FreeFlight 2101 I/O PLUS Installation And Checkout Manual Download Page 109

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Page C-5

Revision E
May 31, 2006

FreeFlight 2101 I/O Approach Plus GPS Navigation System

C.1.4.4

GNS (Reserved for use with Honeywell Satellite Landing System)

PORT 1 (J2-9 and 15) – Software version 241C and later
PORT 3 (J2-61 and 62) –Software version 241C and later

LABEL

PARAMETER

FORMAT

INPUT

033

TDS Label-SLS Tuning

429

101

GNS HDOP

429

102

GNS VDOP

429

110

GNS Latitude

429

111

GNS Longitude

429

232

TDS label - airport identifier

429

242

TDS label - airport /station identifier

429

243

TDS label - procdure selection

429

244

TDS label - station

429

270

VDL status

429

273

GNS Status

429

355

GNS Maintenance

429

C.1.4.5

RADAR

PORT 2 (J2-60 and 59) – Software version 241C and later
PORT 4 (J2-64 and 63) – Software version 241C and later
PORT 3 (J2-61 and 62) – Software version 241B and earlier

LABEL

PARAMETER

FORMAT

INPUT

324-347

WPT Lat/Lon

429 BNR

Summary of Contents for 2101 I/O PLUS

Page 1: ...INSTALLATION AND CHECKOUT MANUAL Publication Number 82882 FreeFlight 2101 I O Approach Plus GPS Navigation System FreeFlight S Y S T E M S ...

Page 2: ......

Page 3: ...INSTALLATION AND CHECKOUT MANUAL Publication Number 82882 Revision E May 31 2006 FreeFlight 2101 I O Approach Plus GPS Navigation System ...

Page 4: ...ication or any portion thereof by any means without the express written permission of FREEFLIGHT SYSTEMS is prohibited For further information contact Manager Technical Publications FREEFLIGHT SYSTEMS 3700 Interstate 35 S Waco Texas 76706 3756 USA Telephone 1 254 662 0000 ...

Page 5: ...tents iii May 31 2006 Section I General Information 1 1 1 3 1 6 May 31 2006 1 8 1 9 May 31 2006 Section II Installation 2 1 2 6 May 31 2006 2 29 30 May 31 2006 Section III Checkout 3 3 3 16 May 31 2006 Appendix C External Inputs and Outputs C 11 C 13 C 15 May 31 2006 Dates of Original and Change pages are Revision A February 28 1997 Revision B July 14 1997 Revision C April 30 1998 Revision D May 7...

Page 6: ... Revision E May 31 2006 FreeFlight 2101 I O Approach Plus GPS Navigation System Assigned To Job Title Location RECORD OF REVISIONS Rev Revision Insertion Rev Revision Insertion By By No Date Date No Date Date ...

Page 7: ...lation Kit 1 7 1 5 ACCESSORIES NOT SUPPLIED 1 8 1 5 1 Installation 1 8 1 5 2 GPS Cable Requirements 1 8 SECTION II Installation 2 1 GENERAL 2 1 2 2 UNPACKING AND INSPECTING EQUIPMENT 2 1 2 2 1 Physical Inspection 2 1 2 2 2 Electrical Inspection 2 1 2 3 EQUIPMENT INSTALLATION 2 1 2 3 1 Cooling Considerations 2 1 2 3 2 Harness and Cable Fabrication 2 1 2 3 3 GPS Antenna Installation 2 2 2 3 4 Receiv...

Page 8: ...ight 2101 I O Approach Plus Installation Drawing 2 15 2 7 System Inputs 2 17 2 8 System Outputs 2 18 2 9 OLEO Inputs 2 19 2 10 CDI HSI Interconnection 2 20 2 11 Typical System Interconnection 2 21 2 12 Serial Port Input Connections 2 27 2 13 Serial Port Output Connections 2 29 2 14 Bipolar Serial Port Interconnections 2 31 LIST OF TABLES 3 1 AUX I O Configuration 3 3 3 2 ARINC 419 429 Receiver Por...

Page 9: ... 4 B 5 4 Air Data Computer Format B 5 B 6 TRANSMIT PORTS B 7 B 6 1 Configuration B 7 B 6 2 R0 and R1 Data Formats B 7 B 6 3 K0 and K1 Data Formats B 10 B 6 4 X0 and X1 Formats B 13 B 6 5 Data Output Format Example B 17 APPENDIX C External Inputs and Outputs C 1 EXTERNAL INPUTS C 1 C 1 1 Speed Inputs C 1 C 1 2 Heading Input C 3 C 1 3 Discrete Inputs C 3 C 1 4 Digital Data Inputs C 4 C 2 SYSTEM OUTP...

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Page 11: ...FreeFlight 2101 I O Approach Plus GPS Navigation System SECTION I GENERAL INFORMATION ...

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Page 13: ... Display Unit 1 2 1 2 2 GPS Antenna 1 3 1 3 TECHNICAL CHARACTERISTICS 1 4 1 3 1 Receiver Display Units P N 81440 XX 1 4 1 3 2 GPS Antenna P N 81194 1 5 1 3 3 GPS Antenna P N 16248 11 alternate 1 6 1 4 PARTS AND EQUIPMENT 1 7 1 4 1 FreeFlight 2101 I O Approach GPS Receiver Display Unit 1 7 1 4 2 Installation Kit 1 7 1 5 ACCESSORIES NOT SUPPLIED 1 8 1 5 1 Installation 1 8 1 5 2 GPS Cable Requirement...

Page 14: ...Page 1 ii Revision E May 31 2006 FreeFlight 2101 I O Plus Approach GPS Navigation System THIS PAGE INTENTIONALLY LEFT BLANK ...

Page 15: ...mounted unit Each system comprises receivers and antennas to perform specified functions The Jeppesen database cards provide up to date information about airports and other navigation aids around the world The FreeFlight 2101 I O Approach Plus GPS System comprises one Dzus mounted Receiver Display Unit RDU containing a GPS Receiver 12 channel one GPS Antenna Preamp and applicable installation hard...

Page 16: ...sory messages The annunciator lights are the Message MSG Hold HLD Parallel Track PTK Approach APR and Waypoint Alert WPT C Push Button Keys Nine push button keys are used for mode selection and data entry The keys are described as follows Access Navigation Mode Displays enroute navigation information AccessWaypointMode Allowspilottovieworselectairports SIDs STARs Approaches VORs NDBs Intersections...

Page 17: ...itable for use by most CDIs B Annunciator Outputs The external annunciator lights alert the pilot of warning and advisory messages The annunciator lights are Message MSG Hold HLD Waypoint Alert WPT and Approach APR C Serial Inputs Outputs The RDU provides two serial input ports and two serial output ports for general use Data formats are software selectable D Digital Inputs Outputs The RDU provide...

Page 18: ...CITY 800 knots MOUNTING Dzus Rail POWER REQUIREMENTS 1 5 A 28 Vdc Complies with USA export requirements ExternalInterfaces TYPE I O NO PARAMETER Synchro Input 4 TAS HDG Altitude 2 Voltage Ratio Input 1 TAS ARINC 429 Input 4 High or Low Speed Discrete Input 9 Various including Spares Synchro Output 3 Programmable Synchro Resolver Output Autopilot Output 1 Roll Sum Steering Analog Deviation Output 3...

