cobham adahrs (air data attitude heading reference …3. fuel flow. the addition of a fuel flow...

FUEL FLOW & AIR DATA SYSTEMS

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499Order Toll Free1-800-235-3300

Fax: 1-800-828-0623

http://www.edmo.com

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Cobham ADAHRS (Air Data Attitude Heading Reference System) ... 501

Sandia Air Data Computer Systems ................................................ 501 Modular Accessory Remote Cards ............................... 505-506 Modular Accessory Remote Card Enclosures ..................... 505

Shadin Air Data Computer Systems ................................................ 501 Engine Trend Monitors ........................................................ 502 Air Data Converters ............................................................. 502 Fuel Flow Management Systems ................................. 504-505

The most important thing we build is trust

ADAHRS. Precise digital output of aircraft position rate, vector, and acceleration data.

• Reliable. DO-178B, Level A Software

• Lightweight. 3-component product suite

is less than 1.5 lbs.

• Rugged. Meets RTCA/DO-160E

environmental standards

• Compact. 2” x 2.5” x 3.9” (ADAHRS)

The Cobham digital Air Data and solid-state

Attitude/Heading Reference System (ADAHRS)

is lightweight and compact. It incorporates a

Magnetic Sensing Unit (MSU) and separate

Outside Air Temperature (OAT) Probe. This

highly accurate system employs the latest

Micro-Electro-Mechanical System (MEMS)

technology to provide extremely precise

digital output and referencing of aircraft

position rate, vector, and velocity.

© 2009 Cobham, plc. All rights reserved.

Cobham Avionics Integrated Systems

One S-TEC Way

Municipal Airport

Mineral Wells, TX 76067

Tel: (817) 215-7600

Fax: (940) 324-3904

www.cobham.com/avionics

Air Data and Attitude/Heading Reference System (ADAHRS)

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Fax: 1-800-828-0623

http://www.edmo.com

ADAHRS(Air Data AttitudeHeading Reference

System)

ADAHRS

MSU

OAT Probe

The new Cobham digital Air Data and solid state Attitude/Heading Reference System (ADAHRS) is light weight and compact. It incor-porates a Magnetic Sensing Unit (MSU) and separate Outside Air Temperature (OAT) Probe.

This highly accurate system employs the latestMicro-Electro-Mechanical System (MEMS)technology to provide extremely precise digitaloutput and referencing of aircraft position rate,vector and acceleration data.

Mfg P/N: Description42-005001-0001 ADAHRS Independent42-005005-0001 ADAHRS Install Kit42-002001-0001 OAT Probe42-002003-0001 OAT Install Kit42-004001-0001 Magnetic Sensing Unit

(MSU)42-004003-0001 MSU Install Kit

Air Data ComputerSystems

ADC-200This versatile SHADIN Fuel/Airdata computer generates real time fuel and airdata informa-tion and displays that information on selected GPS systems through a standard RS232/422 format. The ADC-200 will calculate and send the following data: IAS, TAS, MACH, P.ALT, D.ALT, OAT, TAT Winds Aloft, Wind Component, Rate of Turn, Fuel Flow, Fuel used, Fuel Remaining, Endurance, L. Fuel Used, R.Fuel Used. The ADC-200 requires ARINC 407 X,Y,Z information from the HSI bootstrap.Size: 6.25” L X 3.125” W X 3.25” H

P/N: Description:962820-1A ADC-200/Digital/High Level IF962820-2A ADC-200/Sine Wave/RS232/RS422962820-3A ADC-200/DC Analog681201-1 OAT Probe/Kit (Sold Separately)

ADC-2000This next generation Fuel/Airdata computer incorporates all the functions of the ADC-200 (listed above) with the addition of the following 3 functions; 1) A standard ARINC 429 driver board with switch selectable output to drive most stan-dard 429 systems. 2) The capability of taking baro-corrected altitude from compatible altimeter systems automatically updating your GPS. 3) A built in, 55,000ft high resolution encoder.Size: 5.5” L x 3.875” W x 3.875” H

