Instrument Landing System Operational Notes Contents i Disclaimer These notes are a reproduction of a booklet origin ally published by the Department… [610235]

Instrument Landing System Operational Notes
Contents

i

Disclaimer
These notes are a reproduction of a booklet origin ally published by the Department of Aviation.
Although these notes are no longer in print, they continue to provide a valuable resource and are
made available as reference materi al for students, pilots and instru ctors. The notes have not been
edited, and as they were written 20 or more y ears ago, may contain information relating to systems
that are no longer in producti on or have been modernised.

1. Introduction ………………………………………………………………………………………………………………. .1-1
2. Basic Principles …………………………………………………………………………………………………………..2-1
3. Ground Equipment ………………………………………………………………………………………………………3-1
3.1 Localiser ……………………………………………………………………………………………………………..3- 1
3.2 Glide Path ……………………………………………………………………………………………………………3-2
3.3 Marker Beacons ……………………………………………………………………………………………………3-3
3.4 Monitoring ……………………………………………………………………………………………………………3-4
4. Airborne Equipment …………………………………………………………………………………………………….4-1
4.1 Receivers …………………………………………………………………………………………………………….4-2
4.2 Aerials ………………………………………………………………………………………………………………. ..4-3
4.3 Instrumentation …………………………………………………………………………………………………….4-4
4.4 Cross Pointer Flag Alarm ……………………………………………………………………………………….4-5
4.5 Marker Receiving Equipment ………………………………………………………………………………….4-6
5. Points to Observe when Flying the ILS …………………………………………………………………………..5-1

Instrument Landing System Operational Notes
1. Introduction

These notes are a reproduction of a booklet originally 1-1
published by the Department of Aviation 1. Introduction

The Instrument Landing System (ILS) is an instrument pres ented, pilot interpreted,
precision approach aid. The system provides the pilot with instrument indications which,
when utilised in conjunction with the normal flight instruments, enables the aircraft to be
manoeuvred along a precise, predet ermined, final approach path.
The ILS ground facilities have been categoris ed by international standardisation as
follows:
Facility Performance Category I
An ILS which provides a specified quality of guidance information from the coverage limit of the ILS to the point at whic h the localiser course line intersects the ILS glide path at a
height of 200 ft or less above the threshold. Using this category of equipment and provided that appropriate supplementary ground and airborne equipment is installed and operating,
operations can be permitted down to a decision height of 200 ft and with a runway visual
range (RVR) of the order of 800 metres.
Facility Performance Category II
An ILS which provides a specified quality of guidance information from the coverage limit of the ILS to the point at whic h the localiser course line intersects the ILS glide path at a
height of 50 ft or less above the threshold. Us ing this category of equipment and provided
that appropriate supplementar y ground and airborne equipment is installed and rating,
operations can be permitted down to a decisi on height of 100 ft and with a RVR of the
order of 400 metres.
Facility Performance Category III
An ILS which, with the aid of ancillary equipm ent where necessary, provides the specified
quality of guidance information from the cove rage limit of the facility to and along the
surface of the runway. Using this categor y of equipment and provided that appropriate
supplementary ground and airborne equipment is installed and operating, operations can be permitted with no decision height limitation and without reliance on external visual
reference.
It should be noted that some equipment presently used in Australia is not categorised.
Ø

Instrument Landing System Operational Notes
1. Introduction

1-2 These notes are a reproduction of a booklet originally
published by the Department of Aviation There are three main elements in the complete ILS:
z A localiser radio beam to furnish direct ional guidance to and along the runway
z A glide path radio beam to furnish vertical guidance at the correct descent angle to the
runway touchdown point
z Fan markers (outer marker and middle ma rker). In some cases DME has been
authorised for use when markers are not available or cannot be installed.
A suitable radio navigation aid is provided on most installations to assist in interception of
the localiser and holding procedures. At some locations two of these aids are provided.
This aid can be either a VOR or a low-powered NDB (Locator).
„

Instrument Landing System Operational Notes
2. Basic Principles
These notes are a reproduction of a booklet originally 2-1
published by the Department of Aviation 2. Basic Principles

