Quiz for 2.2

Basic Radio Wave Quiz

Radio 2.2

Basic Radio
Wave Propagation

2.2 Basic Radio Wave Propagation

2.2.2 Describe the basic characteristics of High Frequency (HF) and Very High Frequency (VHF) in terms of:

(a) range;

(b) surface interference;

(c) clarity of reception.

4.82.22 Procedures to be Followed on Receiving an ELT Signal.

4.82.22 State the procedures to be followed on receiving an ELT signal. AIP GEN

On receiving an ELT signal, pilots must report the following information to the nearest ATS unit:

  • aircraft position and time when the signal was first heard;
  • aircraft position and time when the signal was last heard;
  • aircraft position at maximum signal strength; and
  • aircraft level, strength and frequency of emergency signal on 121.5MHz

4.82.20 Operational Testing of an ELT.

4.82.20 State the requirements for the operational testing of an ELT. AIP GEN

Live testing of 406 MHz is NOT permitted unless coordinated with RCCNZ at least two working days prior to the test

ELT transmitter test is authorised ONLY on 121.5 MHz as follows:

  • tests should be no longer than three audio sweeps and NOT exceed 20 seconds; and
  • tests may be conducted on 121.5 MHz only within the time period made up of the first five minutes after each hour. Emergency tests outside this time must be coordinated with both the nearest ATS unit and RCCNZ. Airborne ELT tests are NOT permitted.

4.82.18 Action Required Following the Inadvertent Transmission of an ELT

4.82.18 State the pilot action required following the inadvertent transmission of an ELT. AIP GEN

Inadvertent activation of ELT has occurred on numerous occasions in New Zealand. It can occur as a result of aerobatics, hard landing, or accidental activation during aircraft servicing. To detect an inadvertent activation pilots should:

  • prior to engine shut down at the end of each flight, tune the aircraft receiver to 121.5 MHz and listen for ELT signals; and
  • if an ELT is heard, ensure that their own aircraft’s ELT is not operating. If it is found that it has been activated, switch it off and take the action described in 6.3.2 then switch it off.

Maintenance may be required before an automatic activation unit is returned to the armed position.

Any person detecting the inadvertent activation of an ELT must report the activation immediately to the nearest ATS unit in order that any RCCNZ action commenced as a result of the transmission may be terminated.

4.82.16 Procedures for the Emergency Activation of an ELT.

4.82.16 State the procedures for the emergency activation of an ELT. AIP GEN

The pilot of an aircraft in a distress situation should activate the ELT while still in flight.

To prevent valuable search time being wasted it is imperative that:

  • All ELTs are registered with RCCNZ.
  • Any ELT that is not automatically activated is switched on as soon as possible before or after any emergency and left on until rescued.
  • If the emergency situation is recovered, ATS or RCCNZ is notified first then the ELT is switched off.
  • If the ELT is switched off and ATS or RCCNZ have not been notified as soon as possible, it will be assumed that the aircraft has crashed and search planning and a SAR response will have commenced.

4.82.14 Procedures for Directing a Surface Craft to a Distress Incident

4.82.14 Describe the procedures for directing a surface craft to a distress incident. AIP GEN

Transmitting precise instructions by any means available. If such precise instructions cannot be transmitted, they should be given by carrying out the following procedure:

  1. circle the surface craft at least once;
  2. cross the projected course of the surface craft close ahead at low altitude:
    (i) rocking the aircraft; or
    (ii) opening and closing the throttle; or
    (iii) changing the propeller pitch.
  3. then head in the direction in which the surface craft is to be directed and
  4. repeat these procedures until the surface craft acknowledges.

Because of the high noise levels on board surface craft the sound of changes in throttle settings and propeller pitch may be less effective than rocking the aircraft, and are regarded as an alternative means of attracting attention.

4.82.12 Ground-Air Visual Signal Codes.

4.82.12 Describe and interpret ground-air visual signal codes. AIP GEN

ground-air visual signal codes.

4.82.10 Speechless Technique

4.82.10 Describe the use of the speechless technique using unmodulated transmissions. AIP ENR

When an unmodulated transmission is heard, the ATS operator will request the pilot activate the transmitter three times; and

if the pilot complies ATS will frame questions requiring “YES” or “NO” answers to determine if the aircraft:

  • can continue visually; or
  • can execute an instrument approach, or has reached a nominated position.

“YES” / “ROGER” – activate transmitter once

“NO” – activate transmitter twice

“SAY AGAIN” – activate transmitter 3 times

“AT NOMINATED POSITION” – activate transmitter 4 times

4.82.8 How ATC will Verify the Transmission of an Emergency SSR Transponder Code.

4.82.8 Describe the means by which ATC will verify the transmission of an emergency SSR transponder code. AIP ENR

Whenever it has been established that an aircraft is transponding on code 7500 the controller will attempt to verify by RTF with the aircraft concerned that the code selection is intentional

“ … (CALL SIGN) … CONFIRM SQUAWKING SEVEN FIVE ZERO ZERO”

If the reply is in the affirmative or if no reply received, this will indicate the aircraft is subjected to unlawful interference.