Stuck servovalves were observed during preflight checkup in some aircraft u
sing MIL-PRF-83282 hydraulic fluid. Analysis of hydraulic fluid samples and
stuck valves provided a link between valve failures and barium dinonylnaph
thalene sulfonate content of the hydraulic fluid. The barium dinonylnaphtha
lene sulfonate contamination was traced to residual MIL-PRF-6083, the prese
rvative fluid for components, which had not been drained from the component
s prior to installation on the aircraft. Validation of that hypothesis was
proven by laboratory tribological experiments using a reciprocating tribonm
eter and grazing angle microscope Fourier transform infrared spectroscopy.
Corrective actions included revising the operational procedures to drain MI
L-PRF-6083 from components and establishing a 10 ppm maximum limit for bari
um in new MIL-PRF-83282.