A320 Air carrier First Officer aircraft reported Hydraulic System Malfunction on descent.
Synopsis
A320 Air carrier First Officer aircraft reported Hydraulic System Malfunction on descent.
Narrative
We were in our initial descent into ZZZ when we received an ECAM for a GRN HYD ENG 1 LO PR. We had fault lights illuminated on the GEN ENG 1 and PTU (Power Transfer Unit) switch. We ran the ECAM which directed us to switch both the GRN ENG 1 and PTU off. The status page listed all the inoperative systems. It also stated that we should attempt to restore GRN ENG 1 to extend the gear and if unable a gravity extension would be required. We then referenced the FM non-normals for review; reviewed the gravity extension and computed the landing distance required. The Captain [advised] Center and requested direct ZZZ. We had XXX [passengers and crew] and around 1:45 minutes of [fuel]. Next the Captain made contact with my Dispatcher through ARINC. He explained the situation and his intentions to land at ZZZ1. We set the aircraft up for a 20 nm final; turned the GRN ENG 1 pump back on and selected gear down. The gear extension was slower than normal but we did receive a 3 GREEN and locked indication. The GRN ENG 1 was switched back off. We touched down in the first 1000 ft. of XXL and came to a stop with 1500 ft. remaining. We ran an after landing flow; then referenced the FM Supplementary section for Tow-in procedures. After shutting down the engines the Fire department informed us we were leaking hydraulic fluid out of the nose wheel area. End of incident; the Captain notified all required authorities.
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Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.