2006 purchase planning handbook - aviation...

Business & Commercial Aviation n May 2006 171www.AviationNow.com/BCA

By Mal Gormley

Gordon Moore, co-founder of Intel,once famously observed that digitaldata density doubles every 18

months, with the result being less expen-sive, faster and more capable computers. Anaviation variant of the so-called Moore’sLaw is trickling down to the cockpits of thenewest light aircraft. As their size and costsdecline, the capabilities of integrated cir-cuits accelerate, creating more exciting pos-sibilities for avionics, especially glass cockpitdisplays and safety technology.

Seeing the trend, the aviation trainingcommunity is responding. Embry-RiddleAeronautical University, for one, is addingglass cockpits with ADS-B avionics to itsnewest Cessna 172s . Similar ly, theUniversity of North Dakota is purchasingseven Piper PA-28s equipped with Avidyne’sFlightMax Entegra integrated flight deck,along with Avidyne-supplied training sta-tions, for use at its John D. Odegard Schoolof Aerospace Sciences. Meanwhile, Avidynereports that Piper is adding glass cockpit ca-pabilities to several of its smaller general

aviation models, and Canada’s SymphonyAircraft will have the first two-seat singleequipped with an integrated glass instru-ment panel. And earlier, Meggitt/S-TECannounced its S-TEC System 55 autopilotswould be available as a factory-installed op-tion in Symphony’s new Avidyne Glass IFRconfiguration Symphony 160.

How does this impact business aviation?Graduates of these leading flight schoolswill be familiar with the integrated glasscockpit environments found in the newestbusiness and commercial aircraft, thus fa-cilitating their transition. Glass cockpits, nolonger a gee-whiz option, are now becom-ing commonplace.

The move to upgrade to ADS-B capabil-ity at this time makes sense in light of theFAA’s stated intention to initiate its ADS-Band SWIM (system-wide information man-agement) projects in its 2007 fiscal year,which begins Oct. 1. ADS-B and SWIMare two of the core capabilities of the FAA’sNext Generation Air TransportationSystem (NGATS). ADS-B will be an im-portant NGATS element because it out-performs radar in accuracy, detectioncapability, update rate and coverage — allat a lower cost, say FAA representatives. Theagency plans to install as many as 400 ADS-B ground stations across the United Statesand to decommission 200 or more radars.

Meanwhile, WAAS — the FAA’s long-overdue wide area augmentation system de-veloped to significantly increase locationaccuracy and reliability of precision ap-proach GPS positioning systems — finallyseems to be materializing. UniversalAvionics recently completed its first WAASflight test of its new “W” series flight man-agement system by conducting approachesat the Farmington, N.M., airport, which hastwo WAAS instrument approaches, and atTucson International Airport. Several hun-dred more WAAS approaches are expected

Avionics

WAAS and ADS-B are at hand, NDBs are near the end and EVS now has a place of its own. The digital revolution continues.

Symphony 160 cockpit with Avidyne Glass IFR B&

CA

172 Business & Commercial Aviation n May 2006

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www.AviationNow.com/BCA

BCA • ISSUE: May 2006PAGE: 172 / Version: #1

SideFront Rear

STANDARD ATR CASE DIMENSIONS

H

W+ 0.140" (3.56 mm)

Max

W+ 0.140" (3.56 mm)

Max

H +

0.0

63"

(1.6

0 m

m)

Max

L2

L2 + 2.57" (65.28 mm) Max

WL1

ATR Size Approx. Volume W L1 L2 (Max) H (Max)

In3 Liter ± 0.03 In ± 0.76 mm ± 0.04 In ± 1.0 mm In mm In mm

Dwarf 95 1.56 2.25 57.15 12.52 318.0 12.62 320.5 3.38 85.81/4 Short 215 3.52 2.25 57.15 12.52 318.0 12.62 320.5 7.62 193.51/4 Long 335 5.49 2.25 57.15 19.52 495.8 19.62 498.3 7.62 193.53/8 Short 340 5.57 3.56 90.41 12.52 318.0 12.62 320.5 7.62 193.53/8 Long 530 8.69 3.56 90.41 19.52 495.8 19.62 498.3 7.62 193.51/2 Short 470 7.70 4.88 123.95 12.52 318.0 12.62 320.5 7.62 193.51/2 Long 725 11.88 4.88 123.95 19.52 495.8 19.62 498.3 7.62 193.53/4 Short 720 11.80 7.50 190.50 12.52 318.0 12.62 320.5 7.62 193.53/4 Long 1,120 18.36 7.50 190.50 19.52 495.8 19.62 498.3 7.62 193.51 Short 975 15.98 10.12 257.05 12.52 318.0 12.62 320.5 7.62 193.51 Long 1,510 24.75 10.12 257.05 19.52 495.8 19.62 498.3 7.62 193.511/2 2,295 37.62 15.38 390.65 19.52 318.0 19.62 498.3 7.62 193.5

to become available throughout the year.Incorporated into Universal’s UNS-1Ew,1Fw and 1Lw FMSes, the new SCN 1000software takes advantage of the capabilitiesof WAAS for en route, terminal and instru-ment approach procedures.

In another example of trickle-down tech,Honeywell’s Bendix/King EGPWS (en-hanced ground proximity warning system)will be standard equipment on all CirrusSR20 and SR22 models. Using technologyderived from Honeywell’s air transport EG-PWS, the KGP 560 uses GPS positioninginformation and compares it to an internaldatabase of terrain and obstacles to providea moving map display of potential hazards,along with visual and audio alerts, shouldthe aircraft approach too close. EGPWS isHoneywell’s term for a terrain awarenessand warning system (TAWS).

Other recent avionics developmentsworth noting include:

äAvidyne is offering a new line of activesurveillance traffic systems for helicopters.The TAS600 series include Heads UpAudible Position Alerting and other featuresbeginning at $9,900. The company, whichacquired Ryan International in 2005, utilizesactive surveillance technology from Ryan’s

popular 9900BX system. The three newTAS600 series systems have a range of fea-tures that allow helicopter owners to selectthe price-performance level that best fitstheir aircraft and mission. The systems arecertified for installation on most helicoptersand are available as an option on newEurocopter EC135, EC145 and EC155 mod-els as well as the Agusta A119. The series,ranging in price up to $20,990, provides in-truder squawk codes and N-numbers ofMode S-equipped aircraft and show stan-dard TCAS symbology on display systemsfrom 15 different manufacturers includingAvidyne, Garmin, Honeywell, Collins,

Chelton, Sandel and others.äCMC Electronics and Jeppesen have

teamed up to integrate various componentsfrom each company to produce upgradedClass 2 electronic flight bags (EFB).Jeppesen will provide its software, data andapplications, including digital terminal chartand content administration tools, along withits airport moving map, and its soon-to-be-released en route moving map. CMC,maker of the Class 2 PilotView EFB sys-tem, will supply its installation-relatedSTCs and post-sale support services andwill serve as the system integrator. CMC’sEFB has been certified on the GlobalExpress and Pilatus PC-12, and will soon becertified on the Falcon 10 and 50, theGulfstream IV, and all Boeing 737 models,including the BBJ.

äMeanwhile, the FAA has approvedJeppesen’s terminal chart viewer, which wasspecifically designed for portable and semi-integrated Class 1 and 2 EFBs. Because ofthe FAA’s OK, Jeppesen claims it is the firstand only provider of digital aeronauticalcharts to have received operational approvalfor all three EFB classes. Jeppesen, alongwith its parent company, Boeing, already re-ceived operational approval for its Class 3

Cirrus SR20 and SR22 models will haveBendix/King EGPWS standard.

EFB chart viewing software, which offersthe same basic functionality as these Class1 and 2 systems. To qualify for the FAA ap-proval, Jeppesen’s terminal chart applicationneeded to satisfy a number of criteria, in-cluding human factors considerations andits ability to functionally replace papercharts. Even though the Jeppesen applica-tions are operationally approved, U.S. aircarriers must still gain specific approvalfrom their principal operations inspectorsand complete a six-month evaluation usingelectronic charts.

äWhen was the last time you shot anNDB approach? Although we still includeAutomatic Direction Finders in our listingsbecause they still show up on many opera-tors’ MELs, they soon may become mu-seum pieces. The FAA will cancel morethan 200 NDB-based flight procedures onJuly 7 and another group of more than 200on Sept. 7. This action follows a proposalin the U.S. Federal Register on March 3,2005, to eliminate what have become re-dundant instrument approaches. That no-tice included a listing of 480 NDBs slatedfor possible cancellation. The NationalFlight Procedures Office considered morethan 680 comments during the commentperiod. Since the agency is moving to satel-lite navigation, it wants to concentrate re-sources on the development, f l ightinspection and life-span maintenance ofnew WAAS-capable RNAV procedures. Tomeet the FAA’s criteria for NDB cancella-tion, the target NDB and an RNAV proce-dure must serve the same runway end.



CMC Electronic Flight Bag


äIn news from a technology you mayhave thought was already extinct: ARINCsays that its high-frequency data link(HFDL) is becoming more popular bothbecause of its high availability over muchof the globe, and its relatively low cost. Thecompany said there are more than 500 air-craft now using its GLOBALink/HF, in-cluding 125 that have signed up in the lastnine months alone. Michelle Kyle, who

manages ARINC’s HF business, says,“Many carriers are using HFDL instead ofsatellite, or as a backup.” Partly, it’s becauseof HFDL’s “seamless” coverage, especiallyat high polar latitudes where satcom cover-age becomes unavailable, and also over re-mote regions where ground-based VHFstations don’t exist. Airbus and Boeing havecertified most of their models for HFDL,and airlines often order new aircraft with

HFDL as standard, Kyle said. And becauseof the lower cost of HFDL avionics com-pared to satcom, it is considered cost effec-tive and reliable for digital data linkmessages. This is particularly true for cargocarriers and passenger carriers that are notplanning for passenger communications.ARINC launched its HFDL service in1998. Because HF signals can travel morethan halfway around the world, only 14HFDL stations are needed to provide re-dundant coverage for North Atlantic routesand supplemental coverage elsewhere, thecompany says. But to improve the network’sfunctionality even more, ARINC is in-stalling new electronics and software at all14 stations during 2006.

äIn related news, Airservices Australiahas begun operating an enhanced HF radiosystem that replaces the nation’s 30-year-oldnetwork. The new system should provide aclearer signal, with a greater range than theold network, and with less atmospheric in-terference, the service provider says. Thereare still a substantial number of aircraft op-erators in Australia’s vast interior that relysolely on HF for communications. In addi-tion, about 70 percent of aircraft inboundand outbound from Australia use HF radio.And a new HF air-ground radio system hasbeen commissioned by the Irish AviationAuthority and Iceland CAA to upgradetheir integrated North Atlantic service.

äARINC Direct is offering VHF digitalMode 2 data link service for Bombardier’snew Challenger 300 and other aircraftequipped with Rockwell Collins Pro Line21 data link equipment. The VDL servicewas deployed in May 2005 to coincide withthe first Challenger 300 customer delivery.In Rockwell’s integrated Pro Line 21 CNS(communications, navigation and surveil-lance) system, its digital VHF-4000 data ra-dio is paired with its RIU-4000 radiointerface unit or CMU-4000 communica-tions management unit to provide VDLMode 2 data link capability, which Rockwellexpects will grow in popularity as morebusiness jet users, as well as airlines, adoptthe technology.

äRockwell Collins says it has receivedthe first C166 TSO approval for ADS-Bfunctionality on Mode-S transponders. Theapproval enables the use of ADS-B to pro-vide enhanced traffic situational awarenesson the airport surface and/or advancedflight procedures, including visual acquisi-tion for see and avoid, sequencing andmerging, crossing and passing maneuvers,and oceanic in-trail operations. Accordingto Rockwell Collins, its TDR-94/94D (-108versions) are the first transponders to befully compliant with the RTCA DO-260Astandard, which ensures the integrity andaccuracy of data necessary to fully support

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the future surveillance applications that arebeing proposed for operations en route, interminal areas, in non-radar areas and onairport surfaces. Besides the FAA TSO, theTDR 94/94D transponders are approvedby the European Aviation Safety Agency(EASA) and standards to support both ele-mentary and enhanced surveillance, whichmeans the transponder can reply to ground-based SSR (secondary surveillance radar)interrogations that give air traffic controllersenhanced surveillance information. TheTDR-94/94D continues to support TCASII functions as well , Rockwell says.Operators with existing Pro Line radio in-stallations can update the TDR-94/94Dtransponders through appropriate servicebulletins.

This year we’ve added, a new category,Enhanced Vision Systems, to the avionicslistings. We invite you to take a look at whatwe believe will become another mainstreamtechnology in coming years. Although en-hanced and synthetic vision systems forcivilian use have been in serious develop-ment for more than a decade, it’s only in thepast few years that their true capabilities andutility have materialized. And like every-thing else we depend upon for flying safelythrough the weather and dark of night, thecost will doubtless continue to come down,making the technology available for an everwider segment of business aviation.

Indeed, Kollsman and Sandel recently an-nounced they are jointly developing EVSand SVS for use on smaller business aviationaircraft such as the new very light jets.Initially, the joint effort will focus on inte-grating Sandel’s advanced displays withKollsman’s ultra-compact HUD, called aMicroHUD. A follow-on program will addKollsman’s new heads-down FLIR capabil-ity, named GAViS, which would give the pi-lot improved visibility in darkness. In bothcases, the goal is to reduce the size and costof these advanced display technologies, mak-ing them affordable to a broader group ofbusiness and general aviation operators.Kollsman wants to get the price of its HUDdown to half the industry-standard $100,000,and to do the same for the infrared imager.The company sees certification of the GAViSoccurring by midyear and late this year forthe new HUD. In addition, Kollsman isflight-testing a combined enhanced and syn-thetic vision system, called ESViS, whichoverlays the sensor image on terrain com-puter-generated from an onboard database,being developed by Jeppesen. ESViS also in-cludes a Sandel TAWS. Its certification is ex-pected in early 2008.

