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Sandel

Avionics

SN3308 Navigation Display

Installation Manual

90106-IM-G(4) Installation Manual W SIG.doc

Appendix-A Page 14

13:

MKR SELECT

CURRENT SELECTION
NONE

NONE

COLLINS AMR-350
KING

KMA-20

KING

KMA-24

KING

KMR-675

KING

KNR-634

KING

KR-21

KING

KR-22

TRIMBLE TMA-340
TRIMBLE TMS-350

Purpose

Changes selection of the marker beacon receiver. If none is
installed select NONE.

Instructions

: Use

and

or HDG control knob to move the cursor, and use

the SET softkey to select.

14:

MKR CHANGE

NONE

MKR VALID

> DISABLED

THRESH

1.0

Volts

Purpose

Changes default settings for the marker beacon receiver
selected on page 13.

Instructions

: Use

and

move the cursor, and use the HDG knob to adjust

the value.

Notes

These settings should be changed only on instructions from the
factory, service bulletin, or service information letter.

Summary of Contents for SN3308

Page 1: ...L W SIG DOC SN3308 Navigation Display Installation Manual Document No 90106 IM Revision G 4 9 25 03 SANDEL AVIONICS 2401 DOGWOOD WAY VISTA CA 92081 PHONE 760 727 4900 FAX 760 727 4899 WEBSITE WWW SAND...

Page 2: ...erface 13 1 4 9 RS232 RS422 Serial Communication 14 1 4 10 GARMIN GNS430 GPS VOR LOC Combination Receiver 15 Required SN3308 Setup Items 16 Required GARMIN GNS430 Setup Items Receiver 1 16 Required GA...

Page 3: ...NSTALLATION 28 3 1 General 28 3 1 1 Unpacking and Inspecting Equipment 28 3 2 Installation Considerations 28 3 2 1 General Considerations 28 3 2 2 Cooling Considerations 28 3 2 3 Mechanical Installati...

Page 4: ...ions 5 11 1 7 Compass System Interface 5 11 1 8 NAV Source Selection 5 11 1 9 BRG Source Selection 6 11 1 10 DME Selection 6 11 1 11 GPS Interface and Control 7 11 1 12 Marker Beacon Interface 8 11 1...

Page 5: ...on numbers updated Post install temperature test Adds information about software 1 09 features Temperature indication Sys page inverter fan speed readout ILS Lockout selection Incorrect FCS ref note r...

Page 6: ...1 Incorporated A R 360 1 4 7 Deleted ref to Radar Altimeter 2 3 2 Deleted ref to Radar Altimeter 2 3 3 Deleted ref to Radar Altimeter P1 32 was triple conductor wire P2 8 Deleted ref to Radar Altimete...

Page 7: ...Sandel Avionics SN3308 Navigation Display Installation Manual 90106 IM G 4 Installation Manual W SIG doc Page 7...

Page 8: ...display which is FAA approved under technical standard order TSO C113 The SN3308 employs a patent pending active matrix liquid crystal AMLCD projection display It is designed to combine the functions...

Page 9: ...separate maintenance menu pages for each equipment function and in most cases the selections are made by equipment make model In addition to connecting the desired equipment the installer must provide...

Page 10: ...ture readout on maintenance page 17 for an approximate temperature rise of approximately 10q C or 18q F This checks proper cooling airflow 5 Perform Ground Test procedures 6 Perform Flight Test proced...

Page 11: ...699 and below These outputs pull only to within 1 volt of ground Serial numbers 2700 and above have 250ma maximum current Serials numbers 2700 and above outputs pull to within 1 ohm of ground Check to...

Page 12: ...agram for details These inputs are not connected with the use of the Garmin GNS430 Arinc Nav receiver which uses ARINC 429 only There are only low level flag inputs If it is desired to use a Superflag...

Page 13: ...long range navigation receivers through the serial ports ADF s can be connected as ARINC 407 synchro or DC sine cosine inputs See the installation drawings for interconnection data and select the appr...

Page 14: ...drawings The KN62 64 panel mount DME s can be remote indicated by connecting CLK DATA DME REQ to the SN3308 as shown in the installation drawings A KDI 572 is not required NOTE when the KN62 64 is swi...

