25-EFIS70E-SW-0007

7.0E

Notes: [1] IDU-III is also called IDU-3.

[2] X = External sensor dash number.

[3] “Series” parameter per AC 20-153A 9.b.(4)(c) is not applicable to this equipment.


Table 5.2 Certified EFIS Equipment (under FAA TSOA)

Make [3]

Model [3]

Part Number

Software Revision Hardware Software

IDU-III [1]

IDU-III [1]

401-045500-0101

401-045500-0202

320-345239-050C

320-345239-060B

5.0C

6.0B-10

25-EFIS70E-SW-0003

25-EFIS70E-SW-0006

25-EFIS70E-SW-0007

7.0E

IDU-IV [2]

IDU-450

42-024001-0001

42-024001-0002

42-024001-0003

25-EFIS70A-SW-0001 7.0A

25-EFIS70B-SW-0001 7.0B

25-EFIS70C-SW-0001

25-EFIS70C-SW-0002 7.0C

25-EFIS70D-SW-0001 7.0D

25-EFIS70E-SW-0001

25-EFIS70E-SW-0002

25-EFIS70E-SW-0004

25-EFIS70E-SW-0005

7.0E

25-EFIS70F-SW-0001

25-EFIS70F-SW-0002

25-EFIS70F-SW-0003

7.0F

25-EFIS80D-SW-0002 8.0D

IDU-IV [2]

IDU-680P 42-006001-0001

42-006001-0004

25-EFIS80A-SW-0003 8.0A

25-EFIS80B-SW-0003 8.0B

25-EFIS80C-SW-0003 8.0C

25-EFIS80D-SW-0003 8.0D

[4] 8.0E

[4] 8.0F

Notes: [1] IDU-III is also called IDU-3.

[2] IDU-IV is also called IDU-4 or IDU-IV Family.

[3] “Series” parameter per AC 20-153A 9.b.(4)(c) is not applicable to this equipment.

[4] Pending TSOA and software release.


5.3 NAVIGATION DATABASE COMPATIBILITY BY SOFTWARE REVISION

Table 5.3 lists the EFIS software revisions and the applicable compatible navigation

database part number prefixes. A navigation database part number must have the listed

prefix to be compatible with the associated EFIS software revision.

Table 5.3 Navigation Database Compatibility

EFIS Software

Revision

Jeppesen Database

NavData Obstacles [2]

NavData Coverage Database Part

Number Prefix

5.0C

6.0B-X [1]

7.0A

7.0B

7.0C

☒ ☒

World CS4001

Americas CS4002

International CS4003

Capstone [3]

CS4CAP

Rega [3]

CS4REG

☒ ☐

World CS2001

Americas CS2002


Capstone [3]

CS2CAP

Rega [3]

CS2REG

7.0D

7.0E

7.0F

8.0A

8.0B

8.0C

☒ ☒

World CS3001

Americas CS3002


Capstone [3]

CS3CAP

Rega [3]

CS3REG

☒ ☐

World CS1001

Americas CS1002


Capstone [3]

CS1CAP

Rega [3]

CS1REG


Table 5.3 Navigation Database Compatibility (Continued)

EFIS Software

Revision

Jeppesen Database

NavData Obstacles [2]

NavData Coverage Database Part

Number Prefix

8.0D

8.0E

☒ ☒

World CS6001

Americas CS6002


Capstone [3]

CS6CAP

Rega [3]

CS6REG

☒ ☐

World CS5001

Americas CS5002


Capstone [3]

CS5CAP

Rega [3]

CS5REG

Notes: [1] X = External sensor dash number.

[2] Obstacle database coverage is always worldwide regardless of the NavData coverage selected.

[3] Capstone and Rega tailored NavData coverage contains World NavData coverage.


APPENDIX 1: EQUIPMENT IDENTIFICATION

IDU-I

Identifying Characteristics

4x5 inch display.

8 line-select keys and 2 rotary encoders knobs at bottom.

SmartMedia card slot at bottom near left rotary encoder knob.

SmartMedia card inserted with contacts facing down.

Bezel cut at 45 degree angle at all corners.

Panel-mounted display.

D-sub connectors on rear.

Physical Features

&

Hardware Part Number

Location

(highlighted in red)

EFIS Software Revision

(shown on

Status Page, highlighted

in red)


IDU-III


4x5 inch display.

8 line-select keys and 2 rotary encoders knobs at bottom.

SmartMedia card slot centered at the bottom between the rotary encoder knobs.

SmartMedia card inserted with contacts facing up.

Square bezel.

Tray-mounted display.

Physical Features

&


Location



(shown on

Status Page, highlighted

in red)


IDU-450


4x5 inch display.

8 line-select keys and 2 rotary encoder knobs at bottom.

USB port centered at the bottom between the rotary encoder knobs.

USB port exposed when sliding the slip or non-slip housing upwards.

Square bezel.


Physical Features

&


Location



(shown on

Status Page along with Software

Part Number, highlighted

in red)


IDU-680


6x8 inch display.

16 line-select keys and 4 rotary encoder knobs at bottom.

USB port centered at the bottom between the inner rotary encoder knobs.

USB port exposed when sliding the slip or non-slip housing upwards.

Rectangular bezel.


Physical Features

&


Location



(shown on

Status Page along with Software

Part Number, highlighted

in red)