Sandel ST3400H HeliTAWS Installation Manual Download Page 75

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8 SENSOR COMPATIBILITY

Note:

Current equipment list is being constantly updated. Please contact factory if equipment

for your installation is not listed.

The following information may be added to and superseded by additional compatibility
information in the future without invalidating the other information in this manual.

8.1 Position

MFG

MODEL

INTERFACE TYPE

Freeflight

1201

RS-232

Garmin

Use with non-WAAS
400/500 series requires
software 1.06 (non Mod-A
ST3400H) / A1.07 (Mod-A
ST3400H) or higher.

GPS/GNS/GNC
400/400W,
420/420W,
430/430W,
500/500W,
530/530W
GTN6XX/7XX

RS-232

8.2 FMS Flight Plan

MFG

MODEL

INTERFACE TYPE

Freeflight

2101

ARINC 429

Garmin

GPS/GNS/GNC
400/400W,
420/420W,
430/430W,
500/500W,
530/530W
GTN6XX/7XX

ARINC 429

Honeywell

KLN-89

RS-232

Honeywell

KLN-90B

ARINC 429

Honeywell

KLN-94

RS-232

8.3 Radar Altimeter

MANUFACTURER

MODEL

INTERFACE TYPE

Bendix/King

KRA405

ANALOG

Bendix/King

KRA405B

ARINC 429

Collins

ALT50

ANALOG

Collins

ALT50A

ANALOG

Collins

ALT55

ANALOG

Freeflight

RA-4500

ARINC 429

Sperry

RT-220/300

ANALOG

Mil - 81296d (As)

RT804/805

ANALOG

Honeywell

APN-209

ANALOG

Various

ARINC 429 Type

ARINC 429

82046-IM-K

ST3400H INSTALLATION MANUAL

Page 8-1

Summary of Contents for ST3400H HeliTAWS

Page 1: ...Helicopter Terrain Awareness Warning System Installation Manual Sandel Avionics 2401 Dogwood Way Vista CA 92081 Phone 760 727 4900 FAX 760 727 4899 Website www sandel com Email support sandel com 820...

Page 2: ...This page intentionally left blank 82046 IM K ST3400H INSTALLATION MANUAL Page ii...

Page 3: ...es to limitations regarding installation location and electrical interconnection information Section 1 4 1 Removed user defined obstacle provision statement Section 1 6 Formatting updated Section 1 6...

Page 4: ...added to indicate NVIS may require additional installation approval Additional inputs added N A Column added Section 7 11 Heading clarified as Optional Interface N A column added Section 7 12 Heading...

Page 5: ...erencing FAA accepted ICA Section 12 List of effective drawings updated G 25 AUG 2014 REVISED IAW AR 1416 Section 1 2 Added note to Limitations regarding display of DME arcs holding patterns and proce...

Page 6: ...d IAW AR1349 Section 4 Added human factors installation considerations Added Section 7 23 Accessibility and Operation D 05 OCT 2011 Revised IAW AR1189 Section 4 6 Rename P2 2 Corrected discrete labels...

Page 7: ...82046 IM K ST3400H INSTALLATION MANUAL Page vii Updated section 12 drawing list 82046 10 sheets 3 7 B 05 AUG 2010 Initial Release...

Page 8: ...This page intentionally left blank 82046 IM K ST3400H INSTALLATION MANUAL Page viii...

Page 9: ...figurations 2 1 2 2 1 Required Sensors Equipment 2 1 2 2 2 Optional Sensors 2 1 2 2 3 Recommended Optional Sensors 2 1 2 3 Pre installation Planning 2 2 2 4 Installation 2 4 2 5 Post Installation Proc...

Page 10: ...e 8 RADALT 6 10 6 9 Page 9 FMS Flight plan 6 12 6 10 Page 10 GPS Position 6 12 6 11 Page 11 TCAS 6 13 6 12 Page 12 STATUS 6 15 6 13 Page 13 BRT AUDIO 6 16 6 14 Page 14 OPTIONS 6 17 6 15 Page 15 POWER...

