The 15 has 3 hydraulic systems, Utility, PC1 and PC2. There are 4 total hydraulic pumps, PC1 and a utility pump driven by left engine, and right utility and PC2 driven by the right engine. The landing gear system, to include brakes, are operated on the utility system so if either engine is down, there is still utility system pressure to run landing gear and brakes. For a utility hydraulic failure, the pilot can pull the “Emergency Brake/Steer” handle which directs pressure from 2 accumulators to the landing gear door locks allowing a free fall, the brake system, and nose wheel steering. Anti-skid will not be available. (Correction edit: the emer brake/steer handle directs accumulator pressure to brakes and NWS, no anti-skid. The Emer landing gear handle directs accumulator pressure to the landing gear door locks. They are two separate handles.)
For a total utility failure, a cable/arresting gear landing would be expected. Sounds like the pilot didn’t want to pull the emer brake/steer handle because he wouldn’t have anti-skid…not sure if that’s squadron policy, but I’m doubting it is. Also sounds like he didn’t want to catch the wire. Although it should be a checklist/no decision item, I could understand that part, as getting the aircraft out of the barrier can be a pain and he’d have to wait for the recovery shop to get to the plane, direct him out of the cable, and then clear him to taxi away or shut down and be towed. Being towed from the runway all the way back to the squadron is a long, hot, annoying ride with no AC.