All of which means we’ll keep watchingthis and other important avionics devel-opments and report on them as they happen. B&CA

Business & Commercial Aviation n May 2006 175

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AAAC — Advisory circular

ACARS — Airline communications addressing and reporting system

ACAS — Aircraft collision avoidance system

ADC — Air data computer

ADI — Attitude direction indicator

ADS — Air data system

ADS-B — Automatic dependent surveillance-broadcast

AES — Aircraft earth station

AFCS — Automatic flight control system

AFIS — Automated flight information system (Honeywell)

AHRS — Attitude-heading reference system

Air Data — Values computed from pitot, static and temperaturemeasurements, usually by means of a digital computer; ARINC 575defines outputs

AMLCD — Active matrix liquid crystal display

AMSS — Aeronautical mobile satellite service

AOA — Angle of attack

AOG — Aircraft on ground

A/P — Autopilot

ARINC — Aeronautical Radio, Inc.; a nonprofit corporation owned bymember airlines to define form, fit and function of avionics equip-ment and to provide radio communication services

ARINC 419 — Digital information transfer characteristics as appliedin ARINC 500-series equipment specifications

ARINC 429 — A standard for broadcast digital information transfersystems for general applications

ARINC 561 — Inertial navigation system specifications

ARINC 571 — Inertial sensor attitude-heading reference systemspecifications

ARINC 575 — Digital air-data system specifications

ARINC 700-series — All-digital equipment specifications for new-generation transport category aircraft

ASCB — Avionics Standard Communication Bus (Honeywell)

A/T — Autothrottle

ATI — Air transport indicator; standard case sizes ranging nominallyfrom 2 ATI to 6 ATI

ATM — Air traffic management

ATN — Aeronautical telecommunications network

ATR — Air transport radio; ARINC form-factor/standard case dimen-sions; 1 ATR = 8 MCU

AVOD — Audio/video on demand

BBBCD beam width — Included angle of weather radar interrogationsignal

B-GAN — Broadband global area network

BITE — Built-in test equipment

B-NAV — Basic area navigation; concept of easing congestion in Eu-ropean airways by requiring aircraft to be fitted with equipment thatwill allow more direct routings by ATC

BRG — Bearing

CCCAT — Clear air turbulence; high-altitude turbulence encounteredwhere no clouds are present

CAT I — An ILS approach providing operation down to a 200-foot de-cision height and an RVR of not less than 2,400 feet

CAT II — An ILS approach providing operation down to a 100-foot de-cision height and an RVR of not less than 1,200 feet

CAT IIIa — An ILS approach providing operation with no decisionheight to and along the surface of the runway with external visualreference during the final phase of landing and with an RVR of notless than 700 feet

CAT IIIb — An ILS approach providing operation with no decisionheight limit to and along the surface of the runway without relianceon external visual reference, and subsequently taxiing with an exter-nal RVR of not less than 150 feet

CAT IIIc — An ILS approach providing operation with no decisionheight limit to and along the surface of the runway and taxiwayswithout reliance on external visual reference

CCD — Cursor control device

CDI — Course deviation indicator

CDMA — Code division multiple access

CDU — Control display unit

CFIT — Controlled flight into terrain

CMOS — Complementary metal oxide semiconductor

CMU — Communications management unit

CNS/ATM — Communication, navigation, surveillance/Air trafficmanagement (supersedes “FANS” terminology)

COM — Communications

Contact Digitizer — A mechanical device that converts analog infor-mation to digital codes by means of electrical contacts

COTS — Commercial off the shelf (i.e., computer hardware, softwareor avionics)

CPDLC — Controller pilot data link communications

CRT — Cathode ray tube

CSDB — Commercial standard data bus

CVR — Cockpit voice recorder

DDDADC — Digital air data computer

DAMA — Demand-assisted multiple access (satcom broadband)

DAP — Datalink aircraft parameters

dB — Decibel; acoustic measurement unit

DBS — Direct broadcast satellite

DFDAU — Digital flight data acquisition unit

DGPS — Differential global positioning system; LA- prefix refers toLocal-Area DGPS; WA- prefix refers to Wide-Area DGPS signal re-transmission schemes

DH — Decision height

Digitizer — Electronic device capable of converting information to adigital format; usually refers to encoding devices that convertsensed altitude into a transponder code

DME — Distance measuring equipment

drms — Distance root mean squared

DRVSM — Domestic reduced vertical separation minimums

DTK — Desired track

DTU — Data transfer unit

Avionics Glossary

Duplex — Separate channels for transmission and receiving

EEE- (as a prefix) — Used with “ADI” or “HSI” to designate an electronic display using a CRT

EAROM — Electrically alterable read-only memory; a type of digital memory device

ECDI — Electronic course deviation indicator

EEPROM — Electrically erasable programmable read-only memory

EFIS — Electronic flight instrumentation system

EGNOS — European geostationary navigation overlay service

EICAS — Engine-indicating and crew-alerting system

EIDS — Electronic information display system

EL — Electroluminescent display

Eurocae — European Organization for Civil Aviation Electronics; a regulatory agency for avionics certification

FFFADEC — Full-authority digital engine control

FBL — Fly-by-light

FBW — Fly-by-wire

FCS — Flight control system

FD — Flight director

FDAU — Flight data acquisition unit

FDE — Fault detection and exclusion (GPS)

FDR — Flight data recorder

FLIR — Forward-looking infrared

FMCS — Flight management computer system

FMS — Flight management system

FOG — Fiber-optic gyro

GGGas Discharge — A type of luminescent digital display

GCR — Ground clutter rejection

GLONASS — Commonwealth of Independent States satellite navigation system

GLS — GPS landing system

GLU — GPS landing unit (provides precision GPS guidance to the runway in CAT III operations)

GNSS — Global navigation satellite system

GPADIRS — Global positioning, air data, inertial reference system

GPS — Global positioning satellite

GPWS — Ground proximity warning system

GS — Groundspeed

G/S — Glideslope

HHHF — High frequency

HFDL — High-frequency data link

HGA — High gain antenna

HIRF — High-intensity radiated field; sometimes seen as HERF (high-energy radio frequency or high-energy radiated fields)

HITS — Highway-in-the-sky

HPA — High-power amplifier

HSD — High-speed data

HSI — Horizontal situation indicator

HUD — Head-up display

Hz or Hertz — Cycles per second; used to describe radio frequencies; usually with the prefix k for kilo (1,000), M for mega (one million) or G for giga (one billion)

IIIAC — Integrated avionics computer; the central processor of a Honeywell integrated cockpit system

IAPS — Integrated avionics processing system; the central processor of a Rockwell Collins integrated cockpit system

ILS — Instrument landing system

Inmarsat — International Mobile Satellite Organization

INS/IRS — Inertial navigation system/inertial reference system

ITU — International Telephone Union, refers to certain HF channels

IVSI — Instantaneous vertical speed indicator

JJJAR — Joint Airworthiness Requirement; issued by the EuropeanJoint Airworthiness Authority (JAA)

LLLAAS — GNSS local area augmentation system

Laser IRS — Inertial reference system deriving angular rate informationby measuring Doppler shift between two contra-rotating light beams

L-band — A radio frequency between 390 and 1550 MHz

LCD — Liquid crystal display

LED — Light-emitting diode

LEO — Low Earth Orbit (satcom)

LNAV — Lateral navigation guidance

LOC — Localizer; the course guidance component of an ILS

Looks per minute — Scanning or sweep rate of a weather radar an-tenna

Loran-C — Hyperbolic grid navigation system based upon measuredtime differences (TD) from pulse transmissions

LPV — Localizer performance approach (WAAS)

LRU — Line replaceable unit

MMMCDU — Multifunctional control display unit; part of FMS

MDAU — Maintenance data acquisition unit

MDU — multifunction display unit

MFD — Multifunction display; the third or fifth tube in an EFIS, it re-places the weather radar screen and displays radar data, navigationmaps, checklists and other information

MNPS — Minimum Navigational Performance Specifications

MOPS — Minimum Operational Performance Standard (RTCA)

MTBF — Mean time between failures

NNNA — Not available

NANU — GPS notice advisory to Navstar users

NAT — North Atlantic Tracks

NMS — Navigation management system

NMU — Navigation management unit

NPA — Non-precision approach

NVM — Nonvolatile memory; digital memory that retains informationthrough system shutdown

OOOEM — Original equipment manufacturer

OM — Outer marker (glideslope)




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Optical Digitizer — Any device using a photo sensor that can convertanalog information to digital code

PPPCU — Passenger control unit (cabin system)

PDU — primary display unit

Peak Power Output — The maximum transmitter power outputmeasured over a short time; usually used to rate pulse transmissions

PEP — Peak envelope power; a standard electronic rating of any ACsource, including a radio transmitter

PFD — Primary flight display

Pulse — A transmission of very brief duration used to carry information by using time measurement or as a series of pulses representing code

PVT — Position, velocity, time (WAAS)

QQQFE — Field elevation pressure

QNH — Sea level pressure

RRRA — (1) Radio altitude; (2) Resolution advisory (TCAS)

RAIM — Receiver autonomous integrity monitoring (GPS)

RAM — Random access memory

RCU — Radio control unit

REACT — Rain echo attenuation compensation technique (Honey-well weather radar feature)

RF — Radio frequency

RFU — Radio frequency unit (satcom component)

RMI — Radio magnetic indicator

RMU — Radio management unit

RNAV — Area navigation

RNP — Required navigation performance

RS-232, RS-422 — Serial digital formats used for data transmission

R-T — Receiver-transmitter combined in a single line-replaceable unit

RTCA, Inc. — An association of U.S. governmental and industry aero-nautical organizations dedicated to advancing aeronautics throughconsensus and recommendations

RVSM — Reduced Vertical Separation Minimums

SSSAMPE — Society for the Advancement of Material and ProcessEquipment

SAR — Search and rescue

Satcom — Satellite communications system

SDU — Satellite data unit (satcom)

SELCAL — Selective calling system (used primarily with HF)

Simplex — Single frequency for both transmitting and receiving incommunications; generally implies a push-to-talk function and verbalprocedures

SITA — Societé Internationale de Telecommunications Aeronautique;an international organization providing global telecommunicationsand information services to the air transport industry

Squitter — The transmission of a specified reply format at a minimum rate without the need to be interrogated (transponders)

SSB — Single sideband; a highly efficient form of radio transmissionwherein information is carried on a sideband instead of the centercarrier in order to gain range performance; usually used in HF com-munication transceivers

SSCVR — Solid-state cockpit voice recorder

STC — Supplemental type certificate

Synchro — Any device capable of converting mechanical positioninto an analog electronic signal

Synthesizer — Frequency synthesizer; an electronic circuit capableof generating multiple frequencies from a single crystal oscillator

TTTA — Traffic advisory (TCAS)

TAS — True airspeed

TAT — Total air temperature

TAWS — Terrain awareness and warning system

TCAS — Traffic alert and collision avoidance system

TIS — Traffic information system

TKE — Track error

TMC — Thrust management computer

TO/GA — Take off/Go around; operating mode

TRK — Track over the ground

TSO — Technical Standard Order; a performance specification andproduction compliance criteria applied to avionics and defined byFARs and RTCA, Inc.

TTG — Time to go

TTS — Time to station

TTR — TCAS II receiver/transmitter

TTW — Time to waypoint

Turbulence Mode — Flight control system mode in which a “softer”response to gust upsets is programmed

UUUHF — Ultra high frequency (300 to 3000 MHz)

UTC — Universal coordinated time

VVVAC — Volts alternating current

VDC — Volts direct current

VDL — VHF data link

VHF — Very high frequency

VNAV — Vertical navigation, or the capability to compute pitch-axismaneuvers and altitude-related points in space

VOR — Very-high-frequency omni range

VSI/TCAS — Vertical speed indicator/traffic alert and collisionavoidance system

VSI/TRA — Vertical speed indicator/traffic, resolution advisory

WWWAAS — GNSS wide area augmentation system

WPS — Words per second; the rate at which a flight data recorderchronicles events

WPT — Waypoint

XXX-band — Frequency range in which most general aviation weatherradars operate

XTK — Cross track; cross-track error

ZZZulu — Greenwich or Universal Coordinated Time


Garmin International1200 E. 151st St.Olathe, Kan. 66062(800) 800-1020(913) 397-8200Fax: (913)397-8282www.garmin.com

Honeywell Aerospace1944 East Sky Harbor Circle Phoenix, Ariz. 85034(800) 601-3099 Fax: (602) 365-3343www.honeywellaes.com

SL40 760 10 1/2.0 $1,495

C37d transmit LED 10 - 40 VDC 6.25 x C38d receive 1.3 x 10.5

C128d stuck mic

Bendix/King 760 7 nominal 1/2.9 $1,410KY 97A

C37c LCD; nvm 14 VDC 6.25 xC38c 1.3 x 10.5


C37c LCD; nvm 28 VDC 6.25 xC38c 1.3 x 10.5


C37c gas discharge; 14 VDC 6.3 xC38c nvm 1.35 x 10.8

Bendix/King 2280 18 nominal 1/3.2 $5,330KY 196B

6.3 x C37c gas discharge 28 VDC 1.35 x 10.8C38c nvm

Built-in two-place VOX intercomand standby frequency monitor-ing functions.

Auto-leveling; auto-squelch;stuck-mic protection; remote-mic keying and channel call-up.

Same as KY 196A but 14 VDCpower input.

Auto-squelch; displays activeand standby frequency; remoteflip-flop; optional remote call-up;optional extended frequencyrange.

Same as KY 196A but 2280 channels and 8.33 kHz channel spacing.

Includes ACARS, display andVDL-mode 2 internal radio.


Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, Iowa52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com

Bendix/King gas discharge 20 2/4.3 $15,490KTR 908

2 1.8 x 28 VDCC37b (9 channels); 5.0 x 11.8C38b 118.0 -

151.975MHz opt.

RCZ 833 color CRT or LCD 20 1/11.0 $14,015($47,702)

C37c/C38c 2 to 12 14.0 xC112 depending 3.4 x 8.9 28 VDC

Class 3A on function

VHF-22A CTL-22 20 2/5.8 $17,878gas discharge

2 x 5C37c serial digital tuning 3/8 ATR-SL 28 VDCC38c

8 frequencies;nvm

VHF REMOTE-MOUNT TRANSCEIVERS

Includes KFS 598A control withdigital display of active/stand-by frequencies, flip-flop 118.0-151.975 MHz.

Price shown is the com portionin the Primus II integratedradio system. Price shown in ()includes a diversity transpon-der; complete built-in diagnos-tics including the RF. Includes8.33 kHz channel spacing andelementary spacing.

Built-in diagnostics; VHF 22B,118.0-151.975 MHz: $19,528.Operates in 25 kHz tuningmovements; includes CTL-22.

Power OutputChannels (peak W) Units/Weight

Model (lb)Channel Power

Manufacturer TSO Display Required Size (in.) Price Remarks

VHF PANEL-MOUNT TRANSCEIVERS

Frequency Units/Weight PriceDisplay (lb)

ModelFrequency Size or Power

Manufacturer TSO Storage Xmit Power (W) Form Factor Required Remarks

A v i o n i c s


A v i o n i c s



Wulfsberg Electronics6400 Wilkinson Dr.Prescott, Ariz. 86301(928) 708-1550(928) 541-7627www.wulfsberg.com

VHF-422A CTL-22 20 2/5.8 $17,870gas discharge

C37c 3/8 ATR-SL 28 VDCC38c 8 frequencies;

nvm

VHF-22C CTL-22C 20 2/5.8 $20,465gas discharge;

C37c 2 x 5 serial tuning 3/8 ATR-SL 28 VDCC38c

8 frequencies;nvm

VHF-422C CTL-22C 20 2/5.8 $22,190gas discharge

C37c 3/8 ATR-SL 28 VDCC38c 8 frequencies;

nvm

VHF-4000 CTL-22 20 2/4.7 see remarksgas discharge

C37d 2.5 MCU 28VDCC38d 8 frequencies;

nvm

VHF-4000E CTL-22C 20 2/4.7 $21,892 -gas discharge $26,264

C37d 2.5 MCUC38d 8 frequencies;

nvm28 VDC

CVC-152 color LCD N/A 1/0.75 $4,347

Control display5 VDC,

5 VAC or2.50 x 3.15 28 VDC

x 4.29

CCN-955 See remarks N/A 1/0.75 $7,643

5 VDC,5 VAC,

2.50 x 3.15 28 VDCx 4.29

CVC-151 118 - 136 MHz 20 1/3.3 $14,040FliteLine 118 -11.975 MHz

4.10 x 2.40 x 18 - 33 VDCC169 color LCD 13.33

VHF REMOTE-MOUNT TRANSCEIVERS

Built-in diagnostics.

Built-in diagnostics; VHF-22D118.0-151.975 MHz, $24,036.VFH-22D. 8.33 kHz/25 kHz tuning; includes CTL-22C.

Built-in diagnostics; compatibleonly with CSDB or ARINC 429controls; VHF-422D, 118.0-151.975 MHZ, $21,756.8.33/25 kHZ tuning; includesCTL-22C.

Built-in diagnostics; compatibleonly with CSDB or ARINC 429controls. Options: 001 baseline: includes CTL-22.101 adds 8.33: includes CTL-22C.201 adds Mode A/2 data; in-cludes CTL-22.301 adds 8.33 and Mode A/2data: includes CTL-22C.Prices range from $13,976 to$21,892.

Built-in diagnostics; compatibleonly with CSDB or ARINC 429controls. Options:101 118.0-151.975 + 8.33 in-cludes CTL-22C.301 adds Mode A/2 data inlcudes CTL-22C.

Gray or black panel.

Optional multi-function display;color LCD displays nav and comdata.

ARINC 429 bus interfact; 8.33or 25 kHz spacing; FM immuni-ty; auto-tune capability. FMSand radio management interfacecapability VDL Mode 2 & 3 provi-sions; color LCD nav and comdata.

Frequency Units/Weight PriceDisplay (lb)

ModelFrequency Size or Power

Manufacturer TSO Storage Xmit Power (W) Form Factor Required Remarks



Rockwell Collins400 Collins Rd. N.E.Cedar Rapids, Iowa52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com

HF-1050 2-29.999 200 PEP 4/29.9 $47,870(SSB)

280,000 RCU: 28 VDCC31d 10.8 x 3.1 xC32d 5.0

KPA 1052: 12.7 x 7.2 x 1.8antenna coupler:13.5 x 4.7 x 7.2 PS-440: 5.375 x2.375 x 2.265

F 9000 System 2 - 29.9999 selectable 3/27.5 $102,292*SSB/AM power output

C31d AM data 10.50, controller: 28 VDCC32d 175 PEP 2.625 x

280,000; 5.75 x 5.8599 operator transceiver:

programmable; 7.625 x176 ITU 5.55 x 12.60

r/t programmed antenna coupler:7.6 x 3.8 x 13.0

Delivers 200W PEP transmitterpower and 4 squelch options.“Once tuned, always tuned” coupler capability provides <20millisecond response. PS-440controller provides 99 user-programmable channels, clarifierfunctional and coupler tunestatus.