P/N: Description:962830-1A Digital/High Level IF/429 Out962830-2A Sine Wave/Baro Correct/429 Out962830-3A DC Analog/Baro Correct/429 Out962830A-1 MS Connector/Digital/High Level

IF/429 Out962830A-2 MS Connector/Sine Wave/Baro

Correct/429 Out962830A-3 MS Connector/DC Analog/Baro

Correct/429 Out681201-1 OAT Probe/Kit (Sold Separately)

ADC-8000Citation 500 Series Pre S/N 275 RVSM SolutionThe Shadin Avion-ics ADC-8000 RVSM System is specifically designed for the early Cessna 500 series air-craft, serial numbers 001 through 274. This Air Data Computer (ADC) System replaces the existing Altitude Hold Controller and provides the aircraft with Reduced Vertical Separation Minimum (RVSM) capability.P/N: CALL FOR INFO!

DigidataPanel mounted version of the ADC-200. Recom-mended for those customers with available panel space. Allows the customer to “customize” their cockpit by displaying fuel flow information at all times in addition to one of the other output functions for the ADC-200. This allows the pilot to avoid leaving their NAV pages in the GPS system and reference the Digidata only. Com-patible with most Loran/GPS systems and will display Fuel/Airdata information on your GPS in selected cases. The Digidata is selectable for single or twin configurations. New and Improved red dot matrix (L.E.D.) display!Size: 3.125” Round x 6.5” Deep

P/N: Description:912802-A Hi-Lo/Freq Input912802-03A DC FF/Analog91280203AG DC FF/Analog/Grey681201-1 OAT Probe/Kit (Sold Separately)

Sandia SAC 7-35Airdata Computer

SANDIA Aero-space has set yet another standard with the SAC 7-35 Airdata Computer for General Aviation. The SAC 7-35 gives you more bang for for your navigation buck Whether you’re upgrading to one of the new generation naviga-tion system or just wanting to get the most out of the system already installed in your aircraft, the SAC 7-35 should be at the top of your system options.

The SAC 7-35 is four systems in one:Altitude Encoder. The SAC 7-35 is FAA TSO 1. Approved as an altitude encoder. It provides standard Gillham Grey code for legacy transponders and RS-232 data for the new generations of transponders.Altitude Alerting. The SAC 7-35 has SANDIA 2. Aerospace’s exclusive AIM (Altitude Inflight Monitoring) that alerts the pilot anytime he deviates more than 100 feet from his selected altitude.Fuel Flow. The addition of a fuel flow trans-3. ducer (two for a twin) and your SAC 7-35 provides all the fuel flow data your navigation systems needs to monitor your fuel situation.Airdata Computer. The SAC 7-35 is a full up 4. TSO’d Airdata Computer offering all of the functions and capabilities of systems costing thousands of dollars more. The SAC 7-35 has multiple interface formats that allow it to provide data to a wide variety of avionics systems.

Designed and manufactured to most exact-ing standards, you can depend on SANDIA Aerospace products to provide years of reliable service. And every product is backed by a three year warranty and personal service support.P/N: 705548-00

Sandia TachGenerator Adapter

The ST 26 is a Tach Generator Adapter that converts the sinusoidal output of Tach Generator to a digital format that can be used by aircraft display and/or control systems.

Physical Characteristics:Width: 5.06”, Depth: 3.35”, Height: .99”Weight: 0.5 lbOperational Characteristics:Operating Voltage: 11-33VdcCurrent: .10 Amps per channel (.40 Amps total all channels)Operating Temp: -55ºC to +70ºCMax Operating Altitude: 55,000 feet


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Order Toll Free1-800-235-3300Fax: 1-800-828-0623

http://www.edmo.com502

Approved Equipment:The ST 26 requires the following input from the on-board Tach Generator.Signal: SinusoidalSignal Frequency Range: 4-100HzSignal Amplitude Range: 4.25-150VPP

Approved Tachometers Include:Globe 22A703AAE 32005-007Electro-Mech EM-8001

The ST 26 Digital Output Signal Is:Pulled up collector to aircraft powerRise time is 15 uS nominal to Aircraft power @ 5VPPFall Time is 10uS nominal @ 5VPPLow Voltage: 0.5VDC, 370 ohmHigh Voltage: Aircraft power through 4.7 K Ohm

