Attachment_04_MEO_B1088C_W58RGZ-16-R-0140.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 1088 Rev C

Mar 9, 2016 50

IUID Parts Marking for the Army UH-60A (NSN 1520-01-035-0266), EH-60A (NSN 1520-01-082-0686) and UH-60L (NSN 1520-01-298-4532) Helicopters

Technical

INTERIM USE OF THIS MEO IS AUTHORIZED

UNTIL AFFECTED DOCUMENT IS UPDATED.

MEO CHANGE TYPE

4) Normal - Can be implemented with normal priorityPRIORITY IMPLEMENTATION CATEGORY

UH60 DAA

DMWR 1-1520-237-1, dtd 9 September 2013 TN 125620C 11/13/2015

TN 151989 - MEC B304566 10/16/2015

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

Rev C: Changes based on MEC B304556 (TN151989) Update the Helicopter/IUID Data Plate Marking Requirements and provide component legacy marking requirements.

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: 2016.01.26 12:39:16 -06'00'

STARK.DAVID.A

NTHONY.108180

Digitally signed by

STARK.DAVID.ANTHONY.1081800584

DN: c=US, o=U.S. Government, ou=DoD, ou=PKI, ou=CONTRACTOR, cn=STARK.DAVID.ANTHONY.1081800584 Date: 2016.01.08 10:53:24 -06'00'

David A. Stark (Camber Corporation)

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: 2016.03.08 14:51:39 -06'00'

Robert Reifenberger Ron Horn PUBLICATION CHANGE REQUEST: REQUEST THAT THE FOLLOWING DATA BE INCLUDED IN THE NEXT

CHANGE OR REVISION TO THE PUBLICATION IDENTIFIED ABOVE.

WP 0002 00 PAGE 00-6:

REPLACE Helicopter Nameplate paragraph with the following:

"Helicopter Nameplate (SS9026)

The helicopter nameplate is located on the forward right side of the lower center console in the cockpit (Figure 5, Detail B). The nameplate may contain some or all of following information; the manufacturer's name, model number, aircraft serial number, manufacturer's serial number, date of manufacture and contract number. If replacement is required, replicate helicopter nameplate using fabrication requirements found in Figure 6. All human readable information shall be replicated on the replacement nameplate."

REPLACE Figure 5 with new Figure found page 7 of this MEO.

ADD Figure 6 found on page 8 of this MEO and insert after Figure 5.

WP 0002 00 PAGE 00-7:

REPLACE Tail Rotor Pylon Identification Data Plate (MS27253-4) paragraph with the following:

"Tail Rotor Pylon Identification Data Plate (MS27253-4). The original tail rotor pylon identification data plate (Figure 7), may contain some or all of following information; aircraft model number, manufacturer's code, part number, contract number, and serial number. It also contains blocks for contractor's and customer's inspection seals. The identification data plate shall be replaced with a Tail Rotor Pylon IUID data plate"

RE-IDENTIFY current Figure 6 as 7 and REPLACE it with new Figure 7 found on page 9 of this MEO.

W58RGZ-16-R-0140

Attachment 0004

Continuation Sheet

MEO NO.

PAGE of

WP 0002 00 PAGE 00-7:

CHANGE "(Figure 7)" in paragraph under Overhaul Data Plate (SS9013-2368) to read "(Figure 8)".

WP 0002 00 PAGE 00-8:

RE-IDENTIFY current Figure 7 to 8.

WP 0002 00 PAGE 00-8:

ADD after Replacement of Data Plate paragraph the following:

NOTE

Items having a 2-D data matrix shall be queried per WP 0003 00.

"ITEM UNIQUE IDENTIFICATION (IUID) DATA PLATES

The helicopter airframe, tail rotor pylon and other components contained within this DMWR may have Machine Readable Information (MRI) in a ECC 200 compliant 2-D data matrix that is encoded with a Construct 1 or 2 Unique Item Identifier (UII) using applicable Data Identifiers (DI) or Text Element Identifiers (TEIs) as the data qualifiers, in accordance with DoD Guide to Uniquely Identifying Item and MIL-STD-130. The 2-D data matrix may reside on the item via data plates, labels or direct part marking (DPM). In addition to the MRI encoded in the 2-D data matrix, the associated format indicator data qualifiers (DIs or TEIs) may also reside on the item as Human Readable Information (HRI), provided there is adequate real estate.

Helicopter IUID Data Plate (OCM A/L Models) (SS9026-3)

This helicopter IUID data plate (Figure 9) was fabricated by Corpus Christi Army Depot (CCAD) and replaced the helicopter nameplate (Figure 5, Detail B) or the helicopter IUID data plate (Figure 5, Detail C), which was previously considered a temporary data plate.

If present, replace the helicopter IUID data plate (Figure 9) with a helicopter nameplate (Figure 5, Detail B), restoring it to it's original helicopter nameplate configuration (non-IUID). All human readable information shall be replicated onto the replacement helicopter nameplate.

The recorded UII (per WP 0003 00, DOD IUID REGISTRY QUERY) encoded in the helicopter IUID data plate (Figure 9), 2-D data matrix shall be used to create a permanent helicopter IUID data plate (Figure 5, Detail C).

Refer to Helicopter IUID Data Plate below.

ADD Figure 9 found on page 10 of this MEO.

Helicopter IUID Data Plate

The helicopter IUID data plate (Figure 5, Detail C) replaces the OCM A/L Model helicopter IUID data plate or the helicopter assigned virtual UII that is recorded in the DoD IUID Registry. The helicopter IUID data plate is located adjacent to or in the vicinity of the helicopter nameplate (Figure 5, Detail B). If there is no helicopter IUID data plate present or if replacement is required per WP 0003 00, DoD IUID REGISTRY QUERY, fabricate or replicate the Helicopter IUID data plate using fabrication requirements found in Figure 10.

ADD Figure 10 found on page 11 of this MEO.

B 1088 Rev C

Continuation Sheet

Helicopter RECAP Modification/IUID Data Plate

If present, the RECAP modification/IUID data plate (Figure 5, Detail D) is installed upon completion of an A to L RECAP overhaul event. The data plate is located on the forward side of the helicopter nameplate. If replacement is required per WP 0003 00, DoD IUID REGISTRY QUERY, replace/replicate the data plate using fabrication requirements found in Figure 11.

ADD Figure 11 found on page 12 of this MEO.

Tail Rotor Pylon IUID Data Plate (SS27253-4)

The tail rotor pylon may arrive with an IUID data plate (Figure 7). The IUID data plate is configured with one ECC 200 compliant 2-D data matrix encoded with a Construct 2 UII. If required (WP 0003 00, DoD IUID REGISTRY QUERY), fabricate replacement IUID data plate in accordance with IUID Data Plate Fabrication and Figure 12.

ADD Figure 12 found on page 13 of this MEO.

Component IUID Data Plates.

