FED-STD-791D
5.4 Petroleum ether (60 - 90C)[1,4,0].
5.5 Platers wax [u,u,u].
5.6 No. 30 grit aluminum oxide.
5.7 Purified crystalline nickelous chloride (NiC12)[u,u,u].
5.8 Reagent grade hydrochloric acid (HC1)[3,0,0].
5.9 Reagent grade crystalline chromium trioxide (Cr03)[u,u,u].
5.10 Reagent grade crystalline silver nitrate (AgNO3)[u,u,u].
5.11 Reagent grade barium carbonate (BaCO3)[u,u,u].
5.12 Hydrochloric acid [3,0,0].
5.13 Nickel bar stock [u,u,u].
5.14 Sheet lead [u,u,u].
5.15 Standard reference oil to be obtained from USAF Aero Propulsion Lab,
AFWAL/POSL, Wright-Patterson AFB, OH 45433-6563 [u,u,u].
6. PROCEDURE.
6.1 Operating Conditions
6.1.1 Throughout the entire test, the test gear temperature is controlled at 220
2.8C (428 5F), or the value required by the applicable lubricant specification. Table
1 presents a list of additional operating conditions which are also controlled within the
limits specified. With the tester operating within the specified limits, the test gears are
loaded first to 34.5 kPa gage (5 psig) load oil pressure (nominal 230 lb/in tooth load), and
then at successive increments of 34.5 kPa gage (5 psi). The duration of each loading
period is 10 min 5 s. At the end of each ten-minute loading period, the tester is stopped
and each tooth of the narrow test gear is examined to determine the percent of tooth area
scuffed.
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