Page 11: ...c 8 3 8 8 Equipment Approval Basis 8 3 8 9 ARINC 429 Master Label List 8 4 9 ENVIRONMENTAL QUALIFICATION FORM 9 1 10 SUPPLEMENTAL TYPE CERTIFICATE 10 1 10 1 STC Permission 10 1 10 2 Part 27 AML STC 10...

Page 12: ...pe or class of aircraft must determine that the aircraft installation conditions are within TSO standards TSO articles must have separate approval for installation in an aircraft The article may be in...

Page 13: ...on annunciation as well as optional collective mounted momentary switches to control certain functions such as alert muting and modes The ST3400H may be installed in a single or dual installation The...

Page 14: ...o guarantee that every obstacle is charted or that every charted obstacle is in the terrain data 1 5 2 Keeping the databases current Updates to the databases can be obtained from the Sandel web site a...

Page 15: ...Airborne Low Range Radio Altimeter Incomplete ST3400H provides display only TSO C113 ETSO C113 Airborne Multipurpose Electronic Display TSO C118 ETSO C118 Traffic Alert and Collision Avoidance System...

Page 16: ...D connector shell Data Loading Front panel USB GPS Position ARINC 429 or RS232 GPS Flight plan ARINC 429 or RS232 Air Data ARINC 429 or Analog Heading ARINC 429 or ARINC 407 XYZ Gear Discrete active h...

Page 17: ...DD44F10JVL0 Connector 44 pin Plastic Hood Slide Lock and Contacts 1 32062 SD15F10JVL0 Connector 15 pin Plastic Hood Slide Lock and Contacts 1 32111 SD9F10JVL0 15 Connector 9 pin Plastic Hood Slide Loc...

Page 18: ...and maintained by the installing agency Another copy must be presented to the aircraft owner for entry into the aircraft maintenance records as well as a copy forwarded to Sandel Avionics along with...

Page 19: ...quipment Configurations 2 2 1 Required Sensors Equipment GPS position Gear only if the helicopter has retractable gear Audio system with available unswitched input 2 2 2 Optional Sensors Heading Displ...

Page 20: ...to step 3 NO Contact Sandel Avionics for guidance Additional FAA approval may be required 3 Determine that the aircraft has the minimum required sensors equipment See section 2 2 1 of this IM YES Go...

Page 21: ...l result in the aircraft remaining within acceptable weight and balance limits Reference section 1 6 2 Physical Dimensions YES Go to step 7 NO Adjust aircraft equipment loading as required to accommod...

Page 22: ...nd voltage checks Pay particular attention to presence of 28V on only the correct pins 0 ohm resistance check on ground pins to airframe ground and presence of inverter 400Hz if used only on the appro...

Page 23: ...For Continued Airworthiness information refer to Instructions for Continued Airworthiness in Section 11 82046 IM K ST3400H INSTALLATION MANUAL Page 2 5...

Page 24: ...32 output and the Flight plan data is connected to the receiver s GAMA ARINC 429 output 3 3 Heading System A Heading input is not required However without a heading system the terrain display will be...

Page 25: ...as well as analog pressure altitude Use of analog pressure altitude requires ST3400H with MOD 1 installed per SIL 3400H 01 3 7 Traffic The ST3400H supports Traffic input via single ARINC 429 input Tr...

Page 26: ...unctions These annunciator discrete outputs are available on J2 Caution Alert Warning Alert Taws Inhibit 3 9 3 External Control Discrete Outputs These control outputs are available Radalt Test TCAS In...

Page 27: ...a nominal level of 25mw or 150mw output by strapping jumpers on J3 If no jumper is installed the headphone output is disabled The speaker output if used must be directly connected to a dedicated 4 or...

Page 28: ...ing or special requirements air from an external avionics blower may be directed near the corner air inlets In helicopter installations it may be desirable to introduce a small amount of cooled air co...

Page 29: ...as follows NOTE Any installation location is acceptable provided the ST3400H is installed adjacent to the helicopter primary displays no greater than 6 between the edges of the bezels its display and...

