Main Rotor System Hardware For AH--64 Blade Fold Kit

*TB 1-1520-238-20-135

DEPARTMENT OF THE ARMY TECHNICAL BULLETIN

MAIN ROTOR SYSTEM HARDWARE FOR AH--64

BLADE FOLD KIT

Headquarters, Department of the Army, Washington, D.C.

30 June 2004

REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS

You can help improve this publication. If you find any mistakes or if you know of a way to

improve the procedures, please let us know. Mail your letter or DA Form 2028 (Recommended

Changes to Publications and Blank Forms) directly to: Commander, US Army Aviation and

Missile Command, ATTN: AMSAM-MMC-MA-NP, Redstone Arsenal, AL 35898-5230. You

may also submit your recommended changes by E-Mail directly to 2028@redstone.army.mil

or by fax (256) 842-6546/DSN 788-6546. A reply will be furnished directly to you. Instruction

for sending an electronic 2028 may be found at the back of this publication.

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.

1. PURPOSE. The purpose of this TB is to enhance transportability.

2. PRIORITY. This TB is classified "Routine".

3. END ITEM. The following end items shall have the hardware and bonding jumpers installed in accordance

with the instructions contained in Paragraph 10.

National

Nomenclature

Stock Number

Type and Model

Serial Number

Helicopter, Attack

1520-01-355-8250

AH-64D

N/A

1520-01-106-9519

AH-64A

4. MODULES (Components,

Assemblies,

Subassemblies,

Boards,

and

Cards)

INSTALLED. Not applicable.

*This TB supersedes TB 1-1520-238-20-135 dated 6 May 2003.