EMS Sky Connect Series Installation guide

Brand: EMS

Model: Sky Connect Series

Type: Installation guide

1616-964-12

Date: 7/27/2011

Rev. 2.1

EMS Aviation, Inc.

Sky Connect Aviation Series

Installation Manual

TRACKER

Part Number 1616-964-12

1616-964-12

Date: 7/27/2011

Rev. 2.1

Aviation Certification Issues

CERTIFICATION – Sky Connect has rights to several Supplemental Type Certificates. Use of

this information is provided with purchase of the equipment. Assistance in certification

efforts to the installers is offered at no charge to the customer or installer. Assistance is

provided on Sky Connect’s scheduling.

Please plan your certification issues with the following in mind; Phone assistance is

provided 8am to 5pm Central Time U.S. based on our available time and work load for the

day.

Certification teams maybe required to perform work on a deadline basis, there will be a fee

for such work at the rate of $150 US per hour. Please contact Sky Connect Technical

Services for assistance.

1616-964-12

Date: 7/27/2011

Rev. 2.1

TABLE of CONTENTS

LIST OF REVISIONS.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v

INDEX OF ACRONYMS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vi

GENERAL INFORMATION.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 1

INTRODUCTION.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 1

SYSTEM DESCRIPTION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 1

TECHNICAL SPECIFICATIONS.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 - 3

INSTALLATION PROCESS.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 1

WIRING DIAGRAM.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 1

SIM CARD ACTIVATION.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 1

ANTENNA PLACEMENT PLAN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 1

INFORMATION NEEDED FOR CONFIGURATION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 1

TRACKER MAPPING SYSTEM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 2

WIRING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 2

CONFIGURATION.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 2

TRACKER RULES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - 2

INSTALLATION - GENERAL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 1

A DISCUSSION ON SIM CARDS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 1

ITEMS REQUIRED BUT NOT SUPPLIED.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 2

GENERAL SYSTEM COMPONENTS THAT APPLY TO ALL SYSTEMS. . . . . . . . . . . . . . 3 - 4

SYSTEM COMPONENTS THAT APPLY ONLY TO TRACKER. . . . . . . . . . . . . . . . . . . . . . 3 - 4

GENERAL INSTALLATION INSTRUCTIONS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 - 6

TRACKER SYSTEM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 1

TRACKER SYSTEM COMPONENTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 1

TRANSCEIVER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 1

CONFIGURATION MODULE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 1

CONFIGURATION/SIM MODULE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 2

TRACKER SOP DIALER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 3

MMU/II (Mission Management Unit). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 3

TRACKER-SOP STRUCTURAL MOUNTING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 5

TRACKER WIRING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 5

POST INSTALLATION TESTING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 8

TRACKER SETUP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 17

TRACKER TESTING.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 17

OPERATION.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 - 19

iii

1616-964-12

Date: 7/27/2011

Rev. 2.1

APPENDIX A Troubleshooting. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 - 1

INSTALLATION AND SYSTEMS DRAWINGS.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 - 1

1616-964-12

Date: 7/27/2011

Rev. 2.1

LIST OF REVISIONS

Revision # Description of Change Date Approval

1.0 Removed all POTS unit information and

created a new manual part number for

Tracker only.

3/24/2007 MLF

1.1 Added Combo antenna, corrected note on

ICSM, revised pin out chart to remove the

400 series references.

3/20/2008 MLF

1.2 Typos corrected, revised MMU/MMU II

recommended installation wiring

drawing

10/3/2008 MLF

1.3 Added spec and part numbers for MMU II 12/15/2008 MLF

1.4 Added configuration details on MMU II

and Combo antenna drawing

1/13/2009 MLF

1.5 Revised to indicate the changes to the

1616-105-01 tray per ECO 10013

6/3/2010 MLF

2.0 Revised to add description of MMU II

features for Wi-Fi MSet Loads and

Performing Tracker Setup through the

MMU II, Added MMU II Master/Slave

Configuration

4/7/2011 MLF

2.1 Revised Annuc. #2 description, includes a

picture of the SOP 11 jumper

7/27/2011 MLF

1616-964-12

Date: 7/27/2011

Rev. 2.1

INDEX OF ACRONYMS

FOI Field Of Interest (a position)

GIS Geographic Information System

IDT Icarus Dial Tone

IMEI International Mobile Equipment Identifier

LBT L Band Transceiver

PBX Private Branch eXchange

POTS Plain Old Telephone System

PUK Personal Unblocking Code

SBD Short Burst Data

SIM Subscriber Identity Module

SMS Short Message Service

For a complete definition of terms see http://www.telestial.com/glossary.htm on the Web.

