COMMANDER TIPS How to Check Hydraulic Fluid

When performing a Twin Commander (non-Skydrol) aircraft preflight check you must first verify two things to get an accurate indication of hydraulic fluid level:

  1. The flaps are fully retracted
  2. Hydraulic system pressure shows 0 PSI

If either of these requirements is not met, the aircraft will present a false low-level indication.  The aircraft gets serviced with what is thought to be the needed amount of the magic red stuff, goes on a trip, comes home, and is parked for a few days. The next time the pilot comes out to the aircraft he finds a puddle of red “blood” on the ground under the left nacelle. Then the questions start flying.

So, how to prevent this loss of the precious fluid? The answer is to perform the following simple process. It does not have to happen right after aircraft shutdown, but should be sometime soon after. First, run the flaps down, then back up to fully retracted, then down part way and finally back up again. This uses some of the residual energy within the accumulator, causing the accumulator piston to move towards the bottom of its bore, pushing hydraulic fluid back into the reservoir. The idea is to drop a lot of the energy out of the accumulator but end up with the flaps retracted before the energy is dissipated.

Now, sitting in the pilot’s seat and while watching the hydraulic pressure gage, work the brake pedals. The hydraulic system pressure will start to decrease, and at some point the pressure will take a sudden dive towards 0 PSI. Note that point. Work the pedals a few more times. If the gauge seems to bounce around 0 PSI whenever you press the pedals you are ready to get a good reading of the fluid level in the aircraft. The reservoir is vented to the atmosphere (not pressurized as was the case with aircraft using Skydrol) so you can open the nacelle cover, turn and lift the cap on the reservoir and note the height of the fluid between the two marker holes in the dipstick. 

The distance between the holes is equivalent to about one quart of fluid. If the reservoir needs to be serviced, use clean hydraulic fluid, put the cap back on, close the nacelle cover, and the system is ready to go.

I bet you think I forgot about the pressure gauge needle drop comment. When you are depressurizing the accumulator the point at which the hydraulic system pressure gauge suddenly drops is a very rough indicator of the accumulator precharge. You expect it to be around 600 PSI or so before it suddenly drops. However, if it suddenly takes a rapid dive towards 0 PSI when you start the process that is an indication of a low accumulator precharge. If that happens I would recommend contacting your favorite Twin Commander Authorized Service Center to have the system checked for an incorrect accumulator precharge that needs to be serviced, or an internal system leak that needs to be fixed.

Eagle Creek Aviation Service’s Mike Grabbe has been servicing Twin Commanders since 1974. He has been a factory service representative, and is currently the Twin Commander Factory Authorized Training Provider. He can be contacted at [email protected].

What Hydraulic Fluid Do You Have in Your System?

The 690/A/B and early Jetprops left the factory with the hydraulic system serviced with MIL-PRF-5606 fluid. In the early 1980s the factory made a production change from MIL-PRF-5606 to MIL-PRF-83282 fluids. There are some differences between the two fluids. The reason for the hydraulic fluid specification change is because MIL-PRF-5606 fluid has a flash point of 180 degrees F and MIL-PRF-83282 fluid has a flash point of 401 degrees F.

Changing from MIL-PRF-5606 fluid to MIL-PRF-83282 fluid is not complicated. Drain the 5606 fluid and reservice the system with 83282. Note that MIL-PRF-83282 fluid is more viscous than MIL-PRF-5606, so we do not, cannot, and will not use it in the landing gear struts. All 680T thru 695B Twin Commanders landing gear are serviced with MIL-PRF-5606 fluid only. If someone services the struts with MIL-PRF-83282 then the shock loads transmitted to the structure will be greater than designed for and damage to the strut and/or aircraft structure may occur.