AeroElectric-List Digest Archive

Mon 06/02/14


Total Messages Posted: 4



Today's Message Index:
----------------------
 
     1. 02:03 AM - Re: Info on MGL Enigma (Jay Hyde)
     2. 06:45 AM - Re: Info on MGL Enigma (Robert L. Nuckolls, III)
     3. 07:45 AM - Re: Info on MGL Enigma (Robert L. Nuckolls, III)
     4. 10:27 AM - Bonding Straps (stearman456)
 
 
 


Message 1


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    Time: 02:03:54 AM PST US
    From: "Jay Hyde" <jay@horriblehyde.com>
    Subject: Info on MGL Enigma
    Here is the reply from Rainier, the owner and founder of MGL: The CR2032 battery is only used to maintain items that change frequently like calculated fuel levels, local pressure settings etc. Setup is stored in a flash memory section of a secondary processor chip in the EFIS. This does not need a backup battery. If setup data stored here is not maintained there is usually only one cause: The supply voltage to that processor is raised briefly (micro-seconds to mill-seconds) above about 8V. This can happen if the supply to the EFIS contains sharp voltage spikes (typically caused by bad regulators or high voltage ignition is coupling into ground or supply). This can also happen if there are static discharges typically caused by airflow over metal parts that are not grounded. Eventually, this will damage the flash memory which is the part that dies first in our experience. When this happens we replace the processor chip. If you have a techie handy - it is a type ATMEL ATMega128. It is a SMD package but easy to solder/desolder if you have the experience. Once replaced I would also recommend replacing the 16Mhz crystal right next to this chip - it tends to wear out over a long time (we replace these as a matter of course when we get an Enigma in for repairs). No specific programming of the new processor needs to be done as the firmware will detect a new processor and do the programming and setup of this chip automatically (the first start-up will take a bit longer and you will see some messages on the display to this effect). Rainier -- MGL Avionics Postal: Postnet Suite X15 Somerset West 7129 South Africa Physical: 5 Fuchsia street Somerset West 7130 South Africa ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ HH Enterprises * Aircraft assembly, repair, wiring and avionics * Flight instruction * General and Electrical Engineering services (NHD Elec Eng, BTech Elec Eng, GDE ELec Eng) * Great dinner parties and conversation * General adventuring, climbing, kayaking and living Blog: www.rawhyde.wordpress.com <http://www.rawhyde.wordpress.com/> Cel: 083 300 8675 Email: jay@horriblehyde.com ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~ From: owner-aeroelectric-list-server@matronics.com [mailto:owner-aeroelectric-list-server@matronics.com] On Behalf Of Charlie England Sent: 31 May 2014 01:20 AM Subject: Re: AeroElectric-List: Info on MGL Enigma On 5/30/2014 5:25 PM, Richard Girard wrote: While trying to fathom why the CHT readings on the MGL Enigma EFIS had stopped on my friend's Rotax 912 powered JA Highlander I delved into the manual for the EFIS and its RDAC unit (the box that all senders report to before their data is passed along to the EFIS). On page 6 or so of the RDAC manual there is a picture of the back of the Enigma with a note that the battery under a rectangular cover should be changed every two years. Upon removing said cover I discovered a CR2032 lithium battery. I checked its voltage output and found it to be 2.9 volts. A new one that the aircraft owner just happened to have in his tool kit (he maintains medical equipment for a living) put out 3.3 volts so we replaced the old one. More investigation into the setup menus for EFIS revealed that there is an option for a Rotax sender for the CHT setup and when we checked the unit we found it had reset to a J type thermocouple. Resetting it to the Rotax sender solved the problem and the EFIS began reporting good CHT values. Curious to find out if the low output of the CR2032 was responsible for the glitch in the CHT setup I delved into the manual for the EFIS and could find no reference to it in the manual's table of contents, index, or during a long skim of its contents. The same was true of the RADC manual with the exception of the picture and note mentioned earlier. Now we find that the same thing has happened to the oil pressure reading. Again the setup has been changed to reflect a different type of sender, only this time restoring it to the Rotax sender option has not fixed it. There are two sender options for each of resistive type senders and voltage type. On either resistive option (the Rotax option is a resistive sender) the bar graph on the EFIS locks up and does not read. When I set it to either of the voltage type it then reads but it reads backward, i.e. as the engine revs up the reading drops and vice versa. The oil pressure sender is a VDO unit and I have located it in VDO's technical offerings online. VDO recommends that the sender be installed dry with no teflon tape or thread sealant so that it will ground properly so we have an investigative path when we return to the airplane this weekend. MGL has taken the Enigma technical info off line and the aircraft's owner has not been able to find any information on the CR2032 battery as to what it does or how to change it properly. Does anyone out there know about it? Thanks, Rick Girard It isn't necessary to have relatives in Kansas City in order to be unhappy. - Groucho Marx I can't help with specific info on the MGL, but using that battery for 'backup' is fairly common in electronics. If you use a desktop PC, odds are good that there's one on the motherboard. My old Garmin III Pilot gps has one in it. (Note that they make that case style in both a lithium 'primary' battery, and a lithium rechargeable battery, & it's sometimes difficult to tell which the mfgr is using.) In the applications I've seen, the battery keeps a CMOS memory alive, and that's where basic configuration settings are stored in a lot of devices. If the battery goes too low to keep the CMOS memory active, the device will forget whatever settings were stored there. I would think that more current tech, especially in an a/c device, would avoid using CMOS memory & the required battery, but some really high dollar avionics still use it. On many PC's, if the battery dies, after battery replacement you sometimes have to do a 'hard reset' by shorting a pair of pins on the motherboard to completely clear the CMOS memory before re-entering all the parameters needed. Sounds like it's time for a Skype call to S Africa. :-) Charlie