1616-964-12

Date: 7/27/2011

Rev. 2.1

1 GENERAL INFORMATION

1.1 INTRODUCTION

This manual contains information relative to the physical, mechanical, and electrical

installation of the Sky Connect Systems. Operating procedures are also included.

1.2 SYSTEM DESCRIPTION

The Sky Connect series satellite communications device consists of a transceiver, an

L-band antenna, and a dialing/audio/data interface device. The remote mounted

transceiver is the heart of the system, and contains the Iridium satellite LBT (L-Band

Transceiver). The LBT can be thought of as the “phone” in the satellite phone

system and the modem in the data system, as it is the connection used to gain access

to the Iridium network. The LBT allows the two way transfer of voice and data.

The LBT is the same in every transceiver of the Sky Connect System though different

modules are added to define the function of the transceiver as a whole. Each Sky

Connect telephone system also has the ability for data transfer at rates up to 10

Kbps (with compression), allowing the user to interface a laptop for in-flight email

capability. The Tracker system offers an optional internal 12 channel G.P.S. module.

Tracker uses the short burst data transfer portions of the Sky Connect suite, though

it can be coupled with any of the phone systems. Any system can exist alone, or

co-exist with another, and upgrades can be done to any system at any time without

incurring additional cost penalties.

The Iridium system can only be occupied by one “call” at a time, whether it is voice,

data, or Short Burst Data. These systems exist simultaneously, but can not be used

simultaneously. Multiple transceivers and antennas are required for multiple

channels of communication. For clarity, two users may be on separate handsets on

the same call, but two users can not be on separate handsets on different calls

without a second transceiver/antenna. Similarly, when a phone call is in progress,

Tracker will be unable to send SBD packets, though as soon as the line is clear, it will

send its stored messages.

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Rev. 2.1

Figure 1

Tracker & Communication Concept Drawing

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Rev. 2.1

1.3 TECHNICAL SPECIFICATIONS

1.3.1 TRANSCEIVERS

Part Numbers 1616-XX0-0X all Transceivers are the same with the exceptions listed

in the below table.

ITEM SPEC

Regulatory Compliance: DO-160D, FAA STC on Part 25, 27, and 29 aircraft. FAA-PMA

Temperature Range: Section 4 Cat D2 (-20C to +55C)

Altitude Range: Section 4 Cat D2 (50,000 feet)

Vibration: Section 8 Cat R

Temp Variation: Section 5 Cat C

Power Input: Section 16 Cat B

DC Spike: Section 17 Cat B

Conducted Emissions Section 21 Cat B

Radiated Emissions Section 21 Cat B

Weight 4.05 lbs.

Add Tracker: .05 lbs.

Add G.P.S. .10 lbs

Add Messenger: .05 lbs.

Physical Dimensions:

Length 10.0 Inches

(Width) 2.5 Inches

(Height) 4.5 Inches

Power Requirements (Voltage): 11-32Vdc

Power Requirements (Current) : <1 Amp @ 28Vdc

Transmit Power Average: 1.5 watts

Mounting: Quick release tray, 4-#8 holes, any configuration

Transmission rate: 2.4Kbps voice and data (10Kbps with compression)

Operating Frequency: 1.616-1.6265 GHz

Inputs/Outputs: POTS (Plain Old Telephone Service), RS232, DSC, dc

level. 8 discrete inputs Lo< 1.2 Hi >1.3

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Rev. 2.1

ITEM SPEC

Connectors: TNC female (Iridium), BNC female G.P.S.,

62 pin High Density D-sub connector

1.3.5.2 SOP DIAL PAD SIX POSITION 1616-051-01/03

SOP 6 Dialer has been discontinued.