If components within this DMWR arrive at the depot with a 2-D data matrix, but the individual WP(s) have no IUID marking requirements, contact the applicable cognizant engineering authority for IUID marking and fabrication requirements.

1. Components having IUID data plates are classified into two types:

a. Manufacturer IUID Data Plate: Data plates that are originally UID-marked and registered during production of the item.

b. Legacy IUID Data Plate: Data plates that are originally UID-marked post-production during an M&O event or in the field by an authorized Army IUID marking agency (commonly referred to as legacy components).

Registration is completed by the owning M&O repair facility or the Army IUID marking agency that created the item's UII.

2. The two types of IUID data plates may be configured with one or two 2-D data matrices.

a. When utilizing two 2-D data matrices, one data matrix is encoded with a Construct 1 or Construct 2 UII using the applicable format indicator data qualifiers (DIs or TEIs) in accordance with MIL-STD-130. The other data matrix is encoded with the component's current part number using an applicable format indicator data qualifier DI (30P) or TEI (PNR). Current part number being the component's part number at the time the item was being IUID marked i.e., at production, in the field or upon completion of the M&O event.

b. When utilizing one 2-D data matrix, the data matrix is encoded with a Construct 1 or Construct 2 UII and the component's current part number using the applicable format indicator data qualifier DI (30P) or TEI (PNR).

c. For specific component IUID data plate marking requirements, refer to applicable component work package."

B 1088 Rev C

Continuation Sheet

IUID DATA PLATE FABRICATION

Prior to fabrication of the IUID data plate, the DoD IUID Registry shall be queried per WP 0003 00, DoD

IUID REGISTRY QUERY.

Refer to applicable component work package for IUID data plate format/configuration, fabrication and application requirements.

The MRI and HRI can be marked on the IUID data plate using Laser Etch (WP 0344 00, Item 65), Metal Photo, Thermo Transfer printer or other acceptable marking technique, as applicable, in accordance with MIL-STD-130.

1. If the tail rotor pylon and components within this DMWR that require IUID are not registered in the DoD IUID Registry as determined per WP 0003 00, DoD IUID REGISTRY QUERY (regardless of how the component is marked) or the UII data and component data does not match that in the registry record, a legacy IUID data plate shall be fabricated as follows:

a. A Construct 1 UII shall be encoded into a ECC 200 compliant 2-D data matrix using TEIs SPL (supplier's CAGE Code) and UCN (supplier's Unique Component Number), IAW DoD Guide to Uniquely Identifying Items and/or MIL-STD-130 and register in the DoD IUID Registry via the Wide Area Work Flow (WAWF) (WP 0338 00, Websites) or AMCOM's The Army Maintenance Management System - Aviation/Maintenance Consolidated Database System, (TAMMS-A/MCDS), Unique Identification (UID) database (WP 0338 00, Websites). The UII can be constructed by the overhaul/repair facility using the overhaul facility's Enterprise Identifier (CAGE Code) SPL and UCN or the overhaul facility can generate an UII via AMCOM's TAMMS-A/MCDS, UID database (WP 0338 00, Websites). The component's manufacturer serial number shall not be used to develop the UII, but shall reside as HRI on the IUID data plate.

b. When utilizing one 2-D data matrix, the component's current part number shall be encoded in the data matrix in addition to the UII using TEI PNR as the data qualifier.

c. When utilizing two 2-D data matrices, a separate 2-D data matrix shall be encoded with the component's

PNR.

For components being marked by a Government Depot facility, registration shall occur prior to the component leaving the facility. For components being marked by other facilities, registration shall occur upon final delivery/DD250.

d. The component shall be registered in the DoD IUID Registry in accordance with the data submission procedures at http://www.acq.osd.mil/dpap/pdi/uid/data_submission_information.html. Additionally, the following shall be recorded in the "Mark Section" of the DoD IUID Registry in accordance with Guidelines for Registering Government Serialization, Type Designation and Ownership of Major End Items, Assemblies and Sub-assemblies and Capital Equipment:

Recorded as Set 1:

1. Manufacturer Serial Number (minus any spaces).

2. National Stock Number (with dashes).

3. Type Designation “UH-60” (with the dash and capital letters).

4. Service/Agency/Command “USARMY” (no space in all capital letters).

5. UII

B 1088 Rev C

Continuation Sheet

IUID DATA PLATE FABRICATION (CONT.)

Recorded as Set 2:

Component Sikorsky Part Number and CAGE Code (if marked on the component and/or component original identification data plate).

Recorded as Set 3 (If applicable):

Component Vendor Part Number and CAGE Code (if marked on the component and/or component original identification data plate).

2. If the tail rotor pylon and components within this DMWR that require IUID, have no IUID data plate, but has a UII that is registered in the DoD IUID Registry and the registry recorded data per WP 0003 00, DoD IUID REGISTRY QUERY matches the data on the component, an IUID data plate shall be fabricated using the recorded data.

a. The recorded UII shall be encoded into a 2-D data matrix. M&O of the component shall not change the UII.

As applicable, for legacy IUID data plates, the component's manufacturer serial number from the original identification data plate and/or component marking shall reside as HRI only (not encoded in the 2-D data matrix) on the IUID data plate.

b. The 2-D data matrix shall be encoded with the current Sikorsky's or Vendor's (if applicable) part number using 30P or PNR (current Part Number) as the data qualifier, as applicable. The 30P or PNR is the component's Sikorsky or Vendor (if applicable) part number upon completion of the M&O.

3. If the tail rotor pylon and components within this DMWR that require IUID have an IUID data plate and the DoD IUID Registry record data matches data on the component per WP 0003 00, DoD IUID REGISTRY QUERY but the IUID data plate must be replaced due to damage and/or change to component data (e.g., part number roll), a replacement IUID data plate shall be fabricated.

a. The recorded UII shall be encoded into a 2-D data matrix. M&O of the component shall not change the UII.

As applicable, for legacy IUID data plates, the component's manufacturer serial number from the original identification data plate and/or component marking shall reside as HRI only (not encoded in the 2-D data matrix) on the IUID data plate.

b. The 2-D data matrix shall be encoded with the current Sikorsky's or Vendor's (if applicable) part number using the 30P or PNR (current Part Number) as the data qualifier, as applicable. The 30P or PNR is the component's Sikorsky or Vendor (if applicable) part number upon completion of the M&O.

The verification for minimum print quality grade applies to compliant IUID data plates that have been removed and will be reapplied. For components having a compliant IUID data plate that is installed (is not being removed during the M&O event), the IUID data plate can remain on the component provided the 2-D data matrix passes a readability check (refer to applicable component work package application procedures).

4. If the tail rotor pylon and components within this DMWR that require IUID have an IUID data plate; is registered in the DoD IUID Registry; the registry record data matches the component data per WP 0003 00, DoD IUID REGISTRY QUERY; the IUID data plate is undamaged; no data changes are required; the IUID data plate can be reapplied to the component on which it was found at PSA, provided the MRI meets the verification requirement for minimum print quality grade per MIL-STD-130. If the 2-D data matrix does not meet the minimum grade requirements, replacement IUID data plate shall be fabricated.