Fiberoptic interface; rapid-tuneantenna coupler (40 milli-sec-ond computer training);BITE.Includes HF receiver/transmitter antenna coupler andradio-tuning unit.*Special order price anddelivery

HF TRANSCEIVERS Frequency Units/Weight

Range (lb) PriceModel

Size or PowerManufacturer TSO Channels Xmit Power (W) Form Factor Required Remarks


Rockwell Collins400 Collins Rd. N.E.Cedar Rapids, Iowa52498(319) 295-4085 Fax: (319) 295-2297www.rockwellcollins.com

Sandel Avionics2401 Dogwood WayVista, Calif. 92081(877) 726-3357(760) 727-4900Fax: (760) 727-4899www.sandel.com

Bendix/King remote analog 4/10.4 $11,610KCS 305

C6c 3°/min.; 4 ATI 115 VAC,600°/min. 400 Hz

Bendix/King remote analog 4/9.4 $11,960*KCS 55A

3°/min.; 3 ATI 14 or 28 VDCC6c 180°/min.

KI 825 Color remote extensive outputs; 1/30 $12,720EHSI/MFD GPS selected

— discretes, EHSI- 3 ATI 11 - 33 VDCC113 ready discretes

C6d, C34eC36e, C40C

C11a

MCS-65 remote analog 3/6.7 $15,608(compass including system) 2.7°/min.; autopilot outputs; ATI 28 VDC

7°/sec. CSDBC6c

SN3500 remote analog 1/2.9 $10,950*EHSI

3 ATI 28 VDCC113 NA

HORIZONTAL SITUATION INDICATORS/COMPASS SYSTEMS

Includes bootstrap heading inHSI; autopilot outputs. Night-vi-sion compatible instrumentsavailable.

Night-vision compatible instru-ments available.Includes RMI output.*$18,790 with KI 825 EHSI.

Integrated EHSI, AMLCD; arcmode; 360 mode; course map;interfaces with numerous navi-gation systems and WX500Stormscope. Priced for a newinstallation and a KCM 100.

Digital interface with EFIS-74CSDB.

*3 x 3 electronic HSI combinesHSI, RMI, color moving map andother features. Accepts syn-chro-stepper motor and ARINC429 gyro inputs. Designed towork with a variety of digitaland analog NAV, GPS, DME,ADF and marker beacon re-ceivers. Compatible with theWX-500 Stormscope and weath-er radar. Optional interfaces fortraffic ($714) and WSI data linkweather ($714). *Helicptperversion, $13,286.

Units/Weight PriceModel Gyro (lb)

Autopilot PowerManufacturer TSO Slave rate Outputs Display case Required Remarks


A v i o n i c s


AUTOMATIC DIRECTION FINDERS



Bendix/King 200-1799 kHz analog 1/6.7 $3,390KR 87 P/M

nvmC41c 6.25 x 11 - 33 VDC

gas discharge 1.3 x 11.23

RNZ-850 100-1799.5 kHz; RS-422 2/13.6 $8,0332181-2183 kHz synchro XYZ ($38,473)

C34d DC sin/cos 14.0 x 3.4 x 8.9C35d 1 freq; nvm 28 VDCC36dC40b CRT or LCDC41dC66b

Bendix/King 190-1799 kHz analog 2/7.4 $18,550KDF 806

nvmC41c 5.0 x 28 VDC

gas discharge 2.0 x 10.0

ADF-60A CTL-62 RMI 2/6.0 $18,472*190-1750 kHz(4-kHz steps)

C41c 3/8 ATR-SL 28 VDC6 frequencies;

nvm

gas discharge,2 frequencies

ADF-462 CTL62 RMI 3/8.0 $17,860*190-1799 kHzand 2182 kHz

C41d emergency freq. 3/8 ATR-SL 28 VDC

6 frequencies;nvm

gas discharge

ADF-4000 190-1799 kHz CSDB 3/6.4 $23,2722182 kHz ARINC 429

C41d emergency freq. 2 MCU 28 VDC

6 frequencies/nvmgas discharge

Times flight and approaches;slaved indicator and RMIs available as options.

Price shown is the ADF portionin the Primus II integrated radiosystem. Price in () includesVOR/ILS and DME; completebuilt-in diagnostics including the RF; remote mount.

Digital control head displays bothactive/standby frequencies; flagcircuitry; strappable for 2182kHz, Gables control optional. Re-mote flip-flop optional; nine fre-quency pilot-programmable. “A”control head optional. Night-vision-goggle-compatible controlhead available.

Remote-mount; dual antenna op-tional. Digital tuning. IncludesANT-60A, CAD-62.Dual system, $35,916.

Built-in diagnostics; compatibleonly with CSDB or ARINC 429controls; digital signal process-ing; dual antenna optional.Includes ANT-462A.*Dual system, $35,892 includestwo receivers, two controls, oneantenna.

Built-in diagonostics; compatibleonly with CSDB or ARINC 429controls; digital signal process-ing; dual antenna optional. In-cludes ANT-462A.

Frequencies Units/Weight(lb) Price

Model Freq. StorageSize or Power

Manufacturer TSO Display Nav Outputs Form Factor Required Remarks


SN4500 remote analog 1/3.75 $18,500EHSI

C113 NA 4 ATI 28 VDC

HORIZONTAL SITUATION INDICATORS/COMPASS SYSTEMS

4 x 4 electronic HSI combinesHSI, RMI, color moving map andother features. Accepts syn-chro- stepper motor and ARINC429 gyro inputs. Designedtowork with a variety of digitaland analog NAV, GPS, DME,ADF and marker beacon re-ceivers. Compatible with theWX-500 Stormscope and weath-er radar. Optional interfaces fortraffic ($714) and WSI data linkweather ($714).

Units/Weight PriceModel Gyro (lb)

Autopilot PowerManufacturer TSO Slave rate Outputs Display case Required Remarks


Channel Units/WeightDisplay (lb) Price

Model Nav OutputsChannel Size or Power

Manufacturer TSO Storage GS/MB Form Factor Required Remarks



Bendix/King gas discharge CDI 1/3.0 $4,470KN 53 Silver Crown Plus

2 nav; GS only 6.31 x $4,340C34c nvm 1.3 x 9.75 Silver CrownC36cC40a 11 - 33 VDC

KLN 94 color GPS 1/3.6 $5,270Color GPS penetrationReceiver phosphor none 2.0 x 6.31 11 - 33 VDC

x 10.72C-129A installed

database

KLN 90B monochrome RS232 1/6.2 $8.880GPS penetration ARINC 429

Receiver phosphor 2.0 x 6.31 11 - 33 VDC13.15

C129 installed noneClass A-1 database*

VIR-4000 CTL-32 CSDB 2/3.9 See remarksgas discharge ARINC 429

C34e 2.5 MCU 28 VDCC36e 6 frequencies; NAC40c nvmC35d

NAV-4500 CTL-32 CSDB 2/4.1 $24,812gas discharge ARINC 429

C34e 2.5 MCU 28 VDCC36e 6 frequencies; NAC40c nvm C35d

NAV-4000 CTL-32 CSDB 2/4.7 $31,584*gas discharge ARINC429

C34e 2.5 MCU 28 VDCC36e 6 frequencies; NAC40c nvmC35dC41d

PANEL-MOUNT NAV RECEIVERS

Displays both active and presetfrequency.

Direct replacement for KLN 89B.Database includes airports,VORs, NDBs, intersections andspecial use airspace.*Quick-tunefeature automatically loads fre-quencies into a KX 155Anav/comm. Features roll steering.

BRNAV compliant and approvedfor IRF en route, terminal andnon-precision approach use. Fea-tures a 3-in. split screen CRT;built-in moving map graphicsshow nearby airports andnavaids. Nav outputs providedata for external moving maps.Complete Americas or interna-tional database.

Special order item and pricing.Combines ADF andVOR/ILS/MKR receivers in a sin-gle package. Internal diagnostics capability.

Built-in diagnostics; compatibleonly with CSDB or ARINC 429controls; digital signal process-ing; includes CTL-32 ($4,624);meets Eurocontrol FM immunitystandards only. RTU 4200,$23,184

Built-in ADF; built-in diagnostics;compatible only with CSDB orARINC 429 controls; digital sig-nal processing; meets Eurocon-trol FM immunity standards.*Various configurations will determine actual cost.

AUTOMATIC DIRECTION FINDERS


DFS-431 190 - 1890 kHz, ARINC 429 1/5.4 $13,6782181 - 2183 kHz analog

6.7 x 2.85 x 13.8 18 - 33 VDCC41c

LCD

ARINC 429 and AFCS bus inter-faces; steering guidanceto/from NDB; self-diagnosticsand auto-calibration. CDF-552color LCD, $4,220; AT-434Aloop sense antenna, $5,200.

Frequencies Units/Weight(lb) Price

Model Freq. StorageSize or Power

Manufacturer TSO Display Nav Outputs Form Factor Required Remarks


A v i o n i c s


Honeywell Aerospace1944 East SkyHarbor Circle Phoenix, Ariz. 85034(800) 601-3099 Fax: (602) 365-3343www.honeywellaes.com



RNZ-850 color CRT OBI; OBS 2/13.6 $19,724synchro XYZ ($38,473)

C34d 1 to 12 RS-22 14 x 3.4C35d depending on x 8.9C36d function; 28 VDCC40b nvmC41dC66b

Bendix/King gas discharge ARINC 429 2/6.5 $26,410KNR 634A CDI, HSI, RMI

C40a 2 nav; 3.0 xC36c nvm 5.0 x 10.0 28 VDCC34cC35d

VIR 32 CTL-32 SIN/COS, 2/5.7 $26,888gas discharge serial digital;

RMI compatibleC34c 6 frequencies; 3/8 ATR-SL 28 VDC,C35d nvm 26 VAC,C36d 400 HzC40b

VIR 432 CTL-32 serial digital 2/5.7 $30,888gas discharge

C34d 3/8 ATR-SL 28 VDC,C35d 6 frequencies; 26 VAC,C36d nvm 400 Hz

CVN-251 108.0 - 117.95 ARINC 429 1/3.31 $20,631MHz

C40c SIN/COS 4.0 x 2.4 18 - 33 VDCC36e x 13.33C34c LCDC35d

1/0.752.5 x 3.15 x 4.29

CVC-152 108.0 - 117.95 ARINC 429 1/3.31 $4,347Control Display MHz

SIN/COS 4.0 x 2.4x 13.33 5 VDC, 5 VAC

or 28 VDCLCD

1/0.752.5 x 3.15 x 4.29

CCN-955 108.0 - 117.95 ARINC 429 1/3.31 $7,643MHz

SIN/COS 4.0 x 2.4x 13.33 5 VDC, 5 VAC

LCD or 28 VDC

1/0.752.5 x 3.15 x 4.29

REMOTE-MOUNT NAV RECEIVERS

Price shown is the VOR/ILSportion in the Primus II inte-grated radio system. Priceshown in () includes a DMEand ADF; complete built-in di-agnostics including RF; Syn-chro XYZ mod filter includedin unit.

Synchro-interface KNI 582RMI optional. Digital display ofactive/standby frequencies.

Replaces VIR-30A directly; includes serial digital control;digital signal processing; built-in diagnostics; rotor modula-tion filter optional (strap).Includes CTL-32. Meets FMimmunity requirements.

Built-in diagnostics; compatible only with CSDB orARINC 429 controls; includesCSDB control, digital signalprocessing. Includes CTL-32.Meets Eurocontrol FM immuni-ty requirements.

ARINC 429 bus interface; 160VOR channels; 40 LOC chan-nels; includes glideslope/marker beacon receivers. FMimmunity standard.

Combines COM and NAV tuning; gray or black panel.

Combines COM and NAV tuning.

Units/Weight PriceChannel Nav (lb)Display Outputs

Size or PowerManufacturer Model Channel Form Factor Required Remarks





Bendix/King gas discharge serial data 1/2.6 $4,690KN 64 Silver Crown Plus

100 6.3 x 1.3 x 12.3C66a $4,890

Silver Crown11 - 33 VDC

Bendix/King gas discharge serial data 1/2.6 $5,960KN 62A P/M

100 11 - 33 VDC6.3 x

1.3 x 12.3

Bendix/King gas discharge serial data 2/3.6 $9,180KN 63

100 6.5 x 11 - 33 VDCC66a 1.1 x 11.55

RNZ-850 LCD ARINC 568 2/13.6 $10,814RS-422 $38,473*

C34d, C35d NAC36d, C40b 40mV/nm 28 VDCC41d,C66b 300

Bendix/King gas discharge, ARINC 429 2/6.3 $18,430KDM 706A slaved indicators ARINC 568 R/M

28 VDCC66b 250 3.0 x

5.25 x 12.8

DME-42 gas discharge, ARINC 568 2/6.2 $18,216serial digital serial digital

C66b 2 x 5 tuning 1/2 ATR-SL 28 VDC300

DME-442 gas discharge ARINC 568 2/6.2 $21,292serial digital

C66b (CSDB) 1/2 ATR-SL 28 VDCARINC 429

300

DME-4000 gas discharge CSDB 2/4.4 $19,907ARINC 429

C66c 2.5 MCU 28 VDC300

CDM-451 LCD 3 ARINC 429 1/3.6 $21,785Fliteline 2 ARINC 568

1 40-bit serial 3.87 x 3,27 x 18 - 33 VDC13.33

C66B 325

SD-442B LCD 3 ARINC 429 1/0.47 $6,580

1 40-bit serial 3.27 x 1.55 x 2.5ARINC 568

325

DISTANCE MEASURING EQUIPMENT

Includes antenna and installa-tion kit; accepts remote chan-neling. Distance accuracy: +0.1nm nominal to 99 nm; +1.0 nm,100 to 389 nm.

Includes antenna and installa-tion kit; accepts remote chan-neling. Distance accuracy: ±0.1nm nominal to 99 nm, ±1.0 nm,100 to 389 nm.

Includes KDI 572 indicator, op-tional slaved indicator. Distanceaccuracy: ±0.1 nm nominal to99 nm, ±1.0 nm, 100 to 389nm.

Price is the DME portion in thePrimus II Integrated Radio Sys-tem. *Includes VOR/ILS; ADF;4-channel scanning DME; com-plete built-in diagnostics includ-ing the RF; remote mount.

Includes KDI 572 indicator; optional slaved indicator;kits/mounts not included.

Includes two-digit-code diagnos-tics; directly replaces DME-40;tracks three channels simultane-ously when used with CTL-32 andIND-42A (special order only)(CTL-32 controls nav receiver);digital signal processing; echomonitor. IND-42A indicator includ-ed. Displays 0-300 nm; 0-999knots; 0-120 min.

Tracks three channels simulta-neously when linked to CTL-32,IND-42A; decodes and displaysstation ident; digital signal pro-cessing; echo monitor; built-indiagnostics; includes IND-42A(special order only).

Tracks three channels simulta-neously when linked to CTL-32,IND-42; decodes and displaysstation ident; digital signal pro-cessing; echo monitor; built-indiagnostics; includes IND-42

Three-channel scanning. ARINC429 interface; nav frequencydisplay in DME hold mode;six-wire analog continuous self-test.

