Re: New EU regulations - civil aviation

2002-09-18 Thread Ken Javor

Thank you for posting what I excerpted below.  At the risk of this thread 
flaring up again, I have to state that just because a cable assembly or loom
does not have an over-braid shield or screen does not qualify it as being
unshielded or unscreened.  The ONLY excuse for an over-braid is
extremely high radiated immunity threats, either swept frequency or time
domain (intentional transmissions or EMP), or lightning protection, either
direct or indirect.  It IS common practice to individually shield signals
which require it, either to contain emissions and/or protect it from
cross-talk or intentional transmissions.  As I pointed out with a numerical
example in an earlier response, an individual shield provides more than
adequate protection to even the smallest signal likely to be carried on such
a wire (usually a twisted, shielded pair) if the function of that signal is
flight critical.

--
From: andrew.p.pr...@baesystems.com
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Tue, Sep 17, 2002, 1:56 AM


By unscreened I mean the cables have no overall screen as used by military
cableforms.

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Re: New EU regulations - civil aviation

2002-09-17 Thread andrew . p . price

We actually tested the equipment with the wiring installation and it took
several months and quite considerable amount of work to get the equipment to
meet DO-160C with the cabling (supplied by Boeing).

No the system is not flight critical however other systems that have been
supplied by our company are and these also use unscreened cable. By
unscreened I mean the cables have no overall screen as used by military
cableforms.

ERA  QinetiQ have tested various PED such as Laptops, CD Walkmans, Portable
DVD players, Video Walkmans, Camcorders, Furbies, etc. Aside from the
Furbies and Laptops the majority rest of the items tested met DO-160C
limits, however, after an incident with a Video walkman which was reported
to open the waste dump valve on a 747 the item was purchased from the owner
by the UKCAA and tested. This was found to be at several frequencies 20-30dB
in excess of limits. Examination of the unit found that it had been modified
at some time. This poses the question what controls are there on PEDS. They
can be tested as new items but their integrity may be compromised when they
are repaired or modified by an unauthorised repairer.

Iam sure that if you get in touch with Eric Stevens of ERA, Dr Nigel Carter
of Qinetiq or Dave Hudson UKCAA they can give you more information.

Regards
Andy

Andrew Price
Principal Development Engineer (EMC Specialist)
BAE SYSTEMS Avionics
A125
Christopher Martin Road
Basildon, Essex
SS14 3EL

tel:   +44 (0) 1268 883308
email: andrew.p.pr...@baesystems.com
 


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RE: New EU regulations - civil aviation

2002-09-17 Thread Cortland Richmond

The navigation systems which are protected by regulation were developments
of the 1940's, and -- except for interference! -- work pretty well.  They
are analog technology, using phase and amplitudes of audio frequency tones
to determine position and/or deviation from course.

For landing, the ILS system transmits amplitude modulated signals between
108 and 112 MHz (if I remember correctly -- it s been a long time) with a
90 Hz modulated beam to one side of the runway, and a 150 Hz modulated beam
on the other. Where the two tones are demodulated at equal strength is
(with a properly aligned and functioning system) along the runway center
line.  The receiver has filters to discriminate between the tones, but
interference can displace the indicated position to one side or the other,
with quite possibly fatal results. The Glide Slope system operates
similarly at around 330 MHz, with beams aligned upwards at an angle such
that equally demodulated tones indicate a correct rate of descent. 

VOR is also an analog system.  VOR operates (if I remember rightly) between
112 and 116 Mhz. Basically, it is a scanning directional array, which
sweeps its azimuthal pattern maximum around 30 times each second.  At the
same time it transmits a subcarrier of (approximately) 10 KHz, which is
frequency modulated with a reference 30 Hz, such that when the beam is
North, the phase of the tones demodulated in an aircraft North of the VOR
station will agree with each other.  The difference in phase between the
received signal modulated as a result of the patterns' rotation, and the
subcarrier's modulation, indicates direction to the aircraft from the VOR
station. 

Again, this is easily interfered with. A substantial area around each VOR
must be restricted for construction, as even multipath from re-radiated
signals will cause the indicated bearing from the station to be off. 

All of these systems have detectors to indicate the absence of a tone, and
a warning flag pops up in its display to show an invalid signal (or none).
However, the flag is only an indicator of total absence of tone. If an
interfering signal presents a tone, the receiver will not distinguish
between it and a valid signal, and the flag will not be displayed.
Consequently, the safety of these systems depends on how well their signals
are received. 



Cortland

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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

I was not arguing that PEDS should be allowed to operate throughout ascent
and descent.  I was responding to Woodgate's comment that if PEDS are
causing a problem, there must be serious immunity issues with aircraft
avionics.  I know in detail what the immunity requirements are, and I know
that PEDS do not emit anywhere near the immunity levels.  PEDS interfere
with radio reception.  Woodgate quite correctly pointed out that unless the
rfi occurred at the radio tuned frequency, it can be considered an antenna
port immunity concern, because immunity requirements can and are levied to
protect radio receiver out-of-band sensitivity.

--
From: Warren Birmingham war...@comfortjets.com
To: Ken Javor ken.ja...@emccompliance.com
Cc: emc-p...@ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 4:01 PM


 Ken, you may be right but it is like trying to convince the FAA that
 there is no harm in using car gas in airplanes.  There are just too
 many ways for uncontrolled fuel to become contaminated from unknown
 sources.

 With respect to the EMC and immunity issues, it is not the technical
 issues that are of concern, but rather the liability and publicity of
 even being accused of causing interference, regardless of how it got
 there.  The potential for it exists, and lives are potentially at
 stake.  Who would argue with this?

 I am also an aviation consultant as well as an engineering one.  Most
 devices are allowed to be used in flight.  Cell Phones and 2-way pagers
 cause too much GROUND interference when used from the air and THAT is
 the primary reason they are not permitted.  They use more resources
 than intended when used from the air.

 By the way, I was consulting to a company that did not even test ANY of
 their equipment to FCC Part 15, and I discovered that they were out of
 specification for Class A by several db.  We had our attorney negotiate
 with the FCC, who wanted to know if ANY of the over-limit frequencies
 fell into the aviation bands.  They did not, so we had to fix the
 problems with no other action required other than submission of new
 compliant verification reports.  There is concern for this even
 originating outside of the aircraft.