Continuation Sheet

IUID DATA PLATE FABRCIATION (CONT.)

5. After fabricating an IUID data plate, use a data matrix grader/verifier (WP 0344 00, Item 67) to verify that the 2-D data matrices have a minimum print quality grade per MIL-STD-130. Validate that data encoded in the 2-D data matrix matches HRI. If the 2-D matrix data failed minimum print quality grade, repeat the applicable marking process until the minimum print quality grade has been achieved.

IUID DATA PLATE APPLICATION

For components within this DMWR that require IUID, refer to applicable work package for IUID data plate application requirements.

Helicopter IUID Data Plate (Figure 5, Detail C) and Helicopter RECAP Modification/IUID Data Plate (Figure 5, Detail D):

WARNING

Isopropyl alcohol is flammable and toxic to eyes, skin, and respiratory tract. Wear protective gloves and goggles/face shield. Avoid repeated or prolonged contact. Use only in well ventilated areas (or use approved respirator as determined by local safety/industrial hygiene personnel). Keep away from open flames, sparks, or other sources of ignition.

1. Clean the IUID data plate application area using cloth (WP 0343 00, Item 26) moistened with isopropyl alcohol (WP 0343 00, Item 59). Ensure all oils and solids are removed from application area.

2. Prior to application, ensure that the IUID data plate data is correct for the aircraft to which it will be applied.

3. Peel liner from the IUID data plate. Avoid adhesive contact with fingers. Place on the application area and firmly press from the middle out. Use a roller or cleaning cloth (WP 0343 00, Item 26) to firmly press the data plate down to ensure 100% contact and to remove any air bubbles.

4. Wipe surface of the IUID data plate with cleaning cloth (WP 0343 00, Item 26) moistened with Isopropyl alcohol (WP 0343 00, Item 59) to remove fingerprint oil, dust, lint, etc.

5. Apply a protective overcoat using matte clear polyurethane coating (WP 0343 00, Item 147) or equivalent with foam brush only (WP 0343 00, Item 148) or an equivalent. The clear polyurethane coating shall completely cover the IUID data plate and extend a minimum of 1/8 to 1/4 inch uniformly around the edges.

6. Allow the polyurethane coating to completely dry. Ensure IUID data plate edges have been secured completely.

7. Using a hand held reader (WP 0344 00, Item 66) or an equivalent; check readability of the 2-D data matrix on the IUID data plate by scanning 2 times. The time to decode any two scans shall be 15 seconds or less. Replace any data matrix that does not meet the readability criteria. Validate that all pertinent information required in the 2-D data matrix, matches the information for that component.

Continuation Sheet

A

B

A Lower Center Console

C

CAG 78286

MOD UH-60

SER XX-XXXXX

C Helicopter IUID Data Plate

Model No.

Serial No.

Mfrs. No.

Date Mfd.

Contract No.

Type Cert. No.

Prod. Cert. No.

Made in the U.S.A.

SS9026

Helicopter Nameplate

B

CONT. INSP. CUST. INSP.

AIRCRAFT MOD. UH-60L

MFR CODE 78286

CONT. NO. N/A

SERIAL NO. XX-XXXXX

SS27253-C4

MODIFICATION INCORPORATED

UH-60A RECAP/Upgrade To UH-60L

NSN: 1520-01-298-4532

Date: Aircraft Hours:

D

D

RECAP Modification/IUID Data Plate

Figure 5. Helicopter Data Plates.

B 1088 Rev C

Continuation Sheet

DRAWING NOTES:

1. Dimensions in inches.

2. The HRI shall be marked on the data plate using Laser Etch, Metal Photo or other acceptable marking technique in accordance with MIL-STD-130.

3. Font lettering and size per MIL-STD-130. Font locations are approximate.

4. Marking edge distance to be a minimum of .060 inch.

5. MATERIAL: Stainless Steel Type 301 or 302 Per MIL-S-5059, .018 in. max thickness.

Model No.

Serial No.

Mfrs. No.

Date Mfd.

Contract No.

Type Cert. No.

Prod. Cert. No.

Made in the U.S.A.

SS9026 SN B000-XXXX

3.00

4.12

.093 DIA

4 HOLES

.16

.16

.12 R TYP

Figure 6. Helicopter Nameplate Fabrication.

B 1088 Rev C

Continuation Sheet

A

B

AIRCRAFT MOD.

MFR. CODE

PART NO.

CONT. NO.

SERIAL NO.

MODIFICATION INCORPORATED

CONT.

INSP.

CUST.

INSP.

MS27253-4

AIRCRAFT MOD.

MFR:

PNO:

SEQ:

MODIFICATION INCORPORATED

CONT. INSP. CUST. INSP.

SS27253-4

OR

B

Original Identification Data Plate IUID Data Plate

AB3926

SA

Figure 7. Tail Rotor Pylon Data Plates

Figure 7. Tail Rotor Pylon Data Plates.

B 1088 Rev C

Continuation Sheet

Model No.

Serial No.

Mfrs. No.

Date Mfd.

Contract No.

Type Cert. No.

Prod. Cert. No.

Made in the U.S.A.

SS9026-3 SN B000-XXXX

Figure 9. Helicopter IUID Data Plate (OCM A and L Model Aircraft).

B 1088 Rev C

Continuation Sheet

1. All dimensions in inches.

2. Drawing not to scale.

3. IUID marking per MIL-STD-130. All font locations are approximate.

4. MATERIAL: 2024 Aluminum per ASTM B209, 1.00 in. X 2.00 in., .016 in Maximum Thickness;

adhesive-backed 3M adhesive transfer tape 467, 468 or an equivalent.

5. FINISH: Black anodize per MIL-A-8625, Type II, Class 2.

6. For metal photographic process: Use photosensitive anodized aluminum PER GG-P-455, Type I, Class 1, Grade A.

7. Quiet zone (free space) around the 2-D data matrix code shall be 0.050 inch minimum in all directions.

8. The recommended part mark size for the 2-D data matrix is 0.25 TO 0.50 inch square. The 2-D data matrix symbol shall not be larger than 1.00 inch square.

9. The 2-D data matrix contains a Construct 2 UII, using TEIs CAGE, PNO and SEQ as data qualifiers (TEIs not shown as HRI on data plate). MRI contains the helicopter’s assigned UII as recorded in the DoD IUID Registry:

CAG 78286

PNO (AIRCRAFT MODEL NO.)

SEQ (AIRCRAFT SERIAL NO.)

CAG 78286

MOD UH-60X

SER XX-XXXXX

1.00 IN.

2.00 IN.

Quiet Zone 0.050 IN.

All Directions

Figure 10. Helicopter IUID Data Plate Fabrication.

