EZY32KL, an easyJet Airbus A319 operating out of London Gatwick (LGW) bound for Valencia, Spain, declared an emergency and returned to Gatwick shortly after departure following multiple hydraulic system failures. Visual evidence from the landing shows the main landing gear doors remaining in the open position, consistent with a loss of hydraulic pressure preventing the normal retraction sequence from completing — or, alternatively, with a gravity/free-fall gear extension executed after hydraulic pressure was lost on the primary system. The aircraft landed without reported structural incident, and no casualties have been confirmed in available reporting.
The A320 family, of which the A319 is a member, employs three independent hydraulic circuits — Green, Blue, and Yellow — each pressurized to approximately 3,000 PSI. Under normal operations, the Green system handles primary landing gear extension and retraction, with the gear doors sequenced hydraulically before and after gear movement. When Green system pressure is unavailable or degraded, crews can execute a gravity extension via the alternate gear extension procedure, which allows the gear to free-fall into the down-and-locked position but does not provide hydraulic power to close the doors. The open door configuration visible in footage of EZY32KL's landing is characteristic of exactly this scenario. A report of *multiple* hydraulic failures complicates the picture further, as simultaneous degradation of more than one system is relatively rare and would trigger cascading ECAM warnings requiring rapid, disciplined crew response under the non-normal checklist hierarchy.
For line pilots operating the A320 family — a fleet numbering over 9,000 aircraft globally and operated by virtually every major low-cost and network carrier in Europe — this incident is a concrete reminder of the importance of hydraulic system flow logic and the alternate gear extension drill. Simulator training covers single hydraulic system failures routinely, but events involving multiple simultaneous system anomalies compress workload significantly and demand precise task-sharing between the pilot flying and pilot monitoring. The fact that the crew successfully returned to LGW, executed a safe landing, and kept the event contained is a testament to both crew resource management and the fundamental redundancy engineered into the A320 platform.
From an operational and maintenance perspective, incidents of this nature at major hub airports like Gatwick draw immediate attention from both the airline's engineering teams and the UK Civil Aviation Authority. Hydraulic system failures on modern transport-category aircraft are categorized events under EASA's occurrence reporting framework, and a multi-system event will almost certainly trigger a mandatory occurrence report and a detailed investigation into the root cause — whether that is a manufacturing defect, a maintenance error, a fluid contamination event, or an in-service failure of a component such as a hydraulic pump, actuator seal, or pressure relief valve. Part 135 and corporate operators flying hydraulically complex aircraft, including the Challenger and Global series or the Gulfstream G-series platforms, should treat incidents like this as prompts to review their own hydraulic abnormal and emergency procedures in their respective flight operations manuals.
The broader trend worth noting is the increasing scrutiny being placed on aging narrowbody fleets as low-cost carriers push aircraft utilization rates to their limits. The A319, the smallest variant of the original A320 family, is being phased out by many operators in favor of the A320neo and A321neo, and older airframes cycling through high-frequency short-haul operations accumulate hydraulic actuator cycles at a rate far exceeding the original design assumptions for long-haul missions. While the root cause of the EZY32KL hydraulic failures has not yet been established, the incident reinforces ongoing industry discussions about maintenance interval adequacy, component life management, and the safety margins inherent — or eroding — in legacy narrowbody platforms operating at the edge of their design envelopes.