1.3.5.3 SOP DIALER ELEVEN POSITION 1616-052-00/02

ITEM SPEC

Weight 8 oz.

Physical Dimensions:

(Depth) 3.375 Inches

(Width) 5.75 Inches

(Height) 1.12 Inches

Power Requirements (Voltage): 6 to 28 volt dimmer connected to two separate busses

Power Requirements (Current) : 100 ma Max.

Inputs: 2 lamp inputs

Outputs: 7 switch grounded outputs

Connectors: DB-15 male

Mounting: Dzus rail

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Rev. 2.1

1.3.5.4 MISSION MANAGEMENT UNIT 1616-055-00/10/11/12/13

ITEM SPEC

Regulatory Compliance: FAA STC on Part 27, and 29 aircraft. (MMU II only part 29) FAA-

PMA

Weight: 15 oz.

Physical Dimensions:

(Depth) 3.375 Inches(MMU) 5.65 (MMU II)

(Width) 5.75 Inches

(Height) 1.875 Inches

Power Requirements (Voltage): 10-33 VDC

Power Requirements (Current) : 250 ma max.

Inputs: RS-232, Wi-Fi Interface for the use of loading Message Sets into

memory.

Outputs: RS-232, four discrete outputs 100ma sinked to ground

Connectors: 2ea. DB-25 male (keyed)

Mounting: Dzus rail

1.3.5.5 SWITCH PANEL Reserved

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Rev. 2.1

1.3.5.6 CONFIGURATION MODULE 1616-905-01

This part has been discontinued, see earlier manuals.

1.3.5.7 CONFIGURATION/SIM MODULE 1616-905-02

ITEM SPEC

Regulatory Compliance: FAA STC on Part 27, and 29 aircraft. FAA-PMA

Weight: 16 oz.

Physical Dimensions:

(Length) 2.5 inches (without mating connectors)

(Width) 2.125 inches

(Height) .625 inches

Power Requirements (Voltage): 12VDC (supplied by transceiver)

Inputs: Serial Buss and DPL Buss

Outputs: Serial Buss and DPL Buss

Connectors: One DE9 female and one DB25 male

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Rev. 2.1

1.3.6 ANTENNAS

1.3.6.1 IRIDIUM LOW PROFILE ANTENNA 1616-880-01 AeroAntenna AT2775-XXX

ITEM SPEC

Regulatory Compliance: TSO C-144, DO-160D

Operating Temp: -55 Deg to +85 Deg C

Weight: .5 Lbs Max.

Physical Dimensions: 3.5 inches in diameter

Frequency: 1595 +/- 30 Mhz

Connectors: TNCF

Altitude: 70,000 feet

Impedance: 50 Ohms

1.3.6.2 IRIDIUM BLADE ANTENNA 1616-880-00 Dayton Grander # L10-780

ITEM SPEC

Regulatory Compliance: FAA STC on Part 27, and 29 aircraft

Weight .7 Lbs Max.

Physical Dimensions:

Length 5.49 Inches

Width 3.09 Inches

Height 3.11 Inches

Speed: 600 Kts.

Impedance: 50 Ohms

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Rev. 2.1

1.3.6.3 SENSOR G.P.S. ANTENNA 1616-880-04

ITEM SPEC

Regulatory Compliance: TSO C-144, DO-160D

Operating Temp: -67 Deg F to +185 Deg F

Weight 5 Oz.

Physical Dimensions: 3.5 inches in diameter X .57 Inches High

Frequency: 1575.42 MHz

Connectors: TNCF

Altitude: 55,000 feet

Impedance: 50 Ohms

Voltage: 4 – 24 VDC

1.3.6.4 ANTCOM COMBO IRIDIUM/GPS ANTENNA 1616-880-13

ITEM SPEC

Regulatory Compliance: TSO C-144, DO-160D, DO-228, MIL-C-5541

Operating Temp: -67 Deg F to +185 Deg F

Weight 7.84 Oz.