Approved Systems Include:Garmin G900X, G1000 Integrated Avionics System

Certification:TSO C49B (Incomplete System) (Pending)DO 160E [(A2)(F2)X]BBB[(S)(B2M)]XXXXXXZZAZ[ZC][RR]M[Z3XXX]XXXX

“The conditions and test required for TSO ap-proval of this article are minimum performance standards. It is the responsibility of those desiring to install the article either on or within a specific type or class of aircraft to demonstrate that the aircraft installation conditions are within the TSO standards. The article may be installed only if installation of the article is approved by the administrator”.P/N: 705662-00

Engine Trend Monitor

Flight data is displayed, recorded and can be reviewed after flight. The removable Datakey™ also lets you download all aircraft and engine information directly to your Computerized Maintenance Management System from your PC. This data provides precise tracking and re-porting of flight time, engine hours, performance variations and exceedences that will allow you to accurately anticipate maintenance and operational problems sooner. Reliable informa-tion, continuously reported from the aircraft, eliminates human error and provides data to substantiate H.S.I. and T.B.O. extensions.P/N: Varies Call EDMO for Information

SYNCHRO TO DIGITAL CONVERTER

Converts angular information received as synchro signals from a fuel flow transmitter into a digital signal suitable of use by a Fuel/Airdata computer and other aviation moni-toring and control systems.

Input signals into the converter, from synchro transmitters, are: X=S1, Y=S3 (S2 is grounded), and reference voltage of 26 Vrms. One unit supports conversion of fuel flow values for two engines.

The design of the unit is based on a built-in microcontroller and unique software, which sup-ports different applicable systems. Rotary micro switch SW1, on the converter, provides switch-ing capabilities to select different fuel flow.P/N: 930502-04

A-429 HS/LS to Serial Converter w/SM Select

Box Size: 3.000”Hx 3.175”L x 3.175”WCompatibility: Any FMS ARINC output to MX-20 moving map or Electronic Flight BagCertification: TSO-C129a Class A1P/N: 933612-02

ADF DC SIN/COS toARINC 429 Converter

Box Size: 1.15”H x 4.30”L x 2.40”WCompatibility: Honeywell KTR-87 ADF Receiver DC Sine/Cosine to ARINC 429 Low Speed (label 162)Certification: TSO-C41dP/N: 933752-00

Synchro Heading Input to A-429 Converter

Magnetic Heading synchro input to ARINC 429 (label 320)P/N: 933753-00

VersatilityIt’s Made Into Shadin.

Fuel Flow Management:Shadin Avionics is a pioneer in the development of fuel flow management systems for general aviation and holds more than 180 airframe and engine installation STCs.

CONVERTER

DIGIFLO-L

Engine Trend Monitoring Systems:

Shadin Avionics gives you the tools you need to maintain and track the performance of fixed-wing and rotorcraft engines to manufacturers’ specifications.

Real benefits of Shadin ETM systems include reduced maintenance costs, ability to take preventive or corrective maintenance action and increased aircraft value with full documentation.

ADC-2000

AMS-2000

ETM

Converters:Shadin converters are world-renowned for reliability, versatility and scope of application. This extensive line allows interface with virtually any manufacturer’s avionicsor aircraft systems.

Air Data Computers:

Look to Shadin for high performance airdata units for all segments of aviation. With applications for general, business, commercial and military aviation, Shadin has a wide range of solutions for any need.

Altitude Management Systems:

Trust Shadin Altitude Management Systems and components for general, business, commercial and military applications.

