Instrument Landing System (ILS) - Ch 6 Flashcards

1
Q

ILS General Info

A

Precision Instrument

VHF 108-112MHZ with odd numbers after decimal

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2
Q

ILS Components

A

Localiser (lateral)
Markers
Glide Slope (Vertical)
DME co-located (markers if not)

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3
Q

Localiser Signal

A

Low 90MHZ Left
High 150MHZ Right (when right of CL = Fly Left)

When difference: Depth of Modulation = same = you are on CL

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4
Q

Coverage

A

17nm Out 35 degrees

25nm Out 10 degrees

Protected Area

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5
Q

Deviation

A

Each Line = 0.5 degrees

Full Deflection = 2.5 degrees

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6
Q

Side Lobes

A

Transmitted out from main lobes - errors of radar

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7
Q

Back Beam

A

Reverse Indication: only used if programmed into FMC

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8
Q

Glide Path General

A
UHF - 90HZ Lobe (light) High
150HZ Lobe (heavy) low
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9
Q

Glide Path Deviation

A

Deviation Dot = 0.14 degrees

Full deflection = 0.7

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10
Q

Glide PAth Antenna

A

300m from RW threshold

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11
Q

Glide Path Coverage

A

3 degrees is standard

Height = 3x distance

Up to 10 miles

Normal Range 1.35 - 5.25

Intercept from below

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12
Q

Glide Path Performance

A

Within half a scale deflection and remaining within half a scale or abort

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13
Q

ILS Frequency

A

Localiser: VHF 108-111.95MHZ (odd)

Glide Path: UHF 328.6 - 335.4MHZ

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14
Q

ROD Calculation

A

ROD = (Theta x Groundspeed (nm/min)) x 100

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15
Q

Height Passing Calculation

A

= (theta x range from touchdown(nm)) x 100

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16
Q

Monitoring

A

Ground equipment is continuously automatically checking itself,

If fault= remove ident, cease transmission, beam bar + Glide slope disappear, flag warning ATC

17
Q

Interference

A

Scalloping: night effect - due to changing density

18
Q

LVP Critical Area

A

Vehicles and AC are excluded from moving

19
Q

LVP Sensitive Area

A

Vehicle/AC movements are controlled