Page 15: ...ssitate connecting the GNS430 VOR LOC to Port 3 ARINC 429 output data from the SN3308 must go to the GNS430 GPS 429 Input port see installation drawing No composite NAV signals are required because th...

Page 16: ...ING TO THE SPARE PINS YOU HAVE SELECTED IN A GNS430 INSTALLATION THIS WILL USUALLY BE P2 11 AND OR P2 29 FORMER MSG WPT ANNUNCIATORS NOT USED Relay Mode MASTER ILS Lockout OFF DME A DUAL GNS430 INSTAL...

Page 17: ...22 14 We suggest that this wiring be installed but capped and stowed until the switch functions are assigned in future versions of software They may be used for remote map functions in later versions...

Page 18: ...for the interface descriptions contained within this Installation Manual It is the responsibility of the installer to ensure that such equipment is compatible with the SN3308 as described and to ensur...

Page 19: ...or outputs are required for use with peripheral equipment This reference excitation must be obtained from the aircraft inverter source The following section describes the technical characteristics whi...

Page 20: ...C 1 5 Ampere Nominal 2 3 Interface Conventions The SN3308 was designed to interface and operate with several generations of avionics equipment It is compatible with DC analog and or ARINC standard syn...

Page 21: ...ut 28 OBS Resolver DC Reference Input for P1 13 10 VHF Nav 2 VOR Composite Input Note 2 29 VHF Nav 1 VOR Composite Input Note 2 11 KG 102 DG Stepper C Input 30 KG 102 DG Stepper A Input 12 DG Synchro...

Page 22: ...27 Reserved for Future Use Reserved 9 Spare Y Output Note 1 28 Spare X Output Note 1 10 DME 1 Hold In 29 WPT Annunciator Input 11 MSG Annunciator Input 30 GPS Selected In 12 ACT Approach Active Annun...

Page 23: ...68 Data King Serial Data GPS 2 429 A PORT3 8 DME 1 568 Clock King Clock In 27 DME 1 568 Sync King DME REQ NAV 429 B PORT2 9 DME 1 568 Data King Serial Data NAV 429 A PORT2 28 GPS 1 ARINC 429 B In PORT...

Page 24: ...115 Waypoint Bearing True 50 BNR 116 Cross Track Distance 50 BNR 121 Horizontal Steering Command 50 BNR 147 Magnetic Variation 1000 BNR 173 LOC Deviation 50 BNR 174 GS Deviation 50 BNR 222 VOR Bearing...

Page 25: ...mounting variation variation color position The L C and R variants signify the position in which the unit is to be mounted within one of the three predominate locations i e Left instrument panel Cente...

Page 26: ...pprovals in regard to specific aircraft make model or type The conditions and tests required for TSO approval of this article are minimum performance standards It is the responsibility of those desiri...

Page 27: ...igible for follow on approval A copy of this memorandum has been attached in the Appendix F The Environmental Qualification Form for the SN3308 is included within this Installation Manual as Appendix...

Page 28: ...should be installed in accordance with standards established by the customer s installing agency and existing conditions as to unit location and type of installation However the following consideratio...

Page 29: ...supplied harness strain relief The strain relief may be attached to the rear of the tray utilizing an adel clamp mounted to the side of the chassis or with an adel clamp and a bracket for strain relie...

Page 30: ...ial caution must be taken to observe 30 Hz OBS resolver connections in order to prevent possible damage to the installed VOR localizer converter See Installation Wiring Diagrams and the MAINTENANCE ME...

Page 31: ...20 milliamperes at extremes in ambient temperature so this pin should be connected to the main power bus not the battery bus P1 3 P1 22 Display Power Return Input Pins 3 and 22 are the aircraft ground...

Page 32: ...se pins control the enabling of the Glideslope pointer They are not related to the bearing pointer operation These signals also control the ILS Lockout logic so the SN3308 can sense when a GPS receive...

Page 33: ...e on P2 4 This function is selected on the Compass maintenance page P1 13 OBS Resolver H Input P1 28 OBS Resolver DC ref Input P1 14 OBS Resolver SIN Output P1 32 OBS Resolver COS Output OBS resolver...