Page 19: ...vailability not implemented 1 3 2 GPS Antenna P N 81194 TSO COMPLIANCE C129 C144 ENVIRONMENTAL COMPLIANCE See Appendix A PHYSICAL DIMENSIONS Height 0 60 in 1 52 cm Width 3 00 in 7 62 cm Length 4 70 in 11 94 cm WEIGHT 0 375 lb 0 17 kg TEMPERATURE 55 C to 85 C ALTITUDE RANGE 100 ft to 55 000 ft MOUNTING External POWER REQUIREMENTS 5 Vdc 40 mA max from RDU SPEED RATING 1300 knots IAS CONNECTOR TNC Us...

Page 20: ...dix A PHYSICAL DIMENSIONS Height 0 80 in 2 0 cm Width 3 75 in 9 53 cm Length 4 00 in 10 16 cm WEIGHT 0 5 lb 0 23 kg TEMPERATURE 55 C to 70 C ALTITUDE RANGE 1000 ft to 55 000 ft MOUNTING External POWER REQUIREMENTS 5 Vdc 80 mA from RDU SPEED RATING 800 knots IAS CONNECTOR TNC Installations utilizing this antenna are limited to aircraft not equipped with Satellite Communications equipment ...

Page 21: ...valent parts without prior notice The contents are listed below P N DESCRIPTION QTY 81448 20 21 81194 GPS Antenna ARINC 743 Hi Speed 1 16248 11 GPS Antenna Preamp 1 80116 Antenna Mounting Gasket 1 16940 NavData Information and Subscription 1 1 80252 37 Pin Connector w pins 1 1 Note 1 80254 66 pin Connector w pins 1 1 Note 1 24633 0016 Connector Backshell 90 37 pin 1 1 25039 0001 Connector Backshel...

Page 22: ...navigation warning flag The display on the 2101 I O is not intended as the primary navigation display however NAV flag triggering capability is available using digital and discrete outputs identified elsewhere in this document 1 5 2 GPSCableRequirements The GPS antenna cable is to be supplied or fabricated by the installation agency to meet the following requirements Insertion Loss 10 dB 1 575 GHz...

Page 23: ...arts for use with RG 393 cable are available from FreeFlight TPN DESCRIPTION QTY VENDOR P N One or two of the following 26479 0495 TNC straight 1 or 2 Amp 1 225550 3 or 26479 0494 Connector RF TNC 90 2 Amp 1 225554 1 Use Crimp Tool AMP P N 220015 1 or DMC P N M22520 5 01 with Die Set DMC P N M22520 5 25 ...

Page 24: ...Page 1 10 Revision E May 31 2006 FreeFlight 2101 I O Approach Plus GPS Navigation System THIS PAGE INTENTIONALLY LEFT BLANK ...

Page 25: ...FreeFlight 2101 I O Approach Plus GPS Navigation System SECTION II INSTALLATION ...

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Page 27: ...OF FIGURES 2 1 FreeFlight 2101 I O Approach Plus J1 37 Pin Pin out 2 6 2 2 FreeFlight 2101 I O Approach Plus J2 66 Pin Pin out 2 7 2 3 GPS Antenna Cable and Connector 2 9 2 4 ARINC 743 Hi Speed GPS Antenna P N 81194 Installation Drawing 2 11 2 5 GPS Antenna P N 16248 11 Installation Drawing alternate 2 13 2 6 FreeFlight 2101 I O Approach Plus Installation Drawing 2 15 2 7 System Inputs 2 17 2 8 Sy...

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Page 29: ...le each individual unit may or may not require forced air cooling the combined heat load of several units operating in a typical avionics location will significantly degrade the reliability of avionics if provisions for cooling are not incorporated in the initial installation Failure to provide cooling will certainly lead to increased avionics maintenance costs and may void the FreeFlight Navigati...

Page 30: ... site selection is to minimize airframe blockage Two other guidelines to be considered in placing the antenna on rotorcraft are listed in order of importance below A Install as far from the main rotor hub as possible At a given RPM the linear velocity of the blade increases as the distance from the rotor hub increases Since the blade blocks the line of sight GPS satellite signal the effect will be...

Page 31: ...1 25 inch diameter Refer to Figure 2 4 Shim Fabrication for Curved Surfaces The GPS antenna is designed for mounting on a flat surface and must not be warped due to mounting surface curvature To fit a curved fuselage fabricate a shim or an adapter plate to fit the antenna Use aluminum 7075 T6 or phenolic material to manufacture the shim Aluminum shims can be riveted to the aircraft To seal the alu...

Page 32: ...ge annunciator MSG pin 14 Hold annunciator HLD pin 15 Waypoint Alert annunciator WPT pin 28 and Approach annunciator APR pin 30 duplicate the annunciators on the front panel These pins are connected to open collector transistors which will sink a maximum of 200 mA If they are connected to a relay for higher current capability the relay must have a protection diode placed across the coil The pins s...

Page 33: ...urce current up to 200 mA max If connected to a relay for higher current capability the relay must have a protection diode placed across the coil The pins will source current when the flag condition is true C When using high speed ARINC 429 communications with connections in excess of 10 feet and with multiple receivers on a single line additional attention may be required to maximize signal integ...

Page 34: ... OUT ONE PULSE PER SECOND J1 13 OUT AUDIO H J1 14 OUT MESSAGE ANNUNCIATOR ACTIVE GND J1 15 OUT HOLD ANNUNCIATOR ACTIVE GND J1 16 IN POWER IN 28 VDC J1 17 IN POWER IN 28 VDC J1 18 RS422 IN RXD3 SEE APPENDIX B J1 19 RESERVED J1 20 GROUND POWER GROUND J1 21 RESERVED J1 22 RESERVED J1 23 RS422 OUT TXD2 SEE APPENDIX B AND PAGE 2 27 28 J1 24 RS422 IN RXD2 SEE APPENDIX B AND PAGE 2 25 26 J1 25 OUT CDI LO...

Page 35: ...ING REFERENCE H J2 22 SYNCHRO IN HEADING Y J2 23 ARINC 419 429 OUT TX1B SEE APPENDIX C PARAGRAPH C 2 8 J2 24 SYNCHRO IN HEADING Z GND TO AIRCRAFT PER ARINC 407 J2 25 26 VAC GROUND HEADING REFERENCE C J2 26 DISCRETE OUT APPROACH ANNUNCIATOR ACTIVE GND J2 27 DISCRETE OUT APPROACH ENABLE ACTIVE GND J2 28 DISCRETE OUT LEG CHANGE ACTIVE GND J2 29 DISCRETE OUT HSI SYNCHRO VALID 28 VDC J2 30 OUT RESERVED...