B 1088 Rev C

Continuation Sheet

2X .625

2X .094

2X .125

2-D Data Matrix

1.250

3.00

SPACES

2.18

4X ø.102 ± .004 4X R.125

MODIFICATION INCORPORATED

UH-60A RECAP/Upgrade To UH-60L

NSN: 1520-01-298-4532

Date: Aircraft Hours:

AIRCRAFT MOD. UH-60L

MFR CODE 78286

CONT. NO. N/A

SERIAL NO. XX-XXXXX

4X .125

CONT. INSP.

SS27253-C4

CONT. INSP.

DRAWING NOTES:

1. All Dimensions in inches. Tolerance: .XXX ± .010 (unless otherwise specified). Drawing not to scale.

2. The MRI and HRI shall be marked on either data plate using Laser Etch, Metal Photo or other acceptable marking technique in accordance with MIL-STD-130.

3. Font lettering and size per MIL-STD-130. Font locations are approximate.

4. MATERIAL: Corrosion resistant steel, annealed per AMS 5510 or ASTM A 240, CLASS 321, .016 in. maximum thickness; adhesive-backing using 3M 467, 3M 468, P/F American International 242-AT or an equivalent.

5. Drill holes is dependent on application requirements.

6. The 2-D data matrix symbol shall be ECC 200 compliant in accordance with ISO/IEC 16022.

7. Marking edge distance to be a minimum of .060 inch.

8. The recommended part mark size for the 2-D data matrix symbol is 0.25 to 0.50 inch square. The 2-D data matrix symbol shall not be larger that 1.00 inch square.

9. 2-D data matrix shall be printed in the location as shown. The 2-D data matrix contains a Construct 2 UII, using TEIs CAGE, PNO and SEQ as data qualifiers (TEIs not shown as HRI on data plate). MRI contains the helicopter’s assigned UII as recorded in the DoD IUID Registry:

CAG 78286

PNO (AIRCRAFT MODEL NO.)

SEQ (AIRCRAFT SERIAL NO.)

Figure 11. RECAP Modification/IUID Data Plate Fabrication.

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Continuation Sheet

1. All Dimensions in inches. Tolerance: .XXX ± .010 (unless otherwise specified). Drawing not to scale.

2. The MRI and HRI shall be marked on either data plate using Laser Etch, Metal Photo or other acceptable marking technique in accordance with MIL-STD-130.

3. Font lettering and size per MIL-STD-130. Font locations are approximate.

4. MATERIAL: Black Anodized Aluminum Sheet, 1100 Temper H-14 Aluminum Alloy per ASTM B209, .032 maximum thickness

5. FINISH: Anodize per MIL-A-8625 TYPE II, CLASS 2. Flat Black per FED-STD-595. Black anodizes plates shall be completely coated with clear polyurethane per MIL-PRF-85285 or equivalent and extend a minimum of 1/4 inch around the edges.

6. The 2-D data matrix symbol shall be ECC 200 compliant in accordance with ISO/IEC 16022.

7. Marking edge distance to be a minimum of .060 inch.

8. The recommended part mark size for the 2-D data matrix symbol is 0.25 to 0.50 inch square. The 2-D data matrix symbol shall not be larger that 1.00 inch square.

9. 2-D data matrix shall be printed in the location as shown.

10. The manufacturer 2-D data matrix contains the following MRI:

CAG (manufacturer’s CAGE code) PNO (original part number) at the time of production SEQ (manufacturer’s serial number)

11. The legacy 2-D data matrix contains the following MRI:

SPL (supplier‘s CAGE Code) UCN (supplier’s unique component number)

12. Legacy IUID Data Plate SERIAL NO: Manufacturer serial number from original identification data plate displayed as HRI only (not encoded in the 2-D data matrix).

1.250

3.00

SPACES

2.18

4X ø.102 ± .004 4X R.125

MODIFICATION INCORPORATED

CONT. INSP. CUST. INSP.

2.188

MODIFICATION INCORPORATED

AIRCRAFT MOD. UH-60

CAG:

PNO:

SEQ:

2X .625

4X .125

2X .094

2X .125

AIRCRAFT MOD. UH-60

SPL:

UCN:

SERIAL NO:

MS27253-4 SS27253-4

Manufacturer IUID Data Plate Legacy IUID Data Plate OR

2-D Data Matrix

CONT. INSP. CUST. INSP.

2-D Data Matrix

Figure 12. Tail Rotor Pylon Data Plate Fabrication.

B 1088 Rev C

Continuation Sheet

WP 0003 00 PAGE 00-3: ADD AFTER “PARTS REMOVAL AND DISASSEMBLY REQUIREMENTS” section:

“DOD IUID REGISTRY QUERY

• Do not remove IUID data plate(s) unless necessitated by damage, maintenance requirements or determination that the item does not meet the criteria below.

• Protect the IUID data plate(s) that are installed on the item during cleaning, maintenance processes and painting.

• If the item arrives with an IUID data plate(s) other than what is depicted within this DMWR, as applicable, contact cognizant AMRDEC engineering or contracting officer representation (COR) for replacement instructions.

The DoD IUID Registry via the WAWF @ https://wawf.eb.mil/ and/or AMCOM's TAMMS-A/MCDS, UID database @ https://tamms-a.redstone.army.mil, shall be queried to determine if the component has been assigned a UII.

1. Inspect the helicopter airframe (WP 0002 00, Figure 5), tail rotor pylon (WP 0002 00, Figure 7) and all other items that are contained within this DMWR for the presence of a 2-D data matrix via an IUID data plate(s).

a. If a 2-D data matrix is present, use a handheld data matrix reader (WP 0344 00, Item 66) or an equivalent and scan the 2-D data matrix. If the scan is successful, proceed to paragraph 1.d and/or 1.e. If the scan is not successful after two attempts, proceed to paragraph 1.b.

Isopropyl alcohol is flammable and toxic to eyes, skin, and respiratory tract. Wear protective gloves and goggles/face shield. Avoid repeated or prolonged contact. Use only in well ventilated areas (or use approved respirator as determined by local safety/industrial hygiene personnel). Keep away from open flames, sparks, or other sources of ignition.

b. Clean the 2-D data matrix with a cloth (WP 0343, Item 26) moistened with isopropyl alcohol (WP 0343 00, Item 59) and scan again. If the third scan is successful, proceed to paragraph 1.d and/or 1.e. If the third scan is not successful, use the HRI to query the DoD IUID Registry (paragraph d.(2)) and/or TAMMS-A/MCDS, UID database (paragraph 1.e.(2)).

c. For items that require IUID marking and that have no 2-D data matrix present (only an original nameplate or marking), proceed to paragraph d.(2) or e.(2).

d. Query the DoD IUID Registry via the WAWF (WP 0338 00, Websites) as follows:

(1) DoD IUID Registry home page, select “Queries”, then “Single Item Query” and place the recorded UII data into the “UII*” field. If the query returns a record, proceed to paragraph 1.f. If the query does not return a record, proceed to d.(2) below.

