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Section 11.13

Landing Gear

The oleo-pneumatic strut, retraction/extension, wheels, brakes and anti-skid, steering and air/ground sensing.

Notes

Landing gear, summary notes

Main ideas
  • The gear supports the aircraft on the ground and absorbs the landing shock through an OLEO-PNEUMATIC strut: on touchdown the strut compresses, forcing oil through an orifice (which DAMPS the energy as heat) while a charge of compressed gas acts as the SPRING.
  • Retraction/extension is normally HYDRAULIC, with up-locks and down-locks, sequenced gear doors, and an alternate (free-fall/gravity) extension for hydraulic failure; a position and warning system shows gear state.
  • WHEELS carry tubeless tyres (nitrogen-filled) and multi-disc BRAKES (steel or carbon); ANTI-SKID modulates brake pressure to prevent wheel lock and skidding, and AUTOBRAKE gives selectable deceleration; brake temperature is monitored.
  • Nose-wheel STEERING (hydraulic or electric), and an AIR/GROUND sensing system (the weight-on-wheels or 'squat' switch on the strut) tells many aircraft systems whether the aircraft is on the ground or airborne.
  • Tyre condition, strut servicing (oil and gas charge) and brake wear are routine maintenance items.
  • ⚠ Exam trap: the oleo strut absorbs shock by forcing OIL through an orifice (damping) with compressed GAS as the spring, not by a steel coil spring; the squat/weight-on-wheels switch provides the air/ground signal to the aircraft systems.
Solved examples
  1. How does an oleo-pneumatic shock strut absorb a landing, and what are the two media doing?

    As the strut telescopes on touchdown, it forces hydraulic OIL through a small metering orifice, this converts the impact energy into heat and DAMPS the motion so the aircraft doesn't bounce. At the same time a charge of compressed GAS (nitrogen) is squeezed, acting as the SPRING that supports the static weight and then extends the strut again. Oil = damping, gas = spring.

Mind map

Landing gear concept map

Landing Gear

Quiz

Landing gear quiz

Landing Gear, quiz

Ref 11.138 of 20Pass 75%
  1. 1. On the landing gear shown, the switch marked S is mounted on the shock strut so that it operates as the strut compresses. It is the:

    actuatordownlockS
    Squat switch
    Downlock switch
    Proximity heater
  2. 2. An oleo-pneumatic strut absorbs shock using:

    Oil forced through an orifice (damping) plus compressed gas (spring)
    A steel coil spring alone, chosen because it returns the stored energy smoothly on the rebound
    Rubber blocks in compression only, which absorb the landing loads and need no servicing in service
  3. 3. In the oleo strut, the compressed gas acts as the:

    Spring
    Damper
    Lubricant
  4. 4. The weight-on-wheels (squat) switch tells systems whether the aircraft is:

    On the ground or airborne
    Turning left or right
    Climbing or descending
  5. 5. Anti-skid braking works by:

    Modulating brake pressure to prevent wheel lock
    Applying maximum pressure always
    Releasing all brakes
  6. 6. Gear retraction/extension is normally powered by:

    Hydraulics
    The battery
    Bleed air only
  7. 7. An alternate gear extension typically uses:

    Gravity free-fall
    The engine starter
    The APU
  8. 8. Aircraft tyres are inflated with:

    Nitrogen
    Oxygen
    Helium