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Table of Contents
- 1 Preservation
- 2 Equipment and Materials
- 3 Installed Engine Preservation Instructions (Six Months or Less)
- 4 Installed Engine Preservation Instructions (more than Six Months)
- 5 Engine Preservation Instructions (Engine Removed from Aircraft)
- 6 If Aircraft Is Not Sheltered During Extreme Wet Conditions
- 7 If Aircraft Is Operated in a Salt Atmosphere or on Air Strips Treated with Salt
- 8 If Aircraft Is Operated over Saltwater below 4000 Feet for more than 30 Minutes
- 9 Сompressor Rinse Procedure
- 10 Restore Engine to Operational Status
- 11 Perform Dry-Out Procedure of Engine
- Download this manual
2.
Preservation
Equipment or Material
NOTE:
Equivalent substitutes may be used for listed items.
Barrier material (MIL-PRF-121)
Barrier material (MIL-PRF-131, Type I, Class III)
Desiccant (MIL-D-3464, Type I)
Humidity indicator card (MX-56789)
Humidity indicator plug (Type II)
(SAE AS26860) or (HUM 2156)
Mineral base oil (Grade 1010) (MIL-PRF-6081)
(Alternate for Oil (Univolt 60 Preservative))
Oil (Univolt 60 Preservative)
Sealer (Metric Model HS-B)
A.
Installed Engine Preservation Instructions (Six Months or Less)
WARNING:
(1)
Allow engine to cool.
(2)
Inspect engine to assure that inlet area is clean and dry.
CAUTION:
(3)
Install inlet and tailpipe plugs.
E Honeywell International Inc. Do not copy without express permission of Honeywell.
LIGHT MAINTENANCE MANUAL
TFE731-5/-5AR/-5R (ATA NUMBER 72-02-75)
Table 302. Equipment and Materials
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.
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.
Manufacturer
Commercially available
Commercially available
Commercially available
AGM Container Controls Inc, P.O. Box 40020,
3526 E Fort Lowell, Tucson, AZ 85717-0020
Commercially available
Commercially available
Exxon Co, USA, P.O. Box 4803, 600 Jefferson St,
Houston, TX 77210-4803
Doboy Inc, 869 S Knowles Ave, New Richmond,
WI 54017-1745
72-00-00
Page 303
Nov 11/05
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Related Manuals for Honeywell TFE731-5
Summary of Contents for Honeywell TFE731-5
- Page 1 SERVICE. TO MINIMIZE OR PREVENT CORROSION, WATER OR CLEANING SOLUTION SHALL NOT BE PERMITTED TO ENTER THE ENGINE INLET AREA. Install inlet and tailpipe plugs. 72-00-00 Page 303 Nov 11/05 E Honeywell International Inc. Do not copy without express permission of Honeywell.
- Page 2 Maintain engine motoring record indicating engine shall be motored every four weeks. Install inlet and tailpipe plugs. 72-00-00 Page 304 Jan 31/00 E Honeywell International Inc. Do not copy without express permission of Honeywell.
- Page 3 If rust or corrosion is evident, take appropriate corrective action. Preserve engine in accordance with Steps through after inspection completed. 72-00-00 Page 305 Jan 16/04 E Honeywell International Inc. Do not copy without express permission of Honeywell.
- Page 4 Run engine at idle speed for a minimum of ten minutes to re- move moisture and salt residue. Perform normal engine shutdown in accordance with Aircraft Flight Manual and/or appropriate aircraft document. 72-00-00 Page 306 Sept 26/94 E Honeywell International Inc. Do not copy without express permission of Honeywell.
- Page 5 Prepare equipment and materials for compressor rinse. Turn water control valve to OFF and attach supply of clean tap water (of drinking purity) to spray mix applicator inlet. 72-00-00 Page 307 Jan 31/00 E Honeywell International Inc. Do not copy without express permission of Honeywell.
- Page 6 Allow starter to cool in accordance with Aircraft Maintenance Manual. Allow engine to drain induced water. 72-00-00 Page 308 Jan 31/00 E Honeywell International Inc. Do not copy without express permission of Honeywell.
- Page 7 [5A, 5-1H] Operate engine at idle speed for approximately 10 minutes. Perform normal engine shutdown in accordance with Aircraft Flight Manual and/or appropriate aircraft document. 72-00-00 Page 309 Jan 31/00 E Honeywell International Inc. Do not copy without express permission of Honeywell.