Page 30: ...talled Later S N aircraft with VEMD installed The ST3400H is installed as a replacement to or in a location provisioned for a radar altimeter ST3400H ST3400H Figure 4 1 Airbus AS350 Series 82046 IM K...

Page 31: ...EC135 P1 T1 EC135 P2 T2 EC135 P2 T2 Figure 4 2 EC135 Series 82046 IM K ST3400H INSTALLATION MANUAL Page 4 4...

Page 32: ...and subscribe to appropriate FAR Parts 23 25 27 and 29 as well as AC 43 13 1 B and 2 A 6 MIL C27500 shielded wire and MIL W 22759 single conductor wire is recommended The use of ferrules or grounding...

Page 33: ...sult shall be 10 milliohms or less between the ST3400H case and the instrument panel Power Wiring To assure that the ST3400H will operate properly down to its rated minimum input voltage ensure that t...

Page 34: ...2 side 422 RS232 Rx 2 Radalt A In A429 A side 429 Radalt Analog DC ALT 50 55 ARINC 552 RT220 300 RT200 32 Radalt B In A429 B side 429 Radalt Analog DC ALT 50 55 ARINC 552 RT220 300 RT200 18 Radalt Val...

Page 35: ...low glideslope fly up indication 37 Lat LL Flag In In Lat LL Flag DC Note For use with external SUPERFLAG requires resistor 429 A side 429 23 Lat LL Flag In In Lat LL Flag DC 429 B side 429 8 Lat LL D...

Page 36: ...Speed 100Kbps 13 RS232TxD Out Spare R232 43 Air Data Valid In Discrete Programmable OPEN GND or OPEN 28 29 BC In In Discrete Programmable OPEN GND or OPEN 28 14 Gear In In Discrete Programmable OPEN G...

Page 37: ...t Ground In System Ground 4 Selectable Discrete Glideslope INH Annunciator default TCAS Inhibit Out Open Drain 12 Selectable Discrete TAWS INH Annunciator default Radalt MINS Annunciator Out Open Drai...

Page 38: ...sed in parentheses indicate functionality that is reserved PIN Name Signal Type dependent on system configuration 1 Reserved Do not connect 6 Strapping Common 500 Ohm out Strapping Common 2 Reserved D...

Page 39: ...H is swapped re using the configuration module will automatically reconfigure the new unit to the original aircraft configuration The ST3400 will may be operated with or without a configuration module...

Page 40: ...Vac rms 400Hz nom 320Hz 480 Hz limits 42Vac 50K Power 22 to 30 3Vdc Note 1 7Adc NA Radalt 30Vdc 33Vdc 100K Ana 13Vdc 14Vdc 100K Outputs Signal Type Nom Range Absolute Note 3 Max Load A429 5Vdc 70mAdc...

Page 41: ...e inactive state if an external connection fails If interfacing to discrete signals which do not supply a hard 0Vdc 27 5Vdc transition any input network may be used that ensures that the discrete inpu...

Page 42: ...ffects of the settings Re enter the maintenance pages by pressing and holding the M button To disable the maintenance menu operation power down and restart normally All configured items are stored in...

Page 43: ...ST3400H TO CM stored The current ST3400H configuration is written to the configuration module and stored NOTE When selecting this option ST3400H configuration data will be written TO the configuratio...

Page 44: ...enus by pressing and holding the M button This will allow normal operation of the unit to test the effects of the settings Re enter the maintenance pages by pressing and holding the M button To disabl...

Page 45: ...sor to the next down selectable item Hold key down to automatically repeat When there are no selectable items the key is disabled VALUE Provides access to read secondary data from a piece of equipment...

Page 46: ...the BRT MINS The SELECT soft key is then pressed to jump to this page When in the Maintenance pages press the OPER soft key to return to the Maintenance Index page The PREV or NEXT soft keys may also...

Page 47: ...isplays UPS CCA revision CPU CCA Rev None Displays CPU CCA revision Software Rev None Displays software revision number Terrain Rev None Displays terrain database revision number Obstacle Rev None Dis...

