MWO effective date is 15 November 2002 and completion date is 15 November2006
MODIFICATION WORK ORDER
ATTACK HELICOPTER AH-64A TO REPLACE
M43 SLIDE MOUNT BRACKET ASSEMBLY P/N 5-1-1317 WITH
M48 BRACKET ASSEMBLY, KEVLAR PANEL P/N 5-1-3502
U.S. Army Aviation and Missile Command
19 December 2002
REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS
You can improvethis manual. If you find any mistakesor if you know of a way to improve these
procedures, please let us know. Mail your letter, DA Form 2028 (Recommended Changes to
Publications and Blank Forms), or DA Form 2028-2 located in the back of this manual, directly
to: Commander, U S Army Aviation and Missile Command, ATTN: AMSAM-MMC-MA-NP,
Redstone Arsenal, AL 358984000. A reply will be furnished to you. You may also provide
DA Form 2028 informationto AMCOM via e-mail, fax, or the World Wide Web. Our fax number
DSN 788-6546 or 'Commercial 256-842-6546.
Our e-mail address is:
firstname.lastname@example.org. Instructionsfor sendingan electronic2028may befound at the back
of this manual immediately preceding the hard copy 2028. For the World Wide Web use:
IDISTRIBUTION STATEMENT A: Approved for public release: distribution is unlimited. I
PURPOSE: The purpose of this modification is to provide instructionsfor the removal of the
current slider plate on the left armored wing of the pilot and co-pilot gunner (CPG) crew
seats, and for installation of a new slider plate in the same location to provide an interface to
accommodate the M48 Mask Lighter Weight Motor Blower.
PRIORITY This modification is classified ROUTINE.
END ITEM OR SYSTEM TO BE MODIFIED:
Aircraft having the following National Stock Numbers will be modified in accordance with
All US Army AH-64A Aircraft
Aircraft modifiedduring validation verification. AH-64A, 8940214.