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EMS Sky Connect Series, Руководство по установке

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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

 

1616-880-13.dwg

4/5/2010

 

4/5/2010

 

B

1  of 1 

1:1

IR

1616-880-13

Iridium/GPS Antenna

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°

GENERAL SPECIFICATIONS:

WEIGHT:    7.84oz

MATERIAL:    6061-T6 ALUMINUM

ALTITUDE:    70,000'

OPERATING TEMP:    -67°F TO 185°F

IRIDIUM SPECIFICATIONS:

FREQUENCY:    1616MHz
POLARIZATION:    RHCP

ANTENNA GAIN:    5.0dB @ ZENITH
VSWR:    <1.5:1

POWER HANDLING:    30W

GPS SPECIFICATIONS:

FREQUENCY:    1575.42MHz
POLARIZATION:    RHCP

ANTENNA GAIN:    4.6dB @ ZENITH
VSWR:    <1.5:1

POWER HANDLING:    1W

REVISION HISTORY

REV

ECO

DESCRIPTION

DATE

APPROVED

IR

N/A

Initial Release

4/5/2010

MLF

5.026

2.200

.800

2.119

4X 

n

.201 THRU

wn

.385 X 100°

FOR 10-32 MOUNTING SCREWS

.143

.937

.784

.148

.572

.406

.721

R6.0

S

O-RING

GPS: TNC FEMALE (BLUE)

IRIDIUM: TNC FEMALE (RED)

Содержание Sky Connect Series

Страница 1: ...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 i ...

Страница 2: ...ered 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...

Страница 3: ...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 MM...

Страница 4: ...1616 964 12 Date 7 27 2011 Rev 2 1 APPENDIX A Troubleshooting 5 1 INSTALLATION AND SYSTEMS DRAWINGS 7 1 iv ...

Страница 5: ... 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...

Страница 6: ...ial 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 vi ...

Страница 7: ...ct 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 ...

Страница 8: ...1616 964 12 Date 7 27 2011 Rev 2 1 Figure 1 Tracker Communication Concept Drawing 1 2 ...

Страница 9: ...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...

Страница 10: ...r 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 1 4 ...

Страница 11: ...5 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 1 5 ...

Страница 12: ... 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 1 6 ...

Страница 13: ...eg 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 1...

Страница 14: ...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 ...

Страница 15: ...ion 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 PLACEMEN...

Страница 16: ... 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 ...

Страница 17: ...cker 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 inpu...

Страница 18: ...ect 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 ...

Страница 19: ... 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 perso...

Страница 20: ...1616 964 12 Date 7 27 2011 Rev 2 1 This page intentionally left blank 2 6 ...

Страница 21: ...e installation testing In the event that the customer provides a SIM card or desires to provide the card it must be de pinned or the system will get blocked Contact the manufacturer if you intend to change SIM cards Sky Connect recommends against customer replacement of SIM cards as it affects unit serviceability Until the Iridium L Band Transceiver has been registered on the network there is very...

Страница 22: ...c If installing a Tracker without the control head ie FlightDeck system with a Tracker and panel mounted switches are desired we offer the following manufacturer part numbers with and without LEDs with and without NVIS non NVIS part numbers are not shown call Vivisun Vivisun LED 42 15 KB 36185 2LA EMER 3S0 Emergency Switch Vivisun LED 40 18 KB 36189 2LA CODE 3J0 Code Switch Vivisun LED 42 12 KB 36...

Страница 23: ...coax connectors and tools customer supplied Table 2 Connector Coax Tool Newark Industrial BNC male RG400 RG142 CTL 1 89F2891 31 4427 BNC male 90 Deg RG400 RG142 CTL 1 39F1443 31 334 TNC female RG400 RG142 220045 2 96F7801 225551 6 TNC female bulkhead RG400 RG142 220045 2 97F8562 225557 6 TNC male RG400 RG142 CTL 1 92B0647 31 4452 TNC male 90deg RG400 RG142 220045 2 90B4658 225554 6 3 3 ...

Страница 24: ...sist of 1 1616 720 07 DD62F00000 Positronics connector 2 1616 721 01 FC8022D Positronics contacts 3 1616 722 06 D37000Z00 Positronics hood 3 5 SYSTEM COMPONENTS THAT APPLY ONLY TO TRACKER Table 4 Description And Part Number Components Product Tracker and Tracker with voice 1616 050 0XA 01A Tracker with GPS no voice 02A Tracker no GPS no voice 03A Tracker with voice and GPS 04A Tracker with voice a...