6831 Oxford Street, St. Louis Park, MN 55426952-927-6500

www.shadin.com


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Fuel Flow Ordering Check ListPLEASE GATHER AND HAVE READY THE FOLLOWING INFORMATION BEFORE ORDERING A SHADIN FUEL FLOW SYSTEM:

Aircraft manufacturer: ❍ Beechcraft ❍ Cessna ❍ Piper

❍ Mooney ❍ Bell

❍ Other: ____________________________________

Model Name & Number: ________________________ Serial Number: _______________

Engine Manufacturer: ❍ Lycoming ❍ Continental ❍ P&W

❍ Wright ❍ Allison

❍ Other: _______________________

Exact Model Number: _________________________________

❍ Single ❍ Twin

❍ Injected ❍ Carburated

Fuel Management System:

❍ Miniflo-L ❍ Microflo-L ❍ Digiflo-L

Fuel Display: ❍ Gallons ❍ Pounds ❍ Liters

Fuel Used: ❍ Avgas ❍ Jet fuel

GPS Input Type, (Make & Model): ____________________________________________

Airdata System:

❍ ADC 200 ❍ ADC 2000 ❍ Digidata

❍ Fuel & Airdata ❍ Airdata Only

Fuel Output: ❍ Gallons ❍ Liters

❍ Pounds (5.8) ❍ Pounds (6.7)

Output To What GPS? __________________________________

What Will The 429 Output Drive?_________________________

Additional Digidata Questions:

Endurance Warning:___________________________________

Total Usable Fuel:_____________________________________

Low Fuel:____________________________________________

Displayed In: ❍ Milibars ❍ HG


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Fax: 1-800-828-0623

http://www.edmo.com

Fuel Flow Management

Digiflo-L

Digiflo-L is a Digital Fuel Management System de-signed to provide complete fuel management informa-tion under real flight condi-tions without any manual entry of data (after entry of the initial fuel on board information). Digiflo-L is connected to the engine fuel flow transducer for fuel flow information and to the Loran-C or GPS receiver serial port for navigation data (ground speed, distance and estimated time en route). This system is also capable of transmitting the fuel information to the Bendix/King KLN-88, KLN-90, and Garmin GPS navigation receiv-ers, for additional calculations and display of fuel management data. Digiflo-L™ is set up to measure the flow of fuel in either gallons, liters, or pounds, and it can be installed on virtually any reciprocating or turbine engine by selecting the proper size fuel flow transducer. Wiring har-nesses & Transducers sold separately.

P/N: Description:910531P Single/Gallons910532P Twin/Gallons910534P Twin/Pounds (5.8)910535P Single/Pounds (6.7l910535TD Single/Pounds (Universal)910536P Twin/Pounds (6.7)910537P Single/Liters910538P Twin/Liters910539P Front/Rear/Gallons91053AP Front/Rear/Liters440501 Digiflo-L Harness (Twin)440502 Digiflo-L Harness (Single)

Miniflo-LMiniflo-L is connected to the engine fuel flow transducer for fuel flow information and to the Loran-C or GPS receiver serial port for naviga-tion data (ground speed, distance and estimat-ed time en route).

This system is also capable of transmitting the fuel information to the Bendix/King KLN-88, KLN-90, and Garmin GPS navigation receivers, for additional calculations and display of fuel management data.P/N: Description:912041TD Single/Gallons912042TD Twin/Gallons912045TD Single/Pounds912046TD Twin/Pounds912047TD Single/LitersIK9121 Kit, Mini-Microflo Digital Connector422110-1 Harness, Miniflo-L422111 Harness, Miniflo Air Tractor422220-1 Harness, Twin/Miniflo(-L)/Microflo(-

L)

Microflo-LMicroflo-L is connected to the engine fuel flow transducer for fuel flow information and to the Loran-C or GPS receiver serial port for naviga-tion data (ground speed, distance and estimat-ed time en route).

This system is also capable of transmitting the fuel information to the Bendix/King KLN-88, KLN-90, and Garmin GPS navigation receivers, except the Garmin 100, for additional calcula-tions and display of fuel management data.P/N: Description:912041T38D Single/Gallons912042T38D Twin/Gallons912045T38D Single/Pounds912046T38D Twin/Pounds912047T38D Single/Liters

Pre-Wired Harnesses For Fuel Flow Systems

EDMO offers pre-wired, high-quality harnesses faturing all shielded wire Both the single and twin engine versions are 20 feet in length.