Page 34: ...eceiver LEFT and RIGHT deviation outputs Two dot deflection is r150 mVDC 24 AWG twisted shielded pair wire is recommended for these functions 3 4 Connector P 2 Pinout Descriptions P2 1 Vertical Superf...

Page 35: ...ernal relay is be required to make this signal active high P2 6 HDG Bootstrap Y out P2 25 HDG Bootstrap X out Z is Ground This function may be used to provide bootstrap output to an RMI or other direc...

Page 36: ...rker Beacon Input P2 34 Middle Marker Beacon Input Marker beacon receiver inputs Normally connected to the external lamp drivers on the marker beacon receiver see the installation drawings Most marker...

Page 37: ...oc Page 37 The selection of the function for these inputs is in the ADF 2 Maintenance Page and the NAV maintenance page When 400Hz differential resolver operation is required ADF 2 operation cannot be...

Page 38: ...by the NAV pushbutton The receiver type is selected on the LNAV 2 maintenance page P3 3 GPS 1 Switching Relay Discrete Output DARLINGTON Can be used to operate a switching relay whenever GPS 1 or Lora...

Page 39: ...output which transmits selected course and selected heading for ARINC 429 Long Range Nav receivers 24 AWG twisted shielded pair wire is required for these functions P3 12 Ch1 RS 232 TX Output P3 30 C...

Page 40: ...cs SN3308 Navigation Display Installation Manual 90106 IM G 4 Installation Manual W SIG doc Page 40 P3 18 High Speed Clock P3 36 High Speed Clock P3 19 High Speed Data P3 37 High Speed Data Reserved f...

Page 41: ...nnot be called up accidentally during flight B Once the Maintenance Menu is entered press the NEXT or LAST softkeys to cycle the MAINTENANCE MENU pages Use the UP DOWN arrow keys for selections and ro...

Page 42: ...n Manual 90106 IM G 4 Installation Manual W SIG doc Page 42 5 Operating Details For an explanation of the operating controls of the SN3308 refer to the Pilot s Guide for the SN3308 Sandel Avionics P N...

Page 43: ...l situation indicator or a CRT or power supply failure within an electronic horizontal situation indicator Sandel Avionics will be demonstrate through service experience that the projection lamp will...

Page 44: ...ssist the jackscrew in this manner turn a turn at a time If you have difficulty in removing the SN3308 the upper two clamp screws may not have been loosened sufficiently DO NOT apply excessive torque...

Page 45: ...mately 10 degrees from vertical The filament of the lamp will line up with two small V notches in the two sides of the lamp housing which can be used as a visual reference Reinstall the top cover usin...

Page 46: ...tray continue rotating the jackscrew counter clockwise until the SN3308 is fully engaged in the tray connectors Reinstall the single size 8 32 screw in the lower left of the SN3308 Tighten the two upp...

Page 47: ...ll associated avionics equipment Enter the change of the projection lamp and inspection and test record into the aircraft maintenance records and present a copy of the description of work accomplished...

Page 48: ...for selections and rotate the right knob to adjust and select On some menus additional soft key legends will appear as prompts Escape the maintenance menus by pressing NEXT repeatedly to step through...

Page 49: ...urns or the fluxgate is turned manually If this is not the case the following troubleshooting procedure can be used to diagnose fluxgate problems It is sometimes difficult to determine wiring errors b...

Page 50: ...Peaking adjustment At a heading of North where X and Y are numerically equal but opposite changing the Peaking adjustment should not allow increasing the X or Y level more than 10 This does not norma...

Page 51: ...ontrol knob to adjust Align the aircraft at each cardinal heading and adjust the corresponding calibration item to the exact heading 4 BRG PTR SETUP BRG NAV 1 429 NAV 2 429 COMP BRG ADF 1 DISABLED ADF...

Page 52: ...lects DISABLED DC SIN COS DC SIN COS for Collins receivers Synchro Normal and Synchro 180 to reverse bearing 180 degrees 5 DME 1 SELECT CURRENT SELECTION NOT INSTALLED NOT INSTALLED ANALOG 40MV MILE S...