Units/WeightNav Outputs (lb) Price

ModelChannel Power Outputs Size or Power

Manufacturer TSO Display (peak W) Form Factor Required Remarks


A v i o n i c s



Rockwell Collins400 Collins Rd. N.E.Cedar Rapids, Iowa 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com

Model Units/Weight(lb) Price

System Type InputsSize or Power

Manufacturer TSO Outputs Form Factor Required Remarks

Laseref V ARINC 429 2/9.9 $180,000Micro IRS

ARINC 429 6.6 x 6.4 x 6.3 28 VDCLaser Gyro IRS

C4c, C5e, C6d

GR-550 ARINC 429 1/6.0 $26,297

GPS sensor ARINC 429 2.6 x 8.5 x 28 VDC(ARINC 743A) 9.5

C-129 B1/C1115 VAC

Laseref IV ARINC 419/429 2/16.9 $237,000

Laser Gyro IRS ARINC 429/ASCB 4.9 x 7.6 x 28 VDC or13.1 115 VAC

C4c, C5e, C6d

Special Missions ARINC 429 2/9.9 $215,000Laseref V

ARINC 429 6.6 x 6.4 x 6.3 28 VDCNA

GPS-4000A ARINC 429 1/6.9 $24,356(complies with

GPS sensor ARINC 743A)

C129 B1 ARINC 429 2 MCU 28 VDC

LONG-RANGE NAVIGATION SENSORS

All digital; passive cooling; automatic mode control; align-in-motion when supplied withARINC 743A GPS imputs.

Complies with ARINC 743A; in-tegral satcom filter.

All digital; 4 MCU ARINC 704.

Upgradable to provide precisionapproach capability.

Garmin International1200 E. 151st St.Olathe, Kan. 66062(800) 800-1020(913) 397-8200Fax: (913) 397-8282www.garmin.com

GTX 330 A, C, S 1/3.0 $4,995

C112 Class 2A 250 1.6 x 6.25 11 - 33 VDC

TRANSPONDERSUnits/Weight

Modes (lb) PriceModel

Power Size or PowerManufacturer TSO Output (W) Form Factor Required Remarks

Solid-state Mode-S, keypad entry, remote ident,front-panel entry for flight ident, altitude monitorwith vice alert, flight timers. TIS compatible in theUnited States.


Garmin International1200 E. 151st St.Olathe, Kan. 66062(800) 800-1020(913) 397-8200Fax: (913) 397-8282www.garmin.com


Rockwell Collins 400 Collins Rd. N.E.Cedar Rapids, Iowa 52498(319) 295-4085Fax: (319) 295-2297www.rockwellcollins.com

Units/WeightModes (lb) Price

ModelPower Size or Power

Manufacturer TSO Output (W) Form Factor Required Remarks

GTX 330D A, C, S 1/3.0 $9,995

C112 Class 2A 250 1.6 x 6.25 x 11 - 33 VDC9.75

GTX 32 A,C 1/2.2 $2,925

C74c Class 1A 200 1.71 x 6.30 x 11 - 33 VDC8.78

Bendix/King A, C 1/3.1 $1,760KT 76A

C47c 250 6.25 x 14 or 28 VDCClass 1B 1.6 x 10.0

Bendix/King A, C 1/3.1 $2,210KT 76C

250 6.25 x 11 - 33 VDCC47c 1.63 x 10.73

Bendix/King A, C 1/3.9 $5,240KT 71

C47c 250 6.25 x 11 - 33 VDCClass 1A 1.63 x 10.0

Bendix/King A, C, S, TIS 1/3.6 $5,230KT 73

200 6.25 x 10 - 32 VDCC112 1.63 x 10.82

Bendix/King A, C, S 1/3.9 $5,350KT 70

250 6.25 x 11 - 33 VDCC112 1.63 x 10.0

Class 1A

RCZ 854G A, C 2/11.0 $9,972

C37c/C38c ($23,514)C74c 250-625 14.0 x 3.0 x 8.9

Class 3A 28 VDC

RCZ 854F A, C. S 2/11.0 $17,262

C37c/C38c ($28,122)C74c 250-625 14.0 x 3.0 x 8.9

Class 3A 28 VDC

Bendix/King A, C, S 2/8.5 $28,340MST 67A

C112 250-630 1/4 ATR 115 VAC,400 Hz

RCZ 833K A, C. S 2/11.0 $29,304(diversity)

C37c/C38c ($46,719)C74c 250-625 14.0 x 3.0 x 8.9

Class 3A 28 VDC

TDR -94D A, C, S 2/9.7 $37,692

C112 250-625 4.9 x 28 VDCClass 3 3.3 x 12.5

TRANSPONDERS

Diversity Mode-S, solid-state keypad entry, remoteident, front panel entry for flight ident, altitude moni-tor with voice alert, flight timers. TIS compatible inthe United States.

Remote mount, solid-state, remote ident capability,flight timers.

Automatic reply-light dimmer; system test; remote-ident capability adapter available. Add $90 for 28VDC converter.

Slide-in replacement for KT 76A. Programmable VFRcode; remote ident capability; gas-discharge digitaldisplay; push-buttom code entry.

Gas discharge display; encoding altimeter output.

Mode S transponder; non-diversity surveillance only;includes discrete address memory module; displaysencoding altimeter output; gas discharge display.

Price shown is the transponder portion in the Primus II integrated radio system. Price in () includes a VHF com; built-in diagnostics includingRF; remote mount.

Price shown is the transponder portion in the Primus II integrated radio system. Price in () includes a VHF com; built-in diagnostics includingRF; remote mount.

Mode S transponder; includes KFS 578A controlhead; non-diversity; TCAS diversity available.

Price shown is the transponder portion in the Primus II integrated radio system. Price in () includes a VHF com; built-in diagnostics includingRF; remote mount.TCAS II Change 7.0 and Elemen-tary Surveillance compatible.

Includes CLT-92E; DSDB control; two stored codes.Mode S transponder. TCAS II Change 7.0 and ModeS specific services compatible.


A v i o n i c s



Bendix/King 10, 20, 10/10 90° or 30° KMD 850 NA 1/9.9 $26,260ART 2000 40. 80,, 12/8 100° EFIS

160 15C63c 4 20-220 4 10. 28 dia. 28 VDC;

mv/det. NA 10, 26,vertical profile, 4 ARINC 115 VAC,ext. STC, tgt., 429 ±15° 400 Hz

wx. alert, atten.,comp., variablegain-map mode

Bendix/King 5, 10, 20, 12/8 90°, 100° ±30° KMD 850 NA 1/9.9 $33,320RDR 2100 40, 80, 10/10 120° pitch & EFIS

160 ,240, roll 10.28 28 VDC;C63c 320 range NA dia. 10, 26,

dependent 20/220 5 115 VAC,Vertical profile; 6.0 mv/deg. 400 Hz extended STC; 15 ARINC 429wx attenuationcompensation; ±15°variable gainin map mode;

wx alert; autotilt

Primus 440 2.5, 5, 10 12/7.9 120° ±30° ARINC 4 2/15.8 $39,38225, 50, 453/708

C63c 100, 200 50 or 200 checklist, 4.8 x 5.0 x 7.6 x 28 VDC2 mv/deg. data nav, 6.25 x 15.0

REACT; 10 or ARINC EFIS, 12.24preset & 12 429 MFD,

variable gain LSZ-860±15°

4

Primus 660 2.5, 5, 10 12/7.9, 60° ±30° ARINC 4 2/15.8 $53,29625, 50, 18/5.6 or 120° 453/708,

C83c 100, 200, 50 or 200 checklist, 4.81 x 5 x 7.6 x 28 VDC300 2 mv/deg. data nav, 6.25 x 15.0

REACT; GMAP or ARINC EFIS, 12.24target alert, 10 12/24 429 MFD,

preset & LSZ-860variable gain ±15°

4

Primus 880 2.5, 5, 12/7.9, 60° ±30° ARINC 5 2/15.8 $85,99810, 25, 18/5.6 or 120° 453/708

C63c 50, 100, 24/4 50 or 200 checklist, 4.8 x 5.0 x 7.6 28 VDC200, 300 2 mv/deg. data nav,’ 6.25 x x 15.0

Doppler or EFIS, 12.24turb. detec., 10 12/24 ARINC MFD,

compensated, 429 LSZ-860tilt, REACT,

GMAP ±15° 5target alert,

preset &variable gain

Primus 700A .5, 1, 10/10, 60° ±30° ARINC 5 4/37 $94,3472.5, 5, 10, 12/7.9, or 120° 429/708

25, 50, 10 x 14/ 50 or 200 checklist, 4.81 x 5.0 x 7.6 28 VDC;C63c 100, 200, 10 x 7.1, 6 mv/deg. data nav, 6.25 x x 15.0 400 Hz

300 18/5.6, or EFIS, 12.24REACT; ground 24/4 12/24 ARINC lightning& sea clutter 10 429 sensor

red.; turb. LSZ-860detect-preset ±15°

& variable gain 5

Primus 701A 1/2, 1, 10/10, 60° or ±30° ARINC 5 4/39 $113,5272.5, 5, 10, 12/7.9, 120° 429/709

25, 50, 10 x 50 or 200 checklist, 4.81 x 5.0 x 7.6 28 VDC;C63c, C102 100, 200, 14/10 x 6 mv/deg. data nav, 6.25 x x 15.0 115 VAC,

300 7.1, or ARINC EFIS, 12.24 400 Hz18/5.6 429 lightning

REACT; ground 10 24/4 12/24 sensorclutter reduction;

turbulence ±15° 6detect-preset

& variable gain

Vertical profile feature:scans horizontally or ver-tically on track line se-lected by pilot.Alpha-numeric display ofrange, function and tiltangle.

Vertical profile feature:scans horizontally or ver-tically on track line se-lected by pilot;Alpha-numeric display ofrange, function and tiltangle. KMD 850 MFD,$13,440.

Single receiver/transmit-ter/antenna pedestalLCD indicator for non-EFIS applications,$27,857.

Radar indicator for non-EFIS applications, add$25,528.Single receiver/transmit-ter/antenna pedestalLCD indicator for non-EFIS applications,$27,857.

Radar indicator for non-EFIS applications, add$35,532.

Short-range and high res-olution system for spe-cial search andsurviellance missions,displayed menus. Mini-mum detect range at450 ft. All full dual-modeoperation pilot and copi-lot; for non-EFIS applica-tion, add $35,532.

Short-range and high-res-olution system for spe-cial search andsurviellance missions;displayed menus and AC90-80A specified clearzones. Allows full dual-mode operation for pilotand copilot; for non-EFISapplication, add$35,532.

Model Ranges Scan Stablztn. ScopeDish Size Display (dia./in.) Units/

TSO Power & Beam Pulse Wdth. Stabl. Sig. Interface Weight PriceOutput Width Indicator

Manufacturer Circuits (Peak KW) (in./deg.) Looks/Min. Ant. Tilt Colors Size RT. Size Power Remarks

WEATHER RADAR


Model Ranges Scan Stablztn. ScopeDish Size Display (dia./in.) Units/

TSO Power & Beam Pulse Wdth. Stabl. Sig. Interface Weight PriceOutput Width Indicator

Manufacturer Circuits (Peak KW) (in./deg.) Looks/Min. Ant. Tilt Colors Size RT. Size Power Remarks


WXR-800 5, 10, 25, 12/8 120° ±30° EFIS-85, varies 2/20.4 $46,78850, 100 pitch EFIS-86, by

C63 200, 300 see & roll MFD 2000 indicator 15.0 x 28 VDCremarks FlightMax 11.5

range- 5 digital 429 950adjusted 14 or 200contour; mv/deg.ground 4

±15°

WXR-840 5, 10, 12/8, 60° ±30° EFIS-85, varies 2/20.4 $78,200*25, 50, 14/7, or 120° pitch EFIS-86, by

C63c 100, 200, 18/6 & roll MFD-2000 indicator 15.0 dia. 28 VDC300 FlightMax x 11.5

range- see digital 429 950adjusted remarks or 200contour; 0.024 mv/deg. 4ground 13clutter ±15°

suppression

TWR-850 5, 10, 25, 12/8, 60° ±30° EFIS-85, varies 2/20.4 *50, 100, 14/7, or 120° pitch & EFIS-86, by

C63c 200, 300 18/6 roll MFD-2000 indicator 15.0 dia. 28 VDCsee FlightMax x 11.5

range- 0.024 remarks digital 429 950adjusted or 200contour; 13 mv/deg.

ground clutter 4supression ±15°

WEATHER RADAR

All solid-state Dopplerpulse weather avoidanceradar; one-piece design;six pluse widths — 1.7°to 28.8°. Separate func-tion switch for eachpilot.

All solid-state Dopplerpulse wx avoidanceradar. One-piece design.Designed as EFIS wxsensor. Six pulse widths,1.7 to 28.8. Separatefunction selection foreach pilot (mode, range,gain, tilt and targetalert). *Special orderpricing

Solid-state Doppler tur-bulence detection, pulsewx avoidance radar; de-signed as EFIS wx sen-sor; six pulse widths, 1.7 to 28.8; separatefunction selection for pilot (mode, range, gain,tilt, turbulence and tar-get alert). *Special orderpricing.

Honeywell Aerospace1944 East SkyHarbor Circle Phoenix, Ariz. 85034(800) 601-3099 Fax: (602) 365-3343www.honeywellaes.com


Bendix/King -20 - 2,500 ft. ±5 ft./ pointer dial 3/3.8 $9,210KRA 10A 50 - 100 ft.,

±20°/±20° ±5%/ 28 VDC100 - 500 ft.,

C87 ±7%/500 - 2,000 ft.

Bendix/King -20 - 2,000 ft. 0 - 100 ft., pointer dial 2/10.7 $21,880KRA 405B 34 ft. or 3%

±20°/±25° whicheveris greater, 28 VDC

C87 500 - 2,500 ft.±5%

AA-300 0 - 2,500 ft. 0 - 100 ft. pointer dial 2/6.5 $24,749± 3 ft.

±20°/±30° 100 - 500 ft. 28 VDC±3%

500 - 2,000 ft.C87 ±4%

ALT-4000 0 - 2,500 ft. ± 2 ft. or 2% EFIS (analog 2/6.8 $27,392version

C87 ±40°/±-50° available) 28 VDC

Continuous DH set; “skewed”antenna optional for mountingon angled aircraft surface.

Compatible with HoneywellMark VI GPWS/EGPWS continu-ous DH set; tracking to 2,500ft.; expanded helicopter versionavailable; night-vision goggleversion available. Optional built-in tone generator.

Includes RA-315 indicator andtwo AT-300 antennas.

Interfaces to EFIS high-intensitymonitor for Cat II/III certifica-tion. Includes two ANT-52 an-tennas.

RADAR ALTIMETERS

Alt. Range PriceModel

Pitch/Roll Units/Weight PowerManufacturer TSO Limits Accuracy Display (lb) Required Remarks


A v i o n i c s



Insight Avionics, Inc.P.O. Box 194Buffalo, N.Y. 14205(716)852-3217Fax: (905) 871-5460www.insightavionics.com

L-3 Avionics Systems5353 52nd St. S.E.Grand Rapids, Mich. 49588(616) 949-6600Fax: (616) 285-4224 www.L-3com.com

LSZ-860 60°, 120°, three unique displays on $20,100360° symbols Honeywell EFIS

C110 represent three of various 28 VDC100 nm rates of sizes

occurrence forvertical lightning 3/10.8in a specific area

Strike Finder 360° LED 3 1/8 (diam.) $4,995*

C110a 200 nm 2/2.3 14 or 28 VDC

WX-500 360° — NA $5,240*

200 nm 2/3.43 11 - 32 VDCC110a

WX-950 360° CRT 3 ATI $6,370*

C110a 200 nm 2/3,74 11 - 33 VDC

WX-1000+ 360° CRT 3 ATI $13,420*AN/AMS-2

200 nm 3/10.95 10 - 32 VDCC110a

WX-1000E 360° — depends on EFIS $13,460*(429 EFIS) system

200 nm 10 - 32 VDCC110a 1/6.67

WX-1000E 360° — NA $10,650*

C110a 200 nm 2/10.95 10 - 32 VDC

WX-1000E 360° — 3 ATI $13,460*(429 Navaid)

200 nm 2/10.95 10 - 32 VDCC110a

THUNDERSTORM DETECTION SYSTEMS

Display stabilized in headingand velocity. Overlays weatherradar display.

LED digital weather avoidance system. *Relative bearing se-lector option, $1,495.B&CA estimate.Storm distance and bearingusing outer- and half-rangerings in conjunction with 30°azimuth markers.

Remote-mount sensor inter-faces with OEM MFDs or radarindicator when paired withRGC250 (sold separately).360° and 120° surveillance in25-200 nm ranges; heading sta-bilization; cell- or strike-modedata selection. *Proccessoronly.