P/N: Description: Engine:D1 HARNESS Digiflow SingleD2 HARNESS Digiflow TwinM1 HARNESS Mini/Microflow SingleM2 HARNESS Mini/Microflow Twin

Modular AccessoryRemote Card Enclosures

P/N: Model: Modules: Description: 305146-00 SRU 1 Single The single module SRU 1 enclosure will house any of the Enclosure MARC 70 modules305018-00 SRU 5 Five The SRU 5 will house up to 5 MARC 70 modules. Supplied Enclosure with 4 blank plates.305014-00 SRU 10 Ten The SRU 10 houses up to ten MARC 70 Modules. Extra slots Enclosure can be reserved for future use.

SRU 1

SRU 5

SRU 10


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Modular Accessory Remote Cards

MARC 35

The SANDIA aerospace MARC Series of remote accessory cards provide the installer with a wide variety of interface circuits needed to inte-grate today’s avionics systems. Each MARC35 comes housed in a single card enclosure. The MARC70 units can be housed in a SRU 1 single enclosure or can be installed in either the SRU 5 or SRU 10 multi-card enclosures. The SRU 5 will hold up to 5 interface modules while the SRU 10 can hold up to 10 modules. The MARC35 units are all PMA’d and certified to 35 thousand feet. The MARC70 units are PMA’d and certified to 55 thousand feet.

P/N: Pole: Description:AIS80 8 Pole HSI/CDI switching unit for switching between

VOR/ILS and Switching Unit GPS. Switches up to eight lines with ILS override. 14 or 28 VDC. PMA’d.

AIS200-35 20 Pole A 20 pole Nav/GPS Switching card for use with GPS’s that Switching Unit use the HSI/CDI’s OBS function. 28 VDC. PMA’d.

AIS200-3514 20 Pole Same as above except it operates on 14 VDC Switching Unit

AIS240-35 24 Pole A general purpose 24 pole avionics switching Switching Unit unit. Operates on 28 VDC. PMA’d.

MARC 70P/N: Model: Description:305005-01 SA 3 Regulator/Dimming Board. Provides .5 amps

of annunciator drive for lighting display an-nunciator. Will provide 1 amp short term for test purposes. Switchable between bright and dim with both modes field adjustable.

305004-01 SA 15 Inverter Board converts a High to a Low or a Low to a High to provide common annuncia-tor power. 14 inverter outputs

305001-01 SA 24 Diode Isolation Module. Provides 23 lines of diode ground in-ground out isolation. Internal FET allows simultaneous test of all lines to ground. Requires 28 Vdc for test.

305001-01 SR 263 Two, six pole nitrogen filled relays. Can be activated simultaneously or individually.

305000-01 SR 343 Three four pole nitrogen filled relays. Can be activated simultaneously or individually.

305002-01 SR 623 The SR 623 has a total of six, two pole relays in nitrogen filled metal cases.

305003-01 SA24 Diode Isolation Module. Provides 23 lines of diode ground in-ground out isolation. Internal FET allows simultaneous test of all lines to ground. Requires 28 Vdc for test.

Three new switching modules that mount in the MARC70 enclosures provide a lower cost solution to your switching requirements. Each of the following units is certified to 50K feet to meet the needs of the larg-est corporate jet. The switching modules use gold, bifurcated relays to ensure long reliable service. The relay contacts in these modules have a two amp rating.

305501-00 12 Pole The SR34 uses three, four-pole sealed relays to provide Switching Module a total of 12 lines of signal level switching.

305498-00 20 Pole Ideally suited for GPS and Long Range Navigation Systems Switching Module that share an HSI/CDI with a VOR/LOC receiver. The twenty poles of switching with built-in fail safe circuitry ensures that ILS steering is always displayed on the indicator should power be lost or if an ILS frequency is se-lected in the NAV receiver.

305499-00 24 Pole Six, four-pole relays to provide a total of 24 lines of switching. Switching Module This multi-purpose switching unit has its relays ar-ranged in a group of four (16 poles) and two single relays (4 poles each).

SA 15

SA3

SR 263SA 24

SR 623SR 343

305498-00305501-00

305499-00

cobham adahrs (air data attitude heading reference …3. fuel flow. the addition of a fuel flow...

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