Page 53: ...ILE SERIAL ARINC 568 SERIAL KING DIGITAL Purpose Selects DME 2 Instructions Use n and p or HDG control knob to choose and use the SET softkey to select When the SET softkey is depressed the active sel...

Page 54: ...E HOLD input ACTIVE HIGH or ACTIVE LOW signals for the DME s selected on page 5 and 6 See drawing DME KING SERIAL AND ANALOG for interface when wiring P2 3 as DME1 NAV2 DME 2 HOLD Allows the DME 2 HOL...

Page 55: ...urpose Changes the output of the heading course datum signals for the flight control system to DC KI 525 or NSD360 emulation or AC IN 831 PN101 emulation The selections by manufacturer name select def...

Page 56: ...1 33 these values were shown in arbitrary units not in volts deg a Engage the autopilot in HDG mode After the aircraft is established on the desired heading move the heading bug a large amount and ens...

Page 57: ...ingle item and have been separated in software 1 34 to support the Sperry SPZ 500 and similar autopilots which use opposite phase on CRS and HDG The other settings in this menu are not for installer a...

Page 58: ...GX RS 232 ENH GARMIN 150 RS 232 GARMIN 250 RS 232 GARMIN 150XL RS 232 GARMIN 250XL RS 232 GARMIN 155 RS 232 GARMIN 165 RS 232 GARMIN 155XL RS 232 GARMIN 300 RS 232 GARMIN 300XL RS 232 GARMIN 150 ARIN...

Page 59: ...s for illustration purposes only To view all the choices of LNAV receiver scroll through the list using the right knob 12 LNAV 1 2 CHANGE NONE ANNUN DISCRETE COURSE KNOB DEVIATION ANALOG IN OBS ROT NO...

Page 60: ...cs SN3308 Navigation Display Installation Manual 90106 IM G 4 Installation Manual W SIG doc Appendix A Page 13 an ARINC 429 interface the OBS information is transmitted to the receiver via the ARINC 4...

Page 61: ...on of the marker beacon receiver If none is installed select NONE Instructions Use n and p or HDG control knob to move the cursor and use the SET softkey to select 14 MKR CHANGE NONE MKR VALID DISABLE...

Page 62: ...s disables ILS Lockout feature of the ILS Energize input pins Disabling lockout will allow total manual control by the pilot See Nav Interface description Normally set to NO COMPOSITE Calibrates the c...

Page 63: ...o VIR 30 or KNR 634 STEP COMMENTS 1 Set nav test set to zero degrees and SN3308 course pointer OBS to zero degrees 2 Go to the NAV maintenance page on the SN3308 and adjust the NAV 1 OBS calibration t...

Page 64: ...on for Garmin GNS receivers when grounded ungrounded This is only used in a dual SN3308 installation which has Pilot Copilot select for the autopilot See installation drawings In a typical pilot only...

Page 65: ...rs If you use P2 19 or P2 37 an EXTERNAL pullup resistor must be tied to aircraft power 10K Ohms is sufficient NAV 1 GPS 1 GPS 2 Enable for any relay when a single relay is operated from the NAV 1 GPS...

Page 66: ...Rev 1 CPU Rev 0 INTERNAL TEMP 30q C 85q F FAN RPM 6600 INVERTER INPUT 400 Hz INVERTER Vp p 36 00 COLOR SELECT PILOT 400 Hz INVERTER DISABLED BOOTSTRAP OUT ENABLED WX DETECTION OFF Purpose Shows some h...

Page 67: ...splay Check the inverter at low and high battery voltage for correct tolerance The displayed voltage is peak voltage which for a sine wave inverter will be approximately 36v and for a square wave inve...

Page 68: ...M PAGE Purpose Displays setup data used in WX 500 installations Refer to the BFG WX 500 installation manual for instructions on the information contained in this page 20 WX 500 DATA WX 500 DISABLED IN...

Page 69: ...the pilot s buttons when the brightness control is turned up Adjust at dusk V Cal 14 I Cal 14 I Cal 28 Factory adjustments Do not change unless on instruction of the factory To prevent inadvertently c...