Страница 25: ...ent Unit 1616 055 00 MMU 1616 055 02 MMU NVG lense 1616 055 10 MMU II 1616 055 11 MMU II without POTS audio no Wi Fi 1616 055 12 MMU II NVG lense 1616 055 13 MMU II NVG lense without POTS audio no Wi Fi Originally the 11 13 part numbers did not exist They were marked as Mod A without the POTS interface and Mod B without Wi Fi ALL MMU IIs ORDERED TO BE USED WITH A 1616 050 SHOULD BE A NON POTS 1616...

Страница 26: ...sition as the Inmarsat transmitting antenna array is electrically steer able depending on azimuth to satellite Inmarsat will disrupt Iridium communications whenever active Inmarsat should be disabled when Iridium is in use alternatively filters are available for Inmarsat systems which essentially act as an Iridium bandpass filter Consult Sky Connect for more information The antenna should be mount...

Страница 27: ...hart as an aid to determine the appropriate cable type for your required installed length Follow industry practices when assembling the TNC connectors RG 142 coax cable is recommended in installations up to 20 feet in length alternative cable types are listed below Pre assembled cable lengths are available from EMTEQ ECS and PIC Table 5 Cable Length EMTEQ ECS PIC 15 feet PFLX195 100 352001 S33141 ...

Страница 28: ...e avionics shelf using approved 6 hardware until the tray was changed to Mod level A which requires 8 hardware Please check the Mod Status on the tray prior to installation to assure you use the correct hardware Tray Mod Level Hardware to be used none 6 32 screw holes are provided if required these may be drilled oversize to accommodate 8 32 screws A 8 32 screw holes are provided If replacing this...

Страница 29: ...re deemed appropriate to the aircraft type by the governing aviation regulatory agency See the appropriate following Sections for the schematics of your system for wiring examples See Table 1 above for recommendations of discreet switches to be installed when not installing a Sky Connect control head with internal switches Note Sky Connect telephony systems are generally considered non essential a...

Страница 30: ...d Out 16 Annunciator 2 Sinks 100ma to Ground Out 17 Annunciator 3 Sinks 100ma to Ground Out 18 Annunciator 4 Sinks 100ma to Ground Out 19 Configure SDA 20 Event switch 1 Gnd Active In 21 11 33VDC positive voltage input In 22 Ground Input Gnd 23 No Connection 24 Program TX Factory Use Do Not Connect 25 DPL Downlink Out 26 DPL Enable Out 27 PC CTS Data Connections only Out 28 Configure SCL In 29 Com...

Страница 31: ...rogram md1 Factory Use Do Not Connect 54 Program RST Factory Use Do Not Connect 55 Event switch 8 Gnd Active configuration switch style mom alt dial sqt In 56 Event switch 7 same as pin 55 In 57 Event switch 6 same as pin 55 In 58 Event switch 5 same as pin 55 In 59 Event switch 4 same as pin 55 In 60 Event switch 3 same as pin 55 In 61 Event switch 2 same as pin 55 In 62 11 33VDC positive voltage...

Страница 32: ...LO 6 7 Unit ID 1 7 8 Unit ID 2 8 9 Unit ID 4 9 10 Unit ID 8 10 11 Spare I O 1 11 12 Ground 12 13 Ground 13 14 Spare I O 2 14 15 Message Alert 15 16 Incoming Call 16 17 DTR Out 17 18 Ground 18 19 DSR In 19 20 Ground 20 21 5V Dimmer Input 21 22 14V Dimmer Input 22 23 28V Dimmer Input 23 24 MMU RS232 Input RX 24 25 MMU RS232 Output TX 25 3 6 7 Outline Drawings of Equipment See the appendix for drawin...

Страница 33: ... a PC via straight PC cable for system configuration The purpose of the module is to alleviate the need to reprogram to an individual aircraft if units are shifted amongst the fleet Removal and replacement of the Sky Connect Transceiver with a different unit will keep the Users stored settings the same though a tail number to serial number configuration mismatch will be logged as a security proced...

Страница 34: ...ws for the swapping of the unit and the SIM card to remain with the aircraft No changes to the aircraft s phone number A secondary advantage would be if the customer changed voice providers the ICSM could be opened and the card installed eliminating maintenance to the transceiver itself NOTE While the 9 pin female connector on the ICM ICSM is designed to be connected directly to a PC for programmi...