Series II Stormscope: self-con-tained processor/display unit;360° and 120° views in 200,100, 50 and 25 nm ranges;heading stabilization; cell- orstrike-mode data selection.*Display/processor only.

Includes heading stabilization.*Processor only.

Provides output on EFIS displayor radar indicator when pairedwith RGC35C (sold separately);includes three levels of activity,bearing and distance; optionaldisplays for checklists.*Processor only.

Same as WX-1000+; acceptsRS232 input from Loran-C andGPS receivers.*Processor only.

Navaid option for use withARINC 429-based nav systems.*Processor only.

SearchArc Price

Model Display SizeMax Information Power

Manufacturer TSO Range Display Units/Weight Required Remarks


Meggitt Avionics/S-TECOne S-TEC WayMunicipal AirportMineral Wells, Texas 76067(800) 872-7832(940) 325-9406Fax: (940) 325-3904www.magic.aero

S-TEC accelero- none none 3/4.0 $5,220System meter

ThirtyALT 14 or28 VDC

C9c DC electric altitude hold

S-TEC 1 rate command VOR/LOC/BC, 3/9,0 $6,170System 40 gyro turn GPS

trackingC9c DC electric none 14 or

28 VDC

S-TEC enclosed in command VOR/LOC, 2/7.0 $6,170System rate gyro turn GPS trackingTwenty

DC electric none 14 orC9c 28 VDC

S-TEC 1 rate hdg. select VOR/LOC/BC, 4/12.0 $7,630System 60-1 gyro GPS/Loran

none capture and tracking

C9c 14 orDC electric 28 VDC

S-TEC no external none GS capture 4/11.0 $7,920System 60 sensors and track

PSSDC electric vertical 14 or

speed 28 VDCC9c hold;

altitudehold;GS

captureand

track

S-TEC 1 rate command VOR/LOC/BC, 5/14.0 $9,670System 50 gyro turn/hdg. GPS, Loran

select trackingC9c optional

DC electric 14 or altitude 28 VDC

hold

S-TEC enclosed in command VOR/LOC/GPS/ 5/13.0 $9,670System rate gyro turn Loran trackingThirty plus pitch

computer altitude 14 or C9c hold 28 VDC

DC electric

S-TEC 1 turn hdg. select VOR/LOC/BC, 7/21.0 $13,510System 60-2 coord., Loran track

1 dir. gyro vertical and approach;speed GS capture

C9c 1 press. and and tracking 14 ortransducer altitude 28 VDC

hold

S-TEC 1 turn hdg. select VOR/LOC/ 5/17.0 $16,760System coord. BC, GPS/Loran

FiftyFiveX tracking and GS 14 or C9c 1 press. digital vertical capture 28 VDC

transducer speed, altitudehold

S-TEC 1 turn hdg. select VOR/LOC/BC, 9/24.0 $24,070System 65 coord., 1 dir. GPS/Loran

gyro capture andC9c manual tracking;

1 press. and GS capturetransducer automatic and tracking 14 or

modes 28 VDC

Can be upgraded to System 50or 60-2.

Can be upgraded to System 30.

Includes interfaces with all popular HSIs. Variable bank angle with airspeed; automaticthree-level radio gain; can be upgraded to 60-2.

Complements existing singleroll-axis autopilot; auto/manual,electric trim optional, $2,195;may be upgraded to 60-2; alti-tude selector/alerter optional,$3,670.

Two-axis, roll and pitch autopilot; trim condition indicator std. Manual electrictrim optional, $2,630. Can beupgraded to 60-2.

DG option, $2,495

Interfaces with all popular HSIs.Automatic/manual electric trimoptional, $3,520; altitude/verti-cal speed selector/alerter op-tional, $3,670; can be upgradedto flight director.

Interfaces with all popularHSIs. Automatic/manual elec-tric trim optional, $3,520. Alti-tude/vertical speedselector/alerter optional,$3,670; can be upgraded toflight director.

BASIC AUTOPILOTSSensor Attitude ModesType Price

Model RollServo Power

Manufacturer TSO Type Pitch Nav Modes Units/Weight Required Remarks


A v i o n i c s


Primus 1000 micro DADC IC-600 28 VDC varies by varies bydigital AHRS or installation version

IRScombined 13.0

Primus 1000 micro DADC IC-615 28 VCDC varies by varies byCDS installation installation

Digital AHARScombined

Primus 2000 micro DADC IC-800 28 VDC varies by varies bydigital AHRS installation version

or IRScombined 15.0

Primus Epic micro DADC FZ-800 28 VDC varies by varies byCDS digital AHRS or installation installation

IRScombined

Primus Epic air data module integrated 28 VDC varies by varies byand micro IRS modular installation installation

avionics unit

;

Primus Epic See RemarksFly-by-Wire

System

Magic 2100 digital ADAHARS Magic EFIS 14 or 14.5 $65,900DFCS 28 VDC

NA NA NA

FCS-65 AHC-3000 APS-65 28 VDC varies by varies byinstallation installation

EFIS-84remote (two tube) 50.6

vertical gyroor dual AHRS

FCS-85 ADS-86 APS-85 28 VDC, varies by varies by115 VAC, installation installation

dual AHRS EFIS-85 400 HzAHC-3000 (three tube)

Digital fail-passive system. CAT II; ARINC 429 interfaces,two-, three-, four- or five-tubeEFIS. Bombardier Learjet 40, 45and 45XR; Embraer ERJ-135,140 and 145; Cessna Bravo, En-core, Excel and Ultra.

Digital fail-passive system. CATII; ARINC 429 interfaces; two tofive flat-panel LCD EFIS. CessnaCitation XLS

Digital, dual-channel fail-passivesystem. CAT II optional auto-throttle, dual-sensor monitoring;five- or six-tube EFIS. Bom-bardier Global Express and Glob-al 5000; Cessna Citation X;Dassault Falcon 900C, 900EX.

Digital fail-passive system. CATII, ARINC 429 interfaces. Two-,three- four- or five-tube EFIS.Sino Swearingen SJ30-2.

Integrates all traditional avion-ics into modular avionics unit.Digital, dual-channel; full opera-tional system. CAT II optional;auto-throttle, envelope protec-tion. Includes two to five flat-panel LCDs with cursor controls.Agusta/Bell AB139; CitationSovereignDassault Falcon900EX, 2000EX and 7X; Em-braer 170, 175, 190 and 195;Gulfstream G500 and G550;Raytheon Horizon.

Integrates with Primus Epic Sys-tem. Scalable architecture, per-formance and envelopeprotection augmentation. Em-braer 170, 175, 190 and 195.

Optional EFIS ($53,900) andEIDS ($39,900).

Built-in diagnostics; digital Cat II certificated autopilot. Op-tional EFIS and AHRS. STC kitinstaller fabricated. Compatiblewith EFIS-84.

Available only as full, dual- chan-nel, fail-passive, digital system;digital Cat II autopilot, 4- or 5-tube EFIS optional; ARINC 429IRS interface available; includesyaw damper; extensive built-indiagnostics. STC kit installerfabricated. Compatible withEFIS-84


Meggitt Avionics/S-TECOne S-TEC WayMunicipal AirportMineral Wells, Texas76067(800) 872-7832www.magic.aero


Weight PriceAir Data Autopilot

AP Only AP OnlyAttitude Flight

Manufacturer Model Sensors Director Power IFCS IFCS Remarks

INTEGRATED FLIGHT CONTROL SYSTEMS


ACSS, an L-3Communications & Thales Company19810 N. 7th Ave.Phoenix, Ariz. 85023(623) 445-7000Fax: (623) 445-7001www.L-3com.com/acss

Avidyne Corp.55 Old Bedford Rd.Lincoln, Mass. 01773(800) 284-3963Fax: (614) 885-8307www.avidyne.com

L-3 Avionics Systems5353 52nd St. S.W.Grand Rapids, Mich. 49512(616) 949-6600Fax: (616) 285-4224www.L-3com.com

TAWS + MFD, EFIS, weather 2 MCU $778,413*radar display

C151bCLASS A 7.5C129b2

TAWS + Performance MFD, EFIS, weather 2 MCU $91,481*radar display

C151bCLASS A 7.5C129b2

TCAS 2000 MDFD, EFIS, 4 MCU - 16.0 $150,461*RT-950/951 VSI/TCAS display 6 MCU - 16.8

C119B

T2CAS MFD, EFIS, weather 4 MCU - 14.7 $222,820*radar display 6 MCU - 16.8

C119B VSI/TCAS display

C151aCLASS A

C129b2

TAS 600 Avidyne EX500, 3.1 x 7.25 x 11.7 $9,990EX5000

C-147 and MHD 7.2

top and bottomGarmin, Chelton, antennas

Honeywell, Sandel, 3.24 x 2.76 x 5.14Sagem, Universal,Meggitt, Rogerson 22.5 oz. (combined)

Kratos


C-147 and MHD 7.2



Kratos


C-147 and MHD 7.2



Kratos

TCAS791A EFIS, MDFD and IVSI NA $56,460*System(TCAS I) Also displays wx NA

without display radar using RGC-350 Radar Graphics

NA Computer (soldseparately)

C118

TCAS791A See remarks NA $65,870*System(TCAS I) NA

with CD-605 display

NA

C118

COLLISION AVOIDANCE SYSTEMS

Optional GPS; alerts based on stan-dard aircraft climb capability plusTerrain Advisory Line and Avoid Ter-rain features. *B&CA estimate.

Optional GPS; alerts based on ac-tual aircraft climb capability (per-formance) plus Terrain AdvisoryLine and Avoid Terrain features.*B&CA estimate.

Standard positions on many region-al and business jets including Bom-bardier, Cessna, Dassault,Embraer, Gulfstream, Raytheon.(SFE selectable on all Airbus andBoeing aircraft.)*B&CA estimate.

Combined TCAS and TAWS in 4- or6-MCU with optional GPS. STCsavailable on Cessna, Raytheon andPiaggio aircraft.*B&CA estimate.

Designed for single-engine pistonaircraft; seven-nm range, 3,500-foot vertical separation, 18,500-foot service ceiling. Head-upaudible position alerting (“traffic!one o’clock! high! two miles!”);active interrogating, 30-seconddecision and 1,200-knot closurerate.

Designed for mid-performance air-craft and helicopters; 12-nmrange; 3,500-foot vertical separa-tion; 25,000 foot service ceiling.Head-up audible position alerting(“traffic! one o’clock! high! twomiles!); active interrogating, 30-second decision and 1,200-knotclosure rate.

Designed for high-performanceaircraft and rotorcraft; 21-nmmile range; 9,900-foot verticalseparation; 55,000 foot serviceceiling. Head-up audible positionalerting (“traffic! one o’clock!high! two miles!); active interro-gating, 30-second decision and1,200-knot closure rate.

Active Traffic Collision AvoidanceSystem (TCAS-I) designed to dis-play on compatible EFIS, MFD,and IVSI displays. Contact facto-ry for approved interfaces.*Fixed wing, top- or bottom-mount antenna or helicopter bot-tom mount antenna only. Intalla-tion kit and options separate.Other conditions may apply.

Includes TCAS791A Systemabove plus CD-605 DedicatedColor Display: *CD-605 3-ATI Dis-play, $11,410 additional. Installa-tion kit $230 additional. Otherconditions may apply.

Model Processor SizeDisplay Interface

Manufacturer TSO Options Weight (lb) Price Remarks


A v i o n i c s



SKY497 Contact factory NA $13,900*SkyWatch for approved

Traffic Advisory interfaces. Also can NASystem display on wx radar

indicators usingNA RGC-350 Radar

Graphics ComputerNA (sold separately)

SKY497 Includes SkyWatch NA $18,890*SkyWatch Traffic System above plusAdvisory System CRT display

with display NA

NA

NA

SKY899 Displays on compatible NA $20,980*SkyWatch HP Traffic EFIS and MFDs; contact

Advisory System factory for NAapproved interfaces.

NA

NA

SKY899 Includes SkyWatch HP NA $25,980*SkyWatch HP Traffic System above plus

Advisory System CRT display NAwith display

NA

NA

SKY899 See remarks NA $20,980*SkyWatch HP

(TCAS 1) NAwithout display

NA

LandMark See remarks NA $10,620*TAWS 8000

System NA

Class B

C 151a


Active Traffic System usingTransponder interrogation andreply (independent of radar cov-erage). Active surveillance 10nm, tracks up to 30 intruder air-craft, and provides both auraland visual warnings. Single an-tenna system reduces installa-tion costs. *Transmitter/receiver computer only. Installa-tion kit and other options sepa-rate. Other conditions may apply.

*Installation kit and other op-tions separate. Other conditionsmay apply

Active Traffic System usingTransponder interrogation andreply (independent of radar cov-erage). Active surveillance 35nm, tracks up to 35 intruder air-craft, and provides both auraland visual warnings. Single an-tenna system reduces installa-tion costs.*Transmitter/Receiver Computeronly. Intallation kit and other op-tions separate. Other conditionsmay apply.

*Installation kit and other op-tions separate. Other conditionsmay apply.

Active Traffic System usingTransponder interrogation andreply (independent of radar cov-erage). Active surveillance 35nm, tracks up to 35 intruder air-craft, and provides both auraland visual warnings. Single an-tenna system reduces installa-tion costs. Install as a TCAS Iusing a compatible color display(not supplied) and NY156 TCASdirectional antenna. *Installationkit and other options separate.Other conditions may apply.

Remote processor offers predic-tive warning functions using posi-tion data from a GPS receiver,flight configuration and an inter-nal terrain and obstacle data-base. Both aural andvisual warnings are issued when-ever potential controlled flightinto terrain (CFIT) situationsarise. Terrain information can bedisplayed on TAWS-compatibleARINC 453 EFIS, ARINC 453weather radar indicators andcompatible MFDs. Display onnon-ARINC 453 radar indicatorsrequires the RGC350 RadarGraphics Computer (sold sepa-rately). A baro-corrected altitudeinput is required. *Intallation kitand other options separate.Other conditions may apply.






LandMark MFD, EFIS NA $9,750*TAWS 8100 or radar indicator

System NA

Class B

NA

Bendix/King KMD 550 MFD, 2.2 x 4.15 x 6.25 $10,990KGP 560 KMD 850 MFD

and most MFDs 1.5C151

Class B

KGP 860 KMD 550 MFD, 2.2 x 4.15 x 6.25 $13,990KMD 850 MFD

C151 and most FMFDs 1.5Class B

Bendix/King KMD 550 MFD, 4.5 x 7.0 x 13.8 $22,550KTA 870 KMD 850 MFD


Bendix/King KMD 550 MFD, 4.5 x 7.0 x 13.8 $29,990KMH 880 KMD 850 MFD

and most MFDs 8.75C147, C151,

Class B

KTA 970 dual-color, flat-panel 4.5 x 7.0 x 13.8 $28,720LCD combined

C118 IVSI/TA display, 8.75KMD 550 EFIS

KMD 850 or weather radar

Bendix/King KMD 550 MFD, 4.5 x 7.0 x 13.8 $38,280KMH 980 KMD 850 MFD

and most MFDs, 9.68C118, C151

Class B

CAS 66A dual-color, flat-panel 1⁄ 2 ATR-S $95,645LCD combined (4 MCU)

IVSI/TA display, C118 KTA 870, KMH 880, 17.0

EFISor weather radar

CAS 67A dual-color, flat-panel 1⁄ 2 ATR-S $222,360LCD combined (4 MCU)

IVSI/TA/RA displayC119a/b (included in price

shown). Also caninterface with

KMD 550 MFD, KMD 850 MFD, EFIS

or weather radar

Mark XXI KMD 550 MFD, 4.5 x 7.0 x NA $13,790KMD 850

C118 and most MFDs 1.5Class B


Features a WAAS-GPS sensor.Eliminates the need for multipleinputs from other aircraft sensors,simplifying the installation. Com-patible display required to com-plete the installation. Operatingautonomously, can provide thehighest integrity terrain data with-out GPS, ADC, or OAT inputs. 320nmi range. *Installation kit andother options separate. Other con-ditions may apply.

EGPWS exceeds Class B require-ments. Provides aural and visualwarnings; Internal GPS; worldwidedatabase by region.

EGPWS exceeds Class B require-ments. Provides aural and visualwarnings; internal GPS; worldwidedatabase by region. EFIS displaysadditional warning modes.

