Books   Videos  CD-ROM    Avionics Test Equipment
 Classified  How to Advertise  
Title Index  Word Search   Download Free Catalog   Kit Plane Avionics   Home

Practical AvionicsTM  

No 4

Subjects:
Databuses: 
Fiber Optics
Interference: Alternator and DME
Instruments:  Compass Problem in Convair
Transponders:  Mode C Code
Training:  Instructor Qualifications
Lightning: Strikes on Aircraft

Databuses
Fiber Optics
Q.
Are any fiber optic databuses certified for aircraft?
A. Fiber optic databuses for aircraft are still in an early stage.  The airlines. for example, are defining FDDI---the Fiber Optic Digital Data Interface.  SAE has a committee to standardize HSRB (High Speed Data Bus).  The military databus based on copper wire, MIL-STD-1553, has already defined a fiber optic equivalent known as MIL-STD-1773. Widespread use of fiber optic buses, which is sure to happen, must await several developments;  completely new aircraft designs and simpler methods for installing fiber optic connectors in the field.

Interference
Alternator and ADF

Q. I have a King KN85 ADF which works very well when the alternator in my Warrior is turned off.  The alternator brushes were cleaned, diodes checked, shielding installed on the field wiring, a new capacitor installed on the alternator.  There is a Hysonic filter on the firewall.  Several people have said it is not worth trying, but IFR GPS is expensive.

A. Those are certainly good steps to take.  Be absolutely sure, also, that the case of the alternator makes good contact with ground through its mounting, and there is no corrosion to prevent clean metal-to-metal contact.  The same applies to your capacitor, filter and shielded wire. 
   Another item to check is the engine cowllng.  Unless it makes good contact with ground (usually through the hold-downs)  it might even pick up noise and re-radiate it to the ADF antenna. Clean up any grease or corrosion to eliminate this possibility.
   There is a good possibility that much of the problem is in the ADF antenna system. Unless it is working at high efficiency, the receiver is very susceptible to noise. An ADF loop antenna  often lies at the bottom of the belly where  it collects gunk and other foreign matter that corrode the connector pins. This should be the first step in troubleshooting: remove the connector and shine up the pins.   The best material for this is "crocus cloth" which contains a jeweler's rouge that removes rust without scratching the metal.  Also, the female part of the connector  should be sprayed with contact cleaner.  Examine the length of antenna cable for kinks, cuts, breaks or abrasions---which steal signal strength. Inspect the cable where it enters the back of the radio, too. A thorough clean-up or replacement of ADF cable and connectors often restores performance. 

Compass
Convair Compass Problem
Q. I have a problem with the No. 2 compass on a  Convair 580. Whenever I select No. 2 nav on either RMI, I get a No. 2 compass flag. The wires check OK.  (From an FBO in Ft. Lauderdale, FL.)

  A. There are several  possibilities. You said you checked  the wires and found no problem.  But did you also measure the  wires  for shorts to ground? There is a possibility that your continuity checks between wires and connectors were OK, but did not account for shorts to ground.

    Does the airplane have two nav receivers which can be swapped?  If so, exchanging their positions would show whether the trouble is following one receiver.  This could tell whether the  receiver is loading down the system, causing the flag to drop into view.

   You may have a problem at the  junction box, which brings together  all the  associated wiring on terminal strips.  It is a common problem that a meter placed on these terminals will indicate proper continuity, but the terminal will not pass the signal.  Check these terminals in the junction box to be sure they are clean and tight. 

