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5.14 ELECTROMAGNETIC
     ENVIRONMENT



       www.part66.blogspot.com
SYLLABUS
5.14 Electromagnetic Environment – L2
• Influence of the following phenomena on
  maintenance practices for electronic system:
  – EMC-Electromagnetic Compatibility
  – EMI-Electromagnetic Interference
  – HIRF-High Intensity Radiated Field
  – Lightning/lightning protection
THE INCREASED CONCERN IN RECENT
          YEARS BECAUSE:
• Greater dependence on electrical and electronic systems for
  continued safe flight.
• Reduced electromagnetic shielding due greater use of composite
  materials.
• Increased susceptibility of electrical and electronic systems to
  HIRF due to increased data bus and processor operating speeds,
  higher density integrated circuits and cards, and greater
  sensitivities of electronic equipment;
• Expanded frequency usage, especially above 1 gigahertz (GHz);
• Increased severity of the HIRF environment because of an
  increase in the number and radiated power of radio frequency
  (RF) transmitters; and
• Adverse effects experienced by some aircraft when exposed to
  HIRF.


                                                           Ref: AC 20-158
ADVERSED EXPERIENCES
• Gross navigation error in a passenger aircraft
  in USA (from Newark to San Maarten) caused
  by a portable tv set used by a passenger.
• Lap top used by a passenger affected the
  navigation equipment during aircraft take-off
  and landing.
ELECTROMAGNETIC ENVIRONMENT
• Caused by transmission of electrical energy in
  space, e.g from radar, radio or TV.
• Like current flowing in a wire, magnetic fields
  are created.
EMC – Electromagnetic Compatibility
• Electromagnetic compatibility, or EMC means that a
  device is compatible with (i.e., no interference is
  caused by its electromagnetic (EM) environment and it
  does not emit levels of EM energy that cause
  electromagnetic interference (EMI) in other devices in
  the vicinity.
• All electric devices or installations influence each other
  when interconnected or close to each other. Eg your TV
  set, your GSM handset, your radio and nearby washing
  machine or electrical power lines.
• The purpose of electromagnetic compatibility (EMC) is
  to keep all those side effects under reasonable control
EMI
    ELECTROMAGNETIC INTERFERENCE
• Electromagnetic interference or EMI, also
  called radio frequency interference or RFI. It is
  the disturbance that affects an electrical
  circuit due to either electromagnetic induction
  or electromagnetic radiation emitted from an
  external source.
• If avionics equipments are left unprotected,
  may cause serious flight safety issues.
EMI SOURCES (electromagnetic interference)
EMI IN AIRCRAFT
SOURCES OF EXTERNAL
          INTERFERENCES (note P168)
• Two forms of interference
  – Conducted interference
  – Radiated interference
• Sources of interferences
  – External Electrical Systems e.g brushes, switches
  – Engines system – ignition system
  – Inadequate bonding
  – Faulty static discharger/wicks
CONTROLLING THE INTERFERENCE
• Well Located aerials – the interference to the
  comm/nav systems like ADF and VHF
• Electronic equipment to be grounded and the
  related wires to be shielded and grounded.
• The lighting current flows through the outer skin
  and discharge to the extremity.
• Bonding – all equipments to be bonded together,
  min R = 0.05 ohms.
• Static Discharger – provide the low resistance
  path to the admosphere.
WHAT IS HIRF
• It is High Intensity Radiated Fields
  (electromagnetic energy) external to the
  aircraft, of a strength sufficient to have
  adverse affect on aircraft safety.
• Note: The source of energy is external,
  exclude onboard system and static sources.
LIGHTNING
• The high energy and high voltage can affect
  the aircraft hardware as well as the data.
• The high transient discharge current can
  damage the skin of the aircraft and the
  bonding wires.
PROTECTION AGAINST LIGHTNING
• Aircraft skin
• Voltage and current protector at the
  equipment
• Wire shielding
• Static discharger
PERSONAL ELECTRONIC DEVICES (PED)
• Personal Electronic equipments can produce
  signals that affect electronic equipments.
• However there was no definitive proof of
  individual cases. Symptoms and failures went
  off when passengers were asked to switch
  PED.
• The cautions were founded as some of the
  sensitive electronic wires run in close
  proximity to passengers.
EXAMPLE OF HIRF CHECK
TYPICAL INSPECTION   (P166)