(2) Using the human readable manufacturer serial number on the component (may be indicated by SER, Serial No., Ser No., S/N, SN, SER, SEQ, etc.), query the DoD IUID Registry. Select “Queries” then “Mark Query”.

Place “SERIAL NUMBER” in the "Mark Content" field and place the manufacturer serial number (as visible on the component, minus any spaces) in the "Mark Value" field. If the record data matches the component data exactly, proceed to paragraph 1.f. If no registry record can be matched exactly to the component data, (i.e., did not have a registered UII), an IUID data plate(s) shall be fabricated IAW WP 0002 00 and the applicable component's work package.

B 1088 Rev C

Continuation Sheet

DOD IUID REGISTRY QUERY (CONT.)

e. Query the TAMMS-A/MCDS, UID database (WP 0338 00, Websites) as follows:

(1) TAMMS-A/MCDS home page, select `''Apps”, then “UID” from the drop down menu, and place the scanned/recorded UII data into the “UII” field. If the query returns a record, proceed to paragraph1.f. If the query does not return a record proceed to e.(2) below.

(2) Using the human readable manufacturer serial number on the component (indicated by Serial No., Ser No., S/N, SN, SER, (S), SEQ, etc.) query the TAMMS-A/MCDS, UID database by placing the serial number in the “SER” field. The query may return multiple records. Use the additional data from the component (component description, part number, etc.) to determine if one of the database records can be matched to the component. If a database record matches the component data exactly, proceed to paragraph1.f. If no registry record can be matched exactly to the component data, (i.e., did not have a registered UII), an IUID data plate(s) shall be fabricated IAW WP 0002 00 and the applicable component's work package.

f. Record Data.

(1) Ensure the data in the DoD IUID Registry and/or TAMMS-A/MCDS, UID database record matches the component data (resident on the component or within its accompanying historical records). If all data matches, record all pertinent component data required to fabricate the IUID data plate (UII data elements, Sikorsky or Vendor PN (if applicable) and all other data requirements resident on the component and/or in the registry record). It is necessary that all recorded data be matched to the same end item, assembly, or component on which they were found during PSA. Refer to WP 0002 00 and the component's specific work package for IUID data plate marking and fabrication requirements.

(2) If the recorded data in the DoD IUID Registry and/or TAMMS-A/MCDS, UID database record does not match the component data, (i.e., did not have a registered UII), a legacy IUID data plate shall be fabricated IAW WP 0002 00 and the applicable component's work package."

Continuation Sheet

WP 0032 00, PAGE 00-1, paragraph 1. Seat Bucket: ADD new paragraphs d. and e."

d. Inspect seat buckets for the presence of a pilot or co-pilot seat assembly IUID data plate (Figure 2). If present, refer to WP 0003 00, DOD IUID REGISTRY QUERY.

e. If IUID data plate replacement is required, refer to WP 0032 01 for IUID marking and fabrication information.

WP 0032 00, PAGE 00-1, paragraph 3. Attenuator: ADD new paragraphs d. and e."

d. Inspect attenuators for the presence of a IUID data plate (Figure 3). If present, refer to WP 0003 00, DOD

IUID REGISTRY QUERY.

e. If IUID data plate replacement is required, refer to WP 0032 01 for IUID marking and fabrication information.

WP 0032 00, PAGE 00-1, paragraph 4. Seat Frame: ADD new paragraphs d. and e."

d. Inspect seat frame for the presence of a IUID data plate (Figure 4). If present, refer to WP 0003 00, DOD

IUID REGISTRY QUERY.

e. If IUID data plate replacement is required, refer to WP 0032 01 for IUID marking and fabrication information.

WP 0032 00, PAGE 00-2

ADD new Figures 2, 3 and 4 to WP 0032 00, found on pages 17 thru 19 of this MEO.

B 1088 Rev C

Continuation Sheet

CAG 78286

PNO 70500-01151-105

SEQ B1002-10075

NOMENCLATURE: SEAT, CREW, ARMORED CRASHWORTHY

MFR P/N: (100900-11)

NSN NO: 1680-01-494-3019

SPECFICATION: MIL-S-58095 (AV)

WEIGHT: 114.9 LB

CONTRACT NUMBER:

MFR CAGE CODE: (54786) PHOENIX, AZ

AEROSPACE AND DEFENSE GROUP INC.

Figure 2. Pilot-Copilot’s Seat Assembly IUID Data Plate.

DETAIL

A

B 1088 Rev C

Continuation Sheet

NOMENCLATURE: ENERGY ATTENUATOR

PART NUMBER: 100014-X

SERIAL NUMBER: XXXXXXX

MFR CAGE CODE: (54786) PHOENIX, AZ

AEROSPACE AND DEFENSE GROUP INC.

CAGE: 54786

PART NUMBER: 100014-X

SERIAL NUMBER: XXXXXXX

WEIGHT:

ARMOR HOLDINGS

AEROSPACE & DEFENSE GROUP

Attenuators

OR

DETAIL

A

Figure 3. Attenuator IUID Data Plates.

B 1088 Rev C

Continuation Sheet

NOMENCLATURE: FRAME, ENERGY ABSORGING

PART NUMBER: 10000-3-3

NOMENCLATURE: FRAME, ENERGY ABSORBING

PART NUMBER: 100003-3

SERIAL NUMBER: XXXXXXX

WEIGHT:

ARMOR HOLDINGS

AEROSPACE & DEFENSE GROUP

OR

DETAIL

A

Figure 4. Seat Frame IUID Data Plates.

B 1088 Rev C

Continuation Sheet

ADD new work package: “WP 0032 01 PILOT'S/CO-PILOT'S SEAT ASSEMBLY IUID DATA PLATES

REPLACEMENT

INITIAL SETUP

Tools and Special Tools Epilog, CO2 Mini Laser Marking System, WP 0344 00, Item 65 or equivalent Reader, Handheld, WP 0344 00, Item 66 or equivalent

Materials/Parts Cleaning Cloth (Low Lint, Type II, A-A59323), WP 0343 00, Item 26 Isopropyl Alcohol (TT-I-735), WP 0343 00, Item 59 Coating, Polyurethane (MIL-PRF-85285, Type I, Class H), WP 0343 00, Item 147 Brush, Foam (A5281, (1HEN9)), WP 0343 00, Item 148 TESA Tape, TESA Secure 6973 PV6, WP 0343 00, Item 149

References

MIL-STD-130, WP 0338 00

IUID DATA PLATE FABRICATION

The Pilot's/Copilot's seat assemblies, attenuators and seat frame IUID data plates are fabricated out of adhesive-backed black matte anodized aluminum material or polyacrylic material that meets the physical requirements per MIL-DTL-15024, Type L. The MRI and HRI shall be marked on the IUID data plate using CO 2 Laser Etch (WP 0344 00, Item 65), Metal Photo, Thermo Transfer Printer (polyarcylic material only) or other acceptable marking technique in accordance with MIL-STD-130. Refer to Figure 1 for applicable format, configuration, material, size and fabrication requirements.