Page 48: ...ge if applicable and pin pairs of the selected signal Configuration Field Options Comment PA NONE 429 429H Configures the air data PA source Type I Analog DC voltage inversely linear with pressure Ran...

Page 49: ...t If no valid signal is available for the interconnected equipment set this to NONE which will treat the signal inputs as always valid If a VALID signal is available set appropriately to VALID HIGH or...

Page 50: ...se from the HSI discrete input may be ACTIVE LOW or ACTIVE HIGH Valid Sense This is used to inhibit the Glideslope alert GPWS mode 5 Configuration Field Options Comment BCKCRS NONE ACTIVE L ACTIVE H 4...

Page 51: ...NE RA Self Test OUT TCAS S Test SW P2 12 NONE TAWS INH Ind RA MINS Ind P2 14 NONE WARNING Ind TCAS Mode SW P2 7 NONE CAUTION Ind TCAS S Test SW P2 4 NONE GS Inhibit Ind TCAS Inhibit P2 15 NONE MUTE Ac...

Page 52: ...hosen and data will appear in the data VALUE area The data VALUE shows only a single data item This page has an additional soft key labeled VALUE which can be used to scroll through all of the NAV and...

Page 53: ...ent type i e ALT55 for Collins ALT55 altimeter etc Once the equipment is selected the Radar altitude can be read from the data VALUE line to check for correct operation For analog inputs a correspondi...

Page 54: ...V RT805 MIL 81296D AS 40mv Ft Range 0 to 1 000 ft Flags 46 7V APN 209 7mv Ft Range 0 to 1 500 ft Flags 11 275V VALID NONE HIGH LOW Not shown when 429 429H FF RA 429 FF RA 429H or NONE is configured CA...

Page 55: ...ll be automatically made based on the selection chosen and data will appear in the data VALUE area The data VALUE shows only a single data item This page has an additional soft key labeled VALUE which...

Page 56: ...selection chosen and data will appear in the data VALUE area This page has an additional soft key labeled VALUE which can be used to scroll through all of the TCAS DATA coming from the processor Use t...

Page 57: ...l CAS 67 Honeywell CAS 81 Ryan 9900BX TAS Select the appropriate model of GPS from the list Press the SET soft key SENS button to program Note The Goodrich TFC Displays include push buttons to control...

Page 58: ...6 12 Page 12 STATUS The Status page shows a composite status of all the ST3400H inputs 82046 IM K ST3400H INSTALLATION MANUAL Page 6 15...

Page 59: ...ut The low level output acts as master gain Initiate an audio level test by selecting the desired volume level and pressing the TEST soft key This may be used to show the result of changing the audio...

Page 60: ...ropriate line and select ON or OFF for each callout Radar Altimeter input is required for the Callouts to function NORMAL SENS is always configured to be enabled Table 1 below shows the Standard Mode...

Page 61: ...1 Curve STD RUS Used to select GPWS Mode 1 curve Standard STD or Russian RUS The RUS curve is for conformity with Russian certification If RUS is selected the Key field will display allowing entry of...

Page 62: ...Table 1 Standard STD Mode 1 Curve Table 2 Russian RUS Mode 1 Curve 82046 IM K ST3400H INSTALLATION MANUAL Page 6 19...

Page 63: ...Any of these items that are outside normal operating limits will post an on screen error by way of the systems built in test processes 6 16Page 16 SFTWR CRC Displays CRC values for the software and d...

Page 64: ...to the ST3400H connectors before installing the ST3400H 7 3 Install Sandel ST3400H TAWS into aircraft Enter the maintenance mode by press and holding the SENS and MUTE buttons while applying power to...

Page 65: ...r a valid GPS Position FMS may show invalid depending on model until valid Groundspeed is achieved RECORD ST3400H TAWS CONFIGURATION PAGE EQUIPMENT FUNCTION DATA TYPE 3 AIRDATA PA 4 HEADING HDG VALID...