Traffic Advisory System (TAS) isan active system providing auraland visual advisories. Single ordual directional antennas.

Traffic Advisory System (TAS) andEGPWS in one box. Active trafficsystem providing aural and visualadviories. Single or dual direction-al antennas.

TCAS I system.

TCAS I and GA-EGPWS.

TCAS I system. Includes proces-sor, control panel, directional antenna and IVSI/TA display.Does not include installation kits.Upgradable to TCAS II.

TCAS II system. Requires Mode Stransponder. Includes controlpanel, IVSI/TA/RA display.Does not include installation kits.Dual directional antenna.

Helicopter EGPWS





Rockwell Collins400 Collins Rd. N.E.Cedar Rapids, Iowa 52498(319) 295-1000Fax: (319) 295-2297www.rockwellcollins.com

Avidyne (formerly Ryan)55 Old Bedford Rd.Lincoln, Mass. 01773(800) 284-3963www.avidyne.com

Universal AvionicsSystems Corp.3260 E. Universal WayTucson, Ariz. 85706(520) 295-2300(800) 321-5253Fax: (520) 295-2395www.uasc.com

Bendix/King KMD 550 MFD, 2.2 x 4.15 x 6.25 $29,990KMH 880 KMD 850

and most MFDs 1.5C147C151

Class B

Mark VI KMD 550 MFD, 6.2 x 3.0 x 12.1 $26,168KMD 850

and most MFDs 3.5

Bendis/King KMD 550 MFD, 4.5 x 7.0 13.8 $38,280KMH 980 KMD 850


Class B

TCAS 4000 Collins EFIS, MFD 4 MCU $414,044*TCAS compatible

C119 VSI (RA) 17.0(C119a when Collins TVI-920

issued) (RA, TA)

9900BX Avidyne, Chelton, 7.25 x 3.1 x 11.675 $20,600TAS Collins, Garmin,

Honeywell, Universal 6.38 $21,600 with opt.C147 and other MFDs; 1/2 3 ATI

Class A ARINC 429 and RS232; alphanumeric displaysee remarks $28,590

C113 with opt. 3ATI multi-hazard display

TAWS A Universal Avionics 2 MCU LRU TAWS AEFI-890R $37,500

C151b MFD-640C92c UNS FMS 9.6

(5-in. display)

TAWS B Honeywell TAWS Bnumerous weather $23,000

C151b radar, MFD andC92c EFIS displays

Rockwell Collins 28 VDCnumerous weather

radar, MFD andEFIS displays

SmithsBAE ATP EFIS

additional displayoptions available


EGPWS and traffic advisory sys-tem (TAS) in one box. Worldwidedata base by region.

EGPWS exceeds Class A require-ments. Provides aural and visualwarnings; with or without internalGPS. Worldwide database by re-gion.

TCAS I and EGPWS inputs

TCAS II system. European ACAScompatible Mode S Level III.AC/DC in one part number in-cludes control panel and two TREantennas. Displays range/alt. sep-aration from traffic. Max range 3mi. Two surveillance volumes andMSL of traffic. Top/bottom anten-nas to optimize coverage. Up-grades to 8800 Gold.*Typical installation

Active Traffic Advisory System(TAS) with range over 20 miles.Patented top/bottom phase-arrayantennas for optimum coverage.Exclusive “Audible Position Alert-ing” announces “Traffic, 12:00high! 1 mile” for faster visual acqui-sition of target. Capable of operat-ing with four or more displayssimultaneously.

Worldwide terrain database with480+MB data. High-resolution ana-log video views; 3-D perspectiveview; profile view; map view. Mapview of terrain can be output usingARINC 708 or WXPF formats for in-terface with various existingweather radars.




A v i o n i c s



Universal AvionicsSystems Corp.3260 E. Universal WayTucson, Ariz. 85706(520) 295-2300Fax: (520) 295-2395www.uasc.com

CVR solid-state, digital 9.5 x 5.88 x 5.75 $15,997

AR 30 CVR 30 min. 8.8 28 VDC980-6023-001

ED 56A, C123a

CVR solid-state, digital 1⁄ 2 ATR-S $21,770

SSCVR 980 30 min. 11.5 28 VDC6020-011 115 AC

ED 56A, C123

CVR solid-state, digital 9.5 x 5.88 x 5.75 $19,997

AR 120 CVR 120 min. 8.8 28 VDC980-6023-002

ED 56A, C123a

CVR solid-state, digital 1⁄ 2 ATR-S $27,042

SSCVR 980- 120 min. 11.5 28 VDC6022-011 115 AC

ED 56A, C123

FDR solid-state, digital 9.5 x 5.88 x 5.75 $18,814 to$28,201

AR FDR 980- 25 hrs. @64, 128 8.84710-00X 256 wps 28 VDC

ED 55, C124a

FDR solid-state, digital 1⁄ 2 ATR-L or S $19,479 to$33,166

SSFDR 980- 25 hrs. @64, 128, 11.5 (short)4700-0XX 256 wps 13.5 (long) 115 VAC

28 VDCED 55, C124

CVR/FDR solid-state, digital 9.5 x 5.88 x 5.75 $29,046 to$33,166

AR Combi 980- 30 min. voice; 25 hr. 8.86021-06X data @64, 128, 28 VDC

256 wpsC124a, ED 55

CVR/FDR solid-state, digital 9.5 x 5.88 x 5.75 $29,046 to$33,166

AR Combi 980- 60 min. voice; 10 hr. 8.86021-06X data @64, 128, 28 VDC

256 wpsC124a, ED 55 25 hr. data

DVDR/FDR solid-state. digital 1⁄ 2 ATR-S $35,580

AT Combi 980- 120 min. voice; 25 hr. 11.5 28 VDC6025-001 data @64, 128,

256 wpsED-56A, C123a

CVR solid-state, 1⁄ 2 ATR-S $12,500flash-memory

SSCVR-30B 13.0

C123A 30 min. 28 VDC

CVR solid-state, 1⁄ 2 ATR-S $16,500flash memory

SSCVR-120 13.0

C123a 120 min. 28 VDC

COCKPIT VOICE RECORDERS (CVR)/FLIGHT DATA RECORDERS (FDR)

Non-ARINC size, with underwater locator beacon;control panel and mounting traynot required. ARINC 557 andARINC 757.

Solid-state CVR with underwater locator beacon;ARINC 557 and ARINC 757.

Non-ARINC size with underwater locator beacon;control panel and mounting traynot required. ARINC 557 andARINC 757.

Solid-state CVR with underwater locator beacon.ARINC 557 and ARINC 757.

Non-ARINC FDR, ARINC 717,429. Mounting tray not re-quired.

Solid-state FDR; ARINC FormFactor; underwater locator beacon. ARINC 747, 573, 717.fire test to ED 56a.

Combination CVR/FDR; non-ARINC size. Mounting tray notrequired. Three or two crewchannels; one area mic.

Combination CVR/FDR; non-ARINC size. Mounting tray notrequired. Three or two crewchannels; one area mic.

Combination CVR/FDR; ARINCForm Factor. Mounting tray re-quired. Data download throughfront access PCMCIA.

Six channels (4 voice, 1 time, 1rotor speed); maintenance on con-dition; on-board aircraft testing/di-agnostics with portable test set;ED 56A, ARINC 757/557 compati-ble. Several control unit optionsavailable.

Six channels (4 voice, 1 time, 1rotor speed); maintenance on condi-tion; on-board aircraft testing/diag-nostics with portable test set; ED56A, ARINC 757/557 compatible.Several control unit options avail-able.

Type

Model Recording Medium Size Price

Manufacturer TSO Duration Weight (lb) Power Required Remarks


Aspen Avionics8360 Corona Loop N.E.Albuquerque, N.M. 87113(505) 856-5034Fax: (505) 797-1222www.aspenavionics.com

Avidyne Corp.55 Old Bedford Rd.Lincoln, Mass. 01773(800) 284-3963Fax: (614) 885-8307www.avidyne.com

Chelton Flight Systems1109 Main St. #560Boise, Idaho 83702(208) 389-9959www.cheltonflightsystems.com

HEAD UP DISPLAYS

AT300 AMLCD VSI, display 1/1.0 $3,995Hazard GPS

AwarenessDisplay 3.0 in. pilot selectable 3.3 x 3.3 x 12 or

C8d zoom scales 3.8 28 VCDC113 of 5, 10, 20,

40, 60, 80 and 100 nm

Multi-Hazard AMLCD RS 232 ARINC 429 2.0/0.9 kg $7,990Display ARINC429(MHD) 3ATI 3.26 x 3.26 x $10,990

ARINC 568 8.5 with NVGC147 (DME)C118 10 - 30 VDC

9900BX AMLCD see remarks audible position 1/30 oz. $7,999 -MHD alerting and $28,590*

3 ATI integral altitude 28 VDCC147 alerter annunc.

C118, C113 ARINC 429

EFIS LCD ARINC 429, display, — $70,000Stormscope annunciators one screen

6.4-in. diagonal WX500, and aural 5.5 x 6.25 C113 TCAS, TCAD, warnings x 4.5C110a ARINC, RMI, 11 - 33 VDCC151b ADF, FMSC92C

AIRCRAFT SITUATION DISPLAYS

Unit can replace the primaryVertical Speed Indicator in stan-dard 3-inch instrument cutout.Shows aircraft vertical speed,graphically depicts the currentGPS leg and active waypoint onthe moving map display, andshows either side view terrainor textual GPS navigation infor-mation (current wpt, distance,groundspeed, etc.). The unitalso displays airport symbols forall hard surfaced U.S. airports.Continuously displays currentaircraft track and current air-craft height above ground (de-rived from the terrain databaseand barometric altitude). 15Arc Second (1/4 mile) resolu-tion full continental US terrainand obstacle coverage.

Interface applications with Avi-dyne TAS600-Series, Storm-scope WX-500, Honeywell ClassB TAWS (EGPWS), TCAS I, NVGcompatible, DME

4-port MFD interface capability;provides 360° graphical view oftraffic; displays traffic informa-tion at 5-10 mi. range and over20 mi. range; can scale down to1 mi. ADS-B compatible. MFDpartnerships with 16 otherOEMs. Prices shown for stand-alone MHD and with full 9900BXsystem. *B&CA estimate.

TAWS Classes A, B and C avail-able. Other optional adapters,accessories and software avail-able. Terrain database, naviga-tion and obstruction dataavailable by subscription. (Seealso Chelton Synthetic VisionEFIS in MFD category.) Includesall systems.

Inputs Units/Weight (lb) Price

Size or PowerManufacturer Model Outputs Form Factor Required Remarks

Units/Weight PriceModel Display (lb)

PowerManufacturer TSO Display Size Inputs Outputs Size or Form Factor Required Remarks


Rockwell Collins(Flight Dynamics)166000 S.W. 72nd Ave.Portland. Ore. 97224(503) 443-3050Fax: (503) 443-3070www.flightdynamics.com

Honeywell/ ARINC 429, ASCB, 3/53.0 $470,000BAE Systems discretes, analog,

HUD-2020 enhanced vision 1/2 ATR 28 VDCsensor

Visual Guidance digital 3/35.0 (available from System Gulfstream)(VGS*)

28 VDC

HGS-4000 ARINC 429, various 48.0 $524,560discretes, enhanced

NA vision, synthetic NAvision

Certificated for the Gulfstream IV,IV-SP and V. Enchaned Vision Sys-tem (EVS) certified.

Certified for Gulfstream 550.Enhanced Vision System (EVS)certified.*BAE Systems

Category III HUD available on anumber of business and regionaljet aircraft. Non-CAT III on Bom-bardier Challenger 604.


A v i o n i c s


Eventide, Inc.One Alsan WayLittle Ferry, N.J. 07643(201) 641-1200Fax: (201) 641-1640www.eventide.com


L-3 Avionics Systems5353 52nd St. S.E.Grand Rapids, Mich.49512(616) 949-6600Fax: (616) 285-4224www.L-3com.com/as

ARGUS monochrome ARINC, RMI — 5000: 1/3.5 5000:5000/7000 CRT Stormscope, 7000: 1/4.5 $4,495

ADF, Loran, 7000:C113 5000: 3.2 x 3.2 GPS and FMS $5,495

7000: 3.2 x 4.8 via RS 232 or 5000: 3 ATI U.S & No. RS 422* 3.2 x 3.2 x Am. databases;

10.25 $5,995,7000: 3.2 x international4.8 x 10.75 database

11-33 VDC

ARGUS four-color ARINC, RMI — 5000CE: 1/3.5 5000CE:5000CE/ CRT Stormscope, 7000CE: 1/4.5 $6,995 (U.S.7000CE ADF, Loran & No. Am.

5000CE: GPS and FMS database),3.2 x 3.2 via RS 232 or 5000CE: 3 ATI-S $7,495

C113 RS 422* 3.2 x 3.2 (international7000CE: 10.25 database)3.2 x 4.8 7000CE:

3.2 x 4.8 x 7000CE:10.75 $8,995 (U.S.

& No. Am. database),

$9,495(international

database)

Bendix/King LCD RS 232, — 1/3.3 $4,570,KMD 150 WX 500 with GPS

5-in. diagonal 4.0 x 6.25 x $3,870 none 6.9 without GPS

11 - 33 VDC

Bendix/King AMLCD display 1/3.47 $4,630,KMD 250 with GPS

3-in. diagonal 3.0 x 6.31 x $4,140,C113 6.9 without GPS

Bendix/King LCD RS 232, ARINC display 1/5.0 $7,990KMD 550 429, datalink,

5-in. diagonal EGPWS, 4.0 x 6.2 x 11 - 33 VDCC113, C63, traffic, NTSC 10.0

C110a video &WX 500

Bendix/King LCD RS 232, ARINC display 1/5.0 $13,440KMD 850 429, radar,

5-in. diagonal datalink, 4.0 x 6.2 x 11 - 33 VDCC113, C63a, EGPWS, traffic 10.0

C110a NTSC video& WX 500

RGC350 Existing ARINC 429 lightning and 1/1.5 $6,145*radar EFIS and traffic data to

indicator RS 232 pre-existing 1.48 x 5.73 x 18-32 VDCC105 radar indicator 7.91

varies by system


*Optional ARINC 419 and 429adapter, $995; ARINC RMIadapter, $2,450. OptionalARINC weather adapter,$1,990. Other optionaladapters, accessories and soft-ware available. Database up-dates and Internet accessavailable at additional cost.Ryan TCAD display software,$495.

*Optional ARINC 419 and 429adapter, $995; ARINC RMIadapter, $2,450. Optional ARINCweather adapter, $1,990. Otheroptional adapters, accessories andsoftware available. Database up-dates and Internet access avail-able at additional cost.Ryan TCAD display software,$495

Available with or without VFRGPS. Internal terrain databaseincluded.

Multi-function display for IHAS2000. Provides data link trafficand weather in a 3-in. high mov-ing map with terrain and option-al internal VFR GPS.

Multi-function display for IHAS5000 (Integrated Hazard Aware-ness System). Can be interfacedto display GPS, TIS, TAS, FIS,EGPWS, Wx radar 500 and NTSCvideo. Includes internal terrainand obstacle database.

Multi-function display for IHAS8000 (Integrated Hazard Aware-ness System). Can be interfacedto display GPS, TIS, TAS, FIS,EGPWS, Wx radar 500 and NTSCvideo. Includes internal terrainand obstacle database.

Interfaces with a variety ofweather radar display systemsfrom Bendix/King,Honeywell/Sperry/RCA andRockwell Collins. System over-lays existing weather radar dis-play with choice of four modesof traffic and/or lightning dataprovided by Skywatch or TCAS Iand/or Stormscope (WX-100E429 EFIS or WX-500) and/orLandmark TSWS 8000.*B&&CA estimate.




