Sky Connect LLC...ICA-2009-100 Date: 10/7/2009 Rev. A 2 1.2 List of Applicable Publications Any...

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Sky Connect LLC

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS

for

SKY CONNECT VOICE/TRACKER SYSTEM

Installed in the Gulfstream GIV I.A.W. STC# ST02696NY

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RECORD OF REVISIONS

Rev # Issue Date Inserted Change By

IR 1/9/2009 IR M. Freyder

A 10/7/2009 A M. Freyder

Table of Abbreviations

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 satellite terms see http://www.telestial.com/glossary.htm on theWeb.

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TABLE OF CONTENTS

RECORD OF REVISIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ii

TABLE OF CONTENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iii

LIST OF EFFECTIVE PAGES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv

INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Applicability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1List of Applicable Publications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2Distribution . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

SYSTEM DESCRIPTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Transceiver . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Antennas . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3Wiring . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

PARTS CATALOG INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

MAINTENANCE INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8Scheduled Maintenance Program . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8Troubleshooting Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9Recommended Method of Removal/Replacement of Equipment . . . . . . . . . . . . . . . . . . . 9Weight and Balance Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12Checkout Procedures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

AIRWORTHINESS LIMITATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

APPENDIX A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . A-1

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LIST OF EFFECTIVE PAGES

Page Date Revision Page Date Revision

i 10/7/2009 A A-1 WD-2009-10010/7/2009

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ii 10/7/2009 A

iii 10/7/2009 A A-2 2009-1011/9/2009

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iv 10/7/2009 A

1 10/7/2009 A A-3 2009-1021/9/2009

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3 10/7/2009 A A-4 2009-1031/9/2009

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5 10/7/2009 A A-5 2009-1041/9/2009

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7 10/7/2009 A A-6 2009-10510/7/2009

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9 10/7/2009 A A-7 2009-10610/7/2009

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11 10/7/2009 A A-8 Parts List10/7/2009

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1 INTRODUCTION

1.1 Applicability

This document contains the Instructions for Continued Airworthiness for the Sky ConnectVoice and Data Communication System installation on Gulfstream G-IV. This data is insupport of STC certification of the EMS Sky Connect on this aircraft model.

Gulfstream GIV was certified by Federal Aviation Regulation FAR Part 25, as defined inFAA TCD Type Certificate Data Sheet A12EA.

Data contained in this document supplements the original maintenance manual inaccordance with FAR 25.1529 when approving the data required for Supplemental TypeCertificate (STC) issuance. It also supplements or supercedes the information containedin the aircraft maintenance manual. For operating procedures not contained in thissupplement, consult the aircraft maintenance manual.

"Modification of an aircraft by this Supplemental Type Certificate obligates the aircraftoperator to include the maintenance information provided by this document in theoperator's Aircraft Maintenance Manual and the operator's Aircraft ScheduledMaintenance Program."

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1.2 List of Applicable Publications

Any necessary information for inspection, or troubleshooting of equipment of the SkyConnect system can be found in the Sky Connect Forte’ Installation Manual Rev 1.0 orlater revision, and the attached drawings list below which are in Appendix A.

Drawing/Document # Rev. Title

WD-2009-100 A or latest revision System wiring

2009-101 A or latest revision Transceiver Installation

2009-102 A or latest revision Cradle/Base Station Installation

2009-103 A or latest revision Handset Installation

2009-104 A or latest revision Antenna Installation

2009-105 A or latest revision Wire Routing Drawing

2009-106 - or latest revision Network Gateway Installation

1.3 Distribution

Changes to this ICA are posted on the www.skyconnect.aero website for down load bycustomers with the installation of the Sky Connect System. This manual will be listed ina publication index posted on the web, and the customer should check periodically orbefore maintenance is performed to assure oneself that they are using the most currentversion.

http://www.skyconnect.aero

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2.0 SYSTEM DESCRIPTION

The Sky Connect Voice and Data Communication System consists of an Iridium antenna,GPS antenna, a transceiver, corded handset, cordless handset, and audio/data interfacebased on options desired. The transceiver is the heart of the system, which contains thecircuitry for the Iridium Satellite communications system. This unit controls all 2-waycommunication of voice and data. The system is limited to one call at a time, whether it isvoice, data, or short burst data. These systems can exist simultaneously, but cannot beused simultaneously. Data or voice transmission is sent at a rate up to 10kbps (withcompression). An optional Network Gateway is offered for installation with the SkyConnect Transceiver to off the ability to send and receive email in the cabin during flight.

2.1 Transceiver

The transceiver has contained within the L-Band Transceiver (LBT) that communicateswith the satellites. The LBT is connected to an interface that is computer controlled andallows the LBT to be used for tracking and voice communications.

2.2 Antennas

There are two possible antennas used. One is the Iridium antenna which connects to theLBT, and does the sending and receiving of the satellite signals. The other is the optionalGPS antenna used if the transceiver has an internal GPS sensor. This GPS sensor is notconnected in any way to the cockpit and can not be used as a reference for navigation. Itspurpose is only to report the position of the aircraft to the ground map.

2.3 Wiring

Wiring will vary with options selected at the time of installation. The Sky Connect Forte’Installation Manual shows a wide array of options and how they are to be wired.

2.4 Handsets/Cradles/Base Station

The handsets are installed at the option of the customer’s preference. There are basicallytwo designs, a cordless and corded. With the cordless comes the cordless base station. Both options are designed to be used with the POTS interface offered by the transceiver. This is a two wire ring and tip, the same as found commercially all over the world. Up tofour POTS devices may be installed in parallel on the same POTS line. This offers acombination of multiple units of the two designs.

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There are two cradle designs for the cordless handsets. Surface mount as it describes willmount to the surface of a wall or drink rail. Flush mount as it describes is to be mountedflush into a surface. Both have a power supply to recharge the batteries in the handsetwhen power is applied to the aircraft.

Cordless handsets have a great deal of range and can be used anywhere in the cabin, andeven outside the aircraft while on the ground (of course). When the aircraft is to bestored for long periods of time, the handsets should be removed from the aircraft andstored in a dry cool place to preserve the operation of batteries and displays. An officecharger could be used to keep the unit batteries charged.

The corded handset draws power from the aircraft buss and does not have batteries.

2.5 Network Gateway

The Gateway part number 1616-101-31 may be installed as an option to allow passengersto send and receive email while in flight. The gateway interfaces with the transceiverover a dedicated RS-232 serial port to allow the gateway access to the Iridium network.

The Iridium satellite constellation is the pipeline used to send the email data to the earthstation. This pipeline currently has a narrow band width (4800 bps) but is more thansufficient for the use of email as long as the automatic downloading of graphics is turnedoff on the device connected by WIFI to the gateway. Connection is automatic once awireless device is turned on within range of the gateway. Your handheld device shouldsee a service titled “AIRMAIL SERVER” as a WIFI connection point. Selecting thisservice will allow connection of email services.

NOTE: Sky Connect strongly suggest a dedicated transceiver be used wheninstalling the Network Gateway. If not other services such as phone andtracking will be interrupted.

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3.0 PARTS CATALOG INFORMATION

Material List

Qty Part Number Description Source

1 See System Selection

Table 1

TRANSCEIVER Sky Connect

AR See drawing #2009-104 in

Appendix A

Antenna doublers local fabrication

See drawing #2009-101 in

appendix A

Transceiver detail parts Sky Connect

See document PL-2009-100 for a

comprehensive list of parts.

Installation parts See document

1 See drawing 2009-102 for the

installation of the base station and

cordless handset.

Handset and cradle Sky Connect


corded handset installation

Corded handset in cockpit Sky Connect


Network Gateway installation

Network Gateway Sky Connect

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SYSTEM SELECTION TABLE 1

System Name Transceiver Accessories and Description

Aviation POTS 1616-400-01A MMU II, Handset cordless and basestation, and/or handset corded. Cradlemaybe surface mount or flush mounted.

Aviation POTS with Tracker 1616-450-02A MMU II, Handset cordless and basestation, and/or handset corded. Cradlemaybe surface mount or flush mounted.

Aviation POTS with Trackerand internal GPS

1616-450-01A MMU II, Handset cordless and basestation, and/or handset corded. Cradlemaybe surface mount or flush mounted.

Accessory Name Accessory PN Description

Corded Handset 1616-410-00 Corded Handset used in the cockpit tomake and receive calls

Cordless Handset withCradle

1616-121-00 (HS)1616-200-11/12/13/14Cradle

Cordless handset with associated cradle. Cradle can be flush or surface mounted,and contains the handset charger

Base Station 1616-101-11 Cordless base station, used tocommunicate to the handset, and connectsto the transceiver

MMU II (optional) 1616-055-101616-055-12 NVG

Any of the above transceivers when usedas a text terminal or POTS dialer

Network Gateway(optional)

1616-101-3XSee Parts List

Optional gateway to be used for passengeremail in flight

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4.0 MAINTENANCE INSTRUCTIONS

4.1 Scheduled Maintenance Program

Task to be added to the aircraft operator’s appropriate maintenance program are asfollows:

4.1.1 Recommended Periodic Scheduled Preventative Maintenance Test/Checks

Functional test.

4.1.2 Recommended Periodic Scheduled Inspections

During Annual inspections or other scheduled aircraft inspections;1. Inspect the transceiver (1616-4X0-0X), and the two (2) antennas for signs of

corrosion or external damage.2. Inspect the equipment to ensure that it is securely attached.3. Inspect the electrical wiring for insulation damage and chafing. Replace any cable

assemblies that have insulation damage or evidence of chafing.4. Inspect the base station for signs of corrosion or external damage, ensure wiring is

secure and not chafed.Any necessary information for inspection, or troubleshooting of equipment of the SkyConnect system can be found in the Sky Connect Forte’ Installation Manual Rev 1.0 orlater revision.

4.1.3 Recommended Periodic Structural Inspections

During annual inspections or 1200 hour aircraft inspections, inspect the transceiver mountfor signs of corrosion and security.

4.1.4 Special Inspections

4.1.4.1 Hard Landings - Follow instructions for paragraph 4.1.2 above.

4.1.4.2 Lightning Strikes - Verify proper system operation by following system test procedurescalled out in paragraph 4.1.1.

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4.2 Troubleshooting Information

See installation manual Sky Connect Forte’ Installation Manual 1.4 (or later version), fortroubleshooting suggestions prior to taking any further action.

When investigating a system problem, a performance history check is helpful. Checkwith your dispatcher to determine if there have been any indications of recurringperformance anomalies or squawks with this unit. This information may be helpful inisolating the cause of the problem. Of particular importance are any dispatch consoleindications of problems or inconsistencies.

Remember: you must obtain a Case File Number (aka RMA) from Sky ConnectTechnical Support (985-863-0954) prior to returning any materials for repair orreplacement. Have the equipment model and serial number ready when you call for thecase number.

4.3 Recommended Method of Removal/Replacement of Equipment

NOTE: Adjust aircraft weight and balance data, reference Table 4, when components areremoved or installed.

