Narrative:

On descent; while getting vectored for ILS runway xx (airport in sight); at approximately 6;000 feet; the PIC selected flight air brakes. I then noticed the hydraulic level light illuminate on the master caution panel. The PIC retracted the flight air brakes; slowed to gear extension speed; and selected gear down. The gear came down and indicated down and locked. The hydraulic level light extinguished; and normal main system pressure and auxiliary hydraulic pressures were indicated. Normal checklists were completed; and the crew discussed going missed and diverting to a more suitable airport with longer runways if indications of a main hydraulic failure presented. For the duration of the approach; all indications were normal until at least the second half of the landing roll; when hydraulic level light began to flicker and the main system pressure began fluctuating. The PIC was able to use normal braking for the first half; and then they faded and he selected emergency braking. Nose wheel steering was intermittent; but sufficient to get the airplane into the chocks at the FBO. We advised ground that we were experiencing intermittent steering issues and would keep them advised if we needed assistance (tug). Post flight inspection showed hydraulic fluid coming out from the bottom of the right wing under the airbrakes.

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Original NASA ASRS Text

Title: G100 First Officer noted a hydraulic low level light when the Captain selected flight air brakes. The light extinguished when the airbrakes were retracted and the approach was continued to landing. Normal wheel brakes were used during the first half of the ground roll then they fail and emergency brakes are used. A large leak was noted under the right wing after parking.

Narrative: On descent; while getting vectored for ILS Runway XX (airport in sight); at approximately 6;000 feet; the PIC selected flight air brakes. I then noticed the HYD LEVEL light illuminate on the master caution panel. The PIC retracted the flight air brakes; slowed to gear extension speed; and selected gear down. The gear came down and indicated down and locked. The HYD LEVEL light extinguished; and normal main system pressure and auxiliary hydraulic pressures were indicated. Normal checklists were completed; and the crew discussed going missed and diverting to a more suitable airport with longer runways if indications of a main hydraulic failure presented. For the duration of the approach; all indications were normal until at least the second half of the landing roll; when HYD level light began to flicker and the main system pressure began fluctuating. The PIC was able to use normal braking for the first half; and then they faded and he selected Emergency braking. Nose wheel steering was intermittent; but sufficient to get the airplane into the chocks at the FBO. We advised ground that we were experiencing intermittent steering issues and would keep them advised if we needed assistance (tug). Post flight inspection showed hydraulic fluid coming out from the bottom of the right wing under the airbrakes.

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.