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2 INSTALLATION PLANNING AND PROCEDURES

The ST3400H has been designed to ensure maximum interoperability with external avionics.
Contact Sandel with any questions about interfacing to specific avionics equipment not covered
in the installation drawings in this manual.

2.1 General Information

To simplify installation, after signals are wired to the ST3400H pins, on-screen setups are used
in a post-installation procedure. Maintenance menu pages provide a function selection
capability. For most equipment, selections are made by equipment make and model.

Refer to the installation schematics section 12 of this manual, for details on connecting
required components.

2.2 Supported Sensor/Equipment 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

Display: Provides no-track terrain display

•

GPS Flight plan Display: displays flight plan line

•

Radar Altitude

GPWS: Provides callouts;

•

Airdata

GPWS: improves accuracy of certain modes

•

LOC/GS

GPWS: adds Glideslope alert

2.2.3 Recommended Optional Sensors

A Heading Sensor is highly recommended; without a heading system no terrain will be
presented on the display during hover operations or on-ground. When in maintenance mode,
with no heading system and track invalid, unit displays North Up.

Radar Altitude is highly recommended. This not only supplies numerous GPWS alerts, but
provides altitude callouts which provide an additional safety benefit.

82046-IM-K

ST3400H INSTALLATION MANUAL

Page 2-1

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Содержание ST3400H HeliTAWS

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

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

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

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

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

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

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

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

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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