Page 70: ...t perform this calibration if the aircraft is on battery only i e at 12 0v or 24 0v During this operation the lamp will automatically be brought to maximum brightness and measured over a period of 30...

Page 71: ...Sandel Avionics SN3308 Navigation Display Installation Manual 90106 IM G 4 Installation Manual W SIG doc Appendix A Page 24...

Page 72: ...is may be helpful in diagnosing installation wiring problems Please note that AC signals are shown peak so a 26 volt sine wave input will show as approximately 36 volts while a 26 volt square wave wil...

Page 73: ...Break Usually indicates inputs to SN3308 are wired backwards If also associated with framing errors may indicate the wrong baud rate selected from the sender Overrun Usually indicates baud rate of se...

Page 74: ...short time operating 4 5 2 Equipment tested to Table 4 1 High temperature survival 4 5 2 Equipment tested to Table 4 1 High temperature operating 4 5 3 Equipment tested to Table 4 1 In flight loss of...

Page 75: ...19 0 Equipment tested to Category B Radio frequency susceptibility 20 0 Equipment tested to Category W Radio frequency emission 21 0 Equipment tested to Category A Z Lightning induced transient susce...

Page 76: ...rnational GPS 165 GPS Navigation Receiver Approved for En route Terminal and Non precision Approach or as appropriate 2 AlliedSignal Electronics and Avionics KX 165 Communications and Navigation Recei...

Page 77: ...J A system design and analysis was conducted with reference to Advisory Circular 2X 1309 1 or as appropriate K Federal Aviation Regulations 2X 1301 2X 1309 a b and d 23 1311 2X 1321 a b and d 2X 1322...

Page 78: ...d marker beacon and GPS annunciators if the aircraft is appropriately equipped and configured SECTION II LIMITATIONS 1 The SN3308 Navigation Display Pilots Guide SPN 90106 PG applicable revision must...

Page 79: ...o the HSI course pointer and the autopilot ILS override will prevent selection of the GPS as long as an ILS frequency is tuned on VOR ILS 1 This will be annunciated on the SN3308 Navigation Display Th...

Page 80: ...d by the installing agency and a copy must be installed in the aircraft maintenance records A copy must also be forwarded to Sandel Avionics along with the Warranty Registration Form Part Number 10129...

Page 81: ...Installation Manual W SIG doc Appendix E Page 2 COMPANY NAME COMPANY ADDRESS TELEPHONE FAX Ground Test Procedures Report for Sandel Avionics SN3308 Installed in aircraft make and model Registration No...

Page 82: ...gyro Compass input from fluxgate sensor if installed Navigation data inputs VOR ILS GS ADF DME GPS and FMS if installed Annunciator inputs from a marker beacon receiver if installed Annunciator inputs...

Page 83: ...necessary to adjust the externally mounted SN3308 dimmer control to obtain satisfactory brightness level CHECK SOFTWARE OPERATING VERSION NUMBER AS DISPLAYED ON TOP OF SCREEN CHECK WEBSITE OR WITH TEC...

Page 84: ...ass card is displayed in amber AND that a warning message is displayed on the SN3308 which requires operator acknowledgement Completed _______ Comment __________________________________ 11 1 8 NAV Sou...

Page 85: ...ected nav source but instead displays a warning message Completed _______ Comment __________________________________ Verify that the external NAV GPS switch arrangement correctly controls the selected...

Page 86: ..._________________________ If a single DME receiver is installed and is switchable between NAV1 and NAV2 Verify that pushing NAV to select between NAV1 and NAV2 causes either the correct DME readout to...

Page 87: ...a HOLD mode which enables course resolver input Garmin select the OBS or HOLD mode and verify that rotating the course select knob turns the course pointer Verify that the needle centers on the correc...

Page 88: ...urse select knob is turned and the course pointer moves around the SN3308 display Completed _______ Comment __________________________________ 11 1 14 Stormscope Interface If the SN3308 is interfaced...

Page 89: ...____________________________ Repeat for the secondary communications radio Completed _______ Comment __________________________________ Tune the primary navigation radio to 112 MHz and enable the audi...

