*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
AH-64D
N/A
AH-64A
4. MODULES (Components,
Assemblies,
Subassemblies,
Boards,
and
Cards)
TO
BE
INSTALLED. Not applicable.
*This TB supersedes TB 1-1520-238-20-135 dated 6 May 2003.
1