 Warren Birmingham
 Epsilon-Mu Consultants
 (510) 793-4806
 email: war...@epsilon-mu.com
 website: http://www.epsilon-mu.com


 On Monday, Sep 16, 2002, at 09:56 US/Pacific, Ken Javor wrote:


 Most of what you say below meshes with my experience and does not
 contradict
 my basic premise, that PEDs can only interfere through aircraft
 antennas.  I
 am curious what the resolution of the Boeing installation was.
 Equipment
 undergoing EMI qualification must be tested with a representative
 flight
 harness.  Did your company test with screened cables and then try to
 force
 Boeing to use the same?  Bad form.  Did Boeing try to buy an
 off-the-shelf
 system qualified with screened cables and then install the system using
 unscreened cables?  Equally bad form.  This must be worked out before
 design
 and testing for procured equipment, and if the equipment is
 off-the-shelf,
 then the qualification configuration harness must be installed, or the
 equipment must be requalified using the planned/existing configuration
 wiring.  Another question of interest: Was the system you provided
 Boeing
 flight critical?

 There is one place that what you say could be interpreted to imply
 that PED
 emissions get into aircraft wiring:

 It has been found through surveys carried out on aircraft by ERA and
 QinetiQ that the interference appears to get into these systems from
 certain
 locations within the aircraft where cable run reside under certain
 seats.

 Consider the physical parameters.  The PED is small and low power and
 while
 it may not meet RTCA/DO-160, it does not blanket the entire aircraft
 with
 emissions.  The intensity falls off rapidly with separation from the
 source.
 This is clearly a case where the emitting device is electrically small
 over
 almost the entire communications band.

 Assume the emitted radiation intensity were 100 mV/m, 5-6 orders of
 magnitude above CISPR limits.  The transfer function of coupled
 current to a
 cable above ground is 1.5 mA per Volt/meter.  I can supply that
 derivation
 if you like, but it is inherent in both RTCA/DO-160D and
 MIL-STD-461D/E.  It
 is different in IEC 61000-4-6, but that is because the ground plane is
 far
 away or nonexistent in buildings and the cable-under-test is a more
 efficient pick-up device in that environment.  Anyway, the coupled
 current
 would be 150 uA, and that assumes at least one half wavelength of the
 cable
 was immersed in a plane wave with precisely the right orientation
 relative
 to the wire in order to get that.  If the victim circuit contains
 information represented by low potentials, such as below 0.1 Volt,
 then I
 would expect the cable carrying that signal to be shielded, as in a
 twisted
 shielded pair.  150 uA riding on a shield

Re: New EU regulations - civil aviation

2002-09-16 Thread Warren Birmingham
 from a 150  
Ohm
source impedance.]  Given the original 100 mV/m assumption, that  
translates

into a coupled common mode potential of 7.5 mV and the conclusion still
stands: no possibility of interference.

--

From: andrew.p.pr...@baesystems.com
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 8:55 AM





Ken

During the mid 90s we manufactured equipment that was installed on  
747s
which was tested to RTCA/DO-160C and all the cables on that aircraft  
for
that system were unscreened. Boeing informed us that they would not  
permit
screened cables due to the increase in weight that would then affect  
the

passenger cargo carrying capability of the aircraft.

I know that  rf signals are coax and that certain control signals are
screened for flight critical systems.

It isn't so bad for newer aircraft but some of the older ones that  
use Omega
and the earlier flight nav systems have reported interfernce with  
these
systems and the autopilot. When the passengers have been requested to  
switch

off their equipments the interference has dissappeared.

It has been found through surveys carried out on aircraft by ERA and  
QinetiQ

that the interfernce appears to get into these systems from certain
locations within the aircraft where cable run reside under certain  
seats.


Incidents of interfernce breakthough on coms have been more difficult  
to

identify. Investigations are still being carried out.

If you want more data suggest you get in touch wuth Dr Nigel Carter @
QinetiQ or Eric Stevens @ ERA.

Regards
Andy

Andrew Price
Principal Development Engineer (EMC Specialist)
BAE SYSTEMS Avionics
A125
Christopher Martin Road
Basildon, Essex
SS14 3EL

tel:   +44 (0) 1268 883308
email: andrew.p.pr...@baesystems.com



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RE: New EU regulations - civil aviation

2002-09-16 Thread Pettit, Ghery

Bob,

A good idea, but we are dealing with some older technology in many cases.
The VOR (VHF Omni-Range) receivers are based on a pair of pulses from the
navigation station.  The station puts out a rotating pulse with a sync pulse
when the rotating pulse is at 0 degrees (magnetic).  Your receiver sees the
sync pulse and then times the delay to the second one.  30 RPS for the
rotation rate.  If an impulsive emission occurs with enough strength your
receiver responds to it and you can lose track of what radial you are on,
giving a spurious indication on the CDI (course deviation indicator).  No
error checking in this analog system.  Updating it would not be practical
given the number of aircraft equipped to use it and the cost of replacing
the equipment.  The airlines might absorb the cost (by charging higher
fares), but your average GA bugsmasher pilot just isn't going to be too hot
on spending several thousand dollars on new equipment.  It's easier to
control PEDs on the plane.

BTW, I'm one of those GA bugsmasher pilots.  I'm not too hot on my club
having to spend the money, either.  We'd have to charge members more for the
use of the planes.  Yuck.  Welcome aboard and please keep your laptop
computer stowed and turned off for the duration of the flight.  Besides,
there are more interesting things to look at out the windows than on that
screen grin.

Ghery Pettit
Intel
Boring holes in the sky and loving every minute of it!


-Original Message-
From: Robert Johnson [mailto:john...@itesafety.com]
Sent: Monday, September 16, 2002 11:58 AM
To: emc-p...@majordomo.ieee.org
Subject: RE: New EU regulations - civil aviation


One thing that surprises me about avionics is the reports of spurious
and misleading readings from instruments due to interference. It seems
in these days of error checking and verification that we should be able
to make instruments which are either confident of the data received or
capable of reporting the reason they cannot display.

Bob Johnson
ITE Safety
 


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RE: New EU regulations - civil aviation

2002-09-16 Thread Robert Johnson
One thing that surprises me about avionics is the reports of spurious
and misleading readings from instruments due to interference. It seems
in these days of error checking and verification that we should be able
to make instruments which are either confident of the data received or
capable of reporting the reason they cannot display.

Bob Johnson
ITE Safety
 

attachment: Robert Johnson.vcf

Re: New EU regulations - civil aviation

2002-09-16 Thread Cortland Richmond

I've been watching this discussion with interest. It appears you are
agreeing with each other - at some length. (grin)  The subject of
interference to airborne navigation and communications receivers seems
never to go away. Since it was the probability of just such interference
which lead the FAA to impose its PED regulations, this is perhaps
appropriate. I have seen emissions from non-ITE PED's (CD players) that
greatly exceeded the FCC class B limit, and it is not unreasonable to
expect interference to receivers from many kinds of device. 

I seem to recall mention in one of the EMC magazines (Conformity?) a couple
of years ago about a GSM telephone *in checked baggage* having been
identified as causing direct EMI to aircraft systems. This, apparently
because GSM amplitude modulation is more conducive to rectified  logic
upset than a steadily emitting frequency-modulation. And of course the hold
is NOT a typical location for customer-carried PED's.