Rockwell Collins400 Collins Rd. N.E.Cedar Rapids, Iowa 52498(319) 295-4098Fax: (319)295-2297www.rockwellcollins.com

Rogerson-Kratos403 S. RaymondPasadena, Calif. 91109(626) 449-3090www.rogersonkratos.com

Sagem Avionics, Inc.2701 Forum Dr.Grand Prairie, Texas 75052(972) 314-3600Fax: (972) 314-3640www.sagemavionics.com

Western division:16923 Meridian E.Puyallup. Wash. 98375(253) 848-6060Fax: (253) 848-3555


FDS-2000 AMLCD ARINC 407 ARINC 429, 8/38.0 $129,900*419, 429, 453, AC discretes,

C3d, C4c, C5e, 552, 561, 568 DC discretes, five 28 VDCC6d, C34e, analog DC analog 5 ATI displays

C35d, C36e,C40c, C41d,C52b, C66c,C87, C92c,

C113, C115bC117a, C129a

5 ATI EFIS AMLCD flat analog synchro analog synchro 1/7.75 $42,000panel (XYZ, Sin/Cos) (XYZ, Sin/Cos)

C3d, C4c, C5e, variable AC/DC variable AC/DC 5 ATI or 28 VDCC6d, C8d, C9c, 5 ATI discretes & discretes & 6.4 dia. 44 w maxC34e, C35d, digital ARINC digital ARINCC36e, C40c, 429, 419, 453, 429, 419, 453,C41d, C52b, 735, RS-232 735, RS-232C63c, C66c,

C67, C87, C92c,C113, C117a,C118, C119b, C129a, C147,

C161a

MFD 5200 AMLCS RS-232/422 NA CDU: 2.26 $8,995*RPU: 2.50

5-in. diagonalC113 CDU: 4.75 x

6.25 x 2.0 10-35 VDCRPU: 2.0 x 6.25 x 9.25

ICDS-10, AMLCD all units all units ICDS-10: 6.26/ $15,000ICDS-8, provide: provide: 8.2 x 11.12 x all unitsICDS-6 ICDS-10: GPS, engine display, 2.7

10.4 in. diagonal monitor, AHRS annunciators,Stormscope, aural warn. ICDS-8: 4.2/

ICDS-8: video, FLIR mission 6.55 x 9.75C63c 8.4-in diagonal traffic, wx mgt., engine 2.8C110a trendC113 ICDS-6: 4 -RS 232 monitoring ICDS-6: 3.0/

6.4-in diagonal 2 - ARINC 429 5.52 x 7.01 x2 - 453/708 4.025

SA4500 rear analog or NA 1/3.75 $20,000EDAI projection LCD ARINC 429

4 ATI 28 VDC

C4c, C113


Configurable for flexible retrofitapplications; weather radar, FMS maps, TCAS and terrainawareness interfaces. Wide viewing angle. Price includes five SATI displays and three display control panels.*Typical configuration.

One, two or four programmable,self-contained flat-panel AMLCDEADI and EHSIs. Radio altimeterfunctions such as DH, expandedscale for landing helicopter opera-tions, TCASI and II, and EGPWSdisplay capability, in addition tostandard ADI, HSI, bearing point-ers, CDI, autopilot annunciation,flight director cross bars or ‘V’bars. Upgrade packages available.

Moving map and terrain situa-tional awareness with weatheroverlay. Interfaces with mostnavigation systems, BFGoodrichWX500 Stormscope, Ryan (Avi-dyne) TCAD, ARNAV DR-100VHF WxLink, RCOM-100 Sat-com, engine trend monitoringsystem. Optional engine trend-monitoring qualifies for P&WETCM quality assurance pro-gram. Optional satcom or VHFdata link display. *B&CA esti-mate.

When installed in an integratedpanel can display movingmap,GPS, engine information,weather displays, video andother aeronautical informationand PFD. A terrain and obstruc-tion database is standard withunits configured as an MFD.

4 x 4 electronic ADI that ac-cepts input from almost anygyro source. Incorporates flightdirector command bars, glide-slope/localizer deviation scale,fast/slow indicator, rising run-way symbol and mode annuncia-tions. Pin selectable single-cue/split-cue display option.




A v i o n i c s



EFI-550 AMLCD ARINC ARINC 1/7.1 $33,000*6 - 429/419 429/419 (2)

C3d, 3.35 x 4.36 1 - 561/568 RS 422 (2) (EFIS-85 std.) 28 VDCC4c, 2 - 453/708A 6 - analog 4.8 x 5.18 C5e, 5.5-in. dia. 2 - RS 422 8 - discretes x 7.90C6d, 4 - analog (from front C52b, 30 - discretes* mount surface)C105,C113

EFI-640 AMLCD ARINC ARINC 1/7.8 $34,000*6 - 429/419 429 (2)

C3d, 3.86 x 5.14 1 - 561/568 RS 422 (2) 5 x 6 ATI 28 VDCC4c, 2 - 453/708A 6 - analog 5.18 x 6.18C5e, 6.4-in. dia. 2 - RS 422 8 - discretes x 7.9C6d, 4 - analog (from frontC52b, 30 - discretes* mount. surface)C105,C113

EFI-600 AMLCD ARINC ARINC 1/7.8 $34,000*6 - 429/419 2 -429

C3d, 4.21 x 4.21; 1 - 561/568 2 - RS 422 5 ATIC4c, 6.0- in. dia. 2 - 453/708A 6 - analog 5.18 x 5.18C5e, 2 - RS 422 8 - discretes x 7.9 (from 28 VDC

C6d, C52b, 4 - analog front mountC105, C113 30 - discretes surface)

EFI-890R active matrix Analog: Analog: 1/12.0 $58,000*color LCD 6 ARINC 429, 2 ARINC 429,

5 CSDB, 2 CSDB, bezel: 7.84 h 6.3 x 6.3 2 ARINC 708, 1 Manchester x 7.42 w 28 VDC

C2d, C3d, C4c, (8.0 in dia.) 3 Manchester bus port depth: 9.79C5e, C6d, C8d, bus ports (back of bezelC10b, C34e, 2 VGA or to rear ofC35d, C36c, 1 RDR-1E/F & Digital: connector)C40c, C41d, 1 VGS, 5 GND/OPNC52b, C63c, 1 RS 232 discretes, C66c, C87, (maint.) 3 28 VDC/OPNC92c, C95, discretes,

C105, C113, Digital: 6 analog C115b, C118, 28 GND/OPN resolvers, 2 DCC119a, C129a, discretes, differential,

C151a 14 28 VDC/ 2 DC singleOPN ended

4 ARINC 407with 2 ref.

inputs,15 analog DC


*Depending on configuration.

Horizontal viewing angles of+/-60°.; electronically adjustedvertical viewing angle; sunlightreadability with greater than10,000/1 dimming range.*Depending on configuration.

Horizontal viewing angles of+/-60°.; electronically adjustedvertical viewing angle; sunlightreadability with greater than10,000/1 dimming range.*Depending on configuration.

Horizontal viewing angle +60°/-60°, vertical viewingangle +45°/-10°; resolution: 780 x 780 pixels; 124.5 colorgroups per inch (CGPI); sun-light readability with greaterthan 10,000/1 dimming range. *Depending on configuration.




CMC Electronics415 Legget Dr.Ottawa, OntarioCanadaK2K-2B2(613)592-6500Fax: (613) 592-7427www.cmcelectronics.ca

NavAero9-15 W. Hubbard St.5th FloorChicago, Ill. 60610(866) 628-2376Fax: (312) 423-9966www.navaero.com


Pilot-View EFB touch-screen ARINC 429 ARINC 429 2/5.5 $18,842AML CD ethernet ethernet

1024 x 768 wireless-802 wireless-802pixel 11g, 11g

Class 2 resolution USB 2.0 USB 2.0 NAPCMICA PCMICARS 170 RS 170 9 - 36 VDC

6.0 x 8.0 x 1.5 RS 232 RS 232NTSC video

8.4-in diagonal

t-BagC2 color TFT CPU: 1 USB CPU: 1 USB 1/NA $3,495* withEFB LCD resistive slot slot 8.4-in display

touch screen Connectors: Connectors: 93.8 x 113.861 pin sealed 61 pin sealed 23.8 $3,995* with

Class 2 8.4 in or cradle cradle excluding 10.4-in display10.4 connector, connector, connectors

tPad interface, tPad interface and mounting3 USB, 3 USB, hardware 13.8 - 30 VDC

1 RS 232 1 RS 232 60W maximum1 LAN 1 LAN

UCD UCDT II 4 ARINC 429, 1 ARINC 429 Remote UCD $19,500(Universal touch screen 8 discrete, 4 discrete, computerCockpit terminal display 2 NTSC video 10/100 base T 1/8.9 28 VDCDisplay) 1 S video network 1 MCU

10/100 base T capability $13,0005.0 x 6.50 network UCD

capability terminal II powered byClass 2 8.4-in. diagonal 1/2.8 UCD

6.45 x 8.43x 1.48

ELECTRONIC FLIGHT BAGS

Touch-sensitive screen and lineselect keys. Intuitive pilot in-terface. Applications include:electronic charts such as JeppView and JeppFlite Deck,checklists, performance calcu-lations, electronic documents,moving maps and weather.

*Installation kit extra. Class 2EFB can be used to store, re-trieve, display and use a widevariety of required documentsand procedures such as opera-tions specifications, perform-ance data, operations manuals,MELs, control documents andvideo surveillance. CPU: 1 GHzprocessor, 40GB hard drive,512MB memory, Windows XPProfessional OS. RemovableCPU module computer systemcontains CPU, power supplyand emergency battery back-up nickel cadmium power pack.

Provides supplementary displayfor viewing electronic charts,checklists and external videosources. As an electronic flightbag (EFB), the UCD supports aterminal area chart databasevia Jeppesen, Inc. Charts, NO-TAMs and airport informationdownloaded from CD-ROM andstored in flash memory withinUCDC. Flight plan departureand arrival airport informationfrom FMS prompts displays ofdeparture, arrival and approachcharts and airport diagrams.Manual searches accomplishedvia pull-down menu and touch-screen keyboard. Two user-de-fined zoom levels. System over-lays aircraft position ontoapproach charts and airport diagrams.


PowerManufacturer Class Display Size Inputs Outputs Size Required Remarks


A v i o n i c s


CMC Electronics415 Legget Dr.Ottawa, OntarioCanadaK2K-2B2(613)592-6500Fax: (613) 592-7427www.cmcelectronics.ca

Kollsman220 Daniel Webster Hwy.Merrimack, N.H. 03054 (603) 889-2500www.kollsman.com

MAX-VIZ, Inc.16165 SW 72nd. Ave.Portland, OR97224(503) 968-3036www.Max-Viz.com

EVS-1000 head-down single, long- raster capable sensor head: $83,400*IR EVS EVS wave infrared HUDs; 1/2.5

sensor; ARINC independent429 opt. cockpit LCD; 2.8 x 6.8 28 VDC

2.77 video 30 WNA compatible FMS power module:

CDU and MFD; 1/2.5 electronics: ARINC 429 opt. 10 W peak at

3.75 x 5.0 x 28 VCDC;RS-170 output 2.5 environmental:with RS-232 <50 W avg.;

interface 125 W max(with heater)

EVS-2500 head-up or head- dual,long-wave raster capable sensor unit: $350,000*Dual Sensor down EVS infrared sensors HUDs; 1/10.0

IR EVS ARINC 429 opt. independentcockpit LCD; 11.0 x 6.88 x electronics:

video 6.27 10 W typical;compatible FMS 75 W peak at

NA CDU; analog processor 28 VDC pervideo per unit: 1/5.0 DO-160RS-170 1/4 ATR category Z

ARINC 429 opt. environmental:225 W typical;275 W peakwith window

deicer

All Weather HUD/HDD 1 - 5 micron RS 170 3/21.0 (available Window forward-looking analog video; from

Enhanced Vision infrared SMPTE 259; GulfstreamSystem (FLIR) digital video-

sensor; any raster 1/2 ATR 28 VDCARINC capable;

see 427 head-up or remarks head-down

display, like a CRT or LCD

EVS-1000 head-down single long raster capable sensor head: $83,400*IR EVS enhanced wave infrared head-up 2.8-in. dia. x

vision system sensor; displays; 6.8 long/2.5 lb electronics: ARINC 429 independent 10 W typical

opt. cockpit LCD Power module: 25 W peak2.77 dia. displays; video 3.75 x 5.0 x at 28 VDC;

NA compatible 2.5/2.5 lb environmental:FMS CDU; <50 W avg;

video 125 W maxcompatible (with heater)

MFD;ARINC 429 opt.

RS 170 outputwith RS 232

interface

EVS-2500 head-up or head dual long raster capable sensor unit: $350,000*Dual Sensor down enhanced wave infrared head-up 1/10.0

IR EVS vision sensor; displays;system ARINC 429 independent 11.0 x 6.88 x electronics:

opt. cockpit LCD 6.27 in. 50 W typical;NA displays; video 75 W peak at

compatible processor: 28 VDC perFMS CDU; 1/5.0 DO-160

analog video 1/4 ATR category Zper RS 170;

ARINC 429 opt. environmental:225 W typical;275 W peak with window

deicer on

ENHANCED VISION SYSTEMS (EVS)

When used with a HUD as part ofa certified EVS, infrared sensorprovides situational awarenessto pilots for night and low-visibili-ty situations.

Infrared sensor provides situa-tional awareness to pilots fornight and low-visibility situations.

STC’d on Gulfstream GIV, GV,and as an option for the G-300,G400, G500, GV, and GIVSP.Standard equipment on Gulf-stream GVSP (G550) and G450aircraft. Provides real time imageof outside scene of airport run-way lights and surrounding envi-ronment in aircraft's flight path.Provides lower landing minimumcredit per FAR 91.175 EFVS regulations.

Tail/nose mounted infrared cam-era that provides a 40° field ofview to a cockpit display forviewing by the cockpit crew. In-stallation kit and harness not in-cluded. Resolution 320 x 240pixels. Independent cockpit LCD;video compatible FMS CDU;video vompatible MFD. Field ofview (FOV) Head-down display53° x 40° typical; special FOVson request. *B&CA estimate.

Dual sensor version of above.Field of view (FOV): 53° x 40° or30° x 22.5°; others available onrequest. Resolution 320 x 240pixels. Includes wiring harnessand connectors.*B&CA estimate.


PowerManufacturer TSO Display Size Inputs Outputs Size Required Remarks


Manufacturer

Model




RNP Certification










ARINC Radar (in)















Weight, Dimensions & Powe Weight (lb)CDU Height x Width x Length (in.)



Price

Remarks

FreeFlightSystems, Ltd.

2101 Approach Plus

I

D | LED

D

BRNAV

Std. | —4

— | —

A

— | —

Std. | A1— | —| —— | —| —

4/0

—— | —— | —

—

—

— | ———

— | Std.

B

Std.—/——/—

—/———

————

— | —— | —

—

—

25040 | 40

D— | —

E

3.653.0 x 5.75 x 7.68

A | B— | —

—

$7,245

Price includesreceiver, datacard,installation kit (with

antenna), installationmanual and pilot guide.Unit also available with

night vision gogglecompatibility.

GarminInternational

GPS 155 XL TSO

I

P | LCD

D

BRNAV

Std. | ——

— | —

A

— | —

— | —— | —| —— | —| —

1

Std.— | —— | —

—

—

— | ———

— | Std.

B

Std.1/01/0

Std./Opt.—

429

Std.Opt.Opt.Std.

— | Std.Opt. | —

429

—

1,00020 | 31

DStd. | Std.

E, A

2.42.0 x 6.25 x 5.8

A | B— | —

—

$3,995

Twelve-channel parallel GPS receiver with

moving map display.

GarminInternational

GPS 165 TSO

I

Rmks. | Rmks.

D

BRNAV

Std. | ——

— | —

A

— | —

Std. | A1— | —| —— | —| —

2/0

Std.— | —— | —

—

—

— | ———

— | Std.

B

Std.1/01/0

Std./Opt.—

429

Std.Opt.Opt.Std.

Std. | —Opt. | —

429

—

1,00020 | 31

D-- | Std.

E, A

2.02.25 x 5.75 x 5.65

A | B— | —

—

$6,495

Display: vacuumfluorescent; comes with aMultiTrac8 GPS receiver.

FLIGHT MANAGEMENT SYSTEMSGarmin

International

GNC 300 XL TSO

I

P | LCD

D

BRNAV

Std. | ——

— | —

A

— | —

Std. | A1— | —| —— | —| —

1

Std.— | —— | —

—

—

— | ———

— | Std.

B

Std.1/01/0

Std./Opt.—

429

Std.Opt.Opt.Std.

Std. | —Opt. | —

429

—

1,00020 | 31

DStd. | Std.