Страница 35: ...eparate or together 4 1 5 MMU II Mission Management Unit This unit is a computer controlled dialer and is very flexible in operation It communicates with the transceiver over an RS 232 port This unit can be programmed in the aircraft with new message sets There are several versions of the MMU II but the basic operation of all of them are the same See the operators manual for a complete description...

Страница 36: ...1616 964 12 Date 7 27 2011 Rev 2 1 Figure 10 MMU II Figure 11 MMU 4 4 ...

Страница 37: ...of 5 5 4 3 TRACKER WIRING Follow the installation drawing 1616 910 XX for the interconnection of the Tracker system into the aircraft As always pay close attention to the notes that apply to that drawing Wiring of the Tracker system is mission specific Tracker can be entirely standalone or tied to multiple aircraft systems The Tracker system is designed to be extremely flexible with open architect...

Страница 38: ...it will illuminate to full brightness for day light use This is designed for aircraft that loose dimmer voltage when the dimmer is turned off S N 101 and later due to a change in the display the only dimming allowed is through the face plate knob and menu MMU and MMU II P1 are wired identical with the exception listed above on the dimmer MMU II also dims through a menu using the knob MMU II P2 is ...

Страница 39: ...f the tracker software as a portion of the POST power on self test B Indicate the condition of the tracker Steady light with a flicker on the report interval Or flash an SOS pattern when the tracker is seeing a problem condition Annunciator 2 This light will indicate by flashing an incoming call or flash with the ring of an out going call Once the call is picked up or answered this output remains ...

Страница 40: ...done in advance of the installation testing 4 4 1 MMU II CONFIGURATION Entering Installer Configuration mode is one CCW pushed in detent of the rotary knob while pressing the key from either the Ready page or from the initial MMU splash display page The following parameters may be set in Configuration mode 4 4 1 1 Config Version Internal use for informational purposes This description is valid for...

Страница 41: ...er bus 4 4 1 6 Sensor Dimmer High End This value aligns with the dimmer bus voltage or light sensor for the brightest setting of the display and keypad brightness For the light sensor this value is in LUX only appears when brightness control on light sensor or dimmer bus 4 4 1 7 Dial In call Mechanism Determines the handling of the messenger port as well as the mechanism used for establishing phon...

Страница 42: ...407 works for most applications To determine the duration in seconds multiply the value by 246 uSecs For example the default value of 407 times 246 uSecs is 0 1 second only appears when Dial In call mechanism enables DTMF 4 4 1 10 DTMF Output Volume The volume level of DTMF PWM digit tones a value from 0 to 127 Default value is 30 4 4 1 11 Phones Volume The volume level of the phones a value from ...

Страница 43: ...from Configuration mode push n turn the knob one detent to Exit Settings Mode and then tap the knob back to the MMU Ready display A mechanism known as pocket config is available to change volumes and levels while in call To enable pocket config you must first enter Configuration mode and then exit Configuration mode it does not matter if any settings are changed only that you were at one time in t...

Страница 44: ...at is a function of the RS232 control line and not implemented as part of this feature yet Full operation of the MMU II in a master slave relationship will require implementation of the RS485 control bus This is not yet released and when it is all slaves will function as the master does in an installation To configure two MMU IIs to communicate over POTS line with one transceiver follow the below ...

Страница 45: ... display is set at DTMF DTMF M6 If not TAB the knob and the selection will begin to flash M7 Rotate the knob until the DTMF DTMF is displayed Press the knob and hold The screen will display Value Saved SUCCESS M8 Rotate the Knob do not press in clockwise until the Volume Tap appears M9 If required TAP knob and select Offhook KeyIn M10 Press the knob and hold The screen will display Value Saved SUC...

Страница 46: ...ction will begin to flash S6 Rotate the knob until the Pots NoTrkr is displayed S7 Press the knob and hold The screen will display Value Saved SUCCESS S8 Rotate the Knob do not press in clockwise until the Volume Tap page appears S9 The display probably is set at NOT ENABLED S10 Press the knob in and release The selection will begin to flash S11 Rotate the knob until the selection Offhook displaye...

Страница 47: ...lay Incoming Call T4 On the Slave MMU II Controller press the knob to answer the call The Call should be answered after a slight delay and the Call Connected Duration screen appears and the timer starts and the external CALL annunciator if installed illuminates steady T5 Mic and Phone audio should be available to the Slave MMU II Controller T6 Press the knob to end the test call T7 Initiate a call...