 Transponders
Mode C Code

Q. An FAA Airworthiness Directive says  "...any Mode C transponder with a single Gilham code input."  What is a "Gilham" code?
A. The Gilham code is the system to encode altitude information from the aircraft's altitude sensing devices (either a blind encoder or digitizing altimeter). This is sent to the transponder, where it is transmitted as a Mode C reply----thus informing Air Traffic Control of the aircraft's altitude.  When an aircraft receives an interrogation from ATC surveillance radar, it replies with a train of 12 pulses, each a zero or one. Controlled by the altitude encoder, this creates  a possible 4096 number combinations. Actually, altitude is encoded only  every 100 feet, which provides 1,290 different altitudes between -1000 ft and 127,000 ft.
   Since airplanes rarely fly underground, why report  -1000 feet?  The reason is that the encoder is adjusted to  pressure altitude (referenced to 29.92 inches of mercury) and not height above ground or a local altimeter setting.  This also explains a widely held misconception by pilots that when they adjust their altimeter, they are also affecting the altitude reported to ATC.  The encoder is fixed on 29.92 inches (or 1013 millibars) regardless of the local baro pressure. When the signal reaches ATC, it is corrected to local pressure, thus  eliminating a potential source of pilot error.      
   Incidentally, the FAA uses the term "Gilham," but  in the avionics industry is it more  frequently called the "Gray" code. 


Training

Instructor Qualifications

   Q.What are the qualifications for teaching avionics/electrical systems besides having the curriculum approved by the FAA?

A.
According to the Federal Air Regulations (Part 147, Aviation Maintenance Technician Schools) a school must maintain a list of current instructors with their ratings and certificates.   The rules are  not more specific, except to say instructors must hold ratings the FAA Administrator  determines are necessary to provide adequate instruction.  Practically speaking,   these rules apply mainly to instructors teaching airframe and powerplant mechanics and these instructors are expected to have A&P ratings.
   However, the FAA makes an exception when it comes to specialized subjects such as electricity, physics and other areas. Here the rules say that such teachers do not need a mechanics license.  Although the regulations don't spell it out, we can assume this includes the highly specialized  subject of avionics, which is often taught at  A&P schools.
   Thus, the real-world answer to your question is that a Part 147  school will examine  a prospective teacher's credentials and decide on the individual's qualifications to do the job. There is no other formal FAA process.

Lightning
Strikes on Aircraft

Q.  What protects an airplane from lightning?

A.  On the average, an airliner is struck by lightning once a year.  However, there are almost no proven cases where lightning has brought down an airplane.  There are several reasons.  One is that most aircraft are protected by their aluminum skin which blocks the lightning stroke.  On newer airplanes, which have large areas of plastic skin (composites), a mesh of metal wires is embedded to provide similar protection.
   Another factor is that lightning isn't really attracted to  an airplane but strikes it on the way to somewhere else.  Most lightning is caused by large voltage differentials (plus and minus  charges) which exist from cloud-to-cloud and  from cloud to ground.  Lightning occurs when that voltage  breaks down (ionizes)  the air between these areas.    An airplane in flight develops only a minor  charge and is not very electrically attractive.
   Airplanes do suffer lightning damage, but they are rarely fatal.  After a strike, small burn pits or  tiny holes are often observed in the skin of the airframe. Compasses and other instruments  are sometimes affected and need repair.
    One item that does need lightning protection is the radome, or covering,  for the weather radar in the nose of the airplane.  Because it is made of plastic, it is fitted with "diverter strips"---metal runners which fan out from the nose . This helps lead the electrical charge away from the radome  to the metal airframe.
   In recent years, as airplanes acquired digital circuits, they must meet much higher standards of protection  against outside electrical charges.   This is because digital signals are much lower in level than the old analog ones and are more easily upset. Thus, new aircraft use more shielding, bonding, filtering and other measures to reduce the effects of "EMI":---electromagnetic interference.   Lightning fits in that category. 
   A most awesome video was made when an F-4 Phantom fighter was sent directly into a violent thunderstorm on a research flight, with  an on-board camera aimed at the tail.  Lightning could be seen striking the tail again and again.   But the airplane landed safely with no more than the minor effects described above.  

Publisher/Editor -  Len Buckwalter  

Your questions and  comments are welcome: 
Copyright 2000 Avionics Communications Inc. 

Return to top

Index to All Subjects


New Publication
The most up-to-date
avionics text available.
PRINCIPLES
OF AVIONICS

 

Just Released!

Hundreds of connection
diagrams for avionics
equipment, plus
practical reference
material.  See
complete contents:
AVIONICS
INSTALLATION
HANDBOOK