There was also mention further back (this may be on the FAA Web site - a
useful compendium of reports) of a test in which a handy-talky of some type
was, as an experiment, used to transmit inside the cockpit of an airliner,
with noticeable upset to instruments at the flight engineer's station. 
This could be direct interference from a PED, though hardly _likely_ in
flight, especially with today's security restrictions on where passengers
may go. 

I personally recall an incident about 7 years ago in which a product of my
then-employer, a laptop computer, was reported to have caused an aircraft
on a long over-water flight to take a left bank of two degrees, which trim
upset went away when the computer was turned off. However we were unable to
identify emissions which could have caused this. I do not believe that
passenger AC power, MOST likely culprit, was provided at the time, so that
seems to be ruled out, and the energy in the LCD backlight inverter was far
enough away from wiring that it SHOULD not have done so.

Cortland

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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

Most of what you say below meshes with my experience and does not contradict
my basic premise, that PEDs can only interfere through aircraft antennas.  I
am curious what the resolution of the Boeing installation was.  Equipment
undergoing EMI qualification must be tested with a representative flight
harness.  Did your company test with screened cables and then try to force
Boeing to use the same?  Bad form.  Did Boeing try to buy an off-the-shelf
system qualified with screened cables and then install the system using
unscreened cables?  Equally bad form.  This must be worked out before design
and testing for procured equipment, and if the equipment is off-the-shelf,
then the qualification configuration harness must be installed, or the
equipment must be requalified using the planned/existing configuration
wiring.  Another question of interest: Was the system you provided Boeing
flight critical?

There is one place that what you say could be interpreted to imply that PED
emissions get into aircraft wiring:

It has been found through surveys carried out on aircraft by ERA and
QinetiQ that the interference appears to get into these systems from certain
locations within the aircraft where cable run reside under certain seats.

Consider the physical parameters.  The PED is small and low power and while
it may not meet RTCA/DO-160, it does not blanket the entire aircraft with
emissions.  The intensity falls off rapidly with separation from the source.
This is clearly a case where the emitting device is electrically small over
almost the entire communications band.

Assume the emitted radiation intensity were 100 mV/m, 5-6 orders of
magnitude above CISPR limits.  The transfer function of coupled current to a
cable above ground is 1.5 mA per Volt/meter.  I can supply that derivation
if you like, but it is inherent in both RTCA/DO-160D and MIL-STD-461D/E.  It
is different in IEC 61000-4-6, but that is because the ground plane is far
away or nonexistent in buildings and the cable-under-test is a more
efficient pick-up device in that environment.  Anyway, the coupled current
would be 150 uA, and that assumes at least one half wavelength of the cable
was immersed in a plane wave with precisely the right orientation relative
to the wire in order to get that.  If the victim circuit contains
information represented by low potentials, such as below 0.1 Volt, then I
would expect the cable carrying that signal to be shielded, as in a twisted
shielded pair.  150 uA riding on a shield should not cause any problems to
any flight critical signal, even with a pigtailed shield termination.  For
instance, if the pigtail termination yielded a transfer impedance as high as
50 Ohms at some frequency, the resultant common mode coupling to the
interior pair would still only be 7.5 mV.  Again I contend that Boeing and
Airbus would not route a flight critical signal with a threshold of
susceptibility that low.  And if the circuit is totally unshielded, that
implies it is a discrete or other relatively high level signal, where
information is carried in such a away that it takes Volts of induced
potential to cause an upset.  Coupling to an unshielded wire above ground
occurs at a transfer function of 75 mV per Volt/meter. [ Cf. IEC 61000-4-6,
coupling efficiency of 1 Volt per Volt/meter, open circuit from a 150 Ohm
source impedance.]  Given the original 100 mV/m assumption, that translates
into a coupled common mode potential of 7.5 mV and the conclusion still
stands: no possibility of interference.

--
From: andrew.p.pr...@baesystems.com
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 8:55 AM



 Ken

 During the mid 90s we manufactured equipment that was installed on 747s
 which was tested to RTCA/DO-160C and all the cables on that aircraft for
 that system were unscreened. Boeing informed us that they would not permit
 screened cables due to the increase in weight that would then affect the
 passenger cargo carrying capability of the aircraft.

 I know that  rf signals are coax and that certain control signals are
 screened for flight critical systems.

 It isn't so bad for newer aircraft but some of the older ones that use Omega
 and the earlier flight nav systems have reported interfernce with these
 systems and the autopilot. When the passengers have been requested to switch
 off their equipments the interference has dissappeared.

 It has been found through surveys carried out on aircraft by ERA and QinetiQ
 that the interfernce appears to get into these systems from certain
 locations within the aircraft where cable run reside under certain seats.

 Incidents of interfernce breakthough on coms have been more difficult to
 identify. Investigations are still being carried out.

 If you want more data suggest you get in touch wuth Dr Nigel Carter @
 QinetiQ or Eric Stevens @ ERA.

 Regards
 Andy

 Andrew Price
 Principal Development Engineer (EMC Specialist)
 BAE

Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

Very good point.  Obviously the cables could be very long, at least as long
as half the aircraft, if the 12 Vdc supply were situated in the exact center
of the aircraft.  Since the laptops were qualified running of a 50/60 Hz
power mains, the measured CSIPR emissions don't apply to this mode.  Would
it be too much to expect that the adapters for sale for this purpose do meet
stringent RE limits?  Or do they fall in a a regulation crack - CISPR
wouldn't apply and somehow I don't see these devices being qualified to
RTCA/DO-160.

But while all of this is interesting and food for thought, it STILL doesn't
affect my basic premise, that PEDs interfere with aircraft operation via
aircraft antennas, not aircraft wires.

--
From: John Woodgate j...@jmwa.demon.co.uk
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 1:15 AM



 I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
 (in 0h2i001lcfw...@mtaout04.icomcast.net) about 'New EU regulations -
 civil aviation' on Sun, 15 Sep 2002:
My response is that conducted path is so lossy as to be negligible.

 But how long are the cables? I think we have more or less agreed that it
 is *radiation* from consumer devices interfering with aircraft radio
 reception where the potential problem arises. Hence the threat with the
 12 V supplies is *radiation from the cables*, due to conducted emissions
 form the consumer device.
 --
 Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk
 Interested in professional sound reinforcement and distribution? Then go to
 http://www.isce.org.uk
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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

Actually the mil-std appendix does exactly what you suggest; the following
is excerpted from the discussion for RE102, which controls radiated electric
field emissions:

The basic intent of the requirement is to protect sensitive receivers from
interference coupled through the antennas associated with the receiver.
Many tuned receivers have sensitivities on the order of one microvolt and
are connected to an intentional aperture (the antenna) which are constructed
for efficient reception of energy in the operating range of the receiver.
The potential for degradation requires relatively stringent requirements to
prevent platform problems.