Page 36: ... 55 IN RESERVED J2 56 IN RESERVED J2 57 ARINC 419 429 OUT TX2B SEE APPENDIX C PARAGRAPH C 2 8 J2 58 ARINC 419 429 OUT TX2A SEE APPENDIX C PARAGRAPH C 2 8 J2 59 ARINC 419 429 IN RX2B SEE TABLES 3 2 AND 3 3 J2 60 ARINC 419 429 IN RX2A SEE TABLES 3 2 AND 3 3 J2 61 ARINC 419 429 IN RX3A SEE TABLES 3 2 AND 3 3 J2 62 ARINC 419 429 IN RX3B SEE TABLES 3 2 AND 3 3 J2 63 ARINC 419 429 IN RX4B SEE TABLES 3 2...

Page 37: ...Page 2 9 Revision E May 31 2006 FreeFlight 2101 I O Approach Plus GPS Navigation System Figure 2 3 GPS Antenna Cable and Connector P N 26479 0494 GPS ANTENNA CABLE TERMINATION 0 5 010 0 187 010 ...

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Page 39: ...Revision E May 31 2006 FreeFlight 2101 I O Approach GPS Navigation System Figure 2 4 ARINC 743 Hi Speed GPS Antenna P N 81194 Installation Drawing Page 2 11 12 ...

Page 40: ...stem Notes 1 Installations utilizing this antenna are limited to aircraft not equipped with Satellite Communications equipment 2 Recommended mounting screws are 8 32 UNF stainless steel 4 pl Figure 2 5 GPS Antenna P N 16248 11 Installation Drawing alternate Page 2 13 14 ...

Page 41: ...eeFlight 2101 I O Approach Plus Installation Drawing Notes 1 Dimensions shown in parenthesis are in centimeters 2 The isometric view in this drawing illustrates the assembly of an Air Duct attachment kit P N 81515 00 for forced air cooling and can be purchased from FreeFlight Page 2 15 16 ...

Page 42: ...Page 2 17 Revision E May 31 2006 FreeFlight 2101 I O Approach Plus GPS Navigation System Figure 2 7 System Inputs ...

Page 43: ...Page 2 18 Revision E May 31 2006 FreeFlight 2101 I O Approach Plus GPS Navigation System Figure 2 8 System Outputs ...

Page 44: ... 1 Collective in detent or low rotor RPM switches may be used in place of oleo switch when system is installed in helicopters 2 Refer to OLEO logic programming under AUX INSTALL in the Pilot Guide 3 Do not use gear handle or gear door switches for OLEO as this will cause navigation errors during approach and departure ...

Page 45: ...nformation FreeFlight BENDIX OUTPUT 2101 I O BENDIX BENDIX BENDIX COLLINS TERRA KING CENTURY SIGMA TEK COLLINS MID CONT NAME Approach KING KING KING IND 350A TRI NAV C KI 525a NSD 360a IU 445 PN 101 INSTR Plus KI 202 KI 206 KI 207 IND351A P1 NSD 1000 MD40 60 RIGHT CDI CDI COMMON TO FROM NAV FLAG LT FROM FLAG J1 33 j j j 12 6 b 18 18 i 1 J1 31 n n n 11 5 V 17 17 j 2 J1 34 e e e 9 Z 33 33 n 3 J1 25 ...

Page 46: ...ection sheet 1 of 3 TAS Type See Note 1 Serial Shadin ADC 200 Digital Digital 429 DADS 565 AC hi Voltage Ratio ARINC 565 AC high speed 565 AC lo Voltage Ratio ARINC 565 AC low speed 565 DC Voltage Ratio ARINC 565 DC 545 ARINC 545 Synchro input KIFIS A KIFIS A Synchro input KIFIS B KIFIS B Synchro input Page 2 21 22 ...

Page 47: ...Revision E May 31 2006 FreeFlight 2101 I O Approach Plus GPS Navigation System Figure 2 11 Typical System Interconnection sheet 2 of 3 Page 2 23 24 ...

Page 48: ...Revision E May 31 2006 FreeFlight 2101 I O Approach Plus GPS Navigation System Figure 2 11 Typical System Interconnection sheet 3 of 3 Page 2 25 26 ...

Page 49: ...ude information A serializer is required for blind encoders and devices with Gray Code outputs 6 Do not use heading input from the ADC 200 when interfacing synchro inputs FreeFlight 2101 I O Approach Plus Serial Port Input Connections Page 2 27 28 FreeFlight 2101 FreeFlight 2101 ROSETTA ROSETTA RMI ICARUS SHADIN PC SERIAL PC SERIAL SIGNAL I O Approach I O Approach SERIALIZER ENCODER ENCODER 3000 A...

Page 50: ...101 SHADIN ARGUS STORMSCOPE PC SERIAL PC SERIAL SIGNAL I O Approach I O Approach AIRDATA SHADIN SHADIN 3000 5000 WX 1000E PORT PORT NAME Plus Plus ADC 200 MINIFLO L DIGIFLO 7000 NOTE 1 25 PIN D 9 PIN D SERIAL PORT 1 SERIAL PORT 2 NOTE 2 NOTE 2 TXD J1 37 J1 23 3 6 J 4 4 7 5 TXD J1 5 J1 9 4 9 H 16 5 3 2 CABLE J1 3 20 J1 3 20 9 2 D 24 32 1 5 SHIELD SETUP K0 K0 K0 K0 OR ARGUS K0 K0 K0 FreeFlight 2101 ...

Page 51: ...ections CAUTION Consult all revelant Installation Manuals before wiring FreeFlight FreeFlight PC SERIAL PC SERIAL SIGNAL 2101 I O 2101 I O ARTEX PORT PORT NAME Approach Plus Approach Plus ELS 10 25 PIN D 9 PIN D BP PORT 1 BP PORT 2 TXDBP J1 6 J1 10 5 3 2 SERIAL J1 1 J1 1 2 7 5 COMMON CABLE J1 20 J1 20 2 1 5 SHIELD SETUP R0 ANY ANY ...

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Page 53: ...FreeFlight 2101 I O Approach Plus GPS Navigation System SECTION III CHECKOUT ...

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Page 55: ...3 1 3 2 2 Installation Setup 3 1 3 2 3 I O Interface Check 3 12 3 2 4 GPS Receiver Tests 3 14 3 3 FINAL 3 16 3 3 1 Configuration Record Sheet 3 16 LIST OF TABLES 3 1 AUX I O Configuration 3 3 3 2 ARINC 419 429 Receiver Port Options 241B and earlier software versions 3 5 3 3 ARINC 419 429 Receiver Port Options 241C and later software versions 3 6 3 4 User Units 3 8 3 5 Approach Message Options 3 9 ...

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Page 57: ...ed verify that voltage is present on pins 14 15 28 and 30 of P1 and pins 26 27 and of P2 2 Verify that ground is present on pins 3 and 20 of P1 and pins 33 and 34 of P2 and that pin 26 of P1 is not grounded 3 Verify that the GPS antenna coax center conductor is not shorted to its shield or aircraft ground When the above conditions are verified turn off the master power Properly attach the external...

Page 58: ...e the settings by rotating the small inner selector knob 5 Press to complete the entry After setting Serial port 1 continue rotating the large outer knob to set up Serial port 2 Serial port 1 input is set to a default value of Encoder and the output is set to a default value of K0 Serial port 2 is set to a default value of NONE for input and the output is set to K1 Refer to the specifications of t...