Figure 2 is a diagram of a basic ILS installation. The localiser transmitters radiate field
patterns of 90-hertz and 150-hertz modulated energy on opposite sides of the instrument
runway centreline to provide a course for guidance in azimuth. The 150-hertz modulation
is always on the right looking towards the ru nway from the outer ma rker and is known as
the ‘blue sector’. The left side is modulated at 90-hertz and is known as the ‘yellow sector’.
The course line (on-course) is a locus of points of equal 90-150-hert z modulation. It is
aligned along the runway centreline extended in both directions and may be separated at
the localiser antenna into a front course and a back course. In order to obtain the quality in
the front course of the localiser necessary for CAT I and higher, a back course is not
radiated in Australia.
Glide path equipment radiates field patterns of 90-and 150- hertz modulated energy to
provide a path for approach slope guidance. The field patterns are orientated so that a
preponderance of the 150-hertz energy lies belo w the glide path and a preponderance of
the 90-hertz energy is above the g lide path. The line of the glide path (on-path), similar to
the localiser course line, is a locus of poi nts of equal 90-and 150-h ertz modulation and is
aligned at the correct approac h angle for descent to t he runway touchdown point.
Figure 3 illustrates the radiat ion patterns of the lo caliser and glide path.
„

Instrument Landing System Operational Notes
3. Ground Equipment
3.1 Localiser

These notes are a reproduction of a booklet originally 3-1
published by the Department of Aviation 3. Ground Equipment
3.1 Localiser
The localiser aerial is on the runway exte nded centreline at the opposite end to the
approach end, at a distance which ensures that it lies below the runway take-off
obstruction clearance plane. The transmitter build ing is usually loca ted 100–120 metres to
the side of the aerial. The field pattern r adiated by the localiser is illustrated in Figure 3
with the course line lying along the extended r unway centreline. The localiser beam ‘width’,
as it is interpreted by the travel of the localiser needle on the aircraft cross pointer indicator
from full deflection in the blue sector (150-hertz) to full defle ction in the yellow sector (90-
hertz) is normally 5° for uncategorised system s and all other systems are adjusted to 210
metres wide at the landing threshold.
Total width in terms of degrees will depend on position of aerials and length of runway. The equipment is designed to provide a usable on-course signal at a minimum distance of 25 nautical miles from t he runway at a minimum altitude of 2,000 ft above the threshold.
Each localiser is identified aura lly by a coded designator consisti ng of three letters, the first
of which is the letter ‘ I’. The transmitters are usually duplicated, with an automatic
changeover facility from primary to secondar y equipment in the event of failure or
malfunction.
„

Instrument Landing System Operational Notes
3. Ground Equipment
3.2 Glide Path

3-2 These notes are a reproduction of a booklet originally
published by the Department of Aviation 3.2 Glide Path
The transmitter buildings and glide path aerial are in close proximity and are usually
located approximately 225–380 me tres from the approach end and 120–210 metres to the
side of the runway centreline. The field patte rn radiated by the glide path equipment is
illustrated in Figure 3, with the on path line set at an angle of 2½ to 3° from the touchdown
point on the runway. The glide path ‘width’ as it is interpreted by the travel of the glide path
needle on the aircraft cross pointer indicator from a full ‘fly-up’ indication to a ‘fly-down’
indication, varies from 1° to 1.5 °. There is no sector colour identification associated with
the glide path. The transmitters are duplicated, with an automatic change-over facility from
primary to secondary equipm ent in the event of failure or malfunction.
„

Instrument Landing System Operational Notes
3. Ground Equipment
3.3 Marker Beacons

These notes are a reproduction of a booklet originally 3-3
published by the Department of Aviation 3.3 Marker Beacons
The marker beacons used with the ILS are low powered, operate on a frequency of 75
MHz and radiate a fan shaped field pattern. T here are usually two marker beacons:
Outer Marker
The outer marker is located approximately 3. 9 nautical miles from the runway threshold
and is aligned across the front beam of the localiser. Its pur pose is to provide height,
distance and equipment functioning checks to airc raft on final approach. It is modulated at
400-hertz and keyed to transmit dashes conti nuously at a rate of two per second.
Middle Marker
The middle marker, also a fan marker, is ali gned across the front beam of the localiser and
is situated approximately 1050 metres from the runway threshold. Its purpose is to indicate
the imminence, in low visibility conditions, of visual approach guidance. This marker is
modulated at 1300-hertz and keyed to transmit alternate dots and dashes.
Some overseas installations utilise a third marker beacon (inner marker) which is modulated at 3000-hertz, identifi ed by a keyed continuous signal of six dots per second
and is located 75–450 metres from the runway threshold. There are no inner markers
associated with ILS installations in Australia.
„

