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An assembly includes a gas turbine engine, a compartment wall, and a gutter system. The gas turbine engine has a spool connected to a fan shaft via a gear system. The compartment wall is positioned radially outward from the gear system. The gutter system is positioned radially outward from the gear

An assembly includes a gas turbine engine, a compartment wall, and a gutter system. The gas turbine engine has a spool connected to a fan shaft via a gear system. The compartment wall is positioned radially outward from the gear system. The gutter system is positioned radially outward from the gear system for capturing lubricating liquid slung from the gear system and positioned radially inward of the compartment wall. The gutter system includes a gutter and a flow passage fluidically connected to the gutter. The flow passage has a plurality of holes that allow the lubricating liquid to pass through the flow passage into a space between the flow passage and the compartment wall.

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1. An assembly comprising: a gas turbine engine having a spool connected to a fan shaft via a gear system;a compartment wall positioned radially outward from the gear system and enclosing the gear system; anda gutter system positioned radially outward from the gear system for capturing lubricating l

1. An assembly comprising: a gas turbine engine having a spool connected to a fan shaft via a gear system;a compartment wall positioned radially outward from the gear system and enclosing the gear system; anda gutter system positioned radially outward from the gear system for capturing lubricating liquid slung from the gear system and positioned radially inward of the compartment wall, wherein the gutter system includes: a gutter comprising a gutter wall positioned radially outward from the gear system, wherein the gutter wall extends circumferentially around the gear system; andan exterior wall disposed radially outward from the gutter wall, wherein the exterior wall and the gutter wall bound and define a flow passage fluidically connected to the gutter, wherein the exterior wall has a plurality of holes configured to allow the lubricating liquid to exit the flow passage into a space between the exterior wall and the compartment wall. 2. The assembly of claim 1, wherein the flow passage curves circumferentially with respect to a centerline axis of the gas turbine engine. 3. The assembly of claim 1, wherein one or more of the plurality of holes pass through a metered restriction at an end of the flow passage. 4. The assembly of claim 1, wherein the plurality of holes pass through the exterior wall of the flow passage such that lubricating liquid passing through the plurality of holes contacts a surface of the compartment wall. 5. The assembly of claim 4, wherein the plurality of holes extend through the exterior wall of the flow passage at locations vertically higher than a lowest vertical position of the exterior wall. 6. The assembly of claim 4, wherein the plurality of holes extend through the exterior wall where the exterior wall curves circumferentially with respect to a centerline axis of the gas turbine engine. 7. The assembly of claim 4, wherein the plurality of holes have a diameter of about 0.125 inches (3.175 millimeters). 8. The assembly of claim 4, wherein the plurality of holes have a diameter of between about 0.125 inches (3.175 millimeters) and about 0.180 inches (4.572 millimeters). 9. The assembly of claim 1, and further comprising: a reservoir fluidically connected between the gutter and the flow passage, wherein the flow passage is a bypass passage to allow flow from the gutter to bypass the reservoir when the reservoir is substantially full. 10. The assembly of claim 1, and further comprising: a scavenge pump; anda main scavenge passage fluidically connecting the scavenge pump to the space between the gutter system and the compartment wall. 11. An assembly for collecting lubricating liquid from a fan drive gear system of a gas turbine engine, the assembly comprising: a gutter positioned radially outward from the fan drive gear system, wherein the gutter comprises a gutter wall extending circumferentially around the fan drive gear system;a reservoir fluidically connected to the gutter; anda bypass passage extending from the reservoir, wherein the bypass passage is disposed between and bound by the gutter wall and an exterior wall disposed radially outward from the gutter wall, wherein the exterior wall comprises a plurality of holes configured to allow lubricating liquid to pass therethrough. 12. The assembly of claim 11, wherein the gutter and the bypass passage are integrally formed. 13. A method for collecting lubricating liquid from a fan drive gear system of a gas turbine engine, the method comprising: catching lubricating liquid slung from a fan drive gear system with a gutter spaced circumferentially around the fan drive gear system, wherein the gutter comprises a gutter wall;delivering the lubricating liquid from the gutter to a passage, wherein the passage is disposed between and bound by the gutter wall and an exterior wall disposed radially outward from the gutter wall; andpassing the lubricating liquid through a plurality of holes in the exterior wall of the passage to deaerate the lubricating liquid. 14. The method of claim 13, wherein the plurality of holes extend through a wall of the passage and wherein the lubricating liquid is squirted through the plurality of holes against a wall of a bearing compartment so as to deaerate the lubricating liquid. 15. The method of claim 13, and further comprising: collecting the lubricating liquid passed through the plurality of holes in a space inside a wall of a bearing compartment; andscavenging the lubricating liquid from the space inside the wall of the bearing compartment via a scavenge passage connected to a scavenge pump. 16. The method of claim 13, and further comprising: delivering the lubricating liquid from the gutter to an auxiliary reservoir when the auxiliary reservoir is not substantially full, wherein the lubricating liquid is delivered from the gutter to the passage, substantially bypassing the auxiliary reservoir, when the reservoir is substantially full. 17. The assembly of claim 13, wherein one or more of the plurality of holes pass through a metered restriction at an end of the flow passage.