Page 59: ...W INPUT None Serial from ADC via RS 422 RS 232 Digital AVGAS via ARINC 429 Hi Lo Port 4 Digital Jet A via ARINC 429 Hi Lo Port 4 Digital JP4 via ARINC 429 Hi Lo Port 4 OLEO INPUT None Air Aircraft is in the air Ground Aircraft is on the ground DADS 419 575 429 Low Speed See Section 3 2 2 2 1 429 High Speed for setup options for GNS software 241C and later FUEL 429 Low Speed 429 High Speed GNS See ...

Page 60: ...TK True Desired Track BRG Bearing TBRG True Bearing TKE Track Angle Error DA Drift Angle TKE DA Track Angle Error Drift Angle DA TKE Drift Angle Track Angle Error BRG HDG Bearing Heading To reset any of the synchro outputs 1 Press 2 Rotate the small knob to select the output type to be changed 3 Rotate the large knob to move to the phase field 4 Rotate the small knob to change the phase to either ...

Page 61: ...d 2 combinations are available on line 1 of the display based on type and speed selection DADS 419 AHARS 429L DADS 429L AHARS 429L DADS 429H AHARS 429H 3 Data on Ports 3 and 4 must have the same speed setting 4 The following Port 3 and 4 combinations are available on line 2 of the display based on type and speed selection FUEL 429L RADAR 429L FUEL 429H RADAR 429H 3 2 2 2 1 Digital Input Data Setup...

Page 62: ... 429L DADS 429H RADAR 429H FUEL 429L AHARS 429L FUEL 429H AHARS 429H FUEL 429L RADAR 429L FUEL 429H RADAR 429H DADS 429H GNS 429H FUEL 429H GNS 429H GNS 429H AHARS 429H GNS 429H RADAR 429H GNS 429H GNS 429H GNS 429H output parameters are reserved for Honeywell VDL See Section C 1 4 4 ARINC Format Port 1 Port 2 Port 3 Port 4 J2 9 and 15 J2 60 and 59 J2 61 and 62 J2 64 and 63 419 DADS X X 429 Lo DAD...

Page 63: ...he Internal CDI Sensitivity can be modified to 5 2 5 1 0 3 or 0 1 nautical miles full scale When set at 0 1 nautical mile full scale one pixel width on the Navigator display equals approximately 25 feet of course deviation The Navigator can be configured to display the internal CDI sensitivity in nautical miles statute miles or kilometers See Section 3 2 2 5 for information on setting user units N...

Page 64: ...rough each of the User Units categories listed in Table 3 4 At each category press then use the small selector knob to scroll through the choices When the desired choice is displayed press to select that entry User Units Category Estimated Time of Arrival ETA Position Coordinate System 1 and 2 Position Datum Distance Units Speed Display Altitude Display Barometric Set In Temperature Display Fuel C...

Page 65: ...electable parameters will affect the timing for various message types Access the Installation Setup and follow these steps to change the configuration of the advisory messages 1 Rotate the small inner selector knob to display ADVISORY MESSAGES TURN OUTER KNOB 2 Rotate the large outer knob to sequence through each of the Advisory messages categories listed in Tables 3 5 and 3 6 3 At each category p...

Page 66: ...splays next Leg Course and that Turn Point has been reached distance from waypoint dependent on Turn Rate setting Displays time to arrival at waypoint for Flight Plans last waypoint only Indicates Cross Track Error in excess of 4 nm Display inbound and outbound course set messages for procedure turn Auto prompt for pilot entry of fuel status at beginning of flight Navigator power up VNAV messages ...

Page 67: ...e OAT K factor 1 Rotate the small inner selector knob to display OAT K FACTOR then press 2 Use the large knob to move among the editable fields and the small knob to change the K factor for the installed OAT probe 3 Press when the correct K factor is entered 3 2 2 9 Set Track Error Graphic The track error indicator can be combined with the internal CDI display When selected the indicator appears a...

Page 68: ...e enter 0º magnetic variation 3 2 3 I O Interface Check 1 Press the key until the CONFIGURE submode is displayed 2 Rotate the small inner knob to display the I O Interface Check page 3 2 3 1 CDI Annunciator Test Perform the following steps to test the CDI and Annunciator interface 1 Press the key The message CDI 5L indicates the external analog CDI should display full left deflection 2 Rotate the ...

Page 69: ...unciator lit ANNUNCIATOR APR EN Approach Enable annunciator lit ANNUNCIATOR APR MDE Approach Mode annunciator lit DISCRETE TRK CHG Track Change discrete on DISCRETE STR VLD Steering Valid discrete valid DISCRETE SYN VLD Synchro Valid discrete valid The GS flag exists only in the test routine Press the key to test the synchro interfaces 3 2 3 2 OutputVerification AftertheCDIdeflectiontesthasbeencom...

Page 70: ...tellites 3 2 4 1 Satellite Signal Reception To conduct GPS receiver tests press until the SENSOR STATUS submode is selected Rotate the large outer selector knob until a display similar to the one below is shown This display indicates the number of satellites being tracked 6 as well as identifying each satellite tracked by number A flashing satellite number indicates a satellite which is being trac...

Page 71: ...HF antenna to the GPS antenna To minimize front panel to antenna interference ensure that all cabin doors and windows are closed when performing the test This type of interference is also minimized by being away from the ground and ground structures If required the test may be performed in flight Finally the location of the GPS antenna may affect levels of VHF front panel to GPS antenna interferen...

Page 72: ...ecord Sheet will be needed to restore the configuration 3 2 4 4 GPS Position Update To conduct the GPS Position Update test press until the SYSTEM STATUS submode is selected Turn the small knob to display the present position If the displayed position is more than 1000 miles from the actual position press If the GPS has not yet acquired sufficient satellites for a position solution the screen will...

Page 73: ...____________ Installation Agency _________________________________________________ Address ________________________________________________________ ________________________________________________________ ________________________________________________________ Serial Port Configuration I O Setup Configuration Configuration Record Sheet Keep with Installation Manual PARAMETER CONFIGURATION TAS INP...

Page 74: ...its Barometric Display Units Temperature Display Units Fuel Computation Units Advisory Messages WPT Arrival Turn Adv Lead Time Pop Up Down Message Display Time Flight Plan Turn Countdown FPL APR Turn Now Message Waypoint Arrival Countdown Cross Track Error Procedure Turn Messages Fuel Initialization VNAV Messages Countdown VNAV Messages Begin Now VNAV Messages Level Countdown VNAV Messages Level O...

Page 75: ...___________________ Installation Agency _________________________________________________ Address ________________________________________________________ ________________________________________________________ ________________________________________________________ Serial Port Configuration I O Setup Configuration Configuration Record Sheet Pilot Guide Copy PARAMETER CONFIGURATION TAS INPUT HEA...

Page 76: ...its Barometric Display Units Temperature Display Units Fuel Computation Units Advisory Messages WPT Arrival Turn Adv Lead Time Pop Up Down Message Display Time Flight Plan Turn Countdown FPL APR Turn Now Message Waypoint Arrival Countdown Cross Track Error Procedure Turn Messages Fuel Initialization VNAV Messages Countdown VNAV Messages Begin Now VNAV Messages Level Countdown VNAV Messages Level O...