Page 90: ...sual interaction between the transponder DME ADF or Marker Beacon receivers and the SN3308 when switching power to any equipment Completed _______ Comment __________________________________ 11 2 3 Add...

Page 91: ...r the purpose of simplifying the in flight operational check of the SN3308 A copy of this report and the Functional Ground Test Procedures Report in Section C 1 must be retained by the installing agen...

Page 92: ...4 Installation Manual W SIG doc Appendix E Page 13 COMPANY NAME COMPANY ADDRESS TELEPHONE FAX Flight Test Procedures Report for Sandel Avionics SN3308 Installed in aircraft make and model Registratio...

Page 93: ...the person performing the procedure and a space for a description of any observations or anomalies Determination of a successful flight test is made after analysis of these observations 11 5 Test Pro...

Page 94: ...ources as installed Completed _______ Comment __________________________________ Verify proper operation of one or both long range nav receivers as installed both as nav sources and as bearing pointer...

Page 95: ...tions Conduct at least one fully coupled ILS approach in VFR conditions for each VHF nav receiver installed During the approach verify proper operation of x Lateral deviation display CDI in both ARC a...

Page 96: ...VER INTERCONNECT 90106 10 pp 10 G2 GPS SWITCH ANNUNCIATORS 90106 10 pp 11 G2 GYROS XYZ AND KG 102 90106 10 pp 12 G2 GYROS 328 A3G AND XYZ 90106 10 pp 13 G2 GYROS MID CONTINENT S TEC BOOTSTRAP 90106 10...

Page 97: ......

Page 98: ......

Page 99: ...S ARE REQUIRED FOR PS ENGINEERING MARKER RECEIVERS RECOMMENDED FOR OTHER RECEIVERS TO PREVENT FAILURE OF THE SN3308 INDICATION IF THE ASSOCIATED MARKER LIGHT BULB FAILS NOTES 2 SELECT THE APPROPRIATE...

Page 100: ...ENGINEERING MARKER RECEIVERS RECOMMENDED FOR OTHER RECEIVERS TO PREVENT FAILURE OF THE SN3308 INDICATION IF THE ASSOCIATED MARKER LIGHT BULB FAILS NOTES 2 SELECT THE APPROPRIATE MARKER BEACON RECEIVER...

Page 101: ...PS ENGINEERING MARKER RECEIVERS RECOMMENDED FOR OTHER RECEIVERS TO PREVENT FAILURE OF THE SN3308 INDICATION IF THE ASSOCIATED MARKER LIGHT BULB FAILS NOTES 2 SELECT THE APPROPRIATE MARKER BEACON RECEI...

Page 102: ...LLATION PAGE IF SPECIFIC RECEIVER NOT SHOWN USE KMA 24 SETTING NOTE 1 2 10 23 00 G INITIAL RELEASE DATE REV COMMENTS COMPUTER CONTROLLED DRAWING DO NOT REVISE MANUALLY CW 25 6 24 3 7 FLUXGATE EXCITATI...

Page 103: ...AGE WHICH DOES NOT REQUIRE THE RESOLVER SWITCHING RELAY WHERE APPLICABLE 4 THE PREFERRED INSTALLATION IS THE SN3308 P3 3 CONTROLLING AN EXTERNAL SWITCHING RELAY IF AN EXISTING SWITCH CONTROL BOX IS IN...

Page 104: ...PS TO THE AUTOPILOT MAY HAVE TO BE AN ADDITIONAL RELAY SEE THE MANUFACTURERS INSTALLATION DIAGRAMS 5 KLN 90B PINOUTS SHOWN CERTAIN CONNECTIONS SUCH AS GPS_DISPLAYED AND OBS LEG ARE SPECIFIC TO KLN 90B...

Page 105: ...STAR M3 1200 Bd C 12 10 98 B A 3 19 99 PAGE COUNT NOTE 7 CHANGED PAGE COUNT 7 10 98 6 9 98 INCORPORATED A R 126 ADDED SHEETS 17 21 DO NOT REVISE MANUALLY 9 10 98 E COMPOSITE NAV 2 CHANGED TO P1 10 NOT...

