Attachment 0004_MEO B2929.pdf

MAINTENANCE ENGINEERING ORDER

(AMCOM Reg. 750-2)

MEO NO.

DATE PAGE 1 of

TITLE Tolerances Unless otherwise noted, dimensions are in inches and tolerances are:

Fractional ………………… ± 1/32 Decimal ………………... ± 0.010 Angular ………………… ± ½°

APPLICABILITY CSI Critical Characteristic Affected?

Impact Statement Attached?

REFERENCES FOR RDECOM USE ONLY

DOCUMENT(S) AFFECTED

PURPOSE OR PROBLEM

PROJECT ENGINEER ENGINEERING REVIEW ENGINEERING RELEASE

MED FORM 5-DEC-09 1401-R-E

AR 70-62 •11 May 2016 B 2929

Sep 21, 2017 1

MODIFICATIONS UPDATE WP 0023

P/N 70250-12051-045

Technical

INTERIM USE OF THIS MEO IS AUTHORIZED

UNTIL AFFECTED DOCUMENT IS UPDATED.

MEO CHANGE TYPE

3) High - Has a business or process impactPRIORITY IMPLEMENTATION CATEGORY

UH60 DAA

DMWR 1-1620-247 dated 21 July 2017 TN168974A, 177671

DOCUMENT CHANGE IS REQUIRED Verification: Hands-On Table-Top None

Update modifications with correct WP references.

KERNAN.JAMES.

J.JR.1258452760

Digitally signed by

KERNAN.JAMES.J.JR.1258452760

DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=USA, cn=KERNAN.JAMES.J.JR.1258452760 Date: 2017.09.13 10:45:31 -05'00'

SALAZAR.ALBER

TO.JAIME.12571

46258

Digitally signed by

SALAZAR.ALBERTO.JAIME.1257146258

DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=CONTRACTOR, cn=SALAZAR.ALBERTO.JAIME.12571462 Date: 2017.09.13 10:31:43 -05'00'

A.J. SALAZAR (CAMBER)

HORN.REINHOL

D.J.1087783495

Digitally signed by

HORN.REINHOLD.J.1087783495

DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=USA, cn=HORN.REINHOLD.J.1087783495 Date: 2017.09.13 14:51:34 -05'00'

JAMES KERNAN RON HORN

PUBLICATION CHANGE REQUEST: REQUEST THAT THE FOLLOWING DATA BE INCLUDED IN THE NEXT

CHANGE OR REVISION TO THE PUBLICATION IDENTIFIED ABOVE.

WP NO. PAGE

NO.

PARA-

GRAPH

FIGURE/

TABLE

NO.

CHANGES

(EXACT WORDING OF CHANGES MUST BE GIVEN)

0023 3, 4 CHANGE paras 3 and 4 to read:

"3. Repair parts, as required, per WP 0010 through WP 0018.

4. Kneeling valve assembly 70250-12028-042 may be modified to 70250-12028-043 by replacing knob Figure 1, Item 11 Part No.

70250-12038-101 with knob Part No. 70250-12038-102 per WP 0007 and WP 0019.

5. Reassemble main landing gear shock strut assembly per WP 0020 using replacement and/or additional parts listed in Table 1."

Distribution Statement D:- Distribution authorized to Department of Defense and U.S. DoD contractors only to protect critical technology effective as of 26 June 2014. Other requests for this document must be referred to U.S. Army Aviation and Missile Research, Development and Engineering Center, ATTN: RDMR -AEM , Corpus Christi, TX 78419-5211

MED FORM 04 APR 2017