Page 77: ...FreeFlight 2101 I O Approach Plus GPS Navigation System APPENDIX A RTCA DO 160 ENVIRONMENTAL QUALIFICATION FORMS ...

Page 78: ......

Page 79: ...y A Shock 7 0 6 g s 11 ms Vibration 8 0 Categories M N and B Explosion 9 0 Category X Not Tested Waterproofness 10 0 Category X Not Tested Fluids Susceptibility 11 0 Category X Not Tested Sand and Dust 12 0 Category X Not Tested Fungus 13 0 Category X Not Tested Salt Spray 14 0 Category X Not Tested Magnetic Effect 15 0 Category Z Power Input 16 0 Category B Voltage Spike Conducted 17 0 Category A...

Page 80: ...sted Waterproofness 10 0 Category X Not Tested Fluids Susceptibility 11 0 Category X Not Tested Sand and Dust 12 0 Category X Not Tested Fungus 13 0 Category X Not Tested Salt Spray 14 0 Category X Not Tested Magnetic Effect 15 0 Category Z Power Input 16 0 Category B Voltage Spike Conducted 17 0 Category A A F Conducted Susceptibility 18 0 Category B Induced Signal Susceptibility 19 0 Category AC...

Page 81: ...Category F Category F Sand and Dust 12 0 Category D Category D Fungus 13 0 Category F Category F Salt Spray 14 0 Category S Category S Magnetic Effect 15 0 Category X Not Tested Category Z Power Input 16 0 Category X Not Tested Category X Not Tested Voltage Spike Conducted 17 0 Category X Not Tested Category X Not Tested A F Conducted Susceptibility 18 0 Category X Not Tested Category X Not Tested...

Page 82: ...proofness 10 0 Category X Not Tested Fluids susceptibility 11 0 Category X Not Tested Sand and Dust 12 0 Category X Not Tested Fungus 13 0 Category X Not Tested Salt Spray 14 0 Category X Not Tested Magnetic Effect 15 0 Category z Power Input 16 0 Category A Voltage Spike Conducted 17 0 Category A A F Conducted Susceptibility 18 0 Category A Induced Signal Susceptibility 19 0 Category Z Radio Freq...

Page 83: ...FreeFlight 2101 I O Approach Plus GPS Navigation System APPENDIX B SERIAL INTERFACE SPECIFICATION ...

Page 84: ......

Page 85: ...al is negative with respect to the inverting signal Signal Condition MARK Logic 0 The non inverting signal is positive with respect to the inverting signal Signal Condition SPACE RS 422 has the capability of driving up to ten receive devices in parallel from a single transmitter It can drive long cable lengths and has superior noise immunity B 2 2 RS 232 The RS 232 protocol specifies a bipolar unb...

Page 86: ...ote 2 2 RXD3 Receive Port 3 RS 422 See Note 1 4 TXD3BP Transmit Port 3 RS 232 423 See Note 1 5 TXD1 Transmit Port 1 RS 422 6 TXD1BP Transmit Port 1 RS 232 423 7 RXD1 Receive Port 1 8 RXD1 Receive Port 1 9 TXD2 Transmit Port 2 RS 422 10 TXD2BP Transmit Port 2 RS 232 423 18 RXD3 Receive Port 3 See Note 1 23 TXD2 Transmit Port 2 RS 422 24 RXD2 Receive Port 2 29 TXD3 Transmit Port 3 RS 422 See Note 1 ...

Page 87: ...il the desired information is displayed Press to complete the entry B 5 RECEIVE PORTS B 5 1 Configuration Two data formats may be selected to accept input from external altitude encoders gray code to serial altitude converters or the RMI Rocky Mountain Instruments µEncoder Airdata system To select a data format refer to section B 4 The baud rate of each of these formats is automatically set ENCODE...

Page 88: ...acked BCD data message See Table below BYTE NUMBER BYTE NAME DESCRIPTION 01 ID 1 Hex Identifier Byte always FFH 02 ID 2 Hex Identifier Byte always 80H 03 07 IALT Current Indicated Altitude 08 12 PALT Pressure Altitude 13 17 DALT Density Altitude 18 20 KTS Indicated Airspeed in knots 21 23 TAS True Airspeed in knots 24 26 MACH Indicated Airspeed in MACH 27 30 VSI Vertical Speed in fpm multiplied by...

Page 89: ...e serial port is set to ENCODER A packet consists of a set of ASCII message strings The first character of each packet is an ASCII Start of Text STX 02H The last character of each packet will be an ASCII End of Text ETX 03H Each message string begins with one ASCII character to identify it as an Air Data message Z The second character identifies which message it is The rest of the string consists ...

Page 90: ...00 0 to 999 ZDsdddd Pressure Altitude s sign dddd tens of feet 100 to 5999 ZEsdddd Density Altitude s sign dddd tens of feet 800 to 5999 ZFsdd Outside Air Temperature s sign dd celsius 99 to 99 ZGsdd True Air Temperature s sign d celsius 99 to 99 ZHddd Wind Direction ddd magnetic degrees 0 to 359 ZIddd Wind Speed ddd knots 0 to 150 ZJsdd Rate of Turn s sign dd degrees second 20 to 20 ZKsddd Vertic...

Page 91: ...0 baud or 38 4 kbaud The update rate may be set from 1 to 999 seconds for any of the formats The only exception is if the baud rate is 1200 For this case the maximum update rate is 2 seconds The data stream is a string of ten bit serial ASCII characters consisting of one start bit eight data bits and one stop bit No parity is generated Data messages begin with an ASCII Start of Text STX character ...

Page 92: ...ed Track DTK Degrees Mag or True Active Leg Number LEG Flight Plan Leg Number Direct 21 Heading 22 Destination Waypoint Identifier IDENT ASCII Characters Bearing To Destination Waypoint BRG Degrees Parallel Offset PTK Right or Left nautical miles Estimated Position Error Nautical miles Magnetic Variation East or West degrees Time Since Solution Seconds and tenths Warnings Character in Designated F...

Page 93: ... min x 100 C ddd 3 TK deg D sss 3 GS kts E dddddd 6 DIS nm x 100 F hhmm 4 ETE hrs and mins G Lnnnn 5 XTK Error L or R nm x 100 H Ldddd 5 TKE L or R deg x 10 I dddd 4 DTK deg x 10 J ll 2 LEG K ccccc 5 IDENT L dddd 4 BRG deg x 10 M Lnnnn 5 PTK L or R nm x 10 P nnn 3 Estimated Pos Error nm x 100 Q Eddd 4 VAR E or W deg x 10 c ttt 3 Time Since Last Solution s x 10 T A 11 Warnings in Effect d fff 3 MSA...

Page 94: ...ast section In addition the K0 and K1 formats add flight plan information Each waypoint is sent as a separate line terminated with a CR for K0 and a CR LF for K1 The waypoint data lines are followed by a line of waypoint type identifiers If no flight plan is active no flight plan data will be transmitted wdd binary data w Flight plan item designator dd Sequential waypoint number ASCII binary data ...