Page 66: ...PAGE EQUIPMENT FUNCTION DATA TYPE 30 20 10 HIGH 14 OPTIONS LOW TACTICAL OBST ONLY Mode 1 Curve Key 82046 IM K ST3400H INSTALLATION MANUAL Page 7 3...

Page 67: ...atches the aircraft heading displayed on HSI or wet compass within 4 Degrees Heading Valid pull circuit breaker to go invalid HDG VALID Verify value of Mag Heading Valid indicates INVALID DATA Heading...

Page 68: ...ss and hold for 2 seconds invokes TAWS INH function Terrain is removed from the display GS Override GS INH Verify GS INH is displayed on pilot menu when external GS INH switch is pressed momentarily S...

Page 69: ...Set consult the Radar Altimeter Test Set manufacturer for Test Set operating instructions The tests that will be performed to validate the ST3400H operation with the Radar Altimeter will be tests def...

Page 70: ...ers and GPS Altitude 7 14FMS Flight Plan Optional Interface Select ST3400H to Maintenance Page 9 FMS SIGNAL FUNCTION RESULT PASS FAIL N A Flight plan GPS receiver locked on with valid signal 2 FLIGHT...

Page 71: ...f Airport SIGNAL FUNCTION RESULT PASS FAIL N A SENS SENS OFF APT Momentary presses should toggle through configured SENS modes If all SENS modes other than normal are inhibited the text NO ACTION will...

Page 72: ...COMPLETED Comments 7 22 Visibility Verify visibility of the ST3400H display from the pilot s seat View the display from normal expected viewing angles This should include viewing the display from all...

Page 73: ...ovided for equipment not listed EQUIPMENT TYPE Victim PASS FAIL N A GPS LOC GS HEADING GPS FLIGHT PLAN RADAR ALTIMETER AIR DATA 7 25 AUDIO TEST NOTE This test must be conducted with the aircraft engin...

Page 74: ...udio For this test each higher priority audio signal shall be tested separately and determined to be understandable and distinguishable PASS FAIL COMPLETED Comments While operating the self test on th...

Page 75: ...or higher GPS GNS GNC 400 400W 420 420W 430 430W 500 500W 530 530W GTN6XX 7XX RS 232 8 2 FMS Flight Plan MFG MODEL INTERFACE TYPE Freeflight 2101 ARINC 429 Garmin GPS GNS GNC 400 400W 420 420W 430 430...

Page 76: ...ndix King 634A ANALOG ARINC 429 Collins VIR30 31 32 ANALOG Collins VIR432 ARINC 429 Garmin GNS430 530 W ANALOG ARINC 429 Garmin GTN 650 750 ANALOG ARINC 429 8 6 Airdata MFG MODEL INTERFACE TYPE Chelto...

Page 77: ...put Applicable TSO of I F Equip Interface Type s Sandel Approval Required GPS Position YES TSO C145 146 RS 232 YES FMS Flight Plan NO TSO C15 ARINC 429 RS 232 NO Radar Altimeter NO TSO C87 Analog ARIN...

Page 78: ...ecksum 115 WYPT BEARING 136 VFOM 147 Magnetic Variation 150 Time HH MM SS 165 GPS Vertical Speed 167 ANP 247 HFOM 260 DATE 261 GPS Discrete 275 LRN Integrity 303 Waypoint Type 304 Waypoint ID LSB 305...

Page 79: ...elect Limits 016 DITS Control 130 Intruder Range 131 Intruder Altitude 132 Intruder Bearing 203 Pressure Altitude 204 Corrected Barometric Altitude 320 Own Aircraft Heading 270 Vertical Resolution Adv...

Page 80: ...mperature Variation 5 0 Equipment tested to Category B 5 C min Humidity 6 3 2 Equipment tested to Category B 65C 95 RH Operational Shock and Crash Safety 7 0 Equipment tested to Category B DO 160F Tab...

Page 81: ...Protection EUT Op Lightning Induced Transient Susceptibility 22 0 Equipment tested to category A3G33 Transient Protection EUT Op return to normal Op Lightning Direct Effects 23 0 Equipment identified...