There is no implied relationship between this requirement and RS103 that
addresses radiated susceptibility to electric fields.  Attempts have been
made quite frequently in the past to compare electric field radiated
emission and susceptibility type requirements as a justification for
deviations and waivers.  While RE102 is concerned with potential effects
with antenna-connected receivers, RS103 simulates fields resulting from
antenna-connected transmitters.


--
From: John Woodgate j...@jmwa.demon.co.uk
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 1:17 AM



 I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
 (in 0h2i002t0im...@mtaout03.icomcast.net) about 'New EU regulations -
 civil aviation' on Sun, 15 Sep 2002:

Another way to say this is to paraphrase the appendix of MIL-STD-461D/E,
which states categorically that there is no relationship between radiated
emissions and radiates susceptibility requirements, they are for different
purposes and the magnitudes between the respective limits are not to be
considered a design margin.

 That is true, but it would be more helpful if it went on to explain what
 the 'different purposes' are.
 --
 Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk
 Interested in professional sound reinforcement and distribution? Then go to
 http://www.isce.org.uk
 PLEASE do NOT copy news posts to me by E-MAIL!

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RE: New EU regulations - civil aviation

2002-09-16 Thread Price, Ed

This discussion is touching on several aspects of Personal Electronic
Devices (PED's) aboard aircraft. Bruce Donham, of Boeing, has a two-year-old
paper with some hard data at:

http://www.boeing.com/commercial/aeromagazine/aero_10/interfere_story.html

Also, here's a cross reference to PED Electronic regulations:

http://aviation-safety.net/events/ped/ped-regl.htm

And, 106 pages of Aviation Safety Reporting System PED related history,
current to May 2002, at:

http://asrs.arc.nasa.gov/report_sets/ped.pdf


This whole subject is about as confusing as EMF's and cancer.


Regards,

Ed


Ed Price
ed.pr...@cubic.com
Electromagnetic Compatibility Lab
Cubic Defense Systems
San Diego, CA  USA
858-505-2780  (Voice)
858-505-1583  (Fax)
Military  Avionics EMC Is Our Specialty
Shake-Bake-Shock - Metrology - Reliability Analysis


-Original Message-
From: Ken Javor [mailto:ken.ja...@emccompliance.com]
Sent: Monday, September 16, 2002 6:33 AM
To: andrew.p.pr...@baesystems.com; emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation



I do realize there is a big difference in the use of cable 
shielding/screening between general and commercial aviation practices.
However the same general aviation aircraft that get by with 
little or no
cable shielding/screening also have no electronic critical 
flight controls,
so it is a wash.  Any aircraft with flight controls qualified to
RTCA/DO-160A will also have its maximum degree of automation limited to
using the autopilot, possibly in conjunction with navigation 
inputs from
aircraft NAV receivers.  Both the rf (coax) and the base-band 
signal inputs
into the autopilot would be shielded in my experience.  I 
would definitely
NOT expect personal electronics to interfere with such control systems
(except for that all-important radio link).

I would also expect that as an older aircraft gets avionics 
upgrades, with
avionics qualified to RTA/DO-160D, that the cables connecting 
to the new
avionics must be upgraded if the certification is to maintain validity.
Specifically, if a new avionics upgrade were form, fit and function
compatible with the old part, but required a shielded harness to meet
RTCA/DO-160D, then that cable would have to be retrofitted 
along with the
equipment.  Am I being overly idealistic and out of touch here?

In any case I reiterate: basic systems engineering practices 
mandate that a
(non-rf)  signal that carries flight critical information 
should be piped
through the aircraft such that neither cross-talk nor stray 
emissions from
other electronics cause interference.

Along these lines, there are those who mourn the passing of 
the old term,
rfi, because the term evoked the concept of RADIO 
interference, rather than
the general term electromagnetic interference, which is global in its
meaning.  We need to consciously retain the idea that stray 
(unintentional)
rf emissions from non-antenna connected electronics have the 
potential to
create only rfi.
--
From: andrew.p.pr...@baesystems.com
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 1:57 AM



 Firstly all avionic equipment is qualified to RTCA/DO-160 (European
 equivalent EUROCAE ED-14).
 All new equipment is test to DO-160D however there is still equipment
 installed on aircraft that was originally tested to DO-160A.
 Overtime the DO-160 has become more stringent with tighter 
emission levels
 and high immunity test levels which includes HIRF testing.

 There is one problem that arises from this as most of the 
cabling installed
 on the aircraft is unscreened. This is for weight saving reasons.

 Therefore with alot of older aircraft having a mixture of new and old
 equipments installed using cabling that is unscreened it is 
reasonable to
 assume that some Passenger Portable devices such as Gameboys, Laptop
 Computors, Mobile Phones, etc. will if that passenger 
happens to be sitting
 above a cable run cause interference with one or more 
aircraft systems. The
 UKCAA keeps a log of all reported incidents.

 Regards
 Andy


 Andrew Price
 Principal Development Engineer (EMC Specialist)
 BAE SYSTEMS Avionics
 A125
 Christopher Martin Road
 Basildon, Essex
 SS14 3EL

 tel:   +44 (0) 1268 883308
 email: andrew.p.pr...@baesystems.com


---
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Re: New EU regulations - civil aviation

2002-09-16 Thread andrew . p . price

Ken

During the mid 90s we manufactured equipment that was installed on 747s
which was tested to RTCA/DO-160C and all the cables on that aircraft for
that system were unscreened. Boeing informed us that they would not permit
screened cables due to the increase in weight that would then affect the
passenger cargo carrying capability of the aircraft.

I know that  rf signals are coax and that certain control signals are
screened for flight critical systems.

It isn't so bad for newer aircraft but some of the older ones that use Omega
and the earlier flight nav systems have reported interfernce with these
systems and the autopilot. When the passengers have been requested to switch
off their equipments the interference has dissappeared.

It has been found through surveys carried out on aircraft by ERA and QinetiQ
that the interfernce appears to get into these systems from certain
locations within the aircraft where cable run reside under certain seats.

Incidents of interfernce breakthough on coms have been more difficult to
identify. Investigations are still being carried out.

If you want more data suggest you get in touch wuth Dr Nigel Carter @
QinetiQ or Eric Stevens @ ERA.

