LIGHT MAINTENANCE MANUAL
TFE731-5/-5AR/-5R (ATA NUMBER 72-02-75)
Page 303
Nov 11/05
72-00-00
E
Honeywell International Inc. Do not copy without express permission of Honeywell.
2.
Preservation
Table 302. Equipment and Materials
Equipment or Material
Manufacturer
NOTE:
Equivalent substitutes may be used for listed items.
Barrier material (MIL-PRF-121)
Commercially available
Barrier material (MIL-PRF-131, Type I, Class III)
Commercially available
Desiccant (MIL-D-3464, Type I)
Commercially available
Humidity indicator card (MX-56789)
AGM Container Controls Inc, P.O. Box 40020,
3526 E Fort Lowell, Tucson, AZ 85717-0020
Humidity indicator plug (Type II)
(SAE AS26860) or (HUM 2156)
Commercially available
Mineral base oil (Grade 1010) (MIL-PRF-6081)
(Alternate for Oil (Univolt 60 Preservative))
Commercially available
Oil (Univolt 60 Preservative)
Exxon Co, USA, P.O. Box 4803, 600 Jefferson St,
Houston, TX 77210-4803
Sealer (Metric Model HS-B)
Doboy Inc, 869 S Knowles Ave, New Richmond,
WI 54017-1745
A.
Installed Engine Preservation Instructions (Six Months or Less)
WARNING:
MOST PRESERVATIVE SOLUTIONS ARE FLAMMABLE AND
SHOULD NOT BE USED EXCESSIVELY NOR APPLIED TO A
HOT ENGINE. ALLOW ENGINE TO COOL FOR A MINIMUM OF
10 MINUTES BEFORE USING PRESERVATIVE MATERIAL ON
ANY PART OF THE ENGINE.
(1)
Allow engine to cool.
(2)
Inspect engine to assure that inlet area is clean and dry.
CAUTION:
AIRCRAFT INLET AND TAILPIPE PLUGS FOR ENGINE SHALL
BE INSTALLED PRIOR TO WASHING THE AIRCRAFT OR IF
AIRCRAFT IS TO BE PARKED UNSHELTERED WHEN NOT IN
SERVICE. TO MINIMIZE OR PREVENT CORROSION, WATER
OR CLEANING SOLUTION SHALL NOT BE PERMITTED TO
ENTER THE ENGINE INLET AREA.
(3)
Install inlet and tailpipe plugs.