Page 82: ...TAL TYPE CERTIFICATE 10 1STC Permission Please contact Sandel Avionics Inc for permission to use these STC s and to obtain the most recent Approved Model List AML 82046 IM K ST3400H INSTALLATION MANUA...

Page 83: ...10 2 Part 27 AML STC 82046 IM K ST3400H INSTALLATION MANUAL Page 10 2...

Page 84: ...82046 IM K ST3400H INSTALLATION MANUAL Page 10 3...

Page 85: ...82046 IM K ST3400H INSTALLATION MANUAL Page 10 4...

Page 86: ...82046 IM K ST3400H INSTALLATION MANUAL Page 10 5...

Page 87: ...10 3 Part 29 AML STC 82046 IM K ST3400H INSTALLATION MANUAL Page 10 6...

Page 88: ...82046 IM K ST3400H INSTALLATION MANUAL Page 10 7...

Page 89: ...82046 IM K ST3400H INSTALLATION MANUAL Page 10 8...

Page 90: ...82046 IM K ST3400H INSTALLATION MANUAL Page 10 9...

Page 91: ...sure installation integrity Inspect the unit for security of attachment Inspect buttons for legibility Inspect condition of wiring routing and attachment clamping Inspect knob operation Inspect front...

Page 92: ...eets the aircraft instrument panel Tighten all four 4 clamp screws 11 6Database Updates Database updates are not required Information regarding new database releases and the content details of the dat...

Page 93: ...10 sheet 4 D RADALT ANALOG 82046 10 sheet 5 B RADALT ARINC 429 82046 10 sheet 6 B HEADING ARINC 429 82046 10 sheet 7 C HEADING XYZ 82046 10 sheet 8 D NAV LOC ANALOG 82046 10 sheet 9 A NAV LOC ANALOG...

Page 94: ...2 EA 138 32 X 75 PAN HEAD 2 MACHINE SCREW CROSS RECESSED MS35216 29 OR EQ INSTALL 2 EA ADJUSTING SCREWS 164 32 X 2 00 PAN HEAD MACHINE 3 SCREW CROSS RECESSED MS35216 50 COMPLETE INSTALLATION PER INSTA...

Page 95: ...438 1 530 1 530 SUGGESTED PANEL CUT OUT REF ARINC SPECIFICATION 408A 005 M 01 005 M D C B A A B C D SCALE 1 2 NOTED SIZE CAGE CODE B REV 21 22 23 24 25 26 27 28 28 27 26 25 24 23 22 21 VISTA CA 82046...

Page 96: ...7 LAYOUT ST3400H CONFIDENTIAL PROPRIETARY RIGHTS NOTICE ALL RIGHTS RESERVED THIS MATERIAL CONTAINS THE VALUABLE PROPERTIES AND TRADE SECRETS OF SANDEL AVIONICS OF CALIFORNIA UNITED STATES OF AMERICA E...

Page 97: ...FLIGHT DISPLAYS 3 ANY OTHER INSTALLED LOCATION MAY BE ACCEPTABLE IF THE ST3400H DISPLAY IS VISIBLE IT S CONTROLS ARE ACCESSIBLE OR ARE SUITABLY REMOTE CONTROLLED CONTACT THE LOCAL FAA FOR GUIDANCE LT...

Page 98: ...HALL MEET THE INTENT OF 14 CFR 21 31 A AMDT 21 90 BY USING THE FOLLOWING AC43 13 1B CHG 1 CH 11 SEC 3 Inspection of Equipment Installation 11 31 36 SEC 4 Inspection of Circuit Protection Devices 11 49...

Page 99: ...pair Zone D 3 Separated Speaker Interface Zone C 4 Removed note and added reference to note 2 Zone B 3 Changed and revised Note 2 Zone B 1 2 Added Interconnection to audio mixer and strapping Zone A 3...

Page 100: ...101 Zone C 3 Changed note references to triangle notes 3 4 5 6 associated with Garmin Zones D 3 and B 3 Added wire numbers twisted pair ref on each interface 4 places Removed schematic for Trimble RS...