Page 106: ...MOTE CLEAR PWR GND 3 P1 6 WX500 OPTIONAL REMOTE CLEAR NOTE 4 SEE MFG S INSTALL MANUAL FOR HEADING FLAG INTERCONNECT 14 32 RS232 TX P3 RS232 RX 30 J3 20 8 RS 232 2 TX J2 5 RS232 GND 6 7 CONFIG GND CONF...

Page 107: ...E 20 3 22 21 2 13 5 4 K I COMMON NAV CONVERTER INTERCONNECTS ROTOR RET ROTOR DRIVE SIN RET COS RET STATOR REF 10 B D J H 2 11 10 C 3 14 OBS RESOLVER SIN OUT OBS RESOLVER H IN OBS RESOLVER COS OUT 28 3...

Page 108: ...THIS MATRIX USE NEAREST COMPATIBLE SETTING OF THE SAME MANUFACTURER AND INSURE THE TEXT AND COLORS OF THE ON SCREEN ANNUNCIATORS ARE ACCEPTABLE ANNUNCIATORS COMMANDS ARM CMD ARM CMD NOTE 4 NOTE 4 4 M...

Page 109: ...V EXT LO FV Y METER DRV GROUND 5V SLAVE CW CCW P1 7 3 KA 51 SLAVING ACCESSORY REMOVAL NOTE 5 H E B SN3308 GROUND FG EXCITATION KA51 SLAVING ACCESSORY NOT USED N C 3 5 4 E F B C D A KA51 E F C B D J P5...

Page 110: ...INSTALL ACCORDING TO MANUFACTURERS RECOMMENDATION IF FLUX GATE REQUIRES LESS THAN 26VAC USE A PAIR OF SERIES RESISTORS 2 WATT ONE IN EACH DRIVE LEAD TO PROVIDE THE CORRECT DRIVE VOLTAGE 3 THIS INTERC...

Page 111: ...Y Fluxgate Y Fluxgate X Fluxgate Z Fluxgate Z POWER 13 E D 14 5 6444 8100 GYRO AVIONICS BUS B J1 10 GROUND 4 A Exc H DG Y DG X DG Z Exc H Exc C PHASE 1 12 SLAVING 18 17 SLAVING 6444 8140 FLUXGATE STEC...

Page 112: ...D RESOLVER H RESOLVER F RESOLVER D b HDG CT Z HDG CT C Z D L TO c GS DEV DOWN GS DEV UP j 15v v J B c P X LIGHTING CT NAV FLAG H N 15v e SLAVING CT Y HDG ERROR f Y 5v Y HDG CT Y HDG CT H P101 28v NAV...

Page 113: ...50 DC COS 10 12 COLLINS ADF 650A 35 SN3308 P2 17 DC COS DC SIN 18 DC REF DC REF DC SIN DC COS 37 SN3308 P2 19 DC COS DC SIN 36 DC REF DC REF DC SIN DC COS ADF 1 BENDIX KING KR 87 ADF Y X Z SN3308 17 Y...

Page 114: ...MANUALLY COMPUTER CONTROLLED DRAWING 5 26 99 F TOTAL SHEETS CHANGED TO 21 SANDEL SN3308 P2 16 34 15 OM MM IM MARKER RECEIVER OM MM IM LAMP COM NOTE 1 EXTERNAL MARKER LAMPS IF INSTALLED NOTE 2 THESE LO...

Page 115: ...1 or 2 Nav 2 Nav 1 10 23 00 G ADDED KN 64 DME ADDED NOTE 5 DME REQ 27 NOTE 2 9 10 8 DATA DME HOLD DME1 P2 DME1 HOLD SANDEL SN3308 CLK P3 DUAL KING SERIAL DIGITAL DME S CLK DME REQ DATA DME REQ 7 NOTE...

Page 116: ...AS SYNCHRO Z LEGS DO NOT USE FOR DIGITAL SIGNALS OR POWER 1 USE 20AWG WIRE BOTH GROUNDS AND BOTH POWER LEADS REQUIRED 3 MOUNT DIMMER CONTROL NEAR INSTRUMENT WITHIN REACH OF THE PILOT CW INDICATES CLOC...