4.3.1 Antenna - Removal/Replacement

Ensure that power is off, and that the transceiver circuit breaker on the DC bus is open. Refer to Sky Connect drawing numbers in appendix A of this manual to locate theantenna(s) to be removed.

To replace an antenna, remove the four (4) antenna attachment screws and disconnect thecoaxial cable. Connect the replacement antenna to the coaxial cable by finger tightening,then an additional turn on the coaxial connector. Caution: Do NOT over tighten. Mountthe antenna and secure it with the attachment screws, torque to 20 inch-pounds.

4.3.2 Transceiver - Removal/Replacement

Removal - Ensure that power is off, and that the proper circuit breaker on the 28V DCbuss is open. Refer to Sky Connect drawing numbers in appendix A of this manual tolocate the transceiver to be removed on the aircraft.

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Disconnect the antenna coaxial cables from the transceiver. Disconnect P1 on thetransceiver. Loosen the locking screw and remove the transceiver from the mountingtray.

Install - Ensure that the power is off, and that the proper circuit breaker on the 28VDCbuss is open. See removal above if you do not know the location of the breaker.

Slide the transceiver into the mounting tray making sure lip on transceiver connects intotray rear lock. Move the lock into position, and tighten the locking knob. Connect the 62pin connector and connect the Iridium antenna TNC connector. Connect the optionalG.P.S. BNC connector if equipped.

4.3.3 Cradle/Base Station - Remove/Replacement

Position passenger seat to allow access to side panel for removal. Side cabin side panelcan be removed by pulling on the bottom edge of the panel to separate the velcro holdingthe panel on three sides. The top edge is behind a lip in the drink rail. Pull out and downto remove the panel. Disconnect any accessory cables, noting their location to reconnectafter maintenance is complete.

Removal Cradle and handset - Remove the handset from the cradle. Locate the four (4)mounting screws, remove screws and remove the cradle connector. Pull up to remove thecradle and mounting hardware.

Removal Base Station - The base station is mounted to the cabin side panel. To removethe cradle from the side panel, remove the screws holding the base station to the panelmounts.

Install Base Station - locate the position of the base station by placing it over the mountingholes. Install the same hardware removed to re-secure the base station to the cabin sidepanel. Install connector and check to make sure it mates correctly.

Install Cradle - The cradle can be placed over the mounting holes, and the nut plates heldfrom behind. Start the four screws that secure the cradle to the drink rail, continue totighten until all four screws are hand tight. Reinstall the cradle connector.

Install Cabin Side Panel - Connect all disconnected connectors before installing the panel. Cabin side panel will fit into a channel in the bottom of the drink rail. Insert the top edgeof the panel into the channel and push the other three sides so the velcro will secure thepanel to the wall.

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4.3.4 MMU II Removal/Replacement

The MMU II is a Dzus rail mounted unit. Unlock all four Dzus and pull up on the unit toremove it from the panel. Disconnect the two (maybe one depending on options)connectors from the rear of the MMU II.

Install the MMU II by connecting the aircraft harness to the rear, and slide it down into itsopening in the console. Secure by tightening all four Dzus.

4.3.5 Corded Handset

Removal - The corded handset cradle secures with four screws. To remove the handsetpull it off the spring mounted cradle and set aside. Pull up the Dzus panel the handset ismounted to, allowing access to the connector. Disconnect the handset connector from theaircraft harness.

Install - Install the handset connector to the aircraft harness connector locking it in place. Secure the Dzus panel the handset cradle is mounted to in place by securing all four Dzus. Return handset to its cradle.

4.3.6 Network Gateway

Removal - Ensure power is off, and the “Satcom” circuit breaker is open. The gateway is installed on the bottom of the shelf that serves as the floor of the coatcloset ~FS 171. Remove the floor of the closet by removing the 5 ea. #10 screws thatsecure it to the airframe. Pull up on the shelf enough to access the electrical connectors. Remove the electrical connectors that interface the gateway to the transceiver. Removethe Power connector. The gateway is secured to the shelf with four #10 screws, remove allfour screw and remove the gateway from the shelf.

Installation - Ensure power is off, and the “Satcom” circuit breaker is open. Center thegateway over the attach points on the shelf. Start the four screws that secure the gatewayto the shelf, and then tighten all four screws. Connect the power connector, and theinterface connector to the transceiver. Reinstall the shelf to the airframe using the five #10screws removed to access the gateway.

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4.4 Weight and Balance Data

Table 4

Part Weight ARM

Transceiver 4.25 Lbs. 174.0

Iridium Antenna .50 Lbs. 162.0

GPS Antenna .50 Lbs. 162.0

MMU II * .85 Lbs. Cockpit Console

Handset, Cordless andCradle

.60 Lbs. 199.75

Handset, Corded * .50 Lbs. Cockpit Console

Base Station 1.50 Lbs 196.75

Network Gateway 3.3 Lbs. 108.0

Transceiver (optionaldedicated to Gateway)

4.25 111.0

* = Mounted in the center console in an open Dzus rail position.

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4.5 Checkout Procedures

4.5.1 Telephony Units (1616-4X0-0XA)

4.5.1.1 Phone testing

Using ground power, turn on the Aircraft master, avionics master, or what ever is required to fully power all elements of the installed Sky Connect system. The Iridium antenna must have an unimpeded view of the sky. Operating next to a hangar can cause occasional brief signal interruption. Allow at least one minute for the system to register on the Iridium network. This system is a phone, so operation is as with any phone. The Iridium System is an international phone system so when dialing this phone alwaysuse the international country code number of the phone you are dialing to.

4.5.1.2 MMU II (if installed)

Dial Test: Select the Sky Connect system on the audio panel. Rotate the selector knob andselect one of the preprogrammed phone numbers on the MMU and push the knob toinitiate the call, or dial a number from the keypad. A ring should be audible in theheadset. When answered, verify that the connection is clear and free of interference. Pressthe selector knob again to terminate the call.

Receive Call Test: Request the dispatch center to place a call to the Sky Connect Trackersystem installed on the aircraft. Verify that the ring is heard. Answer the call by pressingthe selection knob. Verify that the connection is clear and free of interference. Press theselector knob again to terminate the call.

Send Data Test: Select one of the preprogrammed test messages on the MMU II and pushthe knob to send data. Verify that the data has been received by dispatch. Note: thisprocess may take up to 120 seconds depending on server workload.

Request the dispatch center to send a text message to the Sky Connect Tracker via the webinterface. Verify that the message has displayed on the face of the MMU II. Note: thisprocess may take up to 120 seconds depending on server workload.

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4.5.1.3 Information on dialing

A call to the aircraft from the ground can be done in one of two ways;

1.) Call the aircraft number using the international code of 011-88-163-xxx-xxxx where the xs are the given number.

2.) Call the Iridium phone number 480-768-2500, and then dial the 88-163-xxx-xxxxnumber. This option may not be available to all customers. Use of this optiondepends on activation of this feature at time of purchase.

The second example is cheaper for customers calling within the US, because it offers Iridium users a special rate per minute.

4.5.2 Tracking

4.5.2.1 Tracking (if installed)

In order to fully test Tracker, you will need access to a PC running Sky ConnectTracker-Map, or an approved GIS display system. In the event that this is not available toyou, contact Sky Connect Technical Support where we can remotely aid in your testing. Refer to Appendix A for additional troubleshooting advice.

The Installer can verify the proper wiring of every onboard component with a combinationof the Tracker Setup program and the status annunciator light (if installed). The installercan be assured that their portion of the job is acceptable if the onboard unit consistentlyindicates that it is sending and completing messages. (This is indicated by positiveconfirmation that the message was sent on the MMU II). It is the customer’s responsibilityto choose the manner in which they display their “tracked” aircraft, not the installers.

Note: Only one Iridium source can occupy the network at one time. Ifa Sky Connect voice option is installed and in use, the Tracker willstore and send position reports when the line is free. Configurationswill exist to give Tracker priority, thus discontinuing an in-progresscall. Alternatively, separate transceivers/antenna can be used formultiple systems.

Using ground power, turn on the Aircraft master, avionics master, or what ever is requiredto fully power all elements of the installed Sky Connect components. If a G.P.S. isinterfaced, it must be operating and have acquired satellites. The aircraft must have anunimpeded view of the sky. Operating next to a hangar can cause occasional brief signal

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interruption of both G.P.S. and Iridium functionality. If using an internal G.P.S., allow theunit to run for up to 15 minutes on the initial startup to allow the internal G.P.S. to acquirealmanac data. Allow two minutes for the system to register on the iridium network.

Within this registration time, Tracker will generate a start up message which will be sentvia the Iridium network to our switching network, and then to the mapping system. At thistime, (approximately 24 seconds after the message was generated) a data block will beavailable to your Tracking Provider. With some software systems there may be a delay upto 1 ½ minutes before the aircraft is seen on your GIS. Giving the G.P.S. a destinationwaypoint, and if possible some speed, will send additional parameters to the mappingsystem for display, including Destination, Speed, Altitude, Flight Plan, etc.

IMPORTANT - Using the TRACKER SETUP program, you can testmost of the features of the installation with the exception of the fullnetwork test. Any contact closures that were installed for use withTracker can be tested at this time as well. No messages will becompiled or sent while the Tracker Setup program is connected andrunning. Messages will resume, roughly one minute after the programis discontinued.

From the main page, you can verify the G.P.S. position, speed, and altitude. The unitsIMEI # and G.P.S. input type are displayed when known. The Iridium Signal strength(0-5) and Modem status are displayed and updated in real time.

From the Switch configuration page you can select the type and rate of each switch input,but you can also test to verify the input. The Setup program samples the incomingswitches every ten seconds to see if they are active. The switch status will display as on ifa ground is applied to the corresponding pin, and off if the line is floating.

Each closure will also generate a specific event at the PC running the mapping systemsoftware. The program must have an “assignment” for the event triggers to accomplishtheir task. The assignment for contact closure #2, for example, can be assigned on themapping system PC terminal to annunciate “Mission Aborted.” The important elementhere is that the contact closure number is accurate to the specific switch being tested. Purposes for these switches are defined by the end user. For more clarity on thisprogramming, refer to the mapping system operation manual.

Should you desire to use our Tech Support for these tests, you will need to have availablethe Transceiver Serial Number, IMEI#, aircraft ID, and installed options/configuration.With power applied, Tracker will continue to generate position report updates at its

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programmed interval. Once registered on the network, Tracker interval reports are billedper hour of use including during the testing process.

Note: Programmed interval directly affects customer billing. Consultwith end user regarding all available configuration options beforeaccomplishing.

4.5.3 Network Gateway (if installed)

4.5.3.1 Verify the Data LED is solid Green indicating a successful boot. If not solidGreen, refer to the Network Gateway Installation Manual for troubleshootingprocedures.

4.5.3.2 Confirm the initial setup procedures as outlined in the Network GatewayInstallation Manual have been completed.

4.5.3.3 Using a handheld wireless device, configure the device to acknowledge theNetwork Gateway as the WIFI source.

4.5.3.4 Access and email account with the handheld wireless device and send a test emailto confirm network connectivity, verifying the message was sent.

5.0 AIRWORTHINESS LIMITATIONS

No airworthiness limitations associated with this design change.