Instrument Landing System Operational Notes
3. Ground Equipment
3.4 Monitoring

3-4 These notes are a reproduction of a booklet originally
published by the Department of Aviation 3.4 Monitoring
The localiser, glide path and marker beacons are monitored. Actuation of a particular
monitor will result in the automatic change-over to the second equipme nt of the component
concerned or the component will ‘close down’.
The localiser monitor will be actuated if any of the following conditions occur:
z Shift of the ‘on-course’ line from the runw ay alignment by more than a specified
amount. For equipment up to CAT I this is 10. 5 metres, for CAT II, 7.5 metres and for
CAT III, 3 metres, measured at the landing threshold
z Reduction of power output below a usable level
z A change in sensitivity of 17%. A decrease in sensitivity produces an increase in
course width and an increase in sensitivity shows a narrowing of the course.
The glide path monitor will be actuated if any of the following conditions occur:
z Shift of the glide path angle by more than 0.1° or if the bottom edge of the beam shifts
by more than 0.1°
z Reduction of power below a usable level.
The marker beacon monitors will be actuated by any failure of the modul ation or keying, or
by reduction of power below a usable level.
The tower controller has available a continuous visual indication of the state of each
component of the ILS on a monito r panel and is given warning of failures by a system of
lights and audible signals.
„

Instrument Landing System Operational Notes
4. Airborne Equipment
These notes are a reproduction of a booklet originally 4-1
published by the Department of Aviation 4. Airborne Equipment

The advent of CAT II and higher ILS requires an increase in the amount and quality of
airborne equipment. This extra equipment is in addition to t hat previously carried. There
has been no change in the basic airborne equi pment for ILS use other than receiver
sensitivity and reliability. Mo st of the additional equipment has been added to allow
automatic approach, overshoot or landing and is only utilised in conjunction with a duplex
(two system) or triplex (three system) auto pilot.
There are several different ty pes of airborne equipment and inst allations vary with different
types of aircraft. Basic components of a simp le installation, however, are listed in the
following paragraphs.
„

Instrument Landing System Operational Notes
4. Airborne Equipment
4.1 Receivers

4-2 These notes are a reproduction of a booklet originally
published by the Department of Aviation 4.1 Receivers
The localiser, glide path and sometimes the marker beacon and DME receivers are
actuated by the one control unit. Every loca liser frequency has a corresponding glide path
frequency. This pairing of t he localiser and glide path frequenc ies is determined by ICAO
and is an internationally accepted standard. The glide path receiver aut omatically tunes to
the correct frequency when the lo caliser frequency is selected on the control unit. When
DME is used in lieu of markers, it is simila rly automatically tuned. Examples of localiser
frequencies with their paired gl ide path frequencies and DM E channels are listed below:
Localiser Frequency Glide Path Frequency DME Channel
109.3 MHz 332.0 MHz 30x
109.5 MHz 332.6 MHz 32x
109.7 MHz 333.2 MHz 34x
109.9 MHz 333.8 MHz 36x
The output of the localiser receiver is s eparated into 90-hertz and 150-hertz components
by bandpass filters and after being rectified the two voltages are applied to the vertical needle of the cross pointer indicator. On aircraft with more than one VHF navigation receiver switching is provided to allow the pilot to connect any of the receivers to his indicator.
The glide path receiver output is also s eparated into 90-hertz and 150-hertz components,
rectified and the voltages applied to the horizontal needle of t he cross pointer indicator.
There is no audio identification signal associated with the glide path ( Figure 3).
The output from the marker beacon receiver actuates the appropriate marker beacon lamps and provides an identifying audio signal.
Radio altimeter receiver output information is presented on an appropriate instrument on the pilot’s instrument panel. The radio altimeter is normally only used for auto pilot coupled approaches.
„

Instrument Landing System Operational Notes
4. Airborne Equipment
4.2 Aerials

These notes are a reproduction of a booklet originally 4-3
published by the Department of Aviation 4.2 Aerials
On most modern high speed aircraft flush or recessed localiser aerials are normally
located in the vertical stabiliser. The same aerial may feed two localiser receivers; the
aerial system and receivers are generally used for VO R also. If a third localiser receiver is
installed its aerial is genera lly located in the nose sectio n, typically within the radome
provided for weather radar.
The glide path receiver aerial is normally lo cated on the nose of the aircraft or within the
radome. On very large aircraft, or those which land with an unusually high nose attitude,
locating the glide path aerial on the nose may re sult in the wheels being too low over the
threshold. In this case the aerial may be lo cated on the underside of the aircraft or on the
landing gear so that correct wheel height guidance is obtained.
The radio altimeter aerial is of the flush mounted type usually situated underneath the
aircraft with an unobstructed ‘view’ downwards.
Marker beacon aerials are also of the fl ush variety and are also mounted underneath the
aircraft.
„