Regards
Andy

Andrew Price
Principal Development Engineer (EMC Specialist)
BAE SYSTEMS Avionics
A125
Christopher Martin Road
Basildon, Essex
SS14 3EL

tel:   +44 (0) 1268 883308
email: andrew.p.pr...@baesystems.com
 


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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

I do realize there is a big difference in the use of cable 
shielding/screening between general and commercial aviation practices.
However the same general aviation aircraft that get by with little or no
cable shielding/screening also have no electronic critical flight controls,
so it is a wash.  Any aircraft with flight controls qualified to
RTCA/DO-160A will also have its maximum degree of automation limited to
using the autopilot, possibly in conjunction with navigation inputs from
aircraft NAV receivers.  Both the rf (coax) and the base-band signal inputs
into the autopilot would be shielded in my experience.  I would definitely
NOT expect personal electronics to interfere with such control systems
(except for that all-important radio link).

I would also expect that as an older aircraft gets avionics upgrades, with
avionics qualified to RTA/DO-160D, that the cables connecting to the new
avionics must be upgraded if the certification is to maintain validity.
Specifically, if a new avionics upgrade were form, fit and function
compatible with the old part, but required a shielded harness to meet
RTCA/DO-160D, then that cable would have to be retrofitted along with the
equipment.  Am I being overly idealistic and out of touch here?

In any case I reiterate: basic systems engineering practices mandate that a
(non-rf)  signal that carries flight critical information should be piped
through the aircraft such that neither cross-talk nor stray emissions from
other electronics cause interference.

Along these lines, there are those who mourn the passing of the old term,
rfi, because the term evoked the concept of RADIO interference, rather than
the general term electromagnetic interference, which is global in its
meaning.  We need to consciously retain the idea that stray (unintentional)
rf emissions from non-antenna connected electronics have the potential to
create only rfi.
--
From: andrew.p.pr...@baesystems.com
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Mon, Sep 16, 2002, 1:57 AM



 Firstly all avionic equipment is qualified to RTCA/DO-160 (European
 equivalent EUROCAE ED-14).
 All new equipment is test to DO-160D however there is still equipment
 installed on aircraft that was originally tested to DO-160A.
 Overtime the DO-160 has become more stringent with tighter emission levels
 and high immunity test levels which includes HIRF testing.

 There is one problem that arises from this as most of the cabling installed
 on the aircraft is unscreened. This is for weight saving reasons.

 Therefore with alot of older aircraft having a mixture of new and old
 equipments installed using cabling that is unscreened it is reasonable to
 assume that some Passenger Portable devices such as Gameboys, Laptop
 Computors, Mobile Phones, etc. will if that passenger happens to be sitting
 above a cable run cause interference with one or more aircraft systems. The
 UKCAA keeps a log of all reported incidents.

 Regards
 Andy


 Andrew Price
 Principal Development Engineer (EMC Specialist)
 BAE SYSTEMS Avionics
 A125
 Christopher Martin Road
 Basildon, Essex
 SS14 3EL

 tel:   +44 (0) 1268 883308
 email: andrew.p.pr...@baesystems.com



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Re: New EU regulations - civil aviation

2002-09-16 Thread andrew . p . price

Firstly all avionic equipment is qualified to RTCA/DO-160 (European
equivalent EUROCAE ED-14).
All new equipment is test to DO-160D however there is still equipment
installed on aircraft that was originally tested to DO-160A.
Overtime the DO-160 has become more stringent with tighter emission levels
and high immunity test levels which includes HIRF testing.

There is one problem that arises from this as most of the cabling installed
on the aircraft is unscreened. This is for weight saving reasons.

Therefore with alot of older aircraft having a mixture of new and old
equipments installed using cabling that is unscreened it is reasonable to
assume that some Passenger Portable devices such as Gameboys, Laptop
Computors, Mobile Phones, etc. will if that passenger happens to be sitting
above a cable run cause interference with one or more aircraft systems. The
UKCAA keeps a log of all reported incidents.

Regards
Andy


Andrew Price
Principal Development Engineer (EMC Specialist)
BAE SYSTEMS Avionics
A125
Christopher Martin Road
Basildon, Essex
SS14 3EL

tel:   +44 (0) 1268 883308
email: andrew.p.pr...@baesystems.com
 


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Re: New EU regulations - civil aviation

2002-09-16 Thread John Woodgate

I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
(in 0h2i002t0im...@mtaout03.icomcast.net) about 'New EU regulations -
civil aviation' on Sun, 15 Sep 2002:

Another way to say this is to paraphrase the appendix of MIL-STD-461D/E,
which states categorically that there is no relationship between radiated
emissions and radiates susceptibility requirements, they are for different
purposes and the magnitudes between the respective limits are not to be
considered a design margin.

That is true, but it would be more helpful if it went on to explain what
the 'different purposes' are. 
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
PLEASE do NOT copy news posts to me by E-MAIL!

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Re: New EU regulations - civil aviation

2002-09-16 Thread John Woodgate

I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
(in 0h2i001lcfw...@mtaout04.icomcast.net) about 'New EU regulations -
civil aviation' on Sun, 15 Sep 2002:
My response is that conducted path is so lossy as to be negligible.  

But how long are the cables? I think we have more or less agreed that it
is *radiation* from consumer devices interfering with aircraft radio
reception where the potential problem arises. Hence the threat with the
12 V supplies is *radiation from the cables*, due to conducted emissions
form the consumer device.
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
PLEASE do NOT copy news posts to me by E-MAIL!

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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

I agree that we agree.  The reason I responded in so much depth on this 
thread is that I consider the underlying issue behind the terminology very
important, and I was dismayed during an earlier similar thread at some of
the responses posted on this forum.  The issue I am referring to is that RE
are controlled to protect radio receivers, and not electronics in general.
Another way to say this is to paraphrase the appendix of MIL-STD-461D/E,
which states categorically that there is no relationship between radiated
emissions and radiates susceptibility requirements, they are for different
purposes and the magnitudes between the respective limits are not to be
considered a design margin.

--
From: John Woodgate j...@jmwa.demon.co.uk
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Sun, Sep 15, 2002, 2:29 PM



 I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
 (in 0h2h0068wpv...@mtaout06.icomcast.net) about 'New EU regulations -
 civil aviation' on Sun, 15 Sep 2002:

We are getting off subject, in that the CISPR requirements listed below
don't apply to avionics, only to the personal electronics people carry on
board.

 I thought we were discussing your very restricted 'definition' of
 immunity.

 However, I don't think we really disagree very much on the actual
 issues, just a bit on the terminology.
 --
 Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk
 Interested in professional sound reinforcement and distribution? Then go to
 http://www.isce.org.uk
 PLEASE do NOT copy news posts to me by E-MAIL!

