Construction, requirements, errors, and serviceability of the direct reading magnetic compass used in aircraft.
A compass is an instrument designed to indicate direction relative to a known datum. The magnetic compass uses the horizontal component of the Earth's magnetic field as its datum. Since the Earth's field is not aligned with the true meridian, the angular difference between true and magnetic meridians must be accounted for â this is magnetic variation.
Magnetic influences from iron/steel components and electrical currents in the aircraft further distort the Earth's field, causing the compass to deviate from the magnetic meridian. This is compass deviation.
đ§ True Heading = Compass Heading Âą Deviation Âą Variation
đ The rules: Compass to True: CADET (Compass + Deviation + Error [variation] = True)
Or: TVDM â True â Variation â Deviation â Magnetic/Compass (to go the other way)
There are two basic types of direct indicating (direct reading) magnetic compasses used in aircraft:
This is the most common direct reading compass. It is the main magnetic heading reference in light aircraft and the standby compass in larger aircraft.
The vertical card compass consists of a circular compass card attached directly to the magnet assembly, suspended in liquid within a compass bowl. A vertical lubber line on the glass window allows the heading to be read from the card.
â
Simple, compact, lightweight
â
Can be read during manoeuvres
â Less stable than the grid ring compass
The grid ring compass is found on older aircraft. It is more accurate and stable than the vertical card compass but has significant disadvantages.
â
More accurate and stable
â
Greater periodicity due to damping wires
â Heavier, bulkier, more expensive
â Can only be read in straight and level flight (grid ring must be unclamped and aligned)
| Feature | Vertical Card (B/E-type) | Grid Ring (P-type) |
|---|---|---|
| Reading condition | Any flight attitude | Straight and level only |
| Accuracy | Moderate | Higher |
| Stability | Moderate | Better (damping wires) |
| Weight/size | Light/compact | Heavy/bulky |
| Application | Light a/c main; large a/c standby | Older aircraft; rarely used now |
For the direct reading magnetic compass to function correctly, the pivoted magnet system must satisfy three essential requirements:
Magnets must lie in the horizontal plane during normal straight and level flight to measure direction correctly.
The magnet system must respond quickly and accurately to the horizontal component H of the Earth's field.
The assembly must settle rapidly on a steady reading after displacement â it must be 'dead beat' with no oscillation.
A freely suspended magnet would align with the Earth's total field (both horizontal H and vertical Z components), causing the magnets to dip. They would only be truly horizontal at the magnetic equator.
To achieve horizontality, the magnet assembly is pendulously suspended â the centre of gravity is placed below the supporting pivot.
In the Northern Hemisphere: the vertical component Z pushes the North-seeking (red) end down. The weight couple opposes this, resulting in a very small residual dip of ~2° (red/north-seeking end slightly low) in mid-latitudes.
In the Southern Hemisphere: the South-seeking (blue) end dips slightly.
â ī¸ This residual dip causes turning and acceleration errors â a significant limitation of the direct reading compass (covered in the Aircraft Magnetism chapter).
Sensitivity requires a high magnetic moment in the magnet assembly and low friction at the pivot. This is achieved by:
đ´ Using 2, 4 or 6 short magnets (or a circular magnet) made of high-retentivity alloy â maximizes pole strength without increasing length.
âī¸ An iridium-tipped pivot in a jewelled cup â minimizes pivot friction.
đ§ Compass liquid â lubricates the pivot AND partially buoys the magnet assembly (reducing effective weight on pivot).
Aperiodicity (dead-beat response) is achieved by:
âŦī¸ Multiple short magnets â keeps mass near the centre, reducing moment of inertia, making oscillations easier to damp.
đ§ Damping liquid â the primary purpose of the liquid in the compass bowl is to damp oscillations of the magnet assembly.
đ Damping wires (grid ring compass only) â additional wires attached to the magnet assembly, rotating through the liquid for extra damping.
Before flight, the compass should be checked for:
â Correct fluid level â liquid must fill the bowl completely (no bubbles); a bubble indicates a leak and makes the compass unserviceable.
â Freedom of movement â the card must move freely without sticking.
â Correct illumination â if fitted with lighting, it should function.
â No excessive deviation â residual deviation should be within regulatory limits and a current compass correction card must be displayed.
Deviation is caused by iron/steel components, electrical currents and other magnetic influences within the aircraft distorting the local Earth's field at the compass location. It is the angle between the magnetic meridian and the direction in which the compass magnets are actually pointing.
âŦ ī¸ Easterly Deviation (+) â North-seeking (red) end of magnets points East of magnetic North.
âĄī¸ Westerly Deviation (â) â North-seeking (red) end points West of magnetic North.
đ Deviation varies with heading â it must be measured on multiple headings during a compass swing.
â ī¸ Never place ferromagnetic objects (tools, watches, metal cases) near the compass â they introduce unknown extra deviation.
đĻ Ferromagnetic cargo should be stowed as far from the compass as loading limits permit.
đ A new compass swing may be required if a large ferromagnetic load is carried.
âī¸ The swing must be conducted with: engines running, all electrical/radio services on, aircraft in level attitude.