Страница 48: ... B Wi Fi port on the MMU II if so equipped The MSet Mange software has provisions to select either of the above options The best way to load a MSet into the MMU II is through the connector P J19 as shown in the installation drawings This is a pigtail that is to be provided to the customer so the MSet can be loaded without removing the MMU II from the aircraft Please make sure this connector is pro...

Страница 49: ...staller can be assured that their portion of the job is acceptable if the onboard unit consistently indicates that it is sending and completing messages 6 or 11 position dialer this is indicated by a fast pulse as messages are sent at programmed intervals followed by a solid green indication It is the customer s responsibility to choose the manner in which they display their tracked aircraft not t...

Страница 50: ... Tracker Setup program is terminated From the main page you can verify the G P S position speed and altitude The units IMEI 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 p...

Страница 51: ...le The Tracker utilizes Short Burst Messaging over the Iridium network to send this flight information packet to ground terminals for the monitoring of fleet aircraft Regular reporting intervals of twelve seconds to greater than 30 minutes can be set for the triggering of a flight information packet Three separate rates can be selected based on flight status In addition to interval reporting chang...

Страница 52: ...amp can be used to trigger an event report from the Tracker Relays may be used to isolate required systems from non required or simply diodes The options and variation here are far too complex and vary to cover all of them in a STC project This type of interface will have to be approved by your local airworthiness authority and NOT from this manual as it is only intended to be offered as a guide a...

Страница 53: ...1 and 2 are the VHF Transceivers When a call is initiated Comm 3 is selected and communications happen as they would on a phone without the need to push to talk Meanwhile the pilot is still able to monitor his on board radios and if necessary key the Mic to allow conversations on the VHF Transceiver In a half duplex audio panel keying on any transceiver line will cause the muting of all other sour...

Страница 54: ...es with the transceiver over an RS 232 port This is a three wire port The MMU II is fully user configurable and offers a great deal of flexibility to the system The MMU II was designed to replace our legacy SOP Dialer to enhance the functions offered to the SOP System The MMU II can store a great number of phone numbers with an alpha identifier to better detail who you are dialing The MMU II provi...

Страница 55: ...Load uses the RS 232 port to update the internal software as well as load new message sets into the MMU MMU II uses the Mset Manager to load the MSet The MMU II does not contain the switches found on the legacy SOP Dialer but those switches are offered by part number for parties interested in installing them as an option With MMU II the switches are wired to the Transceiver The MMU II supports dri...

Страница 56: ...iver and the Iridium component internal to the transceiver should be Trkr 4 X and ISOX00X This indicates that the MMU and the transceiver can communicate Next the MMU displays waiting system registation at this point the transceiver is attempting to register with the Iridium satellites checking signal strength and activation of that SIM card If you never get past this message the transceiver is no...

Страница 57: ...y connected to the Tracker Setup Program or the diagnostic port If a separate Data connector 9 wire for PC calls has been installed check shielding of the cable You may need to install an Icarus Instruments data feed through connector Contact Technical Support After running the Tracker Setup software the boxes in the window do not populate Make sure that you waited the full 2 minutes to allow the ...

Страница 58: ...rogram Verify unit is outside clear of obstructions hangars Verify customers service plan is fully activated with Service provider Verify that Inmarsat system if on aircraft is deactivated or properly filtered Verify cable length and type is appropriate to achieve not more than 3dB loss at 1 6 GHz Check antenna placement on aircraft to be free of obstructions or shadowing Verify SIM Card PIN is de...

Страница 59: ...use the MMU should display the Tracker Transceiver software and the software in the LBT This would be at least V4 7 and ISO6004 4 MMU should display Ready and the signal strength If you don t see the MMU version the MMU has failed If you do not see the transceiver version the communication between the MMU and the transceiver has failed Check wiring between the MMU and Transceiver in the later case...

Страница 60: ...nect aero under the support tab and the manuals and guides link ICAs are provided for the various STCs Sky Connect holds on its products These ICAs may be used as reference material to develop your own ICA for an installation not covered by one of the STCs If you require assistance with certification issues please call Technical Services group at 985 863 0954 6 1 ...

Страница 61: ...d as a suggestion on how the system could be installed If you have any question on installation methods or techniques please call Technical Services Electrical Interface of Components Tray 1616 105 01 Antennas 1616 880 00 Iridium 1616 880 01 Iridium 1616 880 02 Iridium 1616 880 04 GPS 1616 880 13 Combo Iridium GPS 7 1 ...