Isopropyl alcohol is flammable and toxic to eyes, skin, and respiratory tract. Wear protective gloves and approved respirator as determined by local safety/industrial hygiene personnel). Keep away from open flames, sparks, or other sources of ignition.

Quality control shall inspect the IUID data plate to ensure proper application and that the HRI and MRI match the previously recorded data for that component.

TESA application: allow TESA Tape label stock to be conditioned to room temperature. Do not attempt to apply the IUID data plate(s) when the component surface temperature is below 50° F.

1. Clean the application area on the component using cleaning cloth (WP 0343 00, Item 26) moistened with isopropyl alcohol (WP 0343 00, Item 59). Ensure all oils and solids are removed from application area.

2. Prior to application, ensure that the IUID data plate data is correct for the component to which it will be applied.

B 1088 Rev C

Continuation Sheet

WP 0032 01 PILOT'S/CO-PILOT'S ASSEMBLY IUID DATA PLATES REPLACEMENT (CONT.)

3. Peel liner from IUID data plate. Avoid adhesive contact with fingers. Place on the application area and firmly press from the middle out. Use a roller or cleaning cloth (WP 0343 00, Item 26) to firmly press the data plate down to ensure 100% contact and to remove any air bubbles.

4. Wipe surface of the IUID data plate with cleaning cloth (WP 0343 00, Item 26) moistened with isopropyl alcohol (WP 0343 00, Item 59) to remove fingerprint oil, dust, lint, etc.

5. Apply a protective overcoat using matte clear polyurethane coating (WP 0343 00, Item 147) or equivalent with foam brush only (WP 0343 00, Item 148) or an equivalent. The clear polyurethane coating shall completely cover the IUID data plate and extend a minimum of 1/4 to 1/8 inch uniformly around the edges.

6. Allow the polyurethane coating to completely dry. Ensure IUID data plate edges have been secured completely.

7. Using a hand held reader (WP 0344 00, Item 66) or an equivalent; check readability of the 2-D data matrix on the IUID data plate by scanning 2 times. The time to decode any two scans shall be 15 seconds or less. Replace any data matrix that does not meet the readability criteria. Validate that all pertinent information required in the 2-D data matrix, matches the information for that component.

ADD new Figure 1 found on pages 22 thru 24 of this MEO."

B 1088 Rev C

Continuation Sheet

CAG 78286

PNO 70500-01151-XXX

SEQ B1002-XXXXX

PNR 70500-01151-XXX

NOMENCLATURE: SEAT, CREW, ARMORED CRASHWORTHY

MFR P/N: (100900-XX)

NSN NO: 1680-01-494-3019

SPECFICATION: MIL-S-58095 (AV)

WEIGHT: 114.9 LB

CONTRACT NUMBER:

MFR CAGE CODE: (54786) PHOENIX, AZ

AEROSPACE AND DEFENSE GROUP INC.

4.00

2.00

.050 MIN QUIET ZONE

ALL DIRECTIONS

PART NUMBER: 100014-X

4.00

.050 MIN QUIET ZONE

2.00

PART NUMBER: 100014-X

SERIAL NUMBER: XXXXXXX

WEIGHT:

4.00

.050 MIN QUIET ZONE

ALL DIRECTIONS

ARMOR HOLDINGS

AEROSPACE & DEFENSE GROUP

NOMENCLATURE: FRAME, ENGERGY ABSORBING

PART NUMBER: 100003-X

4.00

.050 MIN QUIET ZONE

NOMENCLATURE: FRAME, ENERGY ABSORBING

PART NUMBER: 100003-X

SERIAL NUMBER: XXXXXXX

WEIGHT:

4.00

.050 MIN QUIET ZONE

ALL DIRECTIONS

ARMOR HOLDINGS

AEROSPACE & DEFENSE GROUP

Pilot/Copilot Seat Manufacturer IUID Data Plate (Note 12)

Attenuator Manufacturer IUID Data Plates

Seat Frame Manufacturer IUID Data Plates

Figure 1. Pilot/Co-pilot Seat Assembly IUID Data Plates (Sheet 1 of 3).

B 1088 Rev C

Continuation Sheet

SPL XXXXX

UCN XXXXXXX

PNR 70500-01151-XXX

SERIAL NO. B1002-XXXXX

NOMENCLATURE: SEAT, CREW, ARMORED CRASHWORTHY

MFR P/N: (100900-XX)

NSN NO: 1680-01-494-3019

SPECFICATION: MIL-S-58095 (AV)

WEIGHT: 114.9 LB

CONTRACT NUMBER:

MFR CAGE CODE: (54786) PHOENIX, AZ

AEROSPACE AND DEFENSE GROUP INC.

4.00

2.00

.050 MIN QUIET ZONE

PNR: 100014-X

4.00

.050 MIN QUIET ZONE

SPL: XXXXX

UCN: XXXXXXX

NOMENCLATURE: ENERGY ATTENUATOR

PART NUMBER: 100014-X

SERIAL NUMBER: XXXXXXX

WEIGHT:

4.00

.050 MIN QUIET ZONE

ALL DIRECTIONS

ARMOR HOLDINGS

AEROSPACE & DEFENSE GROUP

NOMENCLATURE: FRAME, ENGERGY ABSORBING

PNR: 100003-X

4.00

.050 MIN QUIET ZONE

SPL: XXXXX

UCN: XXXXXXX

NOMENCLATURE: FRAME, ENERGY ABSORBING

PART NUMBER: 100003-X

SERIAL NUMBER: XXXXXXX

WEIGHT:

4.00

.050 MIN QUIET ZONE

ALL DIRECTIONS

ARMOR HOLDINGS

AEROSPACE & DEFENSE GROUP

Pilot/Copilot Seat Legacy IUID Data Plate

Attenuator Legacy IUID Data Plates

Seat Frame Legacy IUID Data Plates

11 10

11 10

Figure 1. Pilot/Co-pilot Seat Assembly IUID Data Plates (Sheet 2 of 3).

B 1088 Rev C

Continuation Sheet

NOTES:

1. All Dimensions in inches. Drawing not to scale.

2. Font lettering and size per MIL-STD-130. Font locations are approximate.

3. Physical characteristics and test requirements per MIL-DTL-15024, Type L.

4. Materials: Black matte anodized aluminum .003 to .005 thickness, with 9485PC adhesive tape

(3M) or TESA Tape, TESA Secure 6973 PV6, matte black top layer with white under layer or an polyacrylic material equivalent. Data plate shall be completely coated with clear polyurethane per MIL-PRF-85285 or equivalent and extend a minimum of 1/4 inch around the edges.