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APPENDIX A-1

WD-2009-100

Installation Wiring Drawings

The following documents are in support of this ICA, and can be found listed in paragraph 1.2.

UNLESS NOTED OTHERWISE, ALL NEW WIRE TO MEET MIL-C-27500 SHIELDED OR MIL-W-22759. INSTALL WIRINGFOLLOWING EXISTING WIRE BUNDLES WHERE PRACTICAL. FOR ROUTING, REFER TO SKY CONNECT DRAWING2009-105, FOR BONDING AND GROUNDING DETAILS, REF: AC43-13-1B CHAPTER 11. WIRE SPLICES ARE DEPICTED BYA SPLICE SYMBOL ( ) WHERE WIRE GAUGE CHANGES OR BY A DOT ( ) WHERE WIRE GAUGE DOES NOTCHANGE. WIRE AND WIRE SPLICES ARE PROVIDED BY INSTALLER.

WHERE POSSIBLE, ALL WIRES TO BE MARKED LEGIBLY AND PERMANENTLY USING INDELIBLE INK, LASER OR OTHEREQUIVALENT MEANS. ALL WIRE BUNDLES SHOULD BE IDENTIFIED AS "SKY CONNECT."

WIRE NUMBER FORMATS ARE: SKY 502 A 22

GROUNDS TO BE AS SHORT AS POSSIBLE UNLESS OTHERWISE INDICATED. GROUNDS UNDER 6" IN LENGTH DO NOTREQUIRE A WIRE NUMBER, SHIELD PREPARATION SHOULD NOT EXCEED 3" FROM CONNECTOR. SHIELD GROUNDSMAY BE ACCOMPLISHED BY DAISY CHAINING, SPLICING OR INDIVIDUALLY GROUNDING SHIELD TO APPROPRIATEGROUND DEVICE.

THE TYPE OF GROUND IS INDICATED BY THE FOLLOWING SYMBOLS:

A

B

C

D

DC GROUND

AC GROUND

SIGNAL GND

AIRFRAME & SHIELD GND

REFERS TO LIKE LETTER IN SYMBOL THIS DWG.

REF GAC GROUND/PROX WINDSHEAR DWG SC41349021-01

6 ITEMS 12, 14 AND 48 INCLUDE HOODS AND 22 GAUGE FEMALE CONTACTS, SKY CONNECT P/N 1616-721-01(POSITRONICS P/N FC8022D)

7 THE CONFIGURATION OPTIONS SHOWN ARE TYPICAL BUT NOT EXCLUSIVE. EACH SKY CONNECT TRANSCEIVER CANSUPPORT UP TO 4 POTS DEVICES IN ANY COMBINATION. REFER TO THE FORTÉ INSTALLATION MANUAL FOR MORECONFIGURATION OPTIONS.

X

1

THE CONFIGURATION MODULE IS AN OPTIONAL ACCESSORY AND IS TYPICALLY USED BY FLEET OPERATORS WHOANTICIPATE SWAPPING TRANSCEIVERS BETWEEN AIRCRAFT. IF THE CONFIGURATION MODULE IS USED WITH A1616-400-01A TRANSCEIVER, THE CONFIGURATION MODULE ACTS ONLY AS A SIM CARD HOLDER AND ONLY WIRESSKY503A22 W/B AND SKY504A22 W/B ARE NEEDED, THEREFORE WIRES SKY501A22 AND SKY502A22 ARE NOTINSTALLED.

THE DIAGNOSTIC CONNECTION (P4) IS USED WITH 1616-450-01A OR 1616-450-02A TRANSCEIVERS EITHER INCONJUNCTION WITH THE CONFIGURATION MODULE TO PLACE THE CONNECTION AT A CONVENIENT LOCATION, ORIN THE ABSENCE OF A CONFIGURATION MODULE TO ALLOW PROGRAMMING OF THE TRANSCEIVER.

IF THE CONFIGURATION MODULE IS USED WITHOUT DIAGNOSTIC CONNECTOR, THE PARTS LIST COUNT IS REDUCEDBY ONE (1) EACH OF ITEMS 15, 16 AND TWO (2) OF ITEM 22.

IF THE DIAGNOSTIC CONNECTION IS USED WITHOUT CONFIGURATION MODULE, THE PARTS LIST COUNT IS REDUCEDBY ONE (1) EACH OF ITEMS 09, 13, 16, 20, AND 22.

IF BOTH THE CONFIGURATION MODULE AND THE DIAGNOSTIC CONNECTION ARE ELIMINATED, THE PARTS LISTCOUNT IS REDUCED BY ONE (1) EACH OF ITEMS 09, 13, 16, 20 AND TWO (2) OF ITEM 22.

8

THE 1616-450-01A AND 1616-450-02A TRANSCEIVERS TRANSMIT GPS POSITION REPORTS. THE 1616-450-01ATRANSCEIVER HAS AN INTERNAL GPS RECEIVER AND REQUIRES ITEM 11, GPS ANTENNA. THE GPS ANTENNA IS NOTUSED WITH 1616-400-01A OR 1616-450-02A TRANSCEIVERS.

IF THE GPS ANTENNA IS ELIMINATED, THE PARTS LIST COUNT IS REDUCED BY ONE (1) EACH OF ITEMS 11, 36 AND 37.

THE 1616-450-02A DOES NOT HAVE AN INTERNAL GPS RECEIVER AND REQUIRES THE EXTERNAL GPS FEED. THEEXTERNAL GPS FEED IS NOT USED ON THE 1616-400-01A TRANSCEIVER AND IS OPTIONAL WITH THE 1616-450-01ATRANSCEIVER. THE EXTERNAL GPS RECEIVER IS OWNER SUPPLIED.

9

2

3

4

5

REF GAC DWG CE41290.

11

10 THE BANDPASS FILTER IS USED IN AIRCRAFT WHEN BOTH IRIDIUM AND INMARSAT SYSTEMS ARE INSTALLED.

IF THE BANDPASS FILTER IS ELIMINATED, THE PARTS LIST COUNT IS REDUCED BY ONE (1) OF ITEM 08 AND TWO (2)OF ITEM 36.

WIRE SKY401B22 FROM P10 TO J11 IS NEEDED TO PROGRAM MESSAGE SETS ONTO THE MMU II. WIRE SKY401A22FROM P11 TO P1 IS ONLY NEEDED FOR THE MESSAGING FUNCTIONS OF THE MMU II AND IS ONLY USED WITH1616-450-01A OR 1616-450-02A TRANSCEIVERS.

12

13

FOR INSTALLATIONS NOT NEEDING THE ILLUMINATED SWITCH, A TOGGLE SWITCH IS ILLUSTRATED BOTH WITH ANDWITHOUT AN EXISTING MUX ANNUN CONTROL.14

SYSNUMBER

AWGSEGMENT

THE RINGER IS OPTIONAL. AN AUDIBLE TONE IS HEARD ON THE HEADSET LINE. THE RINGER IS USED IF THESPECIFIC INSTALLATION REQUIRES RING TONE ON AN EXTERNAL SPEAKER.

THE PROGRAMMING CONNECTOR (P6) IS REQUIRED TO PROGRAM THE WIRELESS BASE STATION TO ADD ORREMOVE HANDSETS.

NOTES

THE MMU II IS AVAILABLE EITHER IN THE STANDARD VERSION (1616-055-10) OR IN A NVIS COMPATIBLE VERSION(1616-055-12) FOR AIRCRAFT ANTICIPATING NIGHT FLYING WITH NIGHT VISION DEVICES.15

16ITEMS 10, 26, 27, 28, 30, 31 AND 35 MAY ALREADY BE EXISTING IN AIRCRAFT IF SKY CONNECT SYSTEM IS REPLACINGAN EXISTING IRIDIUM SATCOM SYSTEM.

17 ITEM 10 IS AVAILABLE WITH TWO SEPARATE SKY CONNECT PART NUMBERS TO REFLECT ANTENNAS FROM TWOMANUFACTURERS. THE ANTENNAS ARE OTHERWISE FUNCTIONALLY IDENTICAL.

23 NEXT ASSEMBLY GIV-2009-100-1.

1234

B

A

4 3 2 1

A

B

1 50 1616-610-34 PROGRAMMING CABLE SKY CONNECT

2 49 M2112LXW01-RO SPST SWITCH

1 48 1616-720-50 (DD44F10Z00) HD D-SUB CONNECTOR KIT (44F) SKY CONNECT(POSITRONIC)

1 471616-720-48(MS27484E8F98S) CONNECTOR, CIRCULAR, 3 CONTACT SKY CONNECT

(AMPHENOL)

3 (OPT) 46 082-5370 CONNECTOR, COAX, N AMPHENOL1 (OPT)

451616-885-01 DIPLEXER (TNC CONNECTOR) SKY CONNECT

1 (OPT) 1616-885-00 DIPLEXER (N CONNECTOR) SKY CONNECT

1 (OPT)

44

1616-101-32(1233-A-0200)

NETWORK GATEWAYSKY CONNECT(SATCOM)1 (OPT) 1616-101-31

(1233-A-1001-01)

1 (OPT) 1616-101-30(1233-A-0100)

1 1 43 M641/6-1 HEADPHONE JACK MIL SPEC

1 1 42 M641/5-1 MIC JACK MIL SPEC

1 1 1 1 41 N/A LABEL "SKY CONNECT RELAY" LOCAL MFR

1 40 N/A LABEL "OFF HOOK" LOCAL MFR

1 39 28519-327 BULB, 28V GE

1 38 MS25041-1 PRESS-TO-TEST INDICATOR MIL SPEC

1 1 1 1 37 31-4427 CONNECTOR, COAX, BNC AMPHENOL

5 5 5 5 36 31-4452 CONNECTOR, COAX, TNC AMPHENOL

1 1 1 1 35 N/A LABEL "SATCOM" LOCAL MFR

1 1 1 34 N/A LABEL "WIRELESS HANDSET" LOCAL MFR

AR AR AR AR 33 N/A COAX CABLE -- RG400 OR EQ. BELDEN

1 1 1 1 32 1N4007 DIODE

1 1 1 1 31 M12883/53-001 MOUNTING RAIL MIL SPEC1 (OPT) 1 1 1 1 30 7274-11-3 CIRCUIT BREAKER KLIXON

1 1 1 1 29 7274-11-2 CIRCUIT BREAKER KLIXON

1 1 1 1 28 M12883/52-002 RELAY SOCKET MIL SPEC

1 1 1 1 27 M83636/6-025M 4PDT RELAY MIL SPEC

1 1 1 126

466-SO45 ANNUN / SWITCH EATON

OPT OPT OPT OPT MS25098-22 SPST SWITCH MIL SPEC

1 1 2 1 1 25 D20419 MALE SCREWLOCK CANNON

1 2 1 1 24 D20418 FEMALE SCREWLOCK CANNON

1 1 1 23 1616-722-08 (206070-8) HOOD, CPC SKY CONNECT(AMP)

1 5 7 5 6 22 1616-722-04 (DE-24657) HOOD 9SKY CONNECT(CINCH)

