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NAVAIR 17-15-50.3
TM 38-301-3
T.O. 33-1-37-3
CGTO 33-1-37-3
MH-60A/UH-60L/MH-60L/MH-60K (U.S. ARMY ONLY) (Cont.)
TAIL ROTOR GEARBOX
b.  When used in gearboxes which had been operated with MIL-L-23699 or MIL-L-7808 lubricant, the
DOD-L-85734 lubricant has a detergent effect. This may cause an increase in wear metal levels as seen in
spectrometric analysis of oil samples. Lab personnel should use caution when analyzing oil samples in these
cases, as the increase in wear metal levels
may give the same indications that component wear would give. After gearboxes which have changed to DOD-L-
85734 have operated for 50 - 100 flight hours, have the unit perform a drain and flush to remove wear metals from
the gearbox.
c.  Oil analysis laboratory personnel should not hesitate to request a drain and flush of the tail rotor
gearbox if they believe it is warranted. Removal of contaminants and wear particles from the gearbox lubricant is
the best method to prolong gearbox life and prevent future problems. Drain and flush procedures are given in
paragraph 7 below.
3.  Oil analysis lab personnel may receive oil samples either from a regular interval sampling, or whenever the
field unit experiences a problem with the tail rotor gearbox on their aircraft. The regular sampling interval is now
50 flight hours. The most common cause for field units to send a special sample to the oil analysis laboratory is
when there are chips present in the gearbox. Table A-1 gives the chip evaluation criteria for tail rotor gearboxes.
This criteria may be used by laboratory personnel to assist in the evaluation of the condition of a tail rotor gearbox
from which chips were identified.
4.  All oil samples submitted for analysis should be checked for water contamination. The limit is 1000 ppm or
0.100%. Gearboxes with water contamination should be drained and flushed per paragraph 7 below in an attempt
to prevent gearbox housing corrosion. See paragraph 6b for further information.
Figure A-1. Tail Rotor Gearbox

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