Page 95: ...ined set to zero ddddddd Latitude degrees mmmmmm Latitude minutes hhhhhhh Latitude hundredths of minutes Where BYTE 10 11 12 BIT 7 6 5 4 3 2 1 0 7 6 5 4 3 2 1 0 7 6 5 4 3 2 1 0 CONTENT s x x x x x x x d d d d d d d d x x m m m m m m BYTE 13 BIT 7 6 5 4 3 2 1 0 CONTENT x h h h h h h h s 0 if East longitude 1 if West longitude x undefined set to zero ddddddd Longitude degrees mmmmmm Longitude minute...

Page 96: ...pe This indicates the type of waypoints in the flight plan according to flight plan order e g Airport VORs NDBs Intersections or User The number of waypoints in the flight plan determines the number of bytes in this field 5 waypoints in the flight plan makes this field 5 bytes long The format is as follows t nnn The following values are acceptable for n a Airport Public Use m Military Base h Helip...

Page 97: ... time tag Offset from GMT Parallel offset Left or right offset in nm Extended Time Time in hours minutes seconds and milliseconds Extended Time Since Solution Time since last position fix in hours minutes seconds and milliseconds Sensor mode Sensor in use GPS LORAN Differential GPS or None GPS mode and of satellites used LORAN transmitters used B 6 4 X0 and X1 Formats The X0 and X1 formats contain...

Page 98: ...cc c Barometric altitude Track Where aaa aa Magnetic Track in degrees bbb bb Desired Track in degrees cdd ddddd Cross Track Error L or R c nautical miles dd ddddd efff ff Track Angle Error L or R e degrees fff ff Vertical Navigation ITEM DESIGNATOR INFORMATION ITEM FORMAT n Vertical Navigation Actual Desired Vertical Error from Profile and Vertical Angle Error abbbb b cdddd d efffff f ghh hh ITEM ...

Page 99: ... dd and seconds ee Data Time Tag Local Offset ITEM DESIGNATOR INFORMATION ITEM FORMAT p Data Time Tag and Local GMT Offset aa bb cc ccc dee e Where aa bb cc Data Time Tag in hours aa minutes bb and seconds cc dee e Local Time Offset or d time in hours ee e Parallel Offset Where abbb bbbb Parallel Offset L or R a nautical miles bbb bbbb Extended Time Where aa bb cc ccc Extended Time hours aa minute...

Page 100: ...erential GPS or No Position Fix GPS bbc GPS Mode bb and Number or satellites used for position fix c bb may be 2D 3D or 0D c is an integer number LOR d LORAN Mode number of transmitters used in fix d integer number Note Other FreeFlight proprietary sentences beginning with an asterisk may appear These are for FreeFlight test equipment They may change or disappear without notice These labels are in...

Page 101: ...min BW 121 5516 LON West 121 55 16 min C137 TK 137 D128 GS 128 knots E071227 DIS 712 27 nm F0534 ETE 5 hrs 34 min GR0018 XTK 0 18 nm Right HR0003 TKE 0 3 Right I1384 DTK 138 4 J11 Active Leg 11 KAUS Destination Waypoint AUS L1389 BRG 138 9 M0000 PTK 0 0 nm P005 Position Error 0 05 nm QE158 Magnetic Variation 15 8 East c001 Time Since Last Solution 0 1 sec T No Warnings are Present d057 MSA 5 700 f...

Page 102: ...E DESCRIPTION kN 37 21 64728 W 121 55 16121 128 3 Current Latitude N 37 21 64728 l 10312 4 GPS Altitude 10 312 4 feet m 137 42 138 4 R0 18 R0 31 Magnetic Track 137 42 Desired Track 138 4 Cross Track Error Right 0 18 nm Track Angle Error Right 0 31 n 0 0 No Vertical Navigation o 712 27314 138 942 5 34 15 Distance to waypoint 712 27314 nm Bearing to waypint 138 942 Time to waypoint 5h 34m 15s p 13 5...

Page 103: ...FreeFlight 2101 I O Approach Plus GPS Navigation System APPENDIX C EXTERNAL INPUTS AND OUTPUTS ...

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Page 105: ... equivalent signal Range High speed 100 to 650 knots Low Speed 0 to 550 knots Resolution 1 0 knots Accuracy 4 knots Index Reference High speed 100 knots Low speed 0 knots Positive Direction Sense Increasing speed in phase with reference voltage and starting at index reference Scale Factor 46 6 knots volt Reference Voltage 11 8 Vac Loading Reference 100kΩ Signal 10kΩ Signal pins J2 10 Sig J2 12 Ref...

Page 106: ... Reference 10kΩ Signal 100kΩ Reference pins J2 18 H J2 7 C Ground Synchro pins J2 10 X J2 12 Y J2 14 Z KIFIS B Synchro Source ARINC 407 three wire transmitter or equivalent Range 200 to 550 knots Resolution 1 0 knot Accuracy 4 0 knots Index Reference 200 knots is equal to 72 electrical Positive Direction Sense Increasing speed for increasing angle Scale Factor 72 electrical rotation 100 knots Refe...

Page 107: ... Input INPUT CHARACTERISTICS DESCRIPTION Heading Synchro Source ARINC 407 three wire synchro or equivalent Range 0 to 360 Resolution 0 1 Accuracy 0 2 Index Reference Magnetic or True North 0 Positive Direction Sense Increasing heading for increasing angle Scale Factor 1 heading equals 1 electrical rotation Reference Voltage 26 Vac 10 400 Hz 20 Hz Loading Reference 10kΩ Signal 100kΩ Reference pins ...

Page 108: ...Altitude Press 419 575 BNR 2W 204 Altitude Baro 419 575 BNR 2W 211 Total Air Temperature Ram Air Temperature 419 575 BNR 2W OR 210 TAS 429 BNR 2W 203 Altitude Press 429 BNR 2W 204 Altitude Baro 429 BNR 2W 211 Total Air Temperature Ram Air Temperature 429 BNR 2W Note Refer to Section C 2 to define format type ARINC 419 or 429 C 1 4 2 AHRS PORT 2 J2 60 and 59 All software versions PORT 4 J2 64 and 6...

Page 109: ...429 2W 102 GNS VDOP 429 2W 110 GNS Latitude 429 2W 111 GNS Longitude 429 2W 232 TDS label airport identifier 429 2W 242 TDS label airport station identifier 429 2W 243 TDS label procdure selection 429 2W 244 TDS label station 429 2W 270 VDL status 429 2W 273 GNS Status 429 2W 355 GNS Maintenance 429 2W C 1 4 5 RADAR PORT 2 J2 60 and 59 Software version 241C and later PORT 4 J2 64 and 63 Software v...

Page 110: ...PTION High Level J1 26 Source Transistor current source Status 0 to 3 5 Vdc Not Valid 18 5 Vdc to 30 Vdc Valid Load 200 mA current source Low Level J1 25 Source Analog voltage source referenced to ground Status 0 to 150 mVdc Not Valid 250 to 900 mVdc Valid Load Up to three 1000Ω loads C 2 3 TO FROM OUTPUT CHARACTERISTICS DESCRIPTION Low Level J1 34 Source Polarity reversing analog current source r...