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EASA PART-66 MODULE 5.14 : ELECTROMAGNETIC ENVIRONMENT

  • 1. 5.14 ELECTROMAGNETIC ENVIRONMENT www.part66.blogspot.com
  • 2. SYLLABUS 5.14 Electromagnetic Environment – L2 • Influence of the following phenomena on maintenance practices for electronic system: – EMC-Electromagnetic Compatibility – EMI-Electromagnetic Interference – HIRF-High Intensity Radiated Field – Lightning/lightning protection
  • 3. THE INCREASED CONCERN IN RECENT YEARS BECAUSE: • Greater dependence on electrical and electronic systems for continued safe flight. • Reduced electromagnetic shielding due greater use of composite materials. • Increased susceptibility of electrical and electronic systems to HIRF due to increased data bus and processor operating speeds, higher density integrated circuits and cards, and greater sensitivities of electronic equipment; • Expanded frequency usage, especially above 1 gigahertz (GHz); • Increased severity of the HIRF environment because of an increase in the number and radiated power of radio frequency (RF) transmitters; and • Adverse effects experienced by some aircraft when exposed to HIRF. Ref: AC 20-158
  • 4. ADVERSED EXPERIENCES • Gross navigation error in a passenger aircraft in USA (from Newark to San Maarten) caused by a portable tv set used by a passenger. • Lap top used by a passenger affected the navigation equipment during aircraft take-off and landing.
  • 5. ELECTROMAGNETIC ENVIRONMENT • Caused by transmission of electrical energy in space, e.g from radar, radio or TV. • Like current flowing in a wire, magnetic fields are created.
  • 6. EMC – Electromagnetic Compatibility • Electromagnetic compatibility, or EMC means that a device is compatible with (i.e., no interference is caused by its electromagnetic (EM) environment and it does not emit levels of EM energy that cause electromagnetic interference (EMI) in other devices in the vicinity. • All electric devices or installations influence each other when interconnected or close to each other. Eg your TV set, your GSM handset, your radio and nearby washing machine or electrical power lines. • The purpose of electromagnetic compatibility (EMC) is to keep all those side effects under reasonable control
  • 7. EMI ELECTROMAGNETIC INTERFERENCE • Electromagnetic interference or EMI, also called radio frequency interference or RFI. It is the disturbance that affects an electrical circuit due to either electromagnetic induction or electromagnetic radiation emitted from an external source. • If avionics equipments are left unprotected, may cause serious flight safety issues.
  • 10. SOURCES OF EXTERNAL INTERFERENCES (note P168) • Two forms of interference – Conducted interference – Radiated interference • Sources of interferences – External Electrical Systems e.g brushes, switches – Engines system – ignition system – Inadequate bonding – Faulty static discharger/wicks
  • 11. CONTROLLING THE INTERFERENCE • Well Located aerials – the interference to the comm/nav systems like ADF and VHF • Electronic equipment to be grounded and the related wires to be shielded and grounded. • The lighting current flows through the outer skin and discharge to the extremity. • Bonding – all equipments to be bonded together, min R = 0.05 ohms. • Static Discharger – provide the low resistance path to the admosphere.
  • 12. WHAT IS HIRF • It is High Intensity Radiated Fields (electromagnetic energy) external to the aircraft, of a strength sufficient to have adverse affect on aircraft safety. • Note: The source of energy is external, exclude onboard system and static sources.
  • 13. LIGHTNING • The high energy and high voltage can affect the aircraft hardware as well as the data. • The high transient discharge current can damage the skin of the aircraft and the bonding wires.
  • 14. PROTECTION AGAINST LIGHTNING • Aircraft skin • Voltage and current protector at the equipment • Wire shielding • Static discharger
  • 15. PERSONAL ELECTRONIC DEVICES (PED) • Personal Electronic equipments can produce signals that affect electronic equipments. • However there was no definitive proof of individual cases. Symptoms and failures went off when passengers were asked to switch PED. • The cautions were founded as some of the sensitive electronic wires run in close proximity to passengers.