E, A

2.42.0 x 6.25 x 5.8

A | B— | —

—

$4,795

Twelve-channel parallel GPS receiver with

moving map display.Five-watt comm

transmitter.

FreeFlightSystems, Ltd.

2101 I/O Approach Plus

I

D | LED

D

BRNAV

Std. | —4

— | —

A

— | —

Std. | A1— | —| —— | —| —

4/0

Std.— | —— | —

—

—

Std. | Std.Std.Std.

Std. | Std.

B

Std.2/02/0

A/B—

429

Std.Std.Std.Std.

Std. | —Opt. | —

A

RS422

25040 | 40

DStd. | Std.

E

3.653.0 x 5.75 x 7.68

A | B— | —

—

$11,500

Price includesreceiver, datacard,installation kit (with

antenna), installationmanual and pilot guide.

Sole means oceanicapproval; interfaces

with EGPWS.



DISPLAY


DATA ENTRY FORMAT


VERTICAL NAV MODES


POWER

A = 10-19 VDCB = 20-40 VDCC = 115 VAC


A v i o n i c s


Manufacturer

Model




RNP Certification










ARINC Radar (in)


















Price

Remarks

GarminInternational

GPS 400

I

P | C

D

RNP-10, BRNAV

Std. | —19

— | —

A

— | —

Std. | A1— | —| —— | —| —

2/0

Std.— | —— | —

—

—

Opt. | Opt.Opt.Opt.

Std. | Std.

A, B

Std.2/02/0

Std./Opt.—

429

Std.Opt.Opt.Std.

Std. | —Opt. | —

429

—

1,00020 | 31

DStd. | Std.

E, A

4.92.65 x 6.25 x 11.0

A | B— | —

—

$6,795

Twelve-channel GPS withcolor moving map. FDEprimary means remote

and oceanic.

GarminInternational

GNS 430/430A*

I

P | C

D

RNP-10, BRNAV

Std. | —19

Std. | —

A

— | —

Std. | A1Std. | — | —— | — | —

2/0

Std.— | —

— | Std.—

—

Opt. | Opt.Opt.Opt.

Std. | Std.

A, B

Std.2/02/0

Std./Opt.—

429

Std.Opt.Opt.Std.

Std. | —Opt. | —

429

—

1,00020 | 31

DStd. | Std.

E, A

6.62.65 x 6.25 x 11.0

A, B— | —

—

$9,250*

Comes with a GPS andVOR/ILS receiver and

8.33-kHz VHF comm. FDEprimary means remote

and oceanic. Terrain advi-sories/TAWS-B. *GNS430A, $14,250; incl.

16-watt min. comm TX.

GarminInternational

GNS 530/530A*

I

P | C

D

RNP-10, BRNAV

Std. | —19

Std. | —

A

— | —

Std. | A1Std. | — |—— | — |—

2/0

Std.— | —

— | Std.—

—

Opt. | Opt.Opt.Opt.

Std. | Std.

A, B

Std.2/02/0

Std./Opt.—

429

Std.Opt.Opt.Std.

Std. | —Opt. | —

429

—

1,00020 | 31

DStd. | Std.

E, A

8.44.6 x 6.25 x 11.0

A, B— | —

—

$14,995*

Comes with a GPS andVOR/ILS receiver and


and oceanic. Terrainadvisories/TAWS-B.

*GNS 530A, $19,995;incl. 16-watt min.

comm TX.

FLIGHT MANAGEMENT SYSTEMSGarmin

International

GPS 500

I

P | C

D

RNP-10, BRNAV

Std. | —19

— | —

A

— | —

Std. | A1— | —— | —

2/0

Std.— | —— | —

—

—

Opt. | Opt.Opt.Opt.

Std. | Std.

A, B

Std.2/02/0

Std./Opt.—

429

Std.Opt.Opt.Std.

Std. | —Opt. | —

429

—

1,00020 | 31

DStd. | Std.

E, A

6.94.6 x 6.25 x 11.0

A, B— | —

—

$12,500

Twelve-channel GPS withcolor moving map. New

model from this OEM. FDEprimary means remote

and oceanic. Terrainadvisories/TAWS-B.

GarminInternational

GNC 420/420A*

I

P | C

D

RNP-10, BRNAV

Std. | —19

— | —

A

— | —

Std. | A1— | — | —— | — | —

2/0

Std.— | —— | —

—

—

Opt. | Opt.Opt.Opt.

Std. | Std.

A, B

Std.2/02/0

Std./Opt.—

429

Std.Opt.Opt.Std.

Opt. | —Std. | —

429

—

1,00020 | 31

DStd. | Std.

E, A

5.82.65 x 6.25 x 11.0

A, B— | —

—

$7,995*

Twelve-channel GPS withcolor moving map and


and oceanic. *GNC 420A,$12,995; incl. 16-watt

min. comm TX. Terrain ad-visories/TAWS-B.



DISPLAY


DATA ENTRY FORMAT


VERTICAL NAV MODES


POWER

A = 10-19 VDCB = 20-40 VDCC = 115 VAC

Manufacturer

Model




RNP Certification










ARINC Radar (in)















Weight, Dimensions & Powe Weight (lb)CDU Height x Width x Length (in.)



Price

Remarks

Honeywell Aero.Electronic Systems

KLN 900

I

D | M

D

RNP-10

Std. | ——

— | Std.

A

— | —

Std. | A1— | — | —— | — | —

3/0

—— | —— | —

—

—

Std. | ———

Std. | Std.

B, C

Std.1/00/1

A, B—

429, 561

Std.Std.Opt.Std.

Std. | —Std. | —

429, 561, 568

—

1,00025 | 30

DStd. | Std.

E

4.53.75 x 5.75 x 9.46

B— | —

—

$17,490

Add $1,000 for KA90 HSIadapter. BRNAV and

primary means oceanicversion available. RAIM

and FDE prediction.Database update via

Internet available.


FMZ-2000

III

F | LCD, C

Std.

RNP-0.3

Std. | Std.23

Std. | Std.

M, A

Rmks. | Std.

Std. | B1, C1Std. | Std. | Std.Std. | — | Opt.

21/0

Std.Std. | Std.— | Std.

Std.

Std.

— | ———

Std. | —

A, C

6/0**

A, B—

429

Std.Std.Std.Std.

Std. | —— | —

429, ASCB

429

1,0003,000 | 100

R— | —

E, A

77.13 x 5.75 x 6.75

B/B2 | 7.9

B/-

$145,420

Performance managementuses Honeywell SmartPerfas standard; Gulfstream

IV/IV-SP uses table-basedperformance.

*HI/LO configurable.

Rockwell Collins

FMS 4200/6000

III

F | C/CRT

Std.

RNP-0.3, -10, BRNAV

Std. | Std.23

Std. | —

M

Std. | Std.

Std. | B1, C1— | Std. | Std.— | Std. | —

4/3

** | ** | *

*

*

* | ***

* | *

*

—0/00/0

A

****——

Std. | Std.— | —

—

—

1001,000 | 100

R— | —

E, A

46.375 x 5.75 x 6.33

BRmks. | 1.9

—

NA

*FMS I/O provided via 4redundant concentrators.See FMS 3000 remarks.FMS 4200 has advisoryVNAV but not FMS to ILSauto transfer. Coupled

VNAV available onFMS 6000.

FLIGHT MANAGEMENT SYSTEMSRockwell Collins

FMS 3000/5000

III

F | C/LCD

Std.

RNP-0.3, -10, BRNAV

Std. | Std.23

Std. | —

M

Std. | Std.

Std. | B1, C1— | Std. | Std.

— | Std. | —

4/3

** | ** | *

*

*

* | ***

* | *

*

—0/00/0

A**

**——

Std. | Std.— | —

—

—

1001,000 | 100

R— | —

E, A

8.96.375 x 5.75 x 6.33

BRmks. | 1.9

—

NA

*FMS I/O provided via 4redundant concentrators.

Remote computer dimensions 1.7 x 8.74 x

6.06 in.; FMS 5000requires radio tuning unit.FMS 3000 radio tuning

is internal.


GNS-XLs

III

F | LCD

D

RNP-0.3, -10.5, BRNAV

Std. | Std.10

— | Std.

A

— | Std.

Std. | A1, B1, C1Opt. | Opt. | Opt.

Opt. | — | —

13/0

Std.Std. | Std.Std. | Std.

Std.

Std.

Std. | Std.Std.Std.

Std. | —

C

—7/07/0

A, B429, 571

429

Std.Std.Std.Std.

Std. | —Std. | —

429, 561, 571

RS-422

99956 | 50

D— | —

E

74.5 x 5.75 x 7.62

B— | —

—

$42,410

Enhanced versionavailable. Optional RPU

will display wx andEGPWS graphics.



DISPLAY


DATA ENTRY FORMAT


VERTICAL NAV MODES


POWER

A = 10-19 VDCB = 20-40 VDCC = 115 VAC



A v i o n i c s


Avidyne FlightMaxEX500

4.35 x 6.25 x 10.75616 x 350

52Yes | No

DYesYesYes

YesYesYesYesNoYesYes

No | YesYes | No

YesYesYesYesYes

YesYesNoYes

Yes | Yes

YesYes

Yes | No

Yes | YesOpt. | No

$11,995

Price includes digitalradar interface andintegrated data link

transceiver. Non-radarversion, $9,995.

Available options: Cmax,TCAS-1 and EGPWS.

Avidyne FlightMaxEX5000

8.50 x 10.70 x 3.80800 x 600

52Yes | No

DYesNoYes

NoYesYesNoNoNoNo

Opt. | YesYes | No

YesYesYesYesYes

NoYesNoYes

Yes | Yes

YesYes

Yes | No

Yes | YesOpt. | No

$12,995

Includes integrateddata link. Available

options: Cmax, TCAS-1and EGPWS.

Chelton FlightLogic Synthetic Vision EFIS

6.25 x 5.5 x 4.5640 x 480 (256 colors)

2.30Yes | Pending

C, AYes

PendingYes

NoGeneric

YesYesNo

PendingYes

Yes | YesNo | No

40/40YesYesYesYes

PendingYes

PendingNo

Pending | No

YesYes

Yes | Yes

Yes | YesYes | Yes

$70,000*

HUD symbology; 3-Dmodeling; Class A,B,C

Taws w/threat diff.; integral GPS/WAAS;

Jeppesen NavData; on-screen full-function

FMS; inertial AHRS; un-usual attitude

recovery mode.*One screen.

Garmin InternationalMX20 Series

5.0 x 6.25 x 8.0640 x 480

20Y | YC, DYesYesYes

NoNo

Yes*YesNoYesNo

No | YesNo | No

YesYesYesYesYes

YesYesYesYes

NA | NA

YesYes

Yes | No

Yes | YesYes | Yes

See Remarks

*Via converter. $6,995to $14,995 depending

on options. TSO’dand/or JTSO’d for

C110a, C113, C118,C63c, C147.

Honeywell MFRD/80-5204

6.242 x 4.815 x 8.3781024 x 768

10Yes | Yes

BYesYesYes

NoYesYesNoNoYesYes

No | YesYes | Yes

YesYesYesYesNo

YesYesNoNo

No | No

NoNo

Yes | Yes

Yes | YesNo | No

$42,500

Combines weatherradar, traffic, terrain,navigation maps and

other data into a singledisplay unit.

MULTI-FUNCTION DISPLAYSManufacturerModel

MFD FeaturesDimensions (H x W x D in inches)

Resolution (i.e., pixels)

Boot-Up Time (Seconds)

FAR Part 23 | FAR Part 25

Do 178 Software Integrity Level

TSO C113 MFD

TSO C63c Wx Radar

TSO C110a Lightning

InterfacesARINC 407 Synchro I/F

ARINC 429 GAMA I/F

ARINC 429 Generic I/F

ARINC TCAS I/F

ARINC 561/568 INS

ARINC 708/453 Wx Radar I/F

ARINC 735 TCAS I/F

Video | RS 232

Honeywell KCPB | Honeywell WXPB

Situational Awareness FunctionsPosition Awareness

F/P Waypoints/Legs

Proximate Navaids

Proximate Airports

Proximate Intersections

Special-Use Airspace

Weather Awareness

Wx: Onboard Radar

Wx: Onboard Lightning Sensor

Wx: Air/Ground FIS-B Downloads

Wx: Air/Ground Other Downloads

Wx: Satcom Data Link | Low-Rate | High-Rate

Traffic Awareness

TIS-B via Mode S Data Link

TAS: TSO C147

TCAS I: TSO C118 | TCAS II: TSO C119

Terrain Awareness

Basic Topography | Basic Cartography

TAWS: TSO C151 Class B | TAWS: TSO C151 Class A

Price

Remarks


L-3 Avionics Systemsi-linc

5.0 x 6.25 x 8.0640 680

20Yes | No

C, DYesYesYes

NoNoYesYesNoYesYes

No | YesNo | No

YesYesYesYesYes

YesYesNoYes

Yes | Yes

NoYes

Yes | No

Yes | YesYes | No

$9,071*

Radar compatible version, $15,422.*B&CA estimate.

L-3 Avionics SystemsPVI Series 600

5.7 x 6.65 x 10.43 120 pixels/line

10Yes | Yes

BYesYesNo

NoYesYesYesNoYesYes

Yes | YesNo | No

NoNoNoNoNo

YesNoNoNo

No | Yes

NoNo

No | No

No | No No | No

See Remarks

$29,900 plus $4,500(B&CA estimate)

for analog weatherradar support

TSOed to C105.

Rockwell CollinsFDS-2000

5.09 x 5.09 x 9.06719 x 719

9No | Yes

AYesYesNo

YesYesYesYesYesYesYes

No | NoNo | No

YesYesYesYesNo

YesNoNoNo

No | No

NoNo

No | Yes

No | No No | Yes

$43,427

Functionalreplacement for

conventional flightdirector indicator.

Supports operations inCNS/ATM environment.

Adapts to multipledisplay configurations.

Sandel ST3400 TAWS

3.285 x 3.285 x 10.31 mega-pixel

15Yes | Yes

CYesNoNo

YesYesYesOpt.NoNo

Opt.No | YesNo | No

YesNoYesNoNo

NoNoNoNo

No | No

NoOpt.

Opt. | No

Yes | NoYes | Yes

See Remarks

TAWS Class A, $34,500;TAWS Class B, $20,950;optional raffic interface,

$2,500.

Universal AvionicsMFD-640

5.18 x 6.68 x 7.1*640 x 480

15Yes | Yes

CYesYesYes

YesYesYesYes

No**YesYes

Yes | NoYes | Yes

YesYesYesNoNo

YesYesNoYes

NA | NA

NoNo

Yes | Yes

NA | NAYes | Yes

$39,500

*6.4-inch display; C105and C119b interfaces;compatible with legacyradar systems, supports

Universal TAWS with3-D video display.

**Displays ARINC 419INS from LTD-92.

MULTI-FUNCTION DISPLAYSManufacturerModel

MFD FeaturesDimensions (H x W x D in inches)

Resolution (i.e., pixels)

Boot-Up Time (Seconds)

FAR Part 23 | FAR Part 25

Do 178 Software Integrity Level

TSO C113 MFD

TSO C63c Wx Radar

TSO C110a Lightning

InterfacesARINC 407 Synchro I/F

ARINC 429 GAMA I/F

ARINC 429 Generic I/F

ARINC TCAS I/F

ARINC 561/568 INS

ARINC 708/453 Wx Radar I/F

ARINC 735 TCAS I/F

Video | RS 232

Honeywell KCPB | Honeywell WXPB

Situational Awareness FunctionsPosition Awareness

F/P Waypoints/Legs

Proximate Navaids

Proximate Airports

Proximate Intersections

Special-Use Airspace

Weather Awareness

Wx: Onboard Radar

Wx: Onboard Lightning Sensor

Wx: Air/Ground FIS-B Downloads

Wx: Air/Ground Other Downloads

Wx: Satcom Data Link | Low-Rate | High-Rate

Traffic Awareness

TIS-B via Mode S Data Link

TAS: TSO C147

TCAS I: TSO C118 | TCAS II: TSO C119

Terrain Awareness

Basic Topography | Basic Cartography

TAWS: TSO C151 Class B | TAWS: TSO C151 Class A

Price

Remarks

2006 purchase planning handbook - aviation...

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