Instrument Landing System Operational Notes
4. Airborne Equipment
4.3 Instrumentation

4-4 These notes are a reproduction of a booklet originally
published by the Department of Aviation 4.3 Instrumentation
There are a number of different types of ILS indicators in operational use. A description of
a basic type of cross pointer indicator is given in this section to best illustrate the function
of the instrument. The cross pointer indicator is a special type of meter, which is located on
the instrument panel in easy view of the pilot.
The indicator is constructed with two needles. The localiser needle is pivoted on the top of
the dial and swings in pendulum fashion from left to right. The glide path needle is pivoted at the left side of the dial and swings up and down.
The stationary scale on the instrument is marked with a target circle in the centre of the
dial, and four radial rows of four dots each, ex tending up, down, le ft and right from the
circle (see Figure 4 ). The perimeter of the ta rget circle is the ‘first dot’ position. These
markings serve to divide the scale of the in strument into equal vertical and horizontal
spaces. At the bottom of the dial the left si de of the scale is marked with blue, the right
side with yellow.
Localiser Indications
The localiser (vertical) needle indicates, by de flection, the colour area of the sector in
which the aircraft is flying. If the aircraft is flying in the blue sector of the localiser, the
vertical needle will be deflected into the blue area of the indicator. Conversely, if the
aircraft is flying in the yellow sector, the nee dle will be deflected into the yellow area of the
indicator. When the aircraft is directly on the localiser course, the needle will be centred
vertically across the circle in the middle of the dial. Regardless of the position or
heading of the aircraft, the localiser needle will always be deflec ted in that colour
area in which the aircraft is flying.
Movement of the needle is very sensitive and will give a full scale deflection (5 dots) when
the aircraft is approximately 2½° to either side of the on-course. This high sensitivity
permits the use of the indicator for a ccurate runway directional guidance.
Glide Path Indications
The glide path (horizontal) needle indicates, by deflection, the position of the glide path in
relation to the aircraft. When the aircraft is above the glide path, the horizontal needle is
deflected downward . Conversely, when the aircraft is be low the glide path, the needle will
be deflected upward . When the aircraft is directly on the glide path, the needle will be
centred horizontally across the circle, in the middle of the dial. The glide path course is
much sharper than the localiser, measuring less t han 1.5° from full ‘fly up’ to full ‘fly down’
on the instrument.
„

Instrument Landing System Operational Notes
4. Airborne Equipment
4.4 Cross Pointer Flag Alarm

These notes are a reproduction of a booklet originally 4-5
published by the Department of Aviation 4.4 Cross Pointer Flag Alarm
Two tiny meters are installed within the case of the cross pointer indicator. Only a current
sufficient to operate the localiser or glide pat h needle will suppress the flag alarm and hold
it out of sight beyond the rim of the dial. The flag alarm, a small red tag, with the word
‘OFF’ clearly inscribed, will move across eit her the localiser needle or the glide path
needle when:
z A usable signal is not being re ceived from the ground equipment
z Either receiver is malfunctioning to such an extent that the output is not sufficient to
hold the flag alarm out of sight.
Figure 4 illustrates the flag alarm.
NOTE: The localiser or glide path should only be used for an instrument approach
when the associated flag alarm is fully suppressed.
„

Instrument Landing System Operational Notes
4. Airborne Equipment
4.5 Marker Receiving Equipment

4-6 These notes are a reproduction of a booklet originally
published by the Department of Aviation 4.5 Marker Receiving Equipment
The marker receiving installation used wit h the 75 MHz ground marker beacons comprises
three basic elements:
a. Receiver
b. Indicator
c. Aerial.
Receiver
The receiver unit, which is fixed-tuned to the frequency of 75 MH z, feeds the signal
received from the marker transmitter through conventional superheterodyne circuits to the
aircraft intercommunication system for aural rec eption of the modulation tones and to the
visual circuits where the modulation tones are fed through special filters to the indicating
lights. The filters allow the signal to ac tuate only the light a ssociated with the one
modulation tone. For example t he blue light is actuated by only a modulation tone of 400
Hz, the amber light by a tone of 1300 Hz, and the white light by a tone of 3000 Hz. Thus
markers may be identified visually as well as aurally.
Indicator
Three lights are provided, blue, amber and wh ite, which are actuated by the 400 Hz,
1300 Hz, and 3000 Hz modulation tones respectively . As the modulation tones identify the
type of marker, the lights are des ignated in the following manner:
Blue (400 Hz Tone)—‘Outer’ (Marker for Ils)
Amber (1300 Hz Tone)—‘Middle’ (Marker for Ils)
White (3000 Hz Tone)—‘Airway’ and ‘Z’ (Also Inner Marker for Ils)
Not used in Australia.
The ‘HI-LO’ switch shown in Figure 1 allows a choice of two sensitivity settings of the
marker receiver. When the switch is in the ‘HI’ position, the rece iver is in its most sensitive
condition and it is in this position the equi pment is normally operated. Changing the switch
to the ‘LO’ sensitivity posit ion decreases, by approximately one half, the time that the
signal may be received.
Ø

