Honeywell TFE731-5 User Manual

LIGHT MAINTENANCE MANUAL
TFE731-5/-5AR/-5R (ATA NUMBER 72-02-75)
Page 30
3
Nov 11/0
5
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.

Honeywell TFE731-5 Specifications

General

Brand	Honeywell
Model	TFE731-5
Category	Engine
Language	English

Summary

Preservation

Installed Engine Preservation (Six Months or Less)

Detailed steps for preserving installed engines for up to six months, including safety warnings.

Installed Engine Preservation (More Than Six Months)

Procedures for preserving installed engines for over six months, with critical safety cautions.

Engine Preservation (Removed from Aircraft)

Instructions for preserving aircraft engines after removal from the airframe.

Engine Preservation in Extreme Wet Conditions

Guidelines for engine preservation when the aircraft is exposed to very wet weather.

Engine Preservation in Salt Atmosphere

Procedures for preserving engines operated in salty environments and air strips.

Compressor Rinse for Saltwater Operation

Steps for performing a compressor rinse after aircraft operation in saltwater.