Page 101: ...2500 4 FOR APN 209 REQUIRES ACTIVE HI VOLTAGE THAT IS AN ENERGIZED SOURCE FROM THE RAD ALT IT COULD BE FROM THE CIRCUIT BREAKER DIRECTLY OR FROM J1 9 ON THE COPILOTS R T LTR DESCRIPTION DATE A Initia...

Page 102: ...AWING DO NOT REVISE MANUALLY 2 4 3 2 TITLE SIZE DWG NO SCALE SHEET REV NONE 2401 DOGWOOD WAY VISTA CA 92081 USA CAGE CODE ST3400H INSTALLATION DRAWING MOD 5 OF 15 CATEGORY RADALT ARINC 429 LTR DESCRIP...

Page 103: ...NSTALLATION DRAWING MOD 6 OF 15 CATEGORY HEADING ARINC 429 LTR DESCRIPTION DATE A Initial Release 04 12 2010 A1 07 30 2011 03 31 2015 REVISIONS Title block format change AR1189 B ARINC 429 TX A ARINC...

Page 104: ...7 Was sheet 6 Added ground to shields twisted pair and wire Nos Zone C 3 REVISIONS TITLE SIZE DWG NO SCALE SHEET REV NONE 2401 DOGWOOD WAY VISTA CA 92081 USA CAGE CODE ST3400H INSTALLATION DRAWING MOD...

Page 105: ...oved KX155 per the B K IM Zone B 3 Corrected Pinouts for LOC Flag and Course Dev signals per B K and Collins IMs Zone B 3 Changed to twisted pairs and added wire numbers Zones A 4 Thru D 4 Changed Not...

Page 106: ...VERT LL DEV IN FLY UP 22 7 GS FLAG GS FLAG GS DN GS UP NAV GS ANALOG VERT LL DEV IN FLY UP P ST9A22 ST9B22 P1 1N4005 DELAYED ILS 28V 28V RELAY ST9C22 ST9D22 ST9E22 17 1 5 COLLINS VIR 30 31 32 VERT LL...

Page 107: ...C 3 REVISIONS Updates for AR1418 Equipment selections added for Garmin GTN 6XX 7XX C TITLE SIZE DWG NO SCALE SHEET REV NONE 2401 DOGWOOD WAY VISTA CA 92081 USA CAGE CODE ST3400H INSTALLATION DRAWING...

Page 108: ...DESCRIPTION DATE A Initial Release 04 12 2010 A1 07 30 2011 REVISIONS Title block format change AR1189 B TITLE SIZE DWG NO SCALE SHEET REV NONE 2401 DOGWOOD WAY VISTA CA 92081 USA CAGE CODE ST3400H I...

Page 109: ...E SHEET REV NONE 2401 DOGWOOD WAY VISTA CA 92081 USA CAGE CODE ST3400H INSTALLATION DRAWING MOD 12 OF 15 CATEGORY AIRDATA ARINC 429 1 2 COLLINS ADC85 J2 Ports 1 3 1 Reqd HONEYWELL AM250 J1 Ports 1 4 1...

Page 110: ...ISE MANUALLY LTR DESCRIPTION DATE A Initial Release 04 12 2010 A1 07 30 2011 08 25 2014 REVISIONS Revised P2 2 text Title block format change AR1189 B REDRAWN AR1477 Was sheet 11 Changed Note 2 ref an...

Page 111: ...l Release 04 12 2010 A1 07 30 2011 08 25 2014 REVISIONS Title block format change AR1189 B REDRAWN AR1477 Was sheet 12 Added Shield Grounds Zones D 3 C 3 B 3 B 2 Added Interconnect Dia Goodrich SKY 49...

Page 112: ...various TITLE SIZE DWG NO SCALE SHEET REV NONE 2401 DOGWOOD WAY VISTA CA 92081 USA CAGE CODE ST3400H INSTALLATION DRAWING MOD 15 OF 15 CATEGORY DISCRETE INPUTS NOT REQUIRED USE ONLY IF PRESENT IN AIRC...

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