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Re: New EU regulations - civil aviation

2002-09-16 Thread Ken Javor

My response is that conducted path is so lossy as to be negligible.  
Consider that the 12 Vdc is developed by conversion from either aircraft 28
Vdc, or 400 cycles.  In either case, that converter or power supply must
meet the conducted emissions requirements of RTCA/DO-160, or its European
equivalent.  The 12 Vdc loads do not interface directly with aircraft power.
Further, aircraft avionics, including radios, must meet stringent conducted
susceptibility/immunity requirements on input power ports.  Although I am
not familiar with the European equivalent, I am sure it is the same way,
because it was a British influence that placed similar requirements in
RTCA/DO-160 and MIL-STD-461.  I refer here mainly to Dr. Nigel Carter of the
UK.  These conducted susceptibility/immunity requirements simulate the
effect of powerful radio transmissions coupling to the aircraft power bus,
and are at levels orders of magnitude above the CE limits placed on aircraft
avionics.  I would say that it is a highly unlikely path for influencing
aircraft avionics, although I would also say that if I, as an EMC engineer
working for a major air-framer, were procuring a 12 Vdc supply for this use,
I would push to characterize its input/output isolation from 0.15 - 400 MHz,
for the sake of completeness.  By input/output in this case I mean injecting
a signal on the 12 Vdc output, and measuring the resultant signal on the
aircraft power side.  And I would measure this both differential and common
mode, as I would expect different performance for different modes.  But that
would be strictly a CYA file, not a hard requirement.

--
From: Warren Birmingham war...@comfortjets.com
To: Ken Javor ken.ja...@emccompliance.com, emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Sun, Sep 15, 2002, 3:41 PM


 This is not so.  Many aircraft now have personal 12v ports under each
 seat for personal electronic devices.

 Warren Birmingham
 Epsilon-Mu Consultants
 (510) 793-4806
 email: war...@epsilon-mu.com
 website: http://www.epsilon-mu.com


 On Sunday, Sep 15, 2002, at 10:28 US/Pacific, Ken Javor wrote:

 The point is that personal electronics carried on board an aircraft
 interact
 with the aircraft ONLY via the radiated emissions route.
 

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Re: New EU regulations - civil aviation

2002-09-15 Thread Warren Birmingham


This is not so.  Many aircraft now have personal 12v ports under each 
seat for personal electronic devices.


Warren Birmingham
Epsilon-Mu Consultants
(510) 793-4806
email: war...@epsilon-mu.com
website: http://www.epsilon-mu.com


On Sunday, Sep 15, 2002, at 10:28 US/Pacific, Ken Javor wrote:

The point is that personal electronics carried on board an aircraft 
interact

with the aircraft ONLY via the radiated emissions route.



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Re: New EU regulations - civil aviation

2002-09-15 Thread John Woodgate

I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
(in 0h2h0068wpv...@mtaout06.icomcast.net) about 'New EU regulations -
civil aviation' on Sun, 15 Sep 2002:

We are getting off subject, in that the CISPR requirements listed below 
don't apply to avionics, only to the personal electronics people carry on
board.  

I thought we were discussing your very restricted 'definition' of
immunity.

However, I don't think we really disagree very much on the actual
issues, just a bit on the terminology.
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
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Re: New EU regulations - civil aviation

2002-09-15 Thread Ken Javor

We are getting off subject, in that the CISPR requirements listed below 
don't apply to avionics, only to the personal electronics people carry on
board.  However, the real issue is not unique to CISPR, or DoD, or
RTCA/DO-160 or the European equivalent.  It has to do with how you control
undesired electromagnetic interactions.  I have a slide which describes this
graphically, which I can send directly to anyone interested, but in keeping
with forum rules, I am not broadcasting an attachment.

What the side does show is that radiated emissions requirements control
interference to antenna-connected radio receivers.  Radiated immunity
requirements impose minimum operational requirements on ordinary (non-radio)
electronics when in close proximity to an intentional rf transmission.

The point is that personal electronics carried on board an aircraft interact
with the aircraft ONLY via the radiated emissions route.  Mr.  Woodgate is
certainly correct that if antenna port immunity requirements are not
adequately administered, then aircraft functions relying on radio reception
are unnecessarily endangered.  I am familiar with US DoD requirements levied
on antenna ports.  Perhaps someone else on the forum can speak to similar
but non-DoD requirements.
--
From: John Woodgate j...@jmwa.demon.co.uk
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Sat, Sep 14, 2002, 11:53 PM



 I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
 (in 0h2g00dsl78...@mtaout02.icomcast.net) about 'New EU regulations -
 civil aviation' on Sat, 14 Sep 2002:

Immunity in the sense used in the EMI world excludes the mechanism by which
an unintentional emission causes rfi.

 The whole object of most CISPR standards is to prevent unintentional
 emissions causing RFI. While most of them deal only with the limitation
 of emissions, CISPR 14-2, 20 and 24 include immunity requirements. In
 the case of CISPR 20, the immunity requirements apply to receivers.

 What IS excluded from 'immunity' is on-channel interference with
 receivers, since the effects of this depend very greatly on things such
 as the type of modulation used for the wanted signals.
 --
 Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk
 Interested in professional sound reinforcement and distribution? Then go to
 http://www.isce.org.uk
 PLEASE do NOT copy news posts to me by E-MAIL!

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Re: New EU regulations - civil aviation

2002-09-15 Thread John Woodgate

I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
(in 0h2g00dsl78...@mtaout02.icomcast.net) about 'New EU regulations -
civil aviation' on Sat, 14 Sep 2002:

Immunity in the sense used in the EMI world excludes the mechanism by which
an unintentional emission causes rfi.  

The whole object of most CISPR standards is to prevent unintentional
emissions causing RFI. While most of them deal only with the limitation
of emissions, CISPR 14-2, 20 and 24 include immunity requirements. In
the case of CISPR 20, the immunity requirements apply to receivers.

What IS excluded from 'immunity' is on-channel interference with
receivers, since the effects of this depend very greatly on things such
as the type of modulation used for the wanted signals.
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
PLEASE do NOT copy news posts to me by E-MAIL!

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Re: New EU regulations - civil aviation

2002-09-14 Thread Ken Javor

See my response to Messrs. Hopkins and Birmingham.  I flagged this very 
issue.  The US DoD has extensive requirements on receiver out-of-band
sensitivity, but there are none in the US commercial equivalent to
MIL-STD-461, RTCA/DO-160, Sections 16-21.  There may well be requirements
elsewhere, I don't know, but I expect someone on this forum would know.
Anyone on this forum from Collins Radio?

--
From: John Woodgate j...@jmwa.demon.co.uk
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Sat, Sep 14, 2002, 2:19 PM



 I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
 (in 0h2f00ctawl...@mtaout03.icomcast.net) about 'New EU regulations -
 civil aviation' on Sat, 14 Sep 2002:

To the best of my knowledge, personal electronics interacts with aircraft
operation by interfering with radio navigation receivers.  That is not an
immunity concern.