Page 111: ...nd C 2 5 Glideslope UP DN OUTPUT CHARACTERISTICS DESCRIPTION Low Level J1 27 Source Polarity reversing analog current for future use source referenced to ground Range 0 to 150 mA into 1000Ω load Resolution 1 17 µA Accuracy 10 µA centering Index Reference Desired Glidepath Positive Direction Sense Fly up when J1 27 is positive with respect to J1 31 Scale Factor 0 3 mA per foot Load Capability Up to...

Page 112: ...tor current sink Status 0 to 1 Vdc Approach Valid Open Approach Invalid Load Capability 200 mA current sink Approach Enable J2 27 Source Transistor current sink Status 0 to 1 Vdc Approach Enabled Open Approach Not Enabled Load Capability 200 mA current sink HSI Synchro Valid J2 29 Source Transistor current source Status 18 5 Vdc to 30 Vdc HSI Valid 0 to 3 5 Vdc HSI Invalid Load Capability 200 mA c...

Page 113: ...sformers DA Type Output Magnetic Drift Angle Load Capability Three paralleled synchro control transformers TKE DA Type Output Track Angle Error minus Drift Angle Load Capability Three paralleled synchro control transformers DA TKE Type Output Drift Angle minus Track Angle Error Load Capability Three paralleled synchro control transformers HDG Type Output Magnetic Heading Load Capability Three para...

Page 114: ...oint 1 Latitude 419 BCD 250 ms 041 Waypoint 1 Longitude 419 BCD 250 ms 042 Waypoint 2 Latitude 419 BCD 250 ms 043 Waypoint 2 Longitude 419 BCD 250 ms 044 Waypoint 3 Latitude 419 BCD 250 ms 045 Waypoint 3 Longitude 419 BCD 250 ms 046 Waypoint 4 Latitude 419 BCD 250 ms 047 Waypoint 4 Longitude 419 BCD 250 ms 050 Waypoint 5 Latitude 419 BCD 250 ms 051 Waypoint 5 Longitude 419 BCD 250 ms 052 Waypoint ...

Page 115: ... 125 GMT 429 BCD 200 ms 200 ms 147 Magnetic Variation 429 BNR 200 ms 200 ms 174 Glideslope Deviation 429 BNR 50 ms 50 ms 233 Flight ID Characters 1 2 429 BNR 800 ms 800 ms 234 Flight ID Characters 3 4 429 BNR 800 ms 800 ms 235 Flight ID Characters 5 6 429 BNR 800 ms 800 ms 236 Flight ID Characters 7 8 429 BNR 800 ms 800 ms 251 Distance 429 BNR 200 ms 200 ms 252 ETE 429 BNR 200 ms 200 ms 260 Date 4...

Page 116: ...oint 0 Latitude 429 BNR 325 Waypoint 0 Longitude 429 BNR 326 Waypoint 1 Latitude 429 BNR 327 Waypoint 1 Longitude 429 BNR 330 Waypoint 2 Latitude 429 BNR 331 Waypoint 2 Longitude 429 BNR 332 Waypoint 3 Latitude 429 BNR 333 Waypoint 3 Longitude 429 BNR 334 Waypoint 4 Latitude 429 BNR 335 Waypoint 4 Longitude 429 BNR Variable sent at 336 Waypoint 5 Latitude 429 BNR 5 WPT per second 337 Waypoint 5 Lo...

Page 117: ...T Latitude GAMA 307 WPT Longitude GAMA 261 GPS Discrete Word 1 GAMA 200 ms 200 ms 326 Latitude Deviation Scale Factor 429 BNR 200 ms 200 ms 327 Vertical Deviation Scale Factor 429 BNR 200 ms 200 ms C 2 9 5 ARINC 429 VDL Output Parameters PORT 1 J2 16 and 23 Software version 241C to 241G PORT 2 J2 58 and 57 Software version 241C to 241G NOTE The following ARINC 429 labels are transmitted in a Burst...

Page 118: ...2 sec 042 Wpt 2 Latitude 419 BCD 2 sec 043 Wpt 2 Longitude 419 BCD 2 sec 044 Wpt 3 Latitude 419 BCD 2 sec 045 Wpt 3 Longitude 419 BCD 2 sec 046 Wpt 4 Latitude 419 BCD 2 sec 047 Wpt 4 Longitude 419 BCD 2 sec 050 Wpt 5 Latitude 419 BCD 2 sec 051 Wpt 5 Longitude 419 BCD 2 sec 052 Wpt 6 Latitude 419 BCD 2 sec 053 Wpt 6 Longitude 419 BCD 2 sec 054 Wpt 7 Latitude 419 BCD 2 sec 055 Wpt 7 Longitude 419 BC...

Page 119: ... 743 BNR 150 ms 101 HDOP 743 BNR 150 ms 102 VDOP 743 BNR 150 ms 103 True Track 743 BNR 150 ms 110 Latitude 743 BNR 150 ms 111 Longitude 743 BNR 150 ms 112 Ground Speed 743 BNR 150 ms 125 UTC 743 BCD 150 ms 130 Horiz Integrity 743 BNR 150 ms 136 Vert FOM 743 BNR 150 ms 147 Mag Variation 743 BNR 150 ms 165 Vertical Speed 743 BNR 150 ms 166 N S Velocity 743 BNR 150 ms 174 E W Velocity 743 BNR 150 ms ...

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Page 121: ...FreeFlight 2101 I O Approach Plus GPS Navigation System APPENDIX D SUPPLEMENTAL TYPE CERTIFICATES AND FLIGHT MANUAL SUPPLEMENTS ...

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Page 123: ...FTP site when they become available You can download these files from the site using your internet browser The address for the site is ftp stcpub2 austin 24 227 190 27 STCPUB To download a file right click Windows or ctrl click Mac the file and choose Copy To Folder The files in this directory are Portable Document Format PDF In order to view and print these files you will need Adobe Acrobat Reade...

Page 124: ...Page D 2 Revision E May 31 2006 FreeFlight 2101 I O Approach Plus GPS Navigation System THIS PAGE INTENTIONALLY LEFT BLANK ...

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Page 127: ... must be attached to the FAA approved Beech 65 A90 FAA Airplane Flight Manual when the FreeFlight 2101 I O Approach Plus GPS Navigation System has been installed in accordance with FAA STC SA09363SC The information contained herein supplements or supersedes the basic Airplane Flight Manual only in those areas listed For limitations procedures and performance information not con tained in this supp...

Page 128: ...exas 76706 with FreeFlight 2101 I O App Plus GPS FAA Approved Page 2 of 14 Date 10 27 97 DOC 83205 Rev B TABLE OF CONTENTS TABLE OF CONTENTS 2 LOG OF REVISIONS 3 GENERAL DESCRIPTION 4 SECTION IV LIMITATIONS 5 SECTION V NORMAL PROCEDURES 7 SECTION VI EMERGENCY PROCEDURES 13 SECTION VII FAA APPROVED PERFORMANCE 14 ...

Page 129: ...nt 3700 Interstate 35 for Beech Model 65 A90 Aircraft Waco Texas 76706 with FreeFlight 2101 I O App Plus GPS FAA Approved Page 3 of 14 Date 10 27 97 DOC 83205 Rev B LOG OF REVISIONS Revision Page Subject Approval Date A All Initial Release See page one ...