Physical Dimensions: L= 5.026" W= 2.2" H= .71"

Frequency: Iridium= 1610 to 1626.5MHz GPS= 1575.42 +/- 13 MHz

Connectors: TNC both GPS (Blue) and Iridium (Red)

Altitude: 70,000 feet

Impedance: 50 Ohms

Voltage: 2.8 to 28VDC (GPS)

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Rev. 2.1

2 INSTALLATION PROCESS

INSTALLATION PROCESS OUTLINE

Note: Make a plan to cover the follow items in depth in this manual.

2.1 WIRING DIAGRAM

2.1.1 G.P.S. interface, or use of an internal G.P.S.

2.1.2 Event switches, optional

2.1.3 Diagnostic port, must be installed for configuration

2.1.4 Configuration/SIM module, optional

2.1.5 Selection of Dialers optional

2.2 SIM CARD ACTIVATION

Check to make sure the card is activated, call Sky Connect

You will need to know the following information;

2.2.1 The IMEI # of your unit

2.2.2 Model #

2.2.3 Serial #

2.2.4 Credit Card or billing information for monthly service

2.2.5 Aircraft type and registration number

2.2.6 Complete contact information for customer using the product

2.2.7 Send in activation form to turn on the unit with satellite system, please fill out the

form as accurately as possible to make the process as smooth as possible

2.2.8 The form may be filled out on the web at http://www.skyconnect.aero/1086.xml

2.3 ANTENNA PLACEMENT PLAN

2.3.1 Pay close attention to the length of coax from the antenna to RT

2.3.2 Follow manual instructions on placement near other Sat COM and Comm antennas

2.4 Notebook computer with “tracker setup” program, CD included with RT

2.5 INFORMATION NEEDED FOR CONFIGURATION

2.5.1 How the event switches were wired

2.5.2 What type of switches, MOM, ALT, Press

2.5.3 What phone numbers need to be entered (optional)

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2.6 TRACKER MAPPING SYSTEM

Decide what mapping system is to be used for tracking the aircraft.

Setup an account with that provider and secure ID and passwords.

Make sure this installation is added to the account that handles the mapping.

It is the responsibility of the owner to add aircraft to the mapping system, Sky

Connect

can NOT do that for you unless it is the Sky Connect Webmap you are using.

2.7 WIRING

2.7.1 Wire system as drawn, you the installer are responsible to the FAA for methods and

practices used during the installation.

2.7.2 Continuity checks.

2.7.3 Power polarity checks.

2.8 CONFIGURATION

2.8.1 Configure RT to work with event switches as connected in wiring

2.8.2 Configure external G.P.S. to talk to Sky Connect RT, Aviation or NMEA RS232 format

data

2.8.3 Enter phone numbers (optional)

2.9 TRACKER RULES ( the ugly 14 rules)

Before the tracker can be used to display data on a map, the rules of operation must

be understood. The following will outline those rules.

2.9.1 The transceiver must send data.

2.9.1.1 In order to send data the transceiver must have an active LBT sending SBD.

This is done from the activation form.

2.9.1.2 The transceiver must have an active SIM card.

2.9.1.3 The transceiver must have been configured for the aircraft type.

2.9.1.4 Helicopters may use collective or squat switches.

2.9.1.5 Airplanes may use squat switches.

2.9.1.6 The transceiver must have the report intervals set.

2.9.1.7 The aircraft must be outside and have a clear view of the sky.

2.9.1.8 The aircraft antenna system must be installed I.A.W. our instructions.

2.9.1.9 To display a complete flight, the aircraft must send Departure, Scheduled

reports, and an Arrival message to define a complete flight. This is done

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through the proper setting of the squat switch, and or software settings from

the tracker setup configuration software.

2.9.1.10 Our server must be set to pass the data on to the proper map program.

2.9.1.11 Our server must have been set up for the customer (activation form

completed and sent in to our office).

2.9.1.12 The map program must be set to receive the data from our server.

2.9.1.13 The map program must have a profile setup to display the aircraft correctly.

2.9.1.14 If email notification is desired we must have the email addresses (activation

form).

