Attachment_0002_MEO_B1295_W58RGZ-19-R-0050.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 15-DEC-09 1401-R-E

B 1295 Aug 27, 2013 7

UH-60 Tail Rotor Blade Depot Maintenance Overhaul Requirements (DMWR) Errata

P/N 70101-11200-044 / -043

Administrative

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 1-1615-287 dtd 30 Dec 2011 TN 125766

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

Correct errors in publication for Change 1, dated 17 June 2013.

SOLBERG.JOH

N.B.1230311427

Digitally signed by

SOLBERG.JOHN.B.1230311427

DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=USA, cn=SOLBERG.JOHN.B.1230311427 Date: 2013.08.21 05:09:43 -05'00'

RADER.KARL.AN

DREW.10443758

Digitally signed by

RADER.KARL.ANDREW.1044375849

DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=CONTRACTOR, cn=RADER.KARL.ANDREW.1044375849 Date: 2013.08.20 16:00:13 -05'00'

Karl Rader

REIFENBERGER

.ROBERT.ANDR

EW.1079786663

Digitally signed by

REIFENBERGER.ROBERT.ANDREW.107978666

DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=USA, cn=REIFENBERGER.ROBERT.ANDREW.107978 Date: 2013.08.21 11:47:02 -05'00'

John Solberg FOR 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)

3-26

3-37

3-67

3-74

3-75

3-78

3-13.7.n

3-13.8.l

Tbl 3-1

OIP 1,

No. 10

Fig 3-10

Fig 3-13

CHANGE Dwell Time to read: "<1"

CHANGE OIP 1, Inspection No. 10, Requisite, "3-13.30.2 to "3-13.30.3."."

REPLACE Figure 3-10 with new figure 3-10 on page 5 of this MEO.

REPLACE the Tail Rotor Blade and Tip Cap drawings in Figure 3-13 (the top two views) with new drawings on page 6 of this MEO.

CHANGE paragraph 3-13.7.n to read: "Cure repair at 140° to 160°F (60° to 71°C) for at least 2 hours."

CHANGE paragraph 3-13.8.l to read: "Cure repair at 140° to 160°F (60° to 71°C) for at least 2 hours while maintaining pressure and contour of repair."

Formatted Cont. Sheet

W58RGZ-17-R-0237

Attachment 0002

Continuation Sheet

MEO NO.

PAGE of

WP NO. PAGE

NO.

PARA-

GRAPH

FIGURE/

TABLE

NO.

CHANGES

MED FORM 15-DEC-09 1401-R-E

3-80

3-81

3-87

3-99

3-100

3-107

3-108

3-109

3-111

3-127

3-128

3-132

3-133

3-137

3-13.9.m

3-13.12.c (9)

3-13.16.n

3-13.16.q (8)

3-13.18.c (1)(c)

3-13.18.c (2)(f)

3-13.18.m

3-13.19.k

3-13.23.6.

d

3-13.24.f

(13)(e)

(14)(h)

3-13.25.r

Fig 3-16

B 1295

CHANGE paragraph 3-13.9.m to read: "Cure repair at 140° to 160°F (60° to 71° C) for at least 2 hours."

CHANGE last line in Note 5 to read: "(APP C, ITEM 56, 60, or 65)."

CHANGE paragraph 3-13.12.c(9) to read: "Vacuum bag repair per paragraph 3-13.33 and cure at 140° to 160°F (60° to 71°C) for at least 2 hours."

CHANGE paragraph 3-13.16.n to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.16.q(8) to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.18.c.(1)(c) to read: "Vacuum bag cure repairs per paragraph 3-13.33 at 140° to 160°F (60°to 71°C) for at least 2 hours."

CHANGE paragraph 3-13.18.c(2)(f) to read: "Vacuum bag cure repairs per paragraph 3-13.33 at 140° to 160°F (60° to 71°C) for at least 2 hours."

CHANGE the second sentence of paragraph 3-13.18.m to read: "Cure repair at 140° to 160°F (60° to 71°C) for at least 2 hours or at room temperature (70° to 85°F/ 21° to 29°C) for at least 24 hours."

CHANGE paragraph 3-13.19.k to read: "Secure patch with masking tape (App C, item 37) and cure repair at 140° to 160°F (60° to 71°C) for at least 2 hours or at room temperature (70° to 85°F/ 21° to 29°C) for at least 24 hours."

CHANGE paragraph 3-13.23.6.d to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.24.f to read: "Repair bond separations in torque tube region (Rotor Station 15.062 - 40.00) as follows:"

CHANGE paragraph 3-13.24.f(13)(e) to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.24.f(14)(h) to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.25.r to read: "Vacuum bag repair per paragraph

Formatted Cont. Sheet

Continuation Sheet

MEO NO.

PAGE of

WP NO. PAGE

NO.

PARA-

GRAPH

FIGURE/

TABLE

NO.

3-144

3-147

3-148

3-151

3-154

3-160

3-162

3-163

3-163

3-166

3-169

3-170

3-13.28.i

3-13.28.1.

d.(4)

3-13.28.1 (j).(5)

3-13.29.1.

r

3-13.29.2.

r

3-13.30.1.

k

3-13.30.1.

aa

3-13.30.2.

e

3-13.30.2.

h

3-13.30.3.

q

3-13.32.1.

w

3-13.32.2.

f

CHANGE paragraph 3-13.28.i to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.28.1.d.(4) to read: "Vacuum bag bond per paragraph

CHANGE first sentence of paragraph 3-13.28.1.(j).(5) to read: "Applying 12-15 psi (nom), cure the nylon wrap-to-spar bond at 140° to 160 °F (60° to 71 °C) for 2 hours, minimum."