Page 117: ...MODE COURSE CHANGES RESPECTIVELY EXCEPT FOR KI 525 THESE VALUES WILL BE IDENTICAL NOTES 7 8 8 20 98 C CENTURY IV CHANGED CENTURY 2 3 MOVED OFF PAGE NOTES CHANGED PAGE COUNT CRS DATUM 7 SN3308 DATUM EX...

Page 118: ...DE AND NAV MODE COURSE CHANGES RESPECTIVELY NORMALLY THESE VALUES WILL BE THE SAME 3 GROUND CONNECTIONS TO SN3308 SIGNAL GROUND 4 DO NOT GROUND ANY CENTURY II III SIGNALS EVEN DURING TROUBLESHOOTING T...

Page 119: ...1901 SN3308 7 CRS HDG DATUM LO 26 4 HDG DATUM HI P2 CRS DATUM HI P1 SIGNAL GND 16 2 28 DC CRS DATUM DC HDG DATUM J2252 J2251 COMMENTS DATE REV DO NOT REVISE MANUALLY COMPUTER CONTROLLED DRAWING 10 23...

Page 120: ...UM SIGNAL GROUND 46 DC HDG HI DC HDG LO DC HDG DATUM 8 4 P1 SIGNAL GND 26 SIGNAL GROUND DC HDG LO 35 S TEC 20 30 T C R C P2 SN3308 DC HDG HI P1 7 SIGNAL GND P2 2 26 SIGNAL GROUND 4 3 SN3308 J3 P1 DC H...

Page 121: ...LL COM ROLL COM HDG SIG CRS SIG HDG DATUM LO HDG DATUM HI CRS DATUM HI CRS DATUM LO C D z t FCS 810 AUTOPILOT P1 4 400 HZ INPUT P6 X BENDIX POWER SUPPLY 3 ANY COMMERCIAL 75MW OR GREATER AUDIO TRANSFOR...

Page 122: ...7 GPS 429 Out A 29 VLOC 429 Out A TO AUTOPILOT P4001 GPS 429 In B Port 1 24 GPS 429 In A 1 2 SN3308 ANALOG 429 Out A P3 1 GPS 429 Out B 10 49 51 P4006 Connection to One Port ONLY 48 49 OR 50 51 VLOC 4...

Page 123: ...5001 P5001 P5006 RELAY POWER 9 429 OUT B 429 OUT A GPS 429 IN A PORT 3 NAV 2 RELAY GPS 429 IN B PORT 1 COMPOSITE IN 2 COMPOSITE IN 1 GPS 429 IN A PORT 1 NAV 429 IN A PORT 2 NAV 429 IN B PORT 2 5 GPS 2...

Page 124: ...mposite Out OBS Resolver H In FROM Nav Left OBS Resolver SIN Out GS Flag GS Down Nav Right OBS Resolver COS Out Nav Flag GS Up OBS Resolver E VREF In Nav Flag TO GS Flag 28 15 19 16 13 36 34 18 14 17...

Page 125: ...27 P3 P1 10 P3 21 26 7 5 P3 10 28 26 7 P5006 RELAY POWER 9 429 OUT B GPS 429 IN A PORT 3 429 OUT A NAV 2 RELAY NAV 2 RELAY GPS 429 IN B PORT 1 COMPOSITE IN 2 COMPOSITE IN 1 NAV 429 IN A PORT 2 GPS 429...

Page 126: ...IN 1 NAV 429 IN A PORT 2 GPS 429 IN A PORT 1 NAV 429 IN A PORT 2 NAV 429 IN B PORT 2 NAV 2 SENSE CDI SRC SEL NAV 429 IN B PORT 2 5 GPS 2 RELAY 10 GPS 429 IN B PORT 3 SANDEL SN3308 P2 P2 RCVR1 2 SENSE...

Page 127: ...PAGE COUNT COMPUTER CONTROLLED DRAWING DO NOT REVISE MANUALLY 5 26 99 F TOTAL SHEETS CHANGED TO 21 NOTE ON DME 40 SOFTWARE 3 DME 40 ARINC 568 DME SUPPORTED IN SOFTWARE 1 32 AND LATER SYNC 27 9 10 8 D...

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