Instrument Landing System Operational Notes
4. Airborne Equipment
4.5 Marker Receiving Equipment

Figure 1. Marker Indicator
The ‘day-nite’ switch allows the lamp brilliance to be adjusted to suit individual
requirements. Normally the switch is placed in the ‘day’ position for f lights in daylight and
‘nite’ for night flying.
The marker receiver is not normally provi ded with a separate audio volume control:
adjustment of level is normally made on t he volume control in the selector box.
Aerial
The marker beacon receiver aerial is in mo st cases mounted on the underside of the
fuselage or wings of the aircraft in a position cl ear of all other aerials and obstructions. In
some aircraft an aerial in a boat shaped housing is used, whilst other installations use an
aerial recessed flush with the skin of the aircraft.
„

These notes are a reproduction of a booklet originally 4-7
published by the Department of Aviation

Instrument Landing System Operational Notes
5. Points to Observe when Flying the ILS
These notes are a reproduction of a booklet originally 5-1
published by the Department of Aviation 5. Points to Observe when Flying the ILS

1. Carefully study the appropriate ILS approach chart before committing the aircraft to an
ILS holding pattern or approach.
2. Ensure that equipment indications are norma l and that the flag al arms are not visible
before committing the aircraft to holding or final approach.
3. Identify the ILS aurally and select t he marker beacon aural switch for aural
identification before commencing final approach.
4. Check the aircraft altitude on reception of the marker beacons with the altitudes given
on the ILS approach chart. This will provide a check that equipment is functioning
normally.
5. Remember that a 5 dot indica tion either from the glide path or localiser course, at the
outer marker, represents a greater physical displacement of the aircraft than at the
middle marker (see Figure 2). In other words, the ‘sensit ivity’ of the glide path and
localiser increases as the aircraft approaches the runway threshold.
6. Major corrections to flight path should not be attempted after passing the outer marker.
The approach should be discontinued if majo r corrections to the flight path are
required at this stage.
7. Momentary fluctuations of the localiser needle may be caused by another aircraft
taking off over the localiser aerials. Similarly, fluctuations of the glide path needle may
be caused by a preceding landing aircraft.
8. If a visual reference has not been estab lished at the authoris ed minimum, commence
a missed approach without delay.
9. On a back beam approach or when outbound on a front beam, the localiser needle will
still indicate the sector in which the aircra ft is flying; but needle movement, in relation
to aircraft heading correcti ons, will be reverse to the movement of the needle on a
normal front beam approach.
10. On a back beam approach, the localiser aerials are situat ed at the landing end of the
runway and, in the final stages of the approach, the localiser needle movements will
be more ‘sensitive’ than on the front beam approach.
11. If any doubt exists about the normality of any component of the ILS, check with the
tower controller before commencing the final approach.
12. With modern localisers course revers als will be experienced outside a sector
approximately 45° either side of the cour se centreline. Before commencing the
approach check aircraft on centreline by reference to other aids.
As with any other skill, perfection in fl ying the ILS is acquired with practice.

Instrument Landing System Operational Notes
5. Points to Observe when Flying the ILS

Figure 2. Instrument Landing System
5-2 These notes are a reproduction of a booklet originally
published by the Department of Aviation

Instrument Landing System Operational Notes
5. Points to Observe when Flying the ILS
Ø

Figure 3. Radiation Pattern
Ø
These notes are a reproduction of a booklet originally 5-3
published by the Department of Aviation

Instrument Landing System Operational Notes
5. Points to Observe when Flying the ILS

Figure 4. Cross Pointer Indicator
„
5-4 These notes are a reproduction of a booklet originally
published by the Department of Aviation