2 21 1616-725-25 (D25000JVL0) HOOD 25 WITH VIBRATION LOCKSKY CONNECT(POSITRIONIC)

1 1 1 1 20 1616-722-02 (DB-24659) HOOD 25SKY CONNECT(CINCH)

9 AR AR AR AR 19 1616-721-04 (M39029/64-369) CONTACT, 20G MALE SKY CONNECT(CINCH)

AR AR AR AR 18 1616-721-02 (M39029/63-368) CONTACT, 20G FEMALE SKY CONNECT(CINCH)

1 1 1 17 1616-720-08 (205839-3) CPC CONNECTOR (28 F) SKY CONNECT(AMP)

1 2 3 2 2 16 1616-720-05 (M24308/4-1F) D-SUB CONNECTOR (9 M) SKY CONNECT(CINCH)

3 4 3 4 15 1616-720-04 (M24308/2-1F) D-SUB CONNECTOR (9 F) SKY CONNECT(CINCH)

1 1 1 14 1616-900-34 (DD15F10JVL0) HD D-SUB CONN KIT (15 M) SKY CONNECT(POSITRONIC)

1 3 1 1 13 1616-720-02 (M24308/2-3F) D-SUB CONNECTOR (25 F) SKY CONNECT(CINCH)

1 (OPT) 1 1 1 1 12 1616-105-02 (DD62F10Z00) HD D-SUB CONN KIT (62 F) SKY CONNECT(POSITRONIC)

1 1 1 1 11 1616-880-04 (S67-1575-39) GPS ANTENNASKY CONNECT(SENSOR SYSTEMS)

1 (OPT) 1 (OPT) 1 (OPT) 1 (OPT) 1 (OPT)10

1616-880-01(AT2775-110GAW-TNCF) IRIDIUM ANTENNA

SKY CONNECT(AERO ANTENNAS)

1 (OPT) 1 (OPT) 1 (OPT) 1 (OPT) 1 (OPT) 1616-880-02 (S67-1575-109) IRIDIUM ANTENNASKY CONNECT(SENSOR SYSTEMS)

1 (OPT) 1 (OPT) 1 (OPT) 1 (OPT) 09 1616-905-02 CONFIGURATION MODULE SKY CONNECT1 (OPT) 1 (OPT) 1 (OPT) 1 (OPT) 08 1616-700-01 BANDPASS FILTER SKY CONNECT

1 (OPT)07

1616-055-12 MMU II NVIS SKY CONNECT1 (OPT) 1616-055-10 MMU II SKY CONNECT

1 1 06 1616-410-00 (DT100-101) CORDED HANDSETSKY CONNECT(DEKLIN)

OPT

05

1616-200-14 AUDIO INTERFACE SKY CONNECT

1 1616-200-13 CHARGING CRADLE W/ AUDIO INTERFACEW/ HANDSET SKY CONNECT

OPT OPT 1616-200-12 CHARGING CRADLE, FLUSH MOUNT,W/ HANDSET SKY CONNECT

1 1 1616-200-11 CHARGING CRADLE, SURFACE MOUNTW/ HANDSET SKY CONNECT

1 1 1 04 1616-101-11 FORTÉ BASE STATION SKY CONNECT

1 1 1 1 1 03 1616-105-01 MOUNTING TRAY SKY CONNECT

1 (OPT) 1 (OPT) 1 (OPT)

02

1616-450-02A TRANSCEIVER SKY CONNECT

1 (OPT) 1 (OPT) 1 (OPT) 1616-450-01A TRANSCEIVER SKY CONNECT

1 (OPT) 1 1 1616-400-01A TRANSCEIVER SKY CONNECT

01 -- FORTÉ 1650S SKY CONNECT

#500 #400 #300 #200 #100 ITEM PART NUMBER DESCRIPTION SUPPLIER

PARTS LIST

19

8

10

8

8

8

8

14

8

9

9

10

15

9

19

16

16

16

16

16

16

1617

ITEM 50, PROGRAMMING CABLE, IS PROVIDED FOR SETUP OF THE NETWORK GATEWAY AND IS NOT INTENDED FORUSE IN FLIGHT. IF A WIRED PORT IS DESIRED FOR THE NETWORK GATEWAY, EQUIVALENT WIRING MAY BEINSTALLED USING A HD26 PIN D-SUB CONNECTOR AND RJ45 PLUG IAW THE INDICATED WIRING.

18

19 THE #500 CONFIGURATION CAN BE INSTALLED INDIVIDUALLY OR IN COMBINATION WITH ONE OF THE OTHERNUMBERED CONFIGURATIONS. THE CONFIGURATION SHOWN IS TYPICAL BUT NOT EXCLUSIVE. THE SKY CONNECTNETWORK GATEWAY IS SHOWN WITH A SKY CONNECT TRANSCEIVER USED AS THE RS-232 DATA COMMUNICATIONEQUIPMENT (DCE). ANY OTHER FAA APPROVED RS-232 DCE DEVICE MAY BE SUBSTITUTED FOR THE SKY CONNECTTRANSCEIVER. WIRING OF SUBSTITUTE DCE SHOULD BE IAW MANUFACTURERS SPECIFICATIONS.

IF THE SKY CONNECT TRANSCEIVER IS NOT USED AS THE DCE, ITEMS 02, 03, 10, 12, 30, 33 AND 36 WILL BE RETAINED,ELIMINATED OR SUBSTITUTED BASED ON THE INSTALLATION OF THE SUBSTITUTE DCE DEVICE.20

THE PART NUMBER SHOWN FOR ITEM 49, SPST SWITCH, IS THE RECOMMENDED SWITCH WHICH HAS ANINTEGRATED LED INDICATOR. THE "X" IN THE LISTED PART NUMBER IS TO BE SUBSTITUTED WITH "E" FOR YELLOWOR "F" FOR GREEN. IF A SUBSTITUTE SWITCH IS USED, THE SPECIFIC SWITCH AND INDICATOR CHOSEN ARE TO BEDETERMINED BY THE INSTALLER, BASED ON THE CONFIGURATION OF THE AIRCRAFT AND THE NEEDS OF THECUSTOMER.

21

ITEM 45, DIPLEXER, IS USED TO INTEGRATE TWO IRIDIUM DEVICES WITH ONE IRIDIUM ANTENNA, IF 45 IS ELIMINATED,ITEM 46 WOULD ALSO BE ELIMINATED.22

LTR ECO Description Date ApprovedA N/A INITIAL RELEASE 01/09/2009 MLF

B N/A ADDED PAGE 5, NETWORK GATEWAY, ANDNOTES 18-22 10/07/2009 MLF

Drawn

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Checked / Approved

Filename Size Sheet Scale Rev

Drawing Number

All dimensions are in inches unlessotherwise specified.Dimensions marked: [X.XX] REF are existing geometry,and are supplied as reference only. [X.XX] TYP are typical dimensionsare are supplied as reference only

Tolerances, unless otherwisespecified:x.x ± .05"x.xx ± .01"x.xxx ± .005"x° ± 2°

This data is provided as a CONFIDENTIAL and PRIVILEGED DOCUMENT by Sky Connect. Any other use orreproduction without the expressed written consent of Sky Connect is expressly forbidden. Any misuse of this documentincluding (but not limited to) quotation in part without written consent of Sky Connect is expressly forbidden.

DER Review

Wesley Hastings 01/09/2009


Michael Freyder 10/07/2009

WD 2009-100.dwg

Forté 1650 G-IV Installation

WD-2009-100

B 1 of 5 N/A B

7

9

22

22

6

21

18

COPILOT CB PANEL

30

29

3

2

28VDCR MAIN BUS

28VDCR MAIN BUS

103CB1 SATCOM

103CB2 WIRELESS HANDSET

D

D

321321321

X1

X2

ESH 3

C

B

AA

D

21421

22

297

3

6243

474930

122819

269

425

13

+28V DC+28V DC

GNDGND

TIPRING

SHIELD

+28V DCGND

C SH 3

D SH 3

235

689

1317

1514

235

CONFIG DATA OUTCONFIG DATA IN

CONFIG GND

CONFIG PWRCONFIG SCLCONFIG SDA

DPL ENABLEDPL GND

DPL TxDPL Rx

SHIELD

DATA OUTDATA IN

DATA LO

CONFIG DATA INCONFIG DATA OUTCONFIG GND

CONFIG PWRCONFIG SCLCONFIG SDA

DPL POWERDPL GND

DPL RxDPL Tx

TRANSCEIVER

CONFIGURATION MODULE

BNC TNC

OPTIONAL

GPS ANTENNA

RS600A18

SHIELD GND

RS700A18

SHIELD GND

RS600B18

RS601A20N

RS805A22 WRS805A22 B


SKY501A22 WSKY501A22 BSKY501A22 O

SKY502A22WSKY502A22 BSKY502A22 O

SKY503A22 WSKY503A22 B


RS600A18RS600B18

RS700A18RS700B18

RS606A22NRS603A22

RS607A22

SKY609A

2222

TNC TNC TNC TNC

OPTIONALBANDPASS FILTER 103A2

TRS ANTIRIDIUM ANTENNA RS602B

5231

RS232 GPS DATA INRS232 GPS LO

SHIELD

RS232 GPS DATA OUTRS232 GPS LO

GPS


RS232 GPS DATA IN

10

N/C

OPTIONAL(USE WITH 1616-450-02A TRANSCEIVER)

OPTIONAL(USE WITH 1616-450-01A TRANSCEIVER)

1202 03

08

33 10

312827

2018 09

11

3636

36

3636

37

35

34

ASH 4

33

504832

RS232 DATA INRS232 DATA OUT

RS232 GND


B SH 3

SKY501B22 WSKY501B22 BSKY501B22 O

235

19 2216 221815

P1

25 P2 P4P3

474930

CONFIG DATA OUTCONFIG DATA IN

CONFIG GND


13SHIELD

235

221815 P4OPTIONAL

8

8

9

10

9

OPTIONAL 13

4

DiagnosticConnector

DiagnosticConnector

321

D

6

2513

7

41SKY CONNECT RELAY

RELAY SHOWNDE-ENERGIZED

MAXIMUM LENGTH: 50.0' +0.00'