CHANGE paragraph 3-13.29.1.r to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.29.2.r to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.30.1.k to read: "Vacuum bag repair per paragraph 3-13.33 and cure at 140° to 160°F (60° to 71°C) for at least 2 hours or at room temperature (70° to 85°F/ 21° to 29°C) for at least 24 hours."

CHANGE paragraph 3-13.30.1.aa to read: "Vacuum bag repair per paragraph 3-13.33 and cure repair at 140° to 160°F (60° to 71°C) for at least 2 hours or at room temperature (70° to 85°F/ 21° to 29°C) for at least 24 hours."

CHANGE third sentence of paragraph 3-13.30.2.e to read: "Vacuum bag repair per paragraph 3-13.33 using a vacuum pressure of 10 to 12 psi (20.4 – 28.5 in Hg vacuum) and cure at 140° to 160°F (60° to 71°C) for at least 2 hours or at 70° to 85°F (21 to 29°C) for a minimum of 24 hours."

CHANGE second sentence of paragraph 3-13.30.2.h to read: "Vacuum bag repair per paragraph 3-13.33 using a vacuum pressure of 10 to 12 psi (20.4 –

28.5 in Hg vacuum) and cure at 140° to 160°F (60° to 71°C) for at least 2 hours or at 70° to 85°F (21° to 29°C) for a minimum of 24 hours."

CHANGE paragraph 3-13.30.3.q to read: "Vacuum bag repair per paragraph 3-13.33 and cure at 140° to 160°F (60° to 71°C) for at least 2 hours or at room temperature (70° to 85°F/ 21° to 29°C) for at least 24 hours."

CHANGE paragraph 3-13.32.1.w to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.32.2.f to read: "Vacuum bag repair per paragraph 3-13.33 and cure assembly at 140° to 160°F (60° to 71°C) for at least 2 hours."

B 1295

Formatted Cont. Sheet

Continuation Sheet

MEO NO.

PAGE of

WP NO. PAGE

NO.

PARA-

GRAPH

FIGURE/

TABLE

NO.

3-172

3-174

3-177

3-184

3-189

C-5

3-13.32.3.

g

3-13.32.4.

d

3-13.33.q

Fig 3-45

Fig 3-49

APP C

CHANGE paragraph 3-13.32.3.g to read: "Vacuum bag repair per paragraph

CHANGE paragraph 3-13.32.4.d to read: "Vacuum bag repair per paragraph

REPLACE the Repair Section II drawing in Figure 3-45 with the corrected Repair Section II drawing on page 7 of this MEO.

CHANGE the fourth sentence of paragraph 3-13.33.q to read: "Cure for at least 2 hours or at room temperature (70° to 85°F/ 21° to 29°C) for at least 24 hours."

CHANGE Note 4 in Figure 3-49 to read: "DO NOT PAINT NICKEL ABRASION

STRIP OR NICKEL ABRASION STRIP ON TIP CAP."

CHANGE Item 83, second entry, Description and U/M, to read:

Description: EA9309.3NA EZ-PAK GRACO SUPPLY(SUPPLIER)

(04347) (ITEM NUMBER)

U/M: 50 grams

B 1295

Formatted Cont. Sheet

Continuation Sheet

MEO NO.

PAGE of

Figure 3-10. Repair Surface Corrosion on Horn Outboard Faces

Formatted Cont. Sheet

W58RGZ-17-R-0237

Attachment 0002

ClaryDL Line

Continuation Sheet

(REMOVED)

A A

Fig 3-13. Repair Tip Cap Attachment Holes or Rib Damage

B 1295

Formatted Cont. Sheet

W58RGZ-17-R-0237

Attachment 0002

Continuation Sheet

REPAIR SECTION II

Figure 3-45. Viton Repair Sections (Sheet 1 of 3)

Formatted Cont. Sheet

W58RGZ-17-R-0237

Attachment 0002

RDMR-AEM

MEMORANDUM FOR RECORD:

SUBJECT: Impact of AED Maintenance Engineering Order (MEO) on maintenance using ,affecting system:

Enclosed MEO is issued by this office and is provided as part of our Technical Data user support mission.

4. THIS MEO CHANGES THE FOLLOWING (Check all that apply):

1.

Consumables

Materials

Expendables

Repairable Bill of Materials (RBOM)Impact

3. PRIORITY IMPLEMENTATION CATEGORY :

6. Comments:

7. Point of contact for this action is

2. FOR AMCOM ACQUISITION CENTER USE ONLY:

This MEO was written as a request from a contractor/KO on an active M&O contract.

Request that MEO be transmitted to the contractor as soon as possible.

b.Items checked in this area are considered Normal Priority Implementation Category.

Illustrated Parts Breakdown Change Mandatory Replacement Part

TSO/TSN Change Configuration Change

Publication New Change

Hardware Tooling Equipment

New/Revised Procedure/Process

Process Improvement Project Inspection

Special Process Testing Cost Savings a.Items checked in this area are considered High Priority Implementation Category.

5. Reason(s) MEO Written:

Other

Other

B 1295

DMWR 1-1615-287 dtd 30 Dec 2011 UH60

B 1295

3)High-MEO has a business or process impact

CCAD Request

Results from review of Change 1 to the DMWR.

John Solberg; 361-961-3551; email: john.b.solberg.CIV@mail.mil Dan Grzelecki; 361-961-4062; daniel.p.grzelecki.civ@mail.mil

SOLBERG.JOHN.B.123031

Digitally signed by SOLBERG.JOHN.B.1230311427 DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=USA, cn=SOLBERG.JOHN.B.1230311427 Date: 2013.08.21 05:09:55 -05'00'

John Solberg