5. The 2-D data matrix symbol shall be ECC 200 compliant in accordance with ISO/IEC 16022.

6. Quiet Zone (Free Space) around the 2-D data matrix code shall be .050 MIN. in all directions.

7. Marking edge distance to be a minimum of .060.

8. The recommended part mark size for the 2-D data matrix symbol is 0.25 to 0.50 inch square.

The 2-D data matrix symbol shall not be larger that 1.00 inch square.

2-D data matrix encoded with a Construct 2 UII using TEIs CAG (manufacturer’s CAGE Code), PNO (original part number) and SEQ (manufacturer’s serial number).

2-D data matrix encoded with a Construct 1 UII using TEIs SPL (CAGE Code of the entity supplying the UII) and UCN (Unique Component Number of the entity supplying the UII).

2-D data matrix encoded with Sikorsky’s or Vender’s current part number using TEI PNR.

PNR being Sikorsky’s or Vendor’s current part number upon completion of an M&O event.

Figure 1. Pilot/Co-pilot Seat Assembly IUID Data Plates (Sheet 3 of 3).

B 1088 Rev C

Continuation Sheet

WP 0033 00, page 0033 00-2:

REPLACE Figure 1 with new found on page 26 of this MEO.

ADD new Figure 2 found on page 27 of this MEO after Figure 1.

Page 0033 00 00-7:

CHANGE "(Figure 2)" in paragraph 24.a to read: "(Figure 3)".

ADD the following paragraphs:

"25. Left and Right Engine Air Inlets:

a. Inspect engine air lets for the presence IUID data plate (Figure 2). If present, refer to WP 0003 00, DOD

IUID REGISTRY QUERY.

b. If IUID data plate replacement is required, refer to WP 0033 01 for IUID marking and fabrication information.

Page 0033 00 00-8:

CHANGE reference to "Figure 2" in figure title to read: "Figure 3".

Continuation Sheet

Figure 1. Main Rotor Pylon.

B 1088 Rev C

Continuation Sheet

NOTE:

The manufacturer PNR data plate application is only utilized/installed on the component when the original part number PNO changes with a new configuration, i.e.

part number roll (dash number change).

DETAIL A

A 25

CAG 78286

PNO 70302-302100-XXX

SEQ XXXX-XXXXX

PNR 70302-302100-XXX

B

B

Figure 2. Engine Air Inlet IUID Data Plate.

B 1088 Rev C

Continuation Sheet

ADD new work package: “WP 0033 01 LEFT/RIGHT ENGINE AIR INLET IUID DATA PLATES REPLACEMENT

INITIAL SETUP

Tools and Special Tools Epilog, CO2 Mini Laser Marking System, WP 0344 00, Item 65 or equivalent Reader, Handheld, WP 0344 00, Item 66 or equivalent

Materials/Parts Cleaning Cloth (Low Lint, Type II, A-A59323), WP 0343 00, Item 26 Isopropyl Alcohol (TT-I-735), WP 0343 00, Item 59 Coating, Polyurethane (MIL-PRF-85285, Type I, Class H), WP 0343 00, Item 147 Brush, Foam (A5281, (1HEN9)), WP 0343 00, Item 148 TESA Tape, TESA Secure 6973 PV6, WP 0343 00, Item 149

References

MIL-STD-130, WP 0338 00

IUID DATA PLATE FABRICATION

The engine air inlet IUID data plates are fabricated out of adhesive-backed black matte anodized aluminum material or polyacrylic material that meets the physical requirements per MIL-DTL-15024, Type L. The MRI and HRI shall be marked on the IUID data plate using CO 2 Laser Etch (WP 0344 00, Item 65), Thermo Transfer Printer (polyarcylic material only) or other acceptable marking technique in accordance with MIL-STD-130. Refer to Figure 2, for format/configuration, material, size and fabrication requirements.

Isopropyl alcohol is flammable and toxic to eyes, skin, and respiratory tract. Wear protective gloves and approved respirator as determined by local safety/industrial hygiene personnel). Keep away from open

Quality control shall inspect the IUID data plate to ensure proper application and that the HRI and MRI

Allow TESA Tape label stock to be conditioned to room temperature. Do not attempt to apply the IUID data plate(s) when the component surface temperature is below 50° F.

1. Clean the application area on the component using cleaning cloth (WP 0343 00, Item 26) moistened with isopropyl alcohol (WP 0343 00, Item 59). Ensure all oils and solids are removed from application area.

2. Prior to application, ensure that the IUID data plate data is correct for the component to which it will be applied.

B 1088 Rev C

Continuation Sheet

WP 0033 01 LEFT/RIGHT ENGINE AIR INLET IUID DATA PLATES REPLACEMENT (CONT.)

3. Peel liner from IUID data plate. Avoid adhesive contact with fingers. Place on the application area and firmly press from the middle out. Use a roller or cleaning cloth (WP 0343 00, Item 26) to firmly press the data plate down to ensure 100% contact and to remove any air bubbles.

4. Wipe surface of the IUID data plate with cleaning cloth (WP 0343 00, Item 26) moistened with isopropyl alcohol (WP 0343 00, Item 59) to remove fingerprint oil, dust, lint, etc.

5. Apply a protective overcoat using matte clear polyurethane coating (WP 0343 00, Item 147) or equivalent with foam brush only (WP 0343 00, Item 148) or an equivalent. The clear polyurethane coating shall completely cover the IUID data plate and extend a minimum of 1/4 to 1/8 inch uniformly around the edges.

6. Allow the polyurethane coating to completely dry. Ensure IUID data plate edges have been secured completely.

7. Using a hand held reader (WP 0344 00, Item 66) or an equivalent; check readability of the 2-D data matrix on the IUID data plate by scanning 2 times. The time to decode any two scans shall be 15 seconds or less. Replace any data matrix that does not meet the readability criteria. Validate that all pertinent information required in the 2-D data matrix, matches the information for that component.

ADD new Figure 1 found on page 30 of this MEO."

B 1088 Rev C

Continuation Sheet

1.50

.050 MIN QUIET ZONE

ALL DIRECTIONS 10

PNR 70302-30100-XXX

.09 R TYP

4 PLS

SS9143-A (NOTE 12)

Manufacturer/Legacy

0.50

1.50

.050 MIN QUIET ZONE

ALL DIRECTIONS 9

CAG 78286

PNO 70302-30100-XXX

SEQ XXX-XXXXX

SS9143-A

Manufacturer

.09 R TYP

4 PLS

0.50

1.50

.050 MIN QUIET ZONE

ALL DIRECTIONS

SPL XXXXX

UCN XXXXXXX

SER NO XXX-XXXXX

SS9143-A

Legacy

NOTES:

1. All Dimensions in inches. Drawing not to scale.

2. Font lettering and size per MIL-STD-130. Font locations are approximate.

3. Physical characteristics and test requirements per MIL-DTL-15024, Type L.

4. SS9143-A Material: TESA Tape, TESA Secure 6973 PV6, matte black top layer with white under layer or an polyacrylic material equivalent and shall be completely coated with clear polyurethane per MIL-PRF-85285 or equivalent and extend 1/16 to 1/8- inch around the edges.