1234

B

A

4 3 2 1

A

B



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Drawing Number




DER Review




WD 2009-100.dwg


WD-2009-100

B 2 of 5 N/A B

2

2

2

2

RS602A

1

2

4

28V DC INPUT

GND

RING

BASE STATION

3TIP

AE SH 2

C SH 2

2221

2324252627

28

94

38271

56

DTRRITxDCTSRxDRTSDCDDSRGND

CHARGING CRADLE

1

11

28V DC INPUT

GND A7GND628V DC INPUT

CORDED HANDSET

1

3

28V DC INPUT

RING4TIP

6GND D SH 2

RS700B18

RS701A20N


SKY703A20N



22

1815

1817

14

04

05

06

23

22

6

CHARGING CRADLE/AUDIO INTERFACE

1

11

28V DC INPUT

GND A7GND628V DC

SKY703A20N

05

10RING15TIP

8HOOK SWITCH LO2HOOK SWITCH HI

13RINGER LO14RINGER HI

5PHONES LO4PHONES HI

9MIC LO3MIC HI

12HOOK BULB

MMU II

2

15

28V DC INPUT

GND14GND

07

5RING6TIP

20RINGER LO8RINGER HI

22PHONES LO10PHONES HI

25MIC LO13MIC HI

1813 20

C SH 2

1

2

4

28V DC INPUT

GND

RING

BASE STATION

3TIP

AE SH 2

2221

2324252627

28

94

38271

56

DTRRITxDCTSRxDRTSDCDDSRGND

RS700B18

RS701A20N

22

04

CORDED HANDSET

1

3

28V DC INPUT

RING4TIP

6GND D SH 2RS807A22 WRS807A22 B

181506 22

1

2

4

28V DC INPUT

GND

RING

BASE STATION

3TIP

AE SH 2

C SH 2

2221

2324252627

28

94

38271

56

DTRRITxD

11

28V DC INPUT

GND A7GND628V DC INPUT

RS700B18

RS701A20N


SKY703A20N

22

04

05

D SH 2RS807A22 WRS807A22 B

#100 CONFIG

C SH 2RS805A22 WRS805A22 B

CHARGING CRADLE

#200 CONFIG

#300 CONFIG

#400 CONFIG

N/C

N/CN/C

CTSRxDRTSDCDDSRGND

1

252412

RS232 DATA OUTRS232 DATA IN

RS232 GND

SKY401B22 WSKY401B22 BSKY401B22 O

B SH 2

128V DC INPUT13GND

235

1

24

19

222522

1815 16

221815

PJ11

P8

P7

P5

P8

P9

P6

1813 20P10

1817

14

23

6

221815

P7

P5

P6

1817

14

23

6

221815

P7

P5

P6

7

13

SKY301A22

SKY302A22SKY303A22SKY304A22SKY305A22SKY306A22

SKY307A22

SKY301A22


SKY307A22

SKY301A22


SKY307A22

12

12

12

MMU II P1

MMU II P2

DSHIELD GND

SHOWN WITH 1616-200-11/-12 SHOWN WITH 1616-200-11/-12

SHOWN WITH 1616-200-13/-14

11 11

15

ProgrammingConnector



N/C2POLARIZING PIN

N/C1POLARIZING PIN

RS

806A

22 W

RS

806A

22 B

RS

806A

22 W

RS

806A

22 B

RS

806A

22 W

RS

806A

22 B

RS

702A

22

RS

702A

22

RS

702A

22

38 39ASKY704A20N2

31

7 7

7

7

7

7

40 OFF HOOK

43

42

43

42

600 Ω

150 Ω

600 Ω

150 Ω

1234

B

A

4 3 2 1

A

B



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Drawing Number




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WD 2009-100.dwg


WD-2009-100

B 3 of 5 N/A B

2

2

2

2

2

2

2

2

SKY413B22 BSKY413B22 W







ON

SATCOMMASTER

RAD ATLVOICE

O' RIDE

CALLO' RIDE

GPWSVOICE

O' RIDE

COPILOT INSTRUMENT PANEL

COPILOT ANNUNCIATOR LAYOUT, TYPICAL(NOT TO SCALE)

HF1

HF2

VHF1

VHF2

VHF3

RADIOTEL

LAV CALLFWD AFT

CABINCALL

TERRINHIB

RAD ATLVOICE

O' RIDE

CALLO' RIDE

GPWSVOICE

O' RIDE

COPILOT INSTRUMENT PANEL

COPILOT ANNUNCIATOR LAYOUT, TYPICAL(NOT TO SCALE)

HF1

HF2

VHF1

VHF2

VHF3

RADIOTEL

LAV CALLFWD AFT

CABINCALL

TERRINHIB

SATCOMMASTER

32

6,911125817

104

125

43

B

W

B

W

ON

SATCOMMASTER

GPWSVOICE

O' RIDE

B

W

B

W

32611

32

A

COPILOT INST PNL

26

5

5

RS603A22RS608A22RS604A22

RS605A22NRS607A22

RS604A22

GP906A22

MUX ANNUN CONTROL

10SATCOM "ON"

REF - Existing Aircraft Equipment

A

26

OPTIONALAlternate Switch Configuration with MUX ANNUN

ASH 2

ASH 2 RS607A22

26 REF

26 REF

EXISTING

EXISTING

RS608A22

MUX ANNUN CONTROL

10SATCOM "ON"

REF - Existing Aircraft Equipment 32

A

26

ASH 2 RS607A22

OPTIONALAlternate Switch Configuration without MUX ANNUN

242522 22PJ1216 191815

14

14

SATCOM MASTER SWITCHSHOWN IN OPEN POSITION

OFFHOOK

OFFHOOK

40 REF39

40 REF39

38

38

1234

B

A

4 3 2 1

A

B



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Drawing Number




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WD 2009-100.dwg


WD-2009-100

B 4 of 5 N/A B

2

2

2

TRANSCEIVER

TRANSCEIVER

NETWORK GATEWAY

392745

513736

PC RTSPC CTS

PC RI

PC RxDPC TxDPC SG

53846

PC DCDPC DTRPC DSR

214262

+28V DC+28V DC+28V DC

12243

GNDGNDGND

789

235

146

D

16 19 2219

222222

3

ABC

+28VDC (H)+28VDC (L)

GND

47

19

2

LAN 1 RX+

LAN 1 TX-1LAN 1 TX+

20LAN 1 RX-

8

19

WIFI ENABLE

LINK STATUS1PPP ENABLE

18WIFI STATUS

42DISCRETE GND33+5 VDC Vcc

44J6 J1

J2

J4

3

21

6

10bT/100bTXETHERNET NIC

(RJ45)

D

229

3020

28VDC

28VDC

50 18

48 649

495VDC

5VDC

21

RTSCTSRI

RXTXSGND

DCDDTRDSR

02 03

TNCIRIDIUM ANTENNAJ2

J1

36

DIPLEXER

N

N

TNCIRIDIUM ANTENNAJ2 36

02 03

4546

46 N46

TNC33 20 36 20 10 17 20

20

1234

B

A

4 3 2 1

A

B



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Drawing Number




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WD 2009-100.dwg


WD-2009-100

B 5 of 5 N/A B

19

22

25

2

2

#500 CONFIG

OPTIONALSKY CONNECT SATCOM INSTALLATION PER #100,#200, #300 or #400 NUMBERED CONFIGURATION.

19

SKY900A18




RS602A

SKY602A

RS602C

SKY913A22 BSKY913A22 W

SKY912A22 BSKY912A22 W

SKY914A22SKY915A22

SKY912A22 N

SKY910A18

SKY900A18

SKY901A20 N

ICA-2009-100Date: 10/7/2009

Rev. A

A-2

APPENDIX A-2

2009-101

Transceiver Installation Drawings

1 1616-105-01 2 MOUNTING TRAY 302

11616-400-01A

1 SKY CONNECT TRANSCEIVER 3011616-450-01A1616-450-02A

12 NAS1836-08 2 INSERT 2132 MS21919 1 ADEL CLAMP 2121 M12883/52-002 1 RELAY SOCKET 2111 M12883/53-001 1 RELAY SOCKET TRACK 210

12 2 NAS1149 F 0332 P 1/2 WASHER 2094 6 NAS1149 F N832 P 1/2 WASHER 208

12 2 MS35207-261 1/2 SCREW 2074 6 MS35206-243 1/2 SCREW 206

2 MS21075-08 1 NUTPLATE 2052 MS21061-L3 1 NUTPLATE 2044 MS21061-L08 1 NUTPLATE 203

4 2 MS21059-L08 1/2 NUTPLATE 2028 20 MS20426AD3 1/2 RIVET 201

1 -103 1 EXISTING AVIONICS SHELF REF REF 1032 -102 4 RAIL (GULFSTREAM P/N 601037) 2024-3511 .068 THK 102

1 -101 3 TRAY ADAPTER 2024-T3C .050 THK 101

-003 2 RAIL INSTALLATION (REF)-002 2 ADAPTER PLATE INSTALLATION-001 1 SKYCONNECT TRANSCEIVER INSTALLATION 001

-003 -002 -001 NUMBER SHT DESCRIPTION MATERIAL SIZE ITEMQUANTITY/

DASH NUMBER LIST OF MATERIALS

REFRH AVIONICS SHELF

FS171 / WL84

-301

-101

-302

LTR Description Date ApprovedA INITIAL RELEASE 1/9/2009 MLF

REF-103

CORE AL ALLOY HONEYCOMB, 2.3-1/4-12. TOP SKIN .016; BOTTOM SKIN .016;1. MAXIMUM LOAD OF SHELF IS 25 LBSSHELF NOTES FOR EXISTING SHELF:

2PL

2X-201

-204

4PL

2X-201

-203

2PL

-208

-206

-2122PL

-209

-207

FWD←OUTBOARD↑

LOCATED IN EXISTING AVIONICS RACK FS171

-301

-302

-103

(NOT SHOWN)-211

-210

4PL

-208

-206

-001 TRANSCEIVER INSTALLATION

1. NEXT ASSEMBLY GIV-2009-100-1NOTES:

Drawn

Revised

Checked / Approved

FilenameSize Sheet Scale Rev

Drawing Number

All dimensions are in inches unless otherwisespecified. Dimensions marked: [X.XX] REF are existing geometry, and are suppliedas reference only.

Tolerences, unless otherwise specified:x.x ± .05"x.xx ± .01"x.xxx ± .005"x° ± 2°

This data is provided as a CONFIDENTIAL and PRIVILEGED DOCUMENT by Sky Connect. Any other use or reproductionwithout the expressed written consent of Sky Connect is expressly forbidden. Any misuse of this document including (but notlimited to) quotation in part without written consent of Sky Connect is expressly forbidden.

