Narrative:

I was the flying pilot and returned to the seat about 45 minutes prior to landing. I received a briefing from the captain and started to set up for an arrival and landing on runway 09L. All aircraft operations appeared normal. We accomplished an arrival briefing and descent checklist. We flew a 30-flap ILS to runway 09L. Shortly after touchdown; right after I deployed the thrust reversers; we received a hydraulic qty right EICAS (engine indicating and crew alerting system). We completed the landing noting that the right (#2) thrust reverser initially failed to stow. I pulled up the EICAS status page and the right hydraulic system quantity read 0.19rf and the pressure was 2900psi. While on roll out; tower notified us that they observed white smoke trailing from the right side of our aircraft. They could not specify exactly where it was coming from. We informed them that we had lost hydraulic fluid and they may want to inspect the runway. We were concerned about the stopping ability of subsequent aircraft being affected. Tower asked us if we needed assistance; we said no. Tower said we would see fire trucks off to the side who would inspect us and follow us to the gate. We thought that was prudent; and arff (airport rescue and firefighting) did not report any indications of a fire. We shut down the right (#2) engine; ran the hydraulic qty (right) QRH; and taxied to the gate. We completed the parking checklist and sent [a logbook] report. When we deplaned and inspected the aircraft; there was a significant hydraulic fluid leak coming from the right (#2) engine strut. Arff had already deployed absorbent material and was monitoring the situation. We were cleared off by ATC and arff.

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Original NASA ASRS Text

Title: B767 First Officer reported a hydraulic system failure during landing rollout.

Narrative: I was the flying pilot and returned to the seat about 45 minutes prior to landing. I received a briefing from the Captain and started to set up for an arrival and landing on Runway 09L. All aircraft operations appeared normal. We accomplished an arrival briefing and descent checklist. We flew a 30-Flap ILS to Runway 09L. Shortly after touchdown; right after I deployed the thrust reversers; we received a HYD QTY R EICAS (Engine Indicating and Crew Alerting System). We completed the landing noting that the right (#2) thrust reverser initially failed to stow. I pulled up the EICAS status page and the Right Hydraulic System Quantity read 0.19rf and the Pressure was 2900psi. While on roll out; Tower notified us that they observed white smoke trailing from the right side of our aircraft. They could not specify exactly where it was coming from. We informed them that we had lost hydraulic fluid and they may want to inspect the runway. We were concerned about the stopping ability of subsequent aircraft being affected. Tower asked us if we needed assistance; we said no. Tower said we would see fire trucks off to the side who would inspect us and follow us to the gate. We thought that was prudent; and ARFF (Airport Rescue and Firefighting) did not report any indications of a fire. We shut down the right (#2) engine; ran the HYD QTY (R) QRH; and taxied to the gate. We completed the parking checklist and sent [a logbook] report. When we deplaned and inspected the aircraft; there was a significant hydraulic fluid leak coming from the right (#2) engine strut. ARFF had already deployed absorbent material and was monitoring the situation. We were cleared off by ATC and ARFF.

Data retrieved from NASA's ASRS site and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.