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The system incorporates two filters that both filter return fluid prior to entering the reservoir.

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The system incorporates two filters: one for filtering fluid leaving the pump and one for filtering return fluid prior to entering the reservoir.

The hydraulic accumulator is used:

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If normal DC power is lost:

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The Mustang uses hydraulic power for retraction and extension of the landing gear, and operation of the brakes. The system includes a single electrically driven hydraulic pump, which functions to maintain and supplement accumulator pressure.

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Access to the hydraulic reservoir sight glass is:

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There are two sight gauges on the hydraulic reservoir that are visible through the forward baggage compartment liner. The reservoir capacity is approximately 2.2 quarts (2 liters) as indicated by the full mark.

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The hydraulic system provides pressure to operate the:

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The hydraulic reservoir is attached to the left forward pressure bulkhead.

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On the ground with the 'HYD PRESS LO' amber message in the CAS window, the MASTER CAUTION:

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The HYD PUMP ON message in the CAS window appears when:

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On preflight inspection, to check accumulator precharge pressure and hydraulic fluid levels:

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Citation Mustang – Hydraulics