Click here to make tpub.com your Home Page

Page Title: TAIL ROTOR GEARBOX
Back | Up | Next

Click here for thousands of PDF manuals

Google


Web
www.tpub.com

Home


   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
   
   

 

NAVAIR 17-15-50.3
TM 38-301-3
T.O. 33-1-37-3
CGTO 33-1-37-3
SH-60B, SH-60F, HH-60H, MH-60S, MH-60R
TAIL ROTOR GEARBOX
JOAP ATOMIC EMISSION ROTRODE
Fe
Ag
Al
Mg
Ti
Cu
Abnormal Trend
See
(PPM Increase
9
3
9
3
Note 1
in 10 hrs)
Normal Range
0-36
0-2
0-26
0-4
0-75
See
Marginal Range
37-41
3
27-32
5
Note 1
See
High Range
42-45
4
33-40
6
Note 1
See
Abnormal
46+
5+
41+
7+
Note 1
Average Concentration Other Elements:
Si < 100 ppm
WATER LIMIT: 1,200 ppm or 0.120%
NOTE 1:
For copper (Cu) wear concentrations, see the following paragraph on copper
The tail rotor gearbox has a self-contained splash lube oil system without an oil filter. Normal wear particles
and/or corrosion particles will continue to increase until the gearbox is drained and reserviced in accordance with
aircraft information manual.
All oil samples shall be checked for water content. Water Limit: 1200 ppm or 0.120 percent. Water content that
exceeds 1500 PPM shall result in a laboratory recommendation of "J": change oil; sample after first flight. Water
content between 1200 and 1500 PPM shall result in a laboratory recommendation "C": do not change oil;
resample after first flight. If resample results in water content still above 1200 PPM, laboratory recommendation
shall be "J": change oil; sample after first flight. Water in the oil can lead to corrosion which will cause iron and/or
magnesium wear metals to appear in the oil analysis. Water in the oil can also lead to the formation and
accumulation of sludge/deposits in the low areas of the gearbox, resulting from a breakdown of the oil. If sludge or
deposits are suspected to contaminate the oil, then remove the tail rotor servo and inspect for sludge deposit
accumulation in the gearbox and the I.D. of the pinion. Remove any accumulation with a clean dry low lint cloth.
The following supplementary information describes sources of individual wear metals and recommended
maintenance actions depending on contamination level and trend. Contact MMHISST.1 at the Naval Air Depot,
Cherry Point, NC for further information or clarification.
NOTE
Recommendation for immediate maintenance before further flight have serious impact
and are to be issued only in accordance with the instructions below. Any
recommendations involving immediate maintenance before further flight shall be
accompanied by a priority Naval message to NAVAVNDEPOT Cherry Point, NC citing
bureau number, operating activity, gearbox  type, serial number, NOAP history, and
recommendation.
Fe -
If accompanied by copper, see the supplementary information for copper.
By itself, iron may indicate wear or corrosion of the pinion gear, bevel gear,
bearings, or liners. If iron level enters the marginal or high range without
accompanying copper, the recommendation shall be "Submit oil samples
approximately each 10 flight hours for the next 30 flight hours. Do not
change oil at this time. If iron level does not increase to abnormal range

Privacy Statement - Press Release - Copyright Information. - Contact Us

Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business