 But it IS an immunity concern. Unless it is claimed that all these
 devices coincidentally interfere with reception by emitting on-channel.
 Some receivers have, AIUI, very limited immunity to off-channel
 emissions.
 --
 Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk
 Interested in professional sound reinforcement and distribution? Then go to
 http://www.isce.org.uk
 PLEASE do NOT copy news posts to me by E-MAIL!

 ---
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 Technical Committee emc-pstc discussion list.

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Re: New EU regulations - civil aviation

2002-09-14 Thread Ken Javor

Mr. Hopkins did NOT disagree with me at all on a technical basis, but he did
misunderstand the meaning of immunity in an EMI frame of reference, and so
did the other gentleman, Mr. Birmingham.

In general, EMI requirements are divided into emissions and immunity, and
these are further subdivided each into conducted and radiated, thus
generating the familiar CE, RE, CI, and RI requirements and test methods.

CE requirements protect radio receivers from interference on their input
power leads.

RE requirements protect radios from interference coupling into their
antennas.

CI (swept frequency) and RI requirements protect non-antenna-connected
electronics from the effects of intentionally transmitting radio antennas in
their immediate vicinity.

Immunity in the sense used in the EMI world excludes the mechanism by which
an unintentional emission causes rfi.  That eventuality must be controlled
by levying RE limits.  If this is unclear to anyone, I will expand upon it
but I think it is an obvious point (with one important exception -
requirements on receiver out-of-band responses).

The final issue that Mr. Hopkins raises about non-rf signal wires being
upset by stray emissions from personal electronics is the one I labeled
impossible or a case of extremely poor systems engineering.  Coupling to
wires from RE even orders of magnitude above RE limits couples sub-millivolt
levels to wiring, not to mention that any sensitive wires are shielded.  I
have worked in aerospace for over twenty years (not continuous) and have
never seen a flight critical system depend on microvolt-level signal
reception - except at an antenna terminal.

--
From: Michael Hopkins michael.hopk...@thermo.com
To: Ken Javor ken.ja...@emccompliance.com, John Woodgate
j...@jmwa.demon.co.uk, emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Sat, Sep 14, 2002, 3:29 PM


 I disagree -- it certainly IS an immunity concern.

 First of all, radio navigation receivers ARE flight-critical avionics since
 they are directly coupled to aircraft controls. Most commercial airliners
 are flown a large part of the time on auto-pilot, which gets its input
 directly from the nav receivers (and now frequently GPS receivers).

 One might argue that it isn't dangerous if the airplane just goes in a
 different direction -- unless of course there is another airplane scheduled
 to be in that airspace -- but landings also are frequently automated via the
 use of ILS receivers which in turn control glideslope -- descent rates,
 engine speed, direction, etc

 As a pilot, I can tell you that a lap top computer, scanners, AM/FM
 receivers can all cause nav and comm receivers to be upset.

 Also, keep in mind autopilot controls are simply electronic boxes connected
 by lots of wires -- these may not be antennas, but I would hope someone is
 concerned about the immunity of this system to rf  -- hate to be on a low
 (zero) visibility approach and has someones laptop suddenly emit the signal
 that upsets any electronics in any way

 My opinion.

 Michael Hopkins
 michael.hopk...@thermo.com




 - Original Message -
 From: Ken Javor ken.ja...@emccompliance.com
 To: John Woodgate j...@jmwa.demon.co.uk; emc-p...@majordomo.ieee.org
 Sent: Saturday, September 14, 2002 1:58 PM
 Subject: Re: New EU regulations - civil aviation



 To the best of my knowledge, personal electronics interacts with aircraft
 operation by interfering with radio navigation receivers.  That is not an
 immunity concern.  Does any one on this forum know of a proven case of
 personal electronics interfering with non-antenna-connected
 flight-critical
 avionics?  I don't, and further I would say it was either impossible, or
 the
 result of extremely poor systems engineering.

 --
 From: John Woodgate j...@jmwa.demon.co.uk
 To: emc-p...@majordomo.ieee.org
 Subject: Re: New EU regulations - civil aviation
 Date: Sat, Sep 14, 2002, 1:50 AM
 

 
  I read in !emc-pstc that Raymond Garner raymond.gar...@casa.eads.net
  wrote (in sr-511...@ieeepstc.mindcruiser.com) about 'New EU
  regulations - civil aviation' on Wed, 11 Sep 2002:
 
 Equipments/systems/aircraft are designed, tested and certified way
 beyond the
 current EMC legislation
 
  They why all the hysteria about passengers' low-power portable equipment
  causing disastrous interference with the aircraft systems? My impression
  is that there is something seriously lacking in the immunity
  requirements for some aircraft systems.
  --
  Regards, John Woodgate, OOO - Own Opinions Only.
 http://www.jmwa.demon.co.uk
  Interested in professional sound reinforcement and distribution? Then go
 to
  http://www.isce.org.uk
  PLEASE do NOT copy news posts to me by E-MAIL!
 
  ---
  This message is from the IEEE EMC Society Product Safety
  Technical Committee emc-pstc discussion list.
 
  Visit our web site at:  http://www.ewh.ieee.org/soc/emcs/pstc

Re: New EU regulations - civil aviation

2002-09-14 Thread Michael Hopkins

I disagree -- it certainly IS an immunity concern.

First of all, radio navigation receivers ARE flight-critical avionics since
they are directly coupled to aircraft controls. Most commercial airliners
are flown a large part of the time on auto-pilot, which gets its input
directly from the nav receivers (and now frequently GPS receivers).

One might argue that it isn't dangerous if the airplane just goes in a
different direction -- unless of course there is another airplane scheduled
to be in that airspace -- but landings also are frequently automated via the
use of ILS receivers which in turn control glideslope -- descent rates,
engine speed, direction, etc

As a pilot, I can tell you that a lap top computer, scanners, AM/FM
receivers can all cause nav and comm receivers to be upset.

Also, keep in mind autopilot controls are simply electronic boxes connected
by lots of wires -- these may not be antennas, but I would hope someone is
concerned about the immunity of this system to rf  -- hate to be on a low
(zero) visibility approach and has someones laptop suddenly emit the signal
that upsets any electronics in any way

My opinion.

Michael Hopkins
michael.hopk...@thermo.com




- Original Message -
From: Ken Javor ken.ja...@emccompliance.com
To: John Woodgate j...@jmwa.demon.co.uk; emc-p...@majordomo.ieee.org
Sent: Saturday, September 14, 2002 1:58 PM
Subject: Re: New EU regulations - civil aviation



 To the best of my knowledge, personal electronics interacts with aircraft
 operation by interfering with radio navigation receivers.  That is not an
 immunity concern.  Does any one on this forum know of a proven case of
 personal electronics interfering with non-antenna-connected
flight-critical
 avionics?  I don't, and further I would say it was either impossible, or
the
 result of extremely poor systems engineering.