Third Angle Projection



2009-101.dwg

Sky Connect Transceiver Installation

2009-101B 1 of 3 1/2 A

2PL (REF)-102

(REF)-103

4PL

2x-201

-202

4PL

-208

-206

-101

12PL

-209

-207

(REF)-103


] REF[1.75

] REF[4.25

] REF[7.88

A

A

] REF[2.94 ] REF[2.94

] REF[1.75

] REF[5.88

12 PL-213

-003 RAIL INSTALLATION

-002 TRAY ADAPTER INSTALLATION

OUTBOARD↑ FWD←

Existing Insert

Drawn

Revised

Checked / Approved


Drawing Number







2009-101.dwg


2009-101B 2 of 3 1/2 A


14.075

2.94

1.50

9.19

9.625

.24

1.835

10.200

1.220

.050

.75

.918

.050RBB

A

AA

AA

A

A

AA

A

.050x.203nB2

.050x.174nA10DESCRIPTIONHOLEQUANTITY

Hole Table

.45 .45

.36

5.17

.92

.59

.51

2.37

.219 .219

-101 TRAY ADAPTER

Drawn

Revised

Checked / Approved


Drawing Number







2009-101.dwg


2009-101B 3 of 3 1:1 A

ICA-2009-100Date: 10/7/2009

Rev. A

A-3

APPENDIX A-3

2009-102

Cradle/Base Station Installation Drawings

View looking Inboard← Aft

17.4

7.5

1 1616-101-11 WIRELESS BASE STATION 302

1 1616-200-11

HANDSET CRADLE 3011 1616-200-12

1 1616-200-13

REF CID A-A-55126 FASTENER TAPE, HOOK AND LOOP 2" 214

AR 1559 A/B EPIBOND ADHESIVE 213

1 1602-852-200-1201 RETENTION PLATE 212

1 1602-852-200-1200 RETENTION PLATE 211

4 NAS1836-08 INSERT 210

2 MS21055-L08 NUTPLATE 209




4 MS24693S47 SCREW 205

4 MS35206-235 SCREW 204

4 MS24693S58 SCREW 203

4 MS24693S25 SCREW 202

8 8 MS20426AD3-4 RIVET 201

1 -107 4 NUTPLATE RETAINER 2024-T3C .040 THK 107

1 -106 4 NUTPLATE RETAINER 2024-T3C .040 THK 106

1 -105 4 ADAPTOR PLATE 2024-T3C .050 THK 105

1 -104 5 HONEYCOMB SPACER 610-10133-250 .250 THK 104

1 -103 3 EXISTING DRINK RAIL REF 103

1 -102 2 EXISTING PHONE STORAGE BOX REF 102

1 -101 1 EXISTING INTERIOR WALL PANEL CCS1004-12-1-1P .125 THK 101

-003 3 FLUSH MOUNT CRADLE INSTALLATION 003

-002 2 SUFRACE MOUNT CRADLE INSTALLATION 002

-001 1 BASE STATION INSTALLATION 001

-003 -002 -001 NUMBER SHT DESCRIPTION MATERIAL SIZE ITEM

QUANTITY/ DASH No LIST OF MATERIALS


101

302105

104

4PL202

4.76

11.65

1.5 LBEXISTING SPEAKER

EXISTING OUTLET

EXISTING MISC

EXISTING WALL PANEL

6. NEXT ASSEMBLY GIV-2009-100-1.5. ALL MANUFACTURED METAL PARTS SHOULD BE FINISHED WITH MIL-P-85582, TYPE I EPOXY POLYAMIDE PRIMER.4. ON ALL MANUFACTURED PARTS, BREAK ALL SHARP EDGES.3. HONEYCOMB SPACER (-104) ATTACHES TO EXISTING PANEL WITH EPIBOND 1559 A/B ADHESIVE OR EQ.2. EXISTING PANEL IS SECURED ON THE TOP BY A FLANGE UNDER THE DRINK RAIL AND ON THE BOTTOM BY HOOK AND LOOP FASTENER.1. EXISTING PANEL (-101) GULFSTREAM COMPLETIONS PART NUMBER CCS1004-12-1-1P, .125" THK.NOTES:

Forward edge of panel at FS 193B +2"

Bottom edge of panel at WL 79

213

214

4PL205

Drawn

Revised

Checked / Approved


Drawing Number







2009-102.dwg

Base Station and Cradle Installation

2009-102B 1 of 5 1/4 A

] REF[12.68

] REF[4.80

] REF[4.33

] REF[3.74

] REF[7°

1.380 1.063

4.688

4.451.30

← Forward← Inboard


102

301

EXISTING PHONE BOX

MATING CONNECTOR AND WIRING SPECIFIED ON WD2009-100

Drawn

Revised

Checked / Approved


Drawing Number







2009-102.dwg


2009-102B 2 of 5 1/2 A


.636R

2.520

7.057

.010R .085

.510R

.385R

301103

212

4PL204

211

SELF-LOCKING NUTSPLC-632-211 AND -212 MANUFACTURED USING PEMHANDSET CRADLE CUTOUT

(FOR OPTIONAL FLUSHMOUNT HANDSET)

Drawn

Revised

Checked / Approved


Drawing Number







2009-102.dwg


2009-102B 3 of 5 1/2 A

10.55

5.12

.050

9.000

.875.875

.29

1.96


7.35

3.35

.78

2.84

.315R

2.50

.85

1.063

105

106107

2PL

2x201

207 2PL

2x201

206

2PL

2x201

2082PL

2x201

209

.040

-105 ADAPTER PLATE

-107 NUTPLATE RETAINER -106 NUTPLATE RETAINER

.531

2.501.380

.690

.85

C C

CC

B

B

B

B

A

A

A

A

A

A

A

A

- .280 X 100°nw

.050x.164nC4

- .050x.138nB4FROM NUTPLATE DRILL GUIDE.

REFERENCE. PATTERN ACUTAL HOLESSPACING OF RIVET HOLES IS GIVEN AS

.181 X 100°nw

.050x.098nA8

NOTESDESCRIPTIONHOLEQUANTITYHole Table

BB

A

A

A

A



.181 X 100°nw

.040x.098nA4


BB

A

A

A

A



.181 X 100°nw

.040x.098nA4


.040

.304

.616

.344

.688

.425 .425

.486

Drawn

Revised

Checked / Approved


Drawing Number







2009-102.dwg


2009-102B 4 of 5 1:1 A


5.04

3.35

.68

.91

7.35

8.39 .250

4PL210

104

-104 Honeycomb PanelNorlam P/N 610-10133-250

6.52

2.84

.82

1.08

Drawn

Revised

Checked / Approved


Drawing Number







2009-102.dwg


2009-102B 5 of 5 1:1 A

ICA-2009-100Date: 10/7/2009

Rev. A

A-4

APPENDIX A-4

2009-103

Cockpit Handset/MMU II Installation Drawings

2.250

.20

] REF[5.38

] REF[5.75

] REF[9.50

] REF[9.00

11616-055-10

1 MMU II DIALER 3021616-055-12

1 1616-410-00 1 HANDSET WITH HANGUP CRADLE 301

1 KEYSTONE 745 1 GROMMET 204

2 NAS1149FN616P 1 WASHER 203

2 MS35206-228 1 SCREW 202

AR 3506-SC37A-Z3CT 1 DZUS FASTENER REF 201

1 -101 1 EXISTING BLANK CONSOLE PANEL 2024 T3 .050 101

-002 1 MMU II INSTALLATION 002

-001 1 HANDSET INSTALLATION 001

-002 -001 NUMBER SHT DESCRIPTION MATERIAL SIZE ITEMQUANTITY/ DASH No LIST OF MATERIALS


302

301

2PL

203

202

6PL201

AIRCRAFT CENTER CONSOLE

301

302

-001 HANDSET INSTALLATION

1.82

1.88

2. NEXT ASSEMBLY GIV-2009-100-1.1. PANEL DIMENSIONS SELECTED BASED ON AVAILABLE BLANK PANEL ON CENTER CONSOLE.NOTES:

Drawn

Revised

Checked / Approved


Drawing Number







2009-103.dwg

Handset Installation

2009-103B 1 of 1 1/2 A

.500n204

4.43

ICA-2009-100Date: 10/7/2009

Rev. A

A-5

APPENDIX A-5

2009-104

Antenna Installation Drawings

FS 133 / ARM 73FS 145 / ARM 85FS 157 / ARM 97FS 169 / ARM 109FS 181 / ARM 121

FS 108 / ARM 48

FS 0

REFFS 171.0 / ARM 111.0

Sky Connect Transceiver1616-400-01A; 1616-450-01A; 1616-450-02A

1 1616-880-04 GPS ANTENNA 3021 1616-880-02 IRIDIUM ANTENNA 301

8 MS24694-C(10) SCREW 2048 MS20426AD3 RIVET 2034 NAS1473A3 NUTPLATE 202

28 NAS1097AD4 RIVET 201

2 -102 3 ANTENNA ADAPTER 2024-T3C .130 THK 1021 -101 3 ANTENNA DOUBLER 2024-T3C .050 THK 101

2 -002 2 DOUBLER INSTALLATION 002-001 2 SKYCONNECT ANTENNA INSTALLATION 001

-002 -001 NUMBER SHT DESCRIPTION MATERIAL SIZE ITEM

QUANTITY/DASH No LIST OF MATERIALS


-301

-302

5. NEXT ASSEMBLY GIV-2009-100-1.4. BREAK ALL SHARP EDGES.3. ALL DETAILS TO BE FINISHED WITH FR PRIME OR EPOXY TOPCOAT BEFORE INSTALLATION.2. ALL RIVETS TO BE INSTALLED WET USING PR1422 SEALANT OR EQUIV.1. -101 AND -102 DOUBLERS TO BE INSTALLED WITH SURFACE SEALANT PR1422 OR EQUIV.NOTES:

Drawn

Revised

Checked / Approved


Drawing Number







2009-104.dwg

Antenna Installation

2009-104B 1 of 3 N/A A

BL 0.0 REFBL 7.54 REF BL 7.54 REF

(0.040 THK)AIRCRAFT TOP SKIN - REF

FORWARD

FORWARD

(VIEW LOOKING FORWARD)ANTENNA INST

VIEW LOOKING UP

VIEW LOOKING DOWN

REFARM 103.0

FS 163.0


4PL

2X-203

-202

4PL

2X-203

-202

4X-204

-302

4X-203

-301

-102

-102

Drawn

Revised

Checked / Approved


Drawing Number







2009-104.dwg


2009-104B 2 of 3 1/2 A

3.50n

1.00n

MAX.13

MIN.10

D

CC

CC

BBB

BB

BB

BBB

BB

BBBB

BB

BBB

BB

BB

BBB

AA

AA

AA

AA

- .050x1.000nD1

- .050x.229nC4FROM ANTENNA AT TIME OF INSTALLATION.AS REFERENCE. PATTERN ACUTAL HOLES

POSITIONING OF NUTPLATE HOLES IS GIVEN .050x.128nB28

FROM NUTPLATE DRILL GUIDE.REFERENCE. PATTERN ACTUAL HOLESSPACING OF RIVET HOLES IS GIVEN AS

.050x.098nA8

NOTESDESCRIPTIONHOLEQUANTITYHole Table - Doubler

3.70n

2.65n

1.65n

x4.688

x4.41

x4.41

B

A

AA

A

-Throughx1.000nB1FROM ANTENNA AT TIME OF INSTALLATION.AS REFERENCE. PATTERN ACUTAL HOLES

POSITIONING OF NUTPLATE HOLES IS GIVENThroughx.229nA4

NOTESDESCRIPTIONHOLEQUANTITYHole Table - Adaptor LTR Description Date Approved

A INITIAL RELEASE 1/9/2009 MLF

-101

-102

4.52

4.52

1.90

1.90 1.90

1.90

CONTOUR TO MATCH AIRCRAFT SKIN.

CONTOUR TO MATCH AIRCRAFT SKIN.

Drawn

Revised

Checked / Approved


Drawing Number







2009-104.dwg


2009-104B 3 of 3 1:1 A

ICA-2009-100Date: 10/7/2009

Rev. A

A-6

APPENDIX A-6

2009-105

Wire Routing Drawings

ICA-2009-100Date: 10/7/2009

Rev. A

A-7

APPENDIX A-7

2009-106

Network Gateway Installation

This data is provided as a CONFIDENTIAL and PRIVILEGED DOCUMENT by Sky Connect. Any other use or reproduction without the expressed written consent of Sky Connect is expressly forbidden. Any misuse of this document including (but not limited to) quotation in part without written consent of Sky Connect is expressly forbidden.

