Abstract: An aircraft seat (1) is disclosed. The aircraft seat (1) comprises a seating surface (51), an armrest (7), and a gas strut (9) configured such that the armrest (7) can be moved between a raised position a lowered position in which an armrest surface (71) is substantially level with the seating surface (51). The gas strut (9) comprises a switch (92) with an unlocked configuration in which the stroke of the gas strut (9) can be adjusted and a locked configuration for locking the stroke of the gas strut (9) so that the armrest (7) can be held at any position between the raised position and the lowered position. A trigger (117) is configured to move the switch (92) between the locked and unlocked configurations upon actuation of an actuatable member (111) that is located upon a surface of the aircraft seat (1).

Abstract: An aircraft seat (1) is disclosed. The aircraft seat (1) comprises a seating surface (51), an armrest (7), and a gas strut (9) configured such that the armrest (7) can be moved between a raised position a lowered position in which an armrest surface (71) is substantially level with the seating surface (51). The gas strut (9) comprises a switch (92) with an unlocked configuration in which the stroke of the gas strut (9) can be adjusted and a locked configuration for locking the stroke of the gas strut (9) so that the armrest (7) can be held at any position between the raised position and the lowered position. A trigger (117) is configured to move the switch (92) between the locked and unlocked configurations upon actuation of an actuatable member (111) that is located upon a surface of the aircraft seat (1).

Abstract: A bush assembly configured to be disposed between a first component and a second component movably coupled to the first component, the bush assembly comprising a first bush portion comprising a self-lubricating material; and a second bush portion, the second bush portion having greater electrical conductivity than the first bush portion, wherein the second bush portion provides a conductive path between the first component and the second component.

Abstract: A bush assembly configured to be disposed between a first component and a second component movably coupled to the first component, the bush assembly comprising a first bush portion comprising a self-lubricating material; and a second bush portion, the second bush portion having greater electrical conductivity than the first bush portion, wherein the second bush portion provides a conductive path between the first component and the second component.

Abstract: An aircraft landing gear arrangement is provided comprising: a first landing gear portion comprising one or more wheels, a second landing gear portion, the first landing gear portion being rotatable with respect to the second landing gear portion; and a sensor for determining a rotational position of the first landing gear portion in relation to the second landing gear portion, the sensor comprising a first magnetic field generator operable to generate a magnetic field and a first magnetic field modulator for modulating said magnetic field, the sensor being operable to sense the magnetic field as modulated by the first magnetic field modulator, the first landing gear portion comprising the first magnetic field generator or the first magnetic field modulator, the second landing gear portion comprising the other of the first magnetic field generator and the first magnetic field modulator.

Abstract: An aircraft landing gear arrangement is provided comprising: a first landing gear portion comprising one or more wheels, a second landing gear portion, the first landing gear portion being rotatable with respect to the second landing gear portion; and a sensor for determining a rotational position of the first landing gear portion in relation to the second landing gear portion, the sensor comprising a first magnetic field generator operable to generate a magnetic field and a first magnetic field modulator for modulating said magnetic field, the sensor being operable to sense the magnetic field as modulated by the first magnetic field modulator, the first landing gear portion comprising the first magnetic field generator or the first magnetic field modulator, the second landing gear portion comprising the other of the first magnetic field generator and the first magnetic field modulator.