 --
 From: John Woodgate j...@jmwa.demon.co.uk
 To: emc-p...@majordomo.ieee.org
 Subject: Re: New EU regulations - civil aviation
 Date: Sat, Sep 14, 2002, 1:50 AM
 

 
  I read in !emc-pstc that Raymond Garner raymond.gar...@casa.eads.net
  wrote (in sr-511...@ieeepstc.mindcruiser.com) about 'New EU
  regulations - civil aviation' on Wed, 11 Sep 2002:
 
 Equipments/systems/aircraft are designed, tested and certified way
beyond the
 current EMC legislation
 
  They why all the hysteria about passengers' low-power portable equipment
  causing disastrous interference with the aircraft systems? My impression
  is that there is something seriously lacking in the immunity
  requirements for some aircraft systems.
  --
  Regards, John Woodgate, OOO - Own Opinions Only.
http://www.jmwa.demon.co.uk
  Interested in professional sound reinforcement and distribution? Then go
to
  http://www.isce.org.uk
  PLEASE do NOT copy news posts to me by E-MAIL!
 
  ---
  This message is from the IEEE EMC Society Product Safety
  Technical Committee emc-pstc discussion list.
 
  Visit our web site at:  http://www.ewh.ieee.org/soc/emcs/pstc/
 
  To cancel your subscription, send mail to:
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Re: New EU regulations - civil aviation

2002-09-14 Thread John Woodgate

I read in !emc-pstc that Ken Javor ken.ja...@emccompliance.com wrote
(in 0h2f00ctawl...@mtaout03.icomcast.net) about 'New EU regulations -
civil aviation' on Sat, 14 Sep 2002:

To the best of my knowledge, personal electronics interacts with aircraft 
operation by interfering with radio navigation receivers.  That is not an
immunity concern. 

But it IS an immunity concern. Unless it is claimed that all these
devices coincidentally interfere with reception by emitting on-channel.
Some receivers have, AIUI, very limited immunity to off-channel
emissions.
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
PLEASE do NOT copy news posts to me by E-MAIL!

---
This message is from the IEEE EMC Society Product Safety
Technical Committee emc-pstc discussion list.

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Re: New EU regulations - civil aviation

2002-09-14 Thread Ken Javor

To the best of my knowledge, personal electronics interacts with aircraft 
operation by interfering with radio navigation receivers.  That is not an
immunity concern.  Does any one on this forum know of a proven case of
personal electronics interfering with non-antenna-connected flight-critical
avionics?  I don't, and further I would say it was either impossible, or the
result of extremely poor systems engineering.

--
From: John Woodgate j...@jmwa.demon.co.uk
To: emc-p...@majordomo.ieee.org
Subject: Re: New EU regulations - civil aviation
Date: Sat, Sep 14, 2002, 1:50 AM



 I read in !emc-pstc that Raymond Garner raymond.gar...@casa.eads.net
 wrote (in sr-511...@ieeepstc.mindcruiser.com) about 'New EU
 regulations - civil aviation' on Wed, 11 Sep 2002:

Equipments/systems/aircraft are designed, tested and certified way beyond the
current EMC legislation

 They why all the hysteria about passengers' low-power portable equipment
 causing disastrous interference with the aircraft systems? My impression
 is that there is something seriously lacking in the immunity
 requirements for some aircraft systems.
 --
 Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk
 Interested in professional sound reinforcement and distribution? Then go to
 http://www.isce.org.uk
 PLEASE do NOT copy news posts to me by E-MAIL!

 ---
 This message is from the IEEE EMC Society Product Safety
 Technical Committee emc-pstc discussion list.

 Visit our web site at:  http://www.ewh.ieee.org/soc/emcs/pstc/

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Re: New EU regulations - civil aviation

2002-09-14 Thread John Woodgate

I read in !emc-pstc that Raymond Garner raymond.gar...@casa.eads.net
wrote (in sr-511...@ieeepstc.mindcruiser.com) about 'New EU
regulations - civil aviation' on Wed, 11 Sep 2002:

Equipments/systems/aircraft are designed, tested and certified way beyond the 
current EMC legislation

They why all the hysteria about passengers' low-power portable equipment
causing disastrous interference with the aircraft systems? My impression
is that there is something seriously lacking in the immunity
requirements for some aircraft systems.
-- 
Regards, John Woodgate, OOO - Own Opinions Only. http://www.jmwa.demon.co.uk 
Interested in professional sound reinforcement and distribution? Then go to 
http://www.isce.org.uk
PLEASE do NOT copy news posts to me by E-MAIL!

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Re: New EU regulations - civil aviation

2002-09-11 Thread Raymond Garner
Amund

Sorry to disappoint you but the short answer is no.  This directive deals with 
aircraft certification and is just tying together the process required in 
getting an Airworthiness Certificate for a new aircraft.
However if you follow the process of certification EMC is included and uses 
either EUROCAE41 or RTCA-DO160 foe civilian aircraft.
I can not recall exactly where it is written but it was agreed quite early on 
that the process of certifying airborne equipments was quite adequate without 
further legislation.
Equipments/systems/aircraft are designed, tested and certified way beyond the 
current EMC legislation

Regards

Ray Garner
CASA.EADS(part of AIRBUS)

[quote]Hi all,

From the EMC guideline document, Chapter 5.5.1.6 (Apparatus totally excluded
(emission and immunity) from the EMC Directive), I quote: Equipment
intended for use in aircraft in flight covered by the Council Regulation
(EEC) No 3922/91 of 16 December 1991

So, EMCD do not apply for equipment installed in an aircraft.

On September 7 2002, the following document was published in the EU Official
Journal:
http://europa.eu.int/eur-lex/en/dat/2002/l_240/l_24020020907en00010021.pdf
or get via http://europa.eu.int/eur-lex/en/oj/2002/l_24020020907en.html


This new regulation, is it the first step for including EMCD and CE marking
for all relevant equipment which shall be installed in aircrafts ?


Best regards
Amund Westin / Oslo, NORWAY




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New EU regulations - civil aviation

2002-09-11 Thread amund

Hi all,

From the EMC guideline document, Chapter 5.5.1.6 (Apparatus totally excluded
(emission and immunity) from the EMC Directive), I quote: Equipment
intended for use in aircraft in flight covered by the Council Regulation
(EEC) No 3922/91 of 16 December 1991

So, EMCD do not apply for equipment installed in an aircraft.

On September 7 2002, the following document was published in the EU Official
Journal:
http://europa.eu.int/eur-lex/en/dat/2002/l_240/l_24020020907en00010021.pdf
or get via http://europa.eu.int/eur-lex/en/oj/2002/l_24020020907en.html


This new regulation, is it the first step for including EMCD and CE marking
for all relevant equipment which shall be installed in aircrafts ?


Best regards
Amund Westin / Oslo, NORWAY




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