Christopher Malpass

Michael Freyder

Bill Pieper

2009-106.dwg

10/7/2009

10/7/2009

B 1 of 4 NTS -

2009-106


Drawn

Revised

Checked / Approved

Filename

DER Review Drawing Number

Size Sheet Scale Rev

All dimensions are in inches unless otherwise specified. Dimensions marked: [X.XX] REF are existing geometry, and are supplied as reference only. [X.XX] TYP are typical dimensions and are supplied as reference only. Tolerances, unless otherwise specified:x.x ± .05"x.xx ± .01"x.xxx ± .005"x° ± 2°

1

1

2

2

3

3

4

4

A A

B B

FS 133/ ARM 73

FS 157/ ARM 97

FS 108/ ARM 48

FS 0

FS 176/ ARM 116

FS 193A (+12.00)/ ARM 145

FS 193E (+12.00)/ ARM 192.5

FS 219.5

FS 193B (+12.00)/ ARM 157

FS 193C (+13.50)/ ARM 170.5

FS 193D (+13.00)/ ARM 183.5

FS 206

FS 145/ ARM 85

FS 193/ ARM 133

RIGHT RADIO RACK COAT CLOSET-

TRANSCEIVER/ NETWORK GATEWAY

INSTALLATION

GULFSTREAM

GIV

REVISION HISTORYREV ECO DESCRIPTION DATE APPROVED

- N/A Initial Release 10/07/2009 MLF

,

1

1

2

2

3

3

4

4

A A

B B


Christopher Malpass

Michael Freyder

Bill Pieper

2009-106.dwg

10/7/2009

10/7/2009

B 2 of 4 1/4 -

2009-106


Drawn

Revised

Checked / Approved

Filename




214WASHER (EXISTING)AN960D10L20

213SCREW (EXISTING)MS27039-1-1011

210SCREW (EXISTING)MS24694-C575

209SCREW (EXISTING)MS27039-1-616

108BOTTOM AFT BRACKET

(EXISTING - FS 176 WL 88)

-1081

107BOTTOM FWD BRACKET


1159F40640-651

106RIGHT RADIO RACK NO 4 SHELF

(EXISTING - WL 88)

1159FH40033-451

105AFT WALL

(EXISTING - FS 176)

-1051

104FWD WALL

(EXISTING - FS 157)

-1041

103AFT SUPPORT RAIL

2024-T3511

.062 THK


-1031

102FWD SUPPORT RAIL

2024-T3511

.09 THK EXTRUSION


-1021

101SHELF

.67 THK ALUMINUM HONEYCOMP PANEL

(EXISTING - WL 97)

-1011

LIST OF MATERIALS

ITEMDESCRIPTIONPART NUMBERQTY

WL 88

WL 97

FS 157 FS 176

209

101

104105

210210

209

102

103

2PL

3PL

3PL

4PL

213

214

5PL

107

209

214

4PL

108

209

214

5PL

213

214

6PL106



(REF) EXISTING AVIONICS BAY

VIEW LOOKING OUTBOARDFORWARD

NOTES:1. EXISTING -101 SHELF INSTALLED IN RIGHT RADIO RACK COAT CLOSET.2. ALL PARTS NOT MARKED AS EXISTING ARE ADDED AS PART OF THE INSTALLATION.

COAT CLOSET

,

1

1

2

2

3

3

4

4

A A

B B


Christopher Malpass

Michael Freyder

Bill Pieper

2009-106.dwg

10/7/2009

10/7/2009

B 3 of 4 1/4 -

2009-106


Drawn

Revised

Checked / Approved

Filename




303MOUNTING TRAY1616-105-011

302SKY CONNECT TRANSCEIVER1616-4X0-0XA1

301NETWORK GATEWAY1233-A-0200

1616-101-30

1616-101-31

1616-101-32

1

208CLAMPMS219192

207WASHERNAS 1149-CN616R4

206SCREWMIL 51957-384

205INSERTNAS 1836-06-124

204WASHERNAS 1149-D0363J4

203SCREWMIL 51958-614

202INSERTNAS 1836-3-124

201HYSOL EPOXY ADHESIVEEA 9309.3NA8

101SHELF

.67 THK ALUMINUM HONEYCOMP PANEL

(EXISTING - WL 97)

-1011

LIST OF MATERIALS


WL 97

OUTBOARD

BOTTOM OF SHELF TOP OF SHELF FORWARD

101

303

302

301

101

303

302

101

301

208

3.31.8

10.2

7.2

2PL

201

205

206

207

4PL

201

202

203

204

4PL



4.7

3.4 8.2

3.0

13.8

17.6

18.5

5.9

,

1

1

2

2

3

3

4

4

A A

B B


Christopher Malpass

Michael Freyder

Bill Pieper

2009-106.dwg

10/7/2009

10/7/2009

B 4 of 4 1/2 -

2009-106


Drawn

Revised

Checked / Approved

Filename




212RIVET (EXISTING)MS 20426-AD36

211NUTPLATE (EXISTING)MS21059-L3K3

103AFT SUPPORT RAIL

2024-T3511

.062 THK


-1031

LIST OF MATERIALS


212RIVET (EXISTING)MS 20426-AD34

211NUTPLATE (EXISTING)MS21059-L3K2

102FWD SUPPORT RAIL

2024-T3511

.09 THK EXTRUSION


-1021

LIST OF MATERIALS


3.780 4.882 4.252 1.451

16.339

.688

9.724

.984

1.181

3.937 3.937.787

-103 AFT SUPPORT RAIL (EXISTING)

-102 FWD SUPPORT RAIL (EXISTING)

1.260

2.008

211

212

3PL

211

212

2PL

X2

X2

1.144

n.190(4 PL)

n.190(3 PL)

.610



1.3005.7875.866

.688

n.190

n.1792X

(3 PL)

n.190n.179

(2 PL)

6.024 2.597

.467

.434

ICA-2009-100Date: 10/7/2009

Rev. A

A-8

APPENDIX A-8

PL-2009-100

Parts List

Doc. No. PL-2009-100Date:10/7/2009

Rev. A

Page 1 of 11

DETAILED PARTS LIST

Make: Gulfstream

GIV

STC Project No. SA6468NY-T

Doc. No. PL-2009-100Date:10/7/2009

Rev. A

Page 2 of 11

Log of Revisions

Date Revision Description By

1/9/2009 IR Initial Release MLF

10/7/2009 A Added Network Gateway MLF

Doc. No. PL-2009-100Date:10/7/2009

Rev. A

Page 3 of 11

PARTS LIST

Qty. Part Number Description Source Item# Conf # Detail

Drawing

Date

Electronic Components List

Opt 1616-450-01A Phone with tracker

feature and internal

GPS

Sky Connect 1616-050 3/24/2007

Opt 1616-450-02A Phone with Tracker

feature no internal

GPS

Sky Connect 1616-050 3/24/2007

Opt 1616-400-01A Phone only, no

tracker, no GPS

Sky Connect 1616-050 3/24/2007

Opt 1616-055-10 MMU II Sky Connect 1616-055 6/6/2008

Opt 1616-055-12 MMU II NVG Sky Connect 1616-055 6/6/2008

Opt 1616-121-00 Handset, Cordless Sky Connect 1616-121 1/9/2009

Opt 1616-200-11 Cradle, Surface

Mount

Sky Connect 1616-200-11 1/9/2009

Opt 1616-200-12 Cradle, Flush

Mount

Sky Connect 1616-200-12 1/9/2009

Opt 1616-200-13 Cradle Surface

w/Audio

Sky Connect 1616-200-13 1/9/2009

Opt 1616-200-14 Audio Interface Sky Connect 1616-200-14 1/7/2009

Opt 1616-410-00 Handset, Corded Sky Connect 1616-410-00 1/9/2009

Opt 1616-905-02 Configuration/SIM

Module

Sky Connect 1616-905-02 6/9/2006

Opt 1616-880-01 Antenna, Iridium Sky Connect 1616-880-01 6/13/2006

Opt 1616-880-04 Antenna, GPS Sky Connect 1616-880-04 6/13/2006

1 ea. 1616-880-02 Antenna, Iridium Sky Connect 1616-880-02 1/9/2009

Opt 1616-101-3X Network Gateway Sky Connect 1616-101-3X 10/7/2009

The Network Gateway has several configurations, and the same part may come from EMS

Aviation Sky Connect division or SATCOM under an alternate part number.

1616-101-30 (Alt #1233-A-0100) is a wired gateway, no wireless, with POTS interface

