SUPPLY KITS/PARTS AND DISPOSITION

TB 1-1520-238-20-135

8. SUPPLY KITS/PARTS AND DISPOSITION --

8.1 TB kits supplied by: PEO Aviation SFAE-AV-AAH-LF.

8.2 TB kits authorized only for: AVUM.

8.3 Bulk and Consumables:

NOMEMCLATURE

PART NUMBER

NSN

Paint, Red

EPB-4-230/D4

N/A

Lubricant, Solid Film

HMS4-1078

9150-01-480-4237

Corrosion Preventative Com-

MIL-C-16173*C2GR4

8030-01-396-5738

pound

Sealing Compound

MIL-S-81733

8030-00-008-7198

Sealing Compound (alt)

HMS16-1097*T2CB-1/2

8030-01-476-2255

8.4 Parts Disposition: Disposition of parts removed and not used during installation of this TB will be in

accordance with proper disposal procedures.

9. SPECIAL TOOLS, JIGS, TEST, MEASUREMENT AND DIAGNOSTIC EQUIPMENT (TMDE), AND

FIXTURES REQUIRED --

NOMEMCLATURE

PART NUMBER

Quantity

Milliohm meter

10. PROCEDURES --

WARNING

Use solid film lubricant only in well ventilated areas. Keep away from

flames or sparks. Harmful if inhaled. If injury occurs, seek medical

aid.

CAUTION

Ensure that a Foreign Object Damage (FOD) prevention program is

implemented during application of this TB in accordance with AR

385-95.

NOTE

Determine run-on torque by using a torque wrench and rotate the nut for a

minimum 180 degrees while observing the torque wrench reading. Ensure

the nut is not seated against the washer and at least one thread protrudes

past the nut. The resultant observed torque should be added to the ranges

listed in the task steps.

10.1 All threads shall be sprayed per HP4-75 or MIL-PRF-46417C, with a coat of HMS4-1078* Type 1

lubricant before installation.

CAUTION

Do not heat ferrous parts over 350 degrees F or nonferrous parts over

250 degrees F damage may result.

Do not cool bearings and bushings below -321 degrees F. Damage

may result.