    Message 2


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    Time: 06:45:55 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Info on MGL Enigma
    At 04:02 AM 6/2/2014, you wrote: Here is the reply from Rainier, the owner and founder of MGL: The CR2032 battery is only used to maintain items that change frequently like calculated fuel levels, local pressure settings etc. Setup is stored in a flash memory section of a secondary processor chip in the EFIS. This does not need a backup battery. If setup data stored here is not maintained there is usually only one cause: The supply voltage to that processor is raised briefly (micro-seconds to mill-seconds) above about 8V. This can happen if the supply to the EFIS contains sharp voltage spikes (typically caused by bad regulators or high voltage ignition is coupling into ground or supply). This can also happen if there are static discharges typically caused by airflow over metal parts that are not grounded. Eventually, this will damage the flash memory which is the part that dies first in our experience. When this happens we replace the processor chip. If you have a techie handy - it is a type ATMEL ATMega128. It is a SMD package but easy to solder/desolder if you have the experience. Once replaced I would also recommend replacing the 16Mhz crystal right next to this chip - it tends to wear out over a long time (we replace these as a matter of course when we get an Enigma in for repairs). No specific programming of the new processor needs to be done as the firmware will detect a new processor and do the programming and setup of this chip automatically (the first start-up will take a bit longer and you will see some messages on the display to this effect). I am exceedingly skeptical of these assertions. I don't know of a single 5v regulator offered to the task of conditioning power for electronics that doesn't handily mitigate any of the commonly known variables on the ship's bus. DO-160 offers a clear and concise path to living confidently in the world of DC powered vehicles. Crystals that 'wear out'? Static discharges ? ! ? ! . . . again, for any piece of hardware to be qualified for installation on a TC aircraft, it has to be capable of withstanding discharges of a 150pF capacitor through 330 ohm resistor fed directly to every input/output pin on the device under test. TEN times for positive spikes, TEN more times for negative spikes. Sound brutal . . . but the components and architecture for designing to this level of stress is rudimentary and has been as common to the designer's toolbox as a hammer is to a carpenter's toolbox. I quit doing the test 25 years ago after learning what it took to pass . . . easily . . . every time. If the stresses cited are genuine risks to MGL's products, then they've failed to understand and embrace the real world stresses found in mobile DC powered system of all stripe . . . not the least of which are airplanes. Bob . . .


    Message 3


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    Time: 07:45:47 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Info on MGL Enigma
    At 04:02 AM 6/2/2014, you wrote: Here is the reply from Rainier, the owner and founder of MGL: The CR2032 battery is only used to maintain items that change frequently like calculated fuel levels, local pressure settings etc. Setup is stored in a flash memory section of a secondary processor chip in the EFIS. This does not need a backup battery. If setup data stored here is not maintained there is usually only one cause: The supply voltage to that processor is raised briefly (micro-seconds to mill-seconds) above about 8V. This can happen if the supply to the EFIS contains sharp voltage spikes (typically caused by bad regulators or high voltage ignition is coupling into ground or supply).=C2 This can also happen if there are static discharges typically caused by airflow over metal parts that are not grounded. Eventually, this will damage the flash memory which is the part that dies first in our experience. When this happens we replace the processor chip. If you have a techie handy - it is a type ATMEL ATMega128. It is a SMD package but easy to solder/desolder if you have the experience. Once replaced I would also recommend replacing the 16Mhz crystal right next to this chip - it tends to wear out over a long time (we replace these as a matter of course when we get an Enigma in for repairs). No specific programming of the new processor needs to be done as the firmware will detect a new processor and do the programming and setup of this chip automatically (the first start-up will take a bit longer and you will see some messages on the display to this effect). I am exceedingly skeptical of these assertions. I don't know of a single 5v regulator offered to the task of conditioning power for electronics that doesn't handily mitigate any of the commonly known variables on the ship's bus. DO-160 offers a clear and concise path to living confidently in the world of DC powered vehicles. Crystals that 'wear out'? Static discharges ? ! ? ! . . . again, for any piece of hardware to be qualified for installation on a TC aircraft, it has to be capable of withstanding 15KV discharges of a 150pF capacitor through 330 ohm resistor fed directly to every input/output pin on the device under test. TEN times for positive spikes, TEN more times for negative spikes. Sound brutal . . . but the components and architecture for designing to this level of stress is rudimentary and has been as common to the designer's toolbox as a hammer is to a carpenter's toolbox. I quit doing the test 25 years ago after learning what it took to pass . . . easily . . . every time. If the stresses cited are genuine risks to MGL's products, then they've failed to understand and embrace the real world stresses found in mobile DC powered system of all stripe . . . not the least of which are airplanes. Bob . . .


    Message 4


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    Time: 10:27:51 AM PST US
    Subject: Bonding Straps
    From: "stearman456" <warbirds@shaw.ca>
    In a mixed construction airplane (steel tube fuselage, wooden wings, aluminum structure flight controls, everything fabric covered) what would the down side be in not having everything electrically bonded? My electrical system is a two wire, 14v system with everything running to a "forest of tabs" ground bus on the firewall. The avionics (SL40 com, GTX 327 txdr) run to their own, dedicated ground bus which in turn is wired to the firewall ground bus. I'm doing the bonding per the original design, but I'm just curious. Would all the various assemblies of the airplane create static charges that would cripple the radios? Dan Read this topic online here: http://forums.matronics.com/viewtopic.php?p=424217#424217




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