Страница 62: ...9 HOOD 25 SKY CONNECT CINCH 1 17 1616 725 25 D25000JVL0 HOOD 25 WITH VIBRATION LOCK SKY CONNECT POSITRONICS 1 16 1616 720 01 M24308 2 2F D SUB CONNECTOR 15 F SKY CONNECT CINCH 1 2 1 15 1616 720 04 M24308 2 1F D SUB CONNECTOR 9 F SKY CONNECT CINCH 1 2 1 14 1616 720 05 M24308 4 1F D SUB CONNECTOR 9 M SKY CONNECT CINCH 1 2 1 13 1616 720 02 M24308 2 3F D SUB CONNECTOR 25 F SKY CONNECT CINCH 1 1 1 12 1...

Страница 63: ...G DATA OUT CONFIG GND CONFIG PWR CONFIG SCL CONFIG SDA DPL POWER DPL GND DPL Rx DPL Tx CONFIGURATION MODULE SKY60A22S W SKY60A22S B SKY60A22S O SKY62A22S W SKY62A22S B SKY62A22S O SKY61A22S W SKY61A22S B SKY65A22S W SKY65A22S B SKY64B22S W SKY64B22S B SKY64B22S O 2 3 5 PJ20 P10 JP9 19 Diagnostic Connector 47 49 30 CONFIG DATA OUT CONFIG DATA IN CONFIG GND 13 SHIELD 2 3 5 P10 Diagnostic Connector O...

Страница 64: ...Y60A22S W SKY60A22S B SKY60A22S O SKY62A22S W SKY62A22S B SKY62A22S O SKY61A22S W SKY61A22S B SKY65A22S W SKY65A22S B SKY64B22S W SKY64B22S B SKY64B22S O 2 3 5 PJ20 P10 JP9 19 Diagnostic Connector 47 49 30 CONFIG DATA OUT CONFIG DATA IN CONFIG GND SKY64A22 W SKY64A22 B SKY64A22 O 13 SHIELD 2 3 5 P10 Diagnostic Connector OR 22 18 23 13 20 22 14 21 20 15 24 23 05 21 20 15 23 01 02 12 GPS DATA FROM G...

Страница 65: ...0 56 TO DIMMER BUSS 12 SKY7A22 EVENT SWITCH 2 EVENT SWITCH 3 EVENT SWITCH 4 EVENT SWITCH 5 EVENT SWITCH 7 EVENT SWITCH 8 EVENT SWITCH 1 29 7 3 AUDIO HI MIC HI COMM LO SKY2A22S W SKY3A22S W N A FOR 1616 050 01A AND 1616 050 02A SKY2A22S B SKY3A22S B 22 19 16 23 COM 3 PHONE HI COM 3 PHONE LO COM 3 MIC HI COM 3 MIC LO AUDIO SHIELD AUDIO PANEL EXISTING 01 02 12 29 1 3 4 47 49 30 12 28 19 26 9 4 25 11 ...

Страница 66: ...ing but not limited to quotation in part without written consent of Sky Connect is expressly forbidden Wesley Hastings Wesley Hastings Michael Freyder 1616 105 01 dwg 4 13 2007 7 14 2010 7 14 2010 B 1 of 1 1 1 C 1616 105 01 Tray Transceiver Mounting Drawn Revised Checked Approved Filename DER Review Drawing Number Size Sheet Scale Rev All dimensions are in inches unless otherwise specified Dimensi...

Страница 67: ...fied x x 05 x xx 01 x xxx 005 x 2 1 900 1 900 R10 00 S 810 650 R 50 600 SPECIFICATIONS FREQUENCY 1595 30 MHz 1 5 dB BAND WIDTH POLARIZATION RIGHT HAND CIRCULAR AXIAL RATIO 3 0dB MAX RADIATION COVERAGE 4 0 dBic θ 0 1 0 dBic 0 θ 75 2 5 dBic 75 θ 80 4 5 dBic 80 θ 85 7 5 dBic θ 90 IMPEDANCE 50 OHMS VSWR 2 0 1 CONNECTOR TNC TYPE FEMALE WEIGHT 8 0 oz MAX MATERIAL BASE A380 ALUMINUM ALLOY CASTING RADOME ...

Страница 68: ......

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Страница 70: ...ied 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 GENERAL SPECIFICATIONS WEIGHT 7 84oz MATERIAL 6061 T6 ALUMINUM ALTITUDE 70 000 OPERATING TEMP 67 F TO 185 F IRIDIUM SPECIFICATIONS FREQUENCY 1616MHz POLARIZATION RHCP ANTENNA GAI...

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