1616-101-31 (Alt #1233-A-0150) is a WAP, no POTS interface

1616-101-32 (Alt #1233-A-0200) is a WAP, POTS, and wired gateway

Doc. No. PL-2009-100Date:10/7/2009

Rev. A


Drawing

Date

Page 4 of 11

Transceiver Installation Parts on Drawing 2009-101

1 ea. NA Tray Adapter Local

Manufacturer

to provided

specs

101 2009-100-102 1/9/2009

20 ea. MS20426AD3 Rivet Any 201 2009-101 1/9/2009

2 ea. MS21059-L08 Nutplate Any 202 2009-101 1/9/2009



6 ea. MS21075-08 Nutplate Any 205 2009-101 1/9/2009

10 ea. MS35206-243 Screw Any 206 2009-101 1/9/2009

2 ea. MS35206-261 Screw Any 207 2009-101 1/9/2009

10 ea. NAS1149 F

N832 P

Washer Any 208 2009-101 1/9/2009

2 ea. NAS1149 F

0332 P

Washer Any 209 2009-101 1/9/2009

1 ea. M12883/53-

001

Socket, Relay Rail Any 210 2009-101 1/9/2009

1 ea. M12883/52-

002

Relay Any 211 2009-101 1/9/2009

2 ea. MS21919-XX Clamps Any 212 2009-101 1/9/2009

Opt 1616-450-02A Phone with Tracker

feature no internal

GPS

WD-2009-100 301 1616-050 3/24/2007

Opt 1616-400-01A Phone only, no

tracker, no GPS

WD-2009-100 301 1616-050 3/24/2007

Opt 1616-450-01A Phone with tracker

feature and internal

GPS

WD-2009-100 301 1616-050 3/24/2007

1 ea. 1616-105-01 Tray, Transceiver Sky Connect 302 1616-105-01 3/24/2007

Doc. No. PL-2009-100Date:10/7/2009

Rev. A


Drawing

Date

Page 5 of 11

Cradle/Base Station Installation Drawing 2009-102

AR 610-10133-

250

Honeycomb Any 104 2009-102 1/9/2009

AR 1559A/B Adhesive Any 213 2009-102 1/9/2009

1 ea. None Adapter Plate Local

Manufacturer

to provided

specs

105 2009-102 1/9/2009

1 ea. None Nutplate Retainer Local

Manufacturer

to provided

specs

106 2009-102 1/9/2009

1 ea. None Nutplate Retainer Local

Manufacturer

to provided

specs

107 2009-102 1/9/2009

8 ea. MS20426AD

3-4

Rivet Any 201 2009-102 1/9/2009

4 ea. MS24693S25 Screw Any 202 2009-102 1/9/2009

4 ea. MS24693S58 Screw Any 203 2009-102 1/9/2009

4 ea. MS35206-235 Screw Any 204 2009-102 1/9/2009

4 ea. MS24693S47 Screw Any 205 2009-102 1/9/2009





4 ea. NAS1836-06 Insert Any 210 2009-102 1/9/2009

1 ea. 1602-852-

200-1200

Retention Plate Sky Connect 211 2009-102 1/9/2009

1 ea. 1602-852-

200-1201

Retention Plate Sky Connect 212 2009-102 1/9/2009

Doc. No. PL-2009-100Date:10/7/2009

Rev. A


Drawing

Date

Page 6 of 11

OPT 1616-200-11 Cradle, Surface

Mount

Sky Connect 301 2009-102 1/9/2009

OPT 1616-200-13 Cradle, Audio Sky Connect 301 2009-102 1/9/2009

OPT 1616-200-12 Cradle, Flush

Mount

Sky Connect 301 2009-102 1/9/2009

1 ea. 1616-101-11 Base Station Sky Connect 302 2009-102 1/9/2009

Handset Installation 2009-103 Drawing Dated 1/9/2009

2 ea. MS35206-228 Screw Any 202 2009-103 1/9/2009

2 ea. NAS1149FN6

16P

Washer Any 203 2009-103 1/9/2009

1 ea. Keystone 745 Grommet Any 204 2009-103 1/9/2009

1 ea. 1616-410-00 Handset Cradle Sky Connect 301 1616-410-00 1/9/2009

OPT 1616-055-12 MMU II NVG Sky Connect 302 1616-055 3/18/2009

OPT 1616-055-10 MMU II Sky Connect 302 1616-055 3/18/2009

Doc. No. PL-2009-100Date:10/7/2009

Rev. A


Drawing

Date

Page 7 of 11

Iridium and GPS Antenna Installation Drawing 2009-104

A/R EA-9394 Hysol Any 2009-104 1/9/2009

1 ea. 2009-104-101 Doubler, Iridium Local

Manufacture

to provided

Specs

101 2009-104 1/9/2009

Opt 2009-104-102 Doubler, GPS Local

Manufacture

to provided

Specs

102 2009-104 1/9/2009

AR 209-104-102 Spacer Local

Manufacture

to provided

Specs

102 2009-104 1/9/2009

AR NAS1097AD4 Rivet Standard Part 201 2009-104 1/9/2009

AR NAS1473A3 Nutplate Standard Part 202 2009-104 1/9/2009

AR MS20426AD3 Rivet Standard Part 203 2009-104 1/9/2009

AR MS24694S68 Screw Standard Part 204 A2005-091-101 3/20/2007

1 ea. 1616-880-02 Antenna, Iridium Sky Connect 301 1616-880-02

Opt 1616-880-01 Antenna, Iridium Sky Connect 301 1616-880-01 6/13/2006

Opt 1616-880-04 Antenna, GPS Sky Connect 302 1616-880-04 6/13/2006

Doc. No. PL-2009-100Date:10/7/2009

Rev. A


Drawing

Date

Page 8 of 11

Wiring Harness Parts Drawing WD-2009-100

1 ea. 1616-400-01A Transceiver Sky Connect 02 100,

400, 500

1616-050 3/24/2007

OPT 1616-450-01A Transceiver Sky Connect 02 200,

300, 500

1616-050 3/24/2007

OPT 1616-450-02A Transceiver Sky Connect 02 200,

300, 500

1616-050 3/24/2007

1 ea. 1616-105-01 Tray, Transceiver Sky Connect 03 all 1616-105-01 6/28/2007

Opt 1616-101-11 Base Station Sky Connect 04 100,

300, 400

1616-101-11 12/16/2008

1 ea. 1616-200-11 Cradle Sky Connect 05 100, 300 1616-200-11 1/9/2009

OPT 1616-200-12 Cradle Sky Connect 05 100, 300 1616-200-11 1/9/2009

OPT 1616-200-13 Cradle Sky Connect 05 100, 300 1616-200-11 1/9/2009

OPT 1616-200-14 Cradle Sky Connect 05 400 1616-200-11 1/9/2009

Opt 1616-410-00 Handset, Corded Sky Connect 06 100, 200 WD-2009-100 10/7/2009

Opt 1616-055-10 MMU II Sky Connect 07 300 1616-055 3/18/2009

Opt 1616-055-12 MMU II Sky Connect 07 300 1616-055 3/18/2009

1 ea. 1616-700-01 Filter Sky Connect 08 all WD-2009-100 10/7/2009

Opt 1616-905-02 Configuration/SIM

Module

Sky Connect 09 all 1616-905-02 6/9/2006

1 ea. 1616-880-02 Antenna, Iridium Sky Connect 10 all 1616-880-02 1/9/2009

Opt 1616-880-01 Antenna, Iridium Sky Connect 10 all 1616-880-01 6/13/2006

Opt 1616-880-04 Antenna, GPS Sky Connect 11 all 1616-880-04 6/13/2007

1 ea. 1616-105-02 Connector, 62 pin

female

Sky Connect 12 all WD-2009-100 10/7/2009

1 ea. 1616-720-02 Hood, 25 pin

connector

Sky Connect 13 all WD-2009-100 10/7/2009

1 ea. 1616-900-34 Kit, Install Sky Connect 14 100,

300, 400

WD-2009-100 10/7/2009

Doc. No. PL-2009-100Date:10/7/2009

Rev. A


Drawing

Date

Page 9 of 11

3 ea.

4 ea.

1616-720-04 Connector Sky Connect 15 200, 400

100, 300

WD-2009-100 10/7/2009

2 ea.

2 ea.

3 ea.

1616-720-05 Connector Sky Connect 16 100, 200

400

300

WD-2009-100 10/7/2009

1 ea. 1616-720-08 Connector Sky Connect 17 100,

300, 400

WD-2009-100 10/7/2009

AR 1616-721-02 Contact Sky Connect 18 all WD-2009-100 10/7/2009

AR 1616-721-04 Contact Sky Connect 19 all WD-2009-100 10/7/2009

1 ea. 1616-722-02 Hood Sky Connect 20 all WD-2009-100 10/7/2009

2 ea. DE24657 Hood Canon 21 300 WD-2009-100 10/7/2009

5 ea.

6 ea.

7 ea.

1616-722-04 Hood Sky Connect 22 200, 400

100

300

WD-2009-100 10/7/2009

1 ea. 1616-722-08 Hood Sky Connect 23 100, 300

400

WD-2009-100 10/7/2009

1 ea. D20418 Female Screwlock Canon 24 100, 200

400

WD-2009-100 10/7/2009

2 ea. 300

1 ea. D20419 Male Screwlock Canon 25 100, 200

400

WD-2009-100 10/7/2009

2 ea. 300

1 ea. 466-SO45 Annunciator/

Switch

Eaton 26 all WD-2009-100 10/7/2009

Opt MS25098-22 Switch Any 26 all WD-2009-100 10/7/2009

1 ea. M83636/6-

025M

Relay Any 27 all WD-2009-100 10/7/2009

1 ea. M12883/52-

002

Socket Any 28 all WD-2009-100 10/7/2009

Doc. No. PL-2009-100Date:10/7/2009

Rev. A


Drawing

Date

Page 10 of 11

1 ea. 7274-11-2 Circuit Breaker Klixon 29 100, 300

400

WD-2009-100 10/7/2009

1 ea. 7274-11-3 Circuit Breaker Klixon 30 all WD-2009-100 10/7/2009

1 ea. M12883/53-

001

Rail Any 31 all WD-2009-100 10/7/2009

1 ea. 1N4007 Diode TI 32 all WD-2009-100 10/7/2009

AR RG400 Coax Any 33 all WD-2009-100 10/7/2009

1 ea. NA Label “Handset” Any - Local

manufacturer

34 100, 300

400

WD-2009-100 10/7/2009

1 ea. NA Label “SATCOM” Any - Local

manufacturer

35 all WD-2009-100 10/7/2009

5 ea. 31-4452 Connector, TNC Amphenol 36 all WD-2009-100 10/7/2009

1 ea. 31-4427 Connector, BNC Amphenol 37 all WD-2009-100 10/7/2009

1 ea. MS25041-1 PTT Indicator Any 38 400 WD-2009-100 10/7/2009

1 ea. 28519-327 Lamp GE 39 400 WD-2009-100 10/7/2009

1 ea. NA Label “Off Hook” Any - Local

manufacturer

40 400 WD-2009-100 10/7/2009

1 ea. NA Label “Sky

Connect Relay”

Any - Local

manufacturer

41 all WD-2009-100 10/7/2009

1 ea. M641/5-1 Mic Jack Any 42 300, 400 WD-2009-100 10/7/2009

1 ea. M641/6-1 Phone Jack Any 43 300, 400 WD-2009-100 10/7/2009

Opt 1616-101-31 Network Gateway Sky Connect 44 500 WD-2009-100 10/7/2009

Opt 1616-885-

00/01

Duplexer Sky Connect 45 500 WD-2009-100 10/7/2009

Opt DB2-5370 Connector, Coax N Amphenal 46 500 WD-2009-100 10/7/2009

1 ea. 1616-720-48 Connector Sky Connect 47 500 WD-2009-100 10/7/2009

1 ea. 1616-720-50 Connector Sky Connect 48 500 WD-2009-100 10/7/2009

Doc. No. PL-2009-100Date:10/7/2009

Rev. A


Drawing

Date

Page 11 of 11

Opt Installer

Supplied

Switch Any 49 500 WD-2009-100 10/7/2009

1 ea. 1616-610-34 Cable Sky Connect 50 500 WD-2009-100 10/7/2009

Network Gateway Installation Drawing 2009-106

- EA 9309.3NA Adhesive Any 201 500 2009-106 10/7/2009

4 ea. NAS 1836-3-

12

Insert Any 202 500 2009-106 10/7/2009

4 ea. MIL 51958-61 Screw Any 203 500 2009-106 10/7/2009

4 ea. NAS1149-

D0363J

Washer Any 204 500 2009-106 10/7/2009

Opt NAS 1836-06-

12

Insert Any 205 500 2009-106 10/7/2009

Opt MIL 51957-38 Screw Any 206 500 2009-106 10/7/2009

Opt NAS1149-

CN616R

Washer Any 207 500 2009-106 10/7/2009

2 ea. MS21919 Clamp Any 208 500 2009-106 10/7/2009

1 ea. 1616-101-3X Gateway Sky Connect 301 500 2009-106 10/7/2009

Opt 1616-4X0-

0XA

Transceiver Sky Connect 302 500 2009-106 10/7/2009

Opt 1616-105-01 Tray Sky Connect 303 500 2009-106 10/7/2009

Sky Connect LLC...ICA-2009-100 Date: 10/7/2009 Rev. A 2 1.2 List of Applicable Publications Any...

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Transcript of Sky Connect LLC...ICA-2009-100 Date: 10/7/2009 Rev. A 2 1.2 List of Applicable Publications Any...