2.10 Sky Connect Tracker Capabilities Notes

The following is a recommendation and suggested options available to the user of

the Sky Connect Tracker Series. We hope not to limit your imagination on how you

can apply the rules of the system, only make some common suggestions.

2.10.1 Event Switch Use

Most important of the options that an end customer can take advantage of

with the tracker is the eight (8) event switches. When one of the switches is

closed or opened, and event report is sent to the ground server alerting the

software to this action. Each event is defined either by the Sky Connect

Server ie Squat switch, or by the end user through the ground mapping

software or the Tracker Configuration software.

Each switch input can be configured to one of the following types of inputs:

2.10.1.1 Toggle Switch - This type of switch selection in the tracker set up software

will send an event report when the switch is closed (set) and when it is again

opened.

2.10.1.2 Press Switch - this is a momentary action switch, and sends one event report

per press.

2.10.1.3 Squat Switch - Has a specific purpose, to report that the aircraft has taken off

(open) or has landed (closed).

2.10.1.4 Dialer - used to dial one of the pre-programmed phone numbers if you are

using the 6 or 11 position dialer panels. Use of the 11 position dialer takes

up 4 of the 8 event switches and limits use for various other inputs.

2.10.1.5 Inhibit - This switch input will prevent the tracker from transmitting the

position data.

The 11 position dialer 1616-052-0X will make use of 7 of the provided 8

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allowing only one left for the squat switch input if desired.

2.10.2 The predetermined functions of the switches on the 11 position dialer are:

2.10.2.1 Emergency - typically to declare and aircraft emergency.

2.10.2.2 Code - used mostly by EMS operators to declare a patient emergency.

2.10.2.3 Position - mark a position of interest to the pilot or crew.

2.10.2.4 Dialer - 4 event switches are used to dial the programmed numbers.

The MMU does not use any of the event switches so all 8 are available.

2.10.3 Suggested uses for the event switches would be:

2.10.3.1 Connect to an oil pressure switch to automatically send an event report when

oil pressure is lost, to the ground.

2.10.3.2 Connect to a low rotor RPM warning when rotor speed is insufficient, to the

ground.

2.10.3.3 Connect to an over temp/torque light to report this event to the ground.

2.10.3.4 Connect to a relay to let the ground know a circuit breaker has been pulled.

This has been used in the past on lease aircraft to allow the leaser to know

when the pilot has made an attempt to disable the time reporting system,

being the Sky Connect system itself.

Any event the operator would wish to know has occurred in flight, can be recorded

to the ground by the use of a switch closure. The logic can be inverse by the use of a

relay. More than one event can be grouped to one event switch by the use of diodes.

Example: the ground might want to know that an event has occurred that would

require ground maintenance. You might not need to know that a specific event has

occurred immediately, but that something has occurred. Connecting all the engine

events to one input isolated by diodes would report such an event.

Note: Connection of aircraft “required systems” through the tracker (a nonessential

system) will require FAA or other airworthiness approval. Engineering showing

compliance with XX.1309 will have to be completed. Minor or major

change/alteration determination is up to the installer.

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2.10.4 Server Software Options

Sky Connect Server Software is capable of the following settings.

2.10.4.1 Sending an email when the unit has missed a report. This is determined in

the software by looking at the report rate interval and making the

determination that an interval has passed without a report from the

transceiver. The system waits an additional 5 minutes, and if another report

has not come through to the server, sends an email(s) to an individual or a

table of addresses for missed report alarm, a.k.a. Overdue.

2.10.4.2 Sending an email for EVERY report the unit makes. Some operators use this

to determine if the unit is tracking in lew of a software program.

2.10.4.3 Flight summary reports can be sent by email, with information on the

distance, time and takeoff/landing locations. This email may be sent to one

or many persons in a email table.

2.10.5 Mapping Software Options

There are many mapping programs designed for either a wide customer

base, or designed for very specific operator use. These programs have their

own manuals and should be consulted based on which program you choose.

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EMS Sky Connect Series Installation guide

EMS Sky Connect Series Installation guide

EMS Sky Connect Series Installation guide

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