Landing gear support

1. A landing gear support comprising:

a gear rib including an upper flange supporting an upper wing skin, a lower flange supporting a lower wing skin, a forward flange attached to a wing spar,

mounts each having a first surface abutting and fastened to the web of the gear rib and a second surface opposite to the first surface, and

pintle supports integral with a respective one of the mounts such that the pintle support and the mount is a single piece component, wherein each of the pintle supports extends outward from the first surface of the mount and each of the pintle supports includes an aperture configured to receive a pintle to rotatably support a landing gear assembly attached to the pintle,

wherein at least one of the mounts is removably attached to the support member separately from another of the mounts.

2. The landing gear support according to claim 1 , wherein each of the mounts is removably attached to the web of the gear rib.

3. The landing gear support according to claim 1 , wherein at least one of the mounts is mechanically fastened to the web of the gear rib.

4. The landing gear support according to claim 1 , a first mount of the mounts is removably attached to the web of the gear rib, and

a second mount of the mounts is removably attached to the web of the gear rib,

wherein the second mount is separately removably attached to the web of the gear rib from the first mount, and

wherein the first mount has only one of the pintle supports and the second mount has at least two of the pintle supports.

5. The landing gear support according to claim 4 , wherein the pintle support arrangement comprises:

a third mount of the mounts is removably attached to the web of the gear rib,

wherein the third mount is a single piece component with only one of the pintle supports,

Wherein the third mount is separately removably attached to the web of the gear rib from the first mount and the second mount.

6. The landing gear support according to claim 1 , wherein a male protrusion or a female recess is on the second surface of each of the mounts, and the male protrusion or female recess is configuration to mate with a corresponding female recess or male protrusion on the web of the gear rib.

7. The landing gear support according to claim 1 , wherein each of the mounts includes one or more flanges integral with the respective mount and extending away from the web of the gear rib, and the flanges are configured to facilitate removable attachment of the mount with the flanges to the web of the gear rib.

8. The landing gear support according to claim 1 , further comprising:

a spacer portion configured to hold the first or second mount in a spaced relationship from the web of the gear rib.

9. The landing gear support according to claim 1 , wherein the at least one of the first and second pintle supports is formed from a material different from a material forming the mount to which the first or second pintle support is integral with.

10. A kit for forming the landing gear support in accordance with claim 1 , the kit comprising the first and second support portions.

11. An aircraft wing comprising a landing gear support in accordance with claim 1 .

12. An aircraft comprising a landing gear support in accordance with claim 1 .

13. A method of making a landing gear support in accordance with claim 1 , the method comprising attaching one or more pintle supports to a support member, thereby providing a pintle support arrangement for holding a pintle on which a landing gear assembly may be rotatably supported.

14. The A landing gear support comprising:

a gear rib including an upper flange configured to support an upper wing skin, a lower flange configured to support a lower wing skin, a forward flange configured to attached to a wing spar,

a first support portion including:

a first mount having a first surface abutting the web of the gear rib and a second surface opposite to the first surface, and

first pintle supports integral with and forming a single piece component with the first mount, the first pintle supports extend outward from the first surface of the first mount, and the first pintle supports each include a first aperture configured to receive a first pintle to rotatably support a landing gear assembly attached to the first pintle,

a second support portion including:

a second mount having a first surface abutting the web of the gear rib and a second surface opposite to the first surface, and

a second pintle support integral with and forming a single piece component with the second mount, the second pintle support extends outward from the first surface of the second mount, and the second pintle support includes a second aperture configured to receive a second pintle to rotatably support the landing gear assembly attached to the second pintle,

wherein the first mount and the first pintle support are removably attached to the web of the gear rib separately from the second mount and the second pintle support.

15. The landing gear support according to claim 14 , wherein the first mount is integral with and a single piece component with at least three of the first pintle supports, and

wherein the second pintle support is the one and only pintle support integral or attached to the second mount.

16. The landing gear support according to claim 14 , wherein the first mount and/or the second mount comprise one or more flanges integral with the first or second mount and configured to facilitate attachment of the first or second mount to the web of the gear rib.

17. The landing gear support according to claim 14 , further comprising one or more fasteners for attaching the first and second support mounts to the web of the gear rib.

18. A method of maintaining an aircraft comprising:

a wing including an upper skin, a lower skin and a front spar and a gear rib, wherein the gear rib includes an upper flange supporting the upper skin, a lower flange supporting the lower skin and a forward flange attached to the front spar,

mounts each having a first surface facing and attached to the web of the gear rib and a second surface opposite to the first surface, and

pintle supports each integral and forming a single piece component with a respective one of the mounts and extending outward from the first surface of the respective one of the mounts and each of the pintle supports includes an aperture configured to receive a pintle to rotatably support a landing gear assembly attached to the pintle,

the method comprising removing one or more of the pintle supports from the gear rib, wherein the removal includes removing at least one of the pintle supports from the web of the gear rib separately from other of the pintle supports.