5. The 2-D data matrix symbol shall be ECC 200 compliant in accordance with ISO/IEC 16022.

6. Quiet Zone (Free Space) around the 2-D data matrix code shall be .050 MIN. in all directions.

7. Marking edge distance to be a minimum of .060.

8. The recommended part mark size for the 2-D data matrix symbol is 0.25 to 0.50 inch square. The 2-D data matrix symbol shall not be larger that 1.00 inch square.

2-D data matrix encoded with a Construct 2 UII using TEIs CAG (manufacturer’s CAGE Code), PNO (original part number) at the time is was marked and SEQ (manufacturer’s serial number).

The 2-D data matrix encoded with Sikorsky’s part number using TEI PNR. PNR being the Sikorsky current part number upon completion of the M&O event.

2-D data matrix encoded with a Construct 1 UII using TEIs SPL (CAGE Code of the entity supplying the UII) and UCN (Unique Component Number of the entity supplying the UII).

12. Manufacturer PNR: The PNR data plate application is only utilized/installed on the component when the original part number PNO changes with a new configuration, i.e. part number roll (dash number change).

Figure 2. Engine Air Inlet Assembly IUID Data Plate Fabrication.

B 1088 Rev C

Continuation Sheet

WP 0035 00, PAGE 00-5, paragraph 11. Servo Beam Fittings and Vertical Tees: ADD new paragraphs 11.k. and 11.l.

"k. Inspect servo beam fittings for the presence of an IUID data plate (Figure 2). If present, refer to WP 0003

00, DOD IUID REGISTRY QUERY.

l. If IUID data plate replacement is required, refer to WP 0148 01 for IUID marking and fabrication information.

PAGE 00-20:

ADD new Figure 2 found on page 32 of this MEO to WP 0035 00 after Figure 1 (Sheet 8 of 8).

Continuation Sheet

SERVO BEAM FITTING, 70209-22103-069 AND -071

SERVO BEAM FITTING, 70209-22103-065

SERVO BEAM FITTING, 70209-22103-067

CAG 78286

PNO 70209-22103-XXX

SEQ A338-XXXXXXX

PNR 70209-22103-XXX

NOTE:

The manufacturer PNR data plate application is only utilized/installed on the component when the original part number PNO changes with a new configuration, i.e.

part number roll (dash number change).

Figure 2. Servo Beam Fittings IUID Data Plate.

B 1088 Rev C

Continuation Sheet

WP 0066 00

PAGE 00-1: ADD new Figure 2 found on page 34 of this MEO.

PAGE 00-3: ADD new paragraphs 7.f. and 7.g. as follows:

f. Inspect stabilator amplifiers for the presence of an IUID data plate (Figure 2). If present, refer to WP 0003 00, DOD IUID REGISTRY QUERY.

g. If IUID data plate replacement is required, refer to WP 0066 01 for IUID marking and fabrication information.

B 1088 Rev C

Continuation Sheet

NOTE:

The manufacturer PNR or 30P data plate application is only utilized/installed on the component where the original part number PNO or 1P changes with a new configuration, i.e. part number roll (dash number change).

CAG or (17V) 78286

PNO or (1P) 70209-02001-XXX

SEQ or (S) A338-XXXXXXX

PNR or (30P) 70209-02001-XXX

A

7 7

A

Figure 2. Stabilator Amplifiers IUID Data Plate.

B 1088 Rev C

Continuation Sheet

ADD new work package: “WP 0066 01 STABILATOR AMPLIFIERS IUID DATA PLATE REPLACEMENT

INITIAL SETUP

Tools and Special Tools Epilog, CO2 Mini Laser Marking System, WP 0344 00, Item 65 or equivalent Reader, Handheld, WP 0344 00, Item 66 or equivalent

Materials/Parts Cleaning Cloth (Low Lint, Type II, A-A59323), WP 0343 00, Item 26 Isopropyl Alcohol (TT-I-735), WP 0343 00, Item 59 Coating, Polyurethane (MIL-PRF-85285, Type I, Class H), WP 0343 00, Item 147 Brush, Foam (A5281, (1HEN9)), WP 0343 00, Item 148 TESA Tape, TESA Secure 6973 PV6, WP 0343 00, Item 149

References

MIL-STD-130, WP 0338 00

IUID DATA PLATE FABRICATION

The engine air inlet IUID data plates are fabricated out of adhesive-backed black matte anodized aluminum material or polyacrylic material that meets the physical requirements per MIL-DTL-15024, Type L. The MRI and HRI shall be marked on the IUID data plate using CO 2 Laser Etch (WP 0344 00, Item 65), Metal Photo, Thermo Transfer Printer (polyarcylic material only) or other acceptable marking technique in accordance with MIL-STD-130.

Refer to Figure 2, for format/configuration, material, size and fabrication requirements.

Isopropyl alcohol is flammable and toxic to eyes, skin, and respiratory tract. Wear protective gloves and approved respirator as determined by local safety/industrial hygiene personnel). Keep away from open

Quality control shall inspect the IUID data plate to ensure proper application and that the HRI and MRI

TESA Tape application: Allow TESA Tape label stock to be conditioned to room temperature. Do not attempt to apply the IUID data plate(s) when the component surface temperature is below 50° F.

1. Clean the application area on the component using cleaning cloth (WP 0343 00, Item 26) moistened with isopropyl alcohol (WP 0343 00, Item 59). Ensure all oils and solids are removed from application area.

2. Prior to application, ensure that the IUID data plate data is correct for the component to which it will be applied.

B 1088 Rev C

Continuation Sheet

WP 0066 01 STABILATOR AMPLIFIERS IUID DATA PLATE REPLACEMENT (cont.)

3. Peel liner from IUID data plate. Avoid adhesive contact with fingers. Place on the application area and firmly press from the middle out. Use a roller or cleaning cloth (WP 0343 00, Item 26) to firmly press the data plate down to ensure 100% contact and to remove any air bubbles.

4. Wipe surface of the IUID data plate with cleaning cloth (WP 0343 00, Item 26) moistened with isopropyl alcohol (WP 0343 00, Item 59) to remove fingerprint oil, dust, lint, etc.

5. Apply a protective overcoat using matte clear polyurethane coating (WP 0343 00, Item 147) or equivalent with foam brush only (WP 0343 00, Item 148) or an equivalent. The clear polyurethane coating shall completely cover the IUID data plate and extend a minimum of 1/4 to 1/8 inch uniformly around the edges.

6. Allow the polyurethane coating to completely dry. Ensure IUID data plate edges have been secured completely.

7. Using a hand held reader (WP 0344 00, Item 66) or an equivalent; check readability of the 2-D data matrix on the IUID data plate by scanning 2 times. The time to decode any two scans shall be 15 seconds or less. Replace any data matrix that does not meet the readability criteria.