Page 130: ...84 NAD 83 chart references in accordance with the criteria of FAA Advisory Circular AC 20 138 and AC 91 49 Navigation data is based upon use of only the global positioning System GPS operated by the United States B EQUIPMENT DESCRIPTION The FreeFlight 2101 I O Approach Plus GPS Navigation System is a Global Positioning Satellite GPS based navigation system consisting of a Receiver Display Unit RDU...

Page 131: ...These included waypoints such as the intersection of two radials DME positions waypoints located on a DME Arc turn waypoints or waypoints to indicate a Final Approach Fix FAF The pilot should review the approach legs and cross check the appropriate publication to ensure the procedure is flown correctly D Instrument approaches must be accomplished in accordance with approved instrument approach pro...

Page 132: ...coordinate datum system for the instrument approach is WGS 84 or NAD 83 The NavData data base used in the FreeFlight 2101 I O Approach Plus only contains WGS 84 geodetic datum referenced data G When GPS integrity Receiver Autonomous Integrity Monitoring RAIM capability is lost en route and terminal IFR operation can be continued provided the Trimble 2101 I O Approach Plus position is verified ever...

Page 133: ...e the procedure is flown correctly 2 A Shadin ADC 200 supplies pressure altitude true airspeed and outside air temperature data to the FreeFlight2101 I O Approach Plus There are no controls or special operating procedures for use of the ADC 200 system This air data information is displayed on the Air Data pages located under the CALC key B SYSTEM ANNUNCIATORS Eight annunciators located on the Capt...

Page 134: ...annunciator alerts the pilot that the approach mode is active approach RAIM is available the aircraft is located on the final approach leg annunciator illuminates at 2 NM inbound to the Final Approach Fix FAF and the aircraft track is within 70 degrees of the inbound course Two annunciators located below the 2101 I O Approach Plus RDU on the center instrument panel and controlled by the NAV GPS sw...

Page 135: ...e pilot should manually select the same Desired Track on the HSI course selector as indicated by the FreeFlight 2101 I O Approach Plus during track leg changes of a flight plan after selecting a course to or from a waypoint or as directed during a SID or STAR procedure E FLIGHT DIRECTOR AUTOPILOT This function is currently inoperative in the King Air A90 F HOLDING If Holding is to be executed at a...

Page 136: ...cedures and pressing the ENT key NOTE Only one approach can be in the flight plan at one time The Approach data cannot be altered added to or deleted from the approach procedure contained in the data base The data base may contain some waypoints which do not appear on the terminal approach procedures Parallel offsets are not allowed when the approach mode is enabled 2 To disable the approach selec...

Page 137: ...quired If the APR annunciator doesn t illuminate DO NOT DESCEND COMPLETE MISSED APPROACH 6 From FAF to MAP there is no pilot input required and RAIM Integrity is continually monitored throughout the approach 7 MAP to Landing The waypoint light will illuminate approaching MAP and at MAP the TO FROM will change to FROM and course guidance presented will be an extension of the inbound track 8 MAP to ...

Page 138: ...2 amp circuit breaker labeled GPS located first officer s instrument panel circuit breaker panel powers the FreeFlight 2101 I O Approach Plus Navigation System 2 A 1 amp circuit breaker labeled ADS Computer located first officer s instrument panel circuit breaker panel powers the ADC 200 3 A 5 amp circuit breaker labeled NAV 1 located first officer s instrument panel circuit breaker panel powers t...

Page 139: ...n continue to navigate using the Trimble 2101 I O Approach Plus or revert to an alternate means of navigation appropriate to the route and phase of flight When continuing to use GPS navigation position must be verified every 15 minutes using another IFR approved navigation system b If during an instrument approach terminate the approach and execute a missed approach if required 2 If the FreeFlight...

Page 140: ...light Manual Supplement 3700 Interstate 35 for Beech Model 65 A90 Aircraft Waco Texas 76706 with FreeFlight 2101 I O App Plus GPS FAA Approved Page 14 of 14 Date 10 27 97 DOC 83205 Rev B SECTION VII FAAAPPROVED PERFORMANCE No Change ...

Page 141: ...FreeFlight 2101 I O Approach Plus GPS Navigation System APPENDIX E LOCAL GEODETIC REFERENCE DATUMS ...

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Page 143: ...n 52 Marcus Is Australian Geodetic 1952 Australia Tasmania Australian Geodetic 1984 Australia Tasmania Bahamas NAD 27 Bahamas except San Salvador Bellevue IGN Efate Erromango Is Bermuda 1957 Bermuda Is Bogota Observatory Colombia Bukit Rimpah Indonesia Camp Area Astro Antarctica Campo Inchauspe Argentina Canada Mean NAD27 Canada incl Newfoundland Canal Zone NAD27 Panama Canal Zone Canton Island 19...

Page 144: ...l Chart Finland Gandajika Base Republic of Maldives Geodetic Datum 49 New Zealand Ghana Ghana Ordinance Survey of Great Britain 36 England Isle of Man Scotland Shetland Isles Wales Greenland NAD27 Greenland Guam 1963 Guam Is Gunung Segara S E Borneo Gunung Serindung 1962 S W Borneo GUX 1 Astro Guadalcanal Is Herat North Afghanistan Hjorsey 1955 Iceland Hong Kong 1963 Hong Kong Hu Tzu Shan Taiwan I...

Page 145: ...lores Is Old Egyptian Egypt Old Hawaiian mean Hwaiian Is Old Hawaiian Maui Maui Old Hawaiian Oahu Oahu Old Hawaiian Kauai Kauai Oman Oman Pico De Las Nieves Canary Is Pitcairn Astro 67 Pitcairn Is Puerto Rico Puerto Rico Virgin Is Quatar National Quatar Qornoq S Kalaallit Nunaat Rome 1940 Sardinia SAD 69 Brazil Brazil Santa Braz Saint Miguel Santa Maria Is Santo DOS Espiritu Santo Is New Hebrides ...

Page 146: ...m Southeast Base Porto Santo Maderia Is Southwest Base Azores Tananarive Observatory 25 Madagascar Thai Viet Indian Thailand Vietnam Timalai 1948 Brunei E Malaysia Tokyo mean Japan Korea Okinawa Tristan Astro 1968 Tristan da Cunha Unites Arab Emirates Nahrwan United Arab Emirate Viti Levu 1916 Viti Levu Is Voirol Algeria Tunisia Wake Eniwetok 60 Marshall Is WGS 72 Former World WGS 84 World Yacare ...

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Page 148: ...3700 Interstate 35 S Waco TX 76706 3756 USA 1 254 662 0000 ...

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Page 150: ...3700 Interstate 35 S Waco TX 76706 3756 USA 1 254 662 0000 ...

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Page 152: ...ts and 1 sided for 11 X 17 sheets 2 Fold 11 x 17 as shown 3 Use card stock for dividers front cover back cover 4 Punch holes in left edge with standard 3 hole punch 5 Insert all pages in a white 3 ring binder with clear plastic cover for inserts 6 Insert front and back cover in clear plastic of binder 7 Insert spine with logo up ...

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