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%rZ' r-*Crfr¿ *¡t,t*,u¿, cc ed,ta'DCI Aerotech Division of Detroit

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UNITEÞ STATES OF AMERICA

DEPARTMENT OF TRANSPORTATIONFEDERAL AVIATION ADM IN ISTRATTON

REPAIR STATION

oor;tÁ,,tÁ,u fi.//o*lny,cra,â'zyø, ..

LIMITED NON-DESTRUCTIVE TESTINGLIMITED SPECIALIZED SERVICELIMITED LANDING GEAR

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September 3.2008 Steven F. Talbott, Manager, EM FSDOA June 23,2014

Ghig €ntiñcsts tg not Gtsnsfngblt, rm rily rÈon su¡cE rì rHE rlsrc FrcrurEs, oR n rHE roc^nor THEREoF,SHATI ¡E ITTEOIAIETY NEPORÍED TO THE IPPROPNIAIE NEGIOIII! O;fICE OF THE FEDERAT TYIATIOi ADTIIIISTRATIOII

Any alaerøtion ol this certíficate is punísløble by a fine ol not erceed,ins 81,000, or ùnprisownent not excee¿ling 3 years, or both

""/"ú ¿u¿/Lendedt on,ø to/*d,INDEFINITELY

FAA Form 8(xþ{ (r-{7) SUPERSEDES FAA FORM 390.

Performance Review Institute (PRI) | 161 Thorn Hill Road | Warrendale, PA 15086-7527

Joseph G. PintoVice President and Chief Operating Of� cerJoseph G. Pinto

In accordance with SAE Aerospace Standard AS7003, to the revision in effect at the time of theaudit,this certificate is granted and awarded by the authority of the Nadcap Management Council to:

DCI Aerotech Div. of Detroit Chrome Inc

7515 Lyndon Ave Detroit, MI 48238

United States

This certificate demonstrates conformance and recognition of accreditation for specific services, aslisted in www.eAuditNet.com on the Qualified Manufacturers List (QML), to the revision in effect at the

time of the audit for:

Aerospace Quality System (AC7004)

Certificate Number: 3616162492Expiration Date: 30 April 2018


Joseph G. PintoExecutive Vice President and Chief Operating Of� cerJoseph G. Pinto

This certificate is granted and awarded by the authority of the Nadcap Management Council to:



United States



Chemical Processing

Certificate Number: 3616157627Expiration Date: 31 July 2017






United States



NonDestructive Testing

Certificate Number: 3616158989Expiration Date: 30 April 2017






United States



Conventional Machining as a Special Process

Certificate Number: 3616165623Expiration Date: 31 January 2018






United States



Surface Enhancement

Certificate Number: 3616154814Expiration Date: 31 October 2016






United States



Coatings

Certificate Number: 3616167508Expiration Date: 31 January 2017

SCOPE OF ACCREDITATION


DCI Aerotech Div. of Detroit Chrome Inc 7515 Lyndon Ave Detroit, MI 48238

This certificate expiration is updated based on periodic audits. The current expiration date and scopeof accreditation are listed at: www.eAuditNet.com - Online QML (Qualified Manufacturer Listing).

In recognition of the successful completion of the PRI evaluation process, accreditation is granted to

this facility to perform the following: AC7126 Rev B - Nadcap Audit Criteria for Conventional Machining as a Special Process(Holemaking, Broaching, Turning, Milling, Grinding, Edge Treatment) AC7126/5 Rev A - Nadcap Audit Criteria for Grinding General Grinding Grinding of Coatings

t-frm-17 17-Jun-10

s-frm-48 Page 1 of 3 01-Mar-16

PERFORMANCE REVIEW INDUSTRY MANAGED PROGRAMS Use of the Mark of Conformity, Program Certificate and Program Name The Performance Review Institute (PRI) has Marks of Conformity that are to be used to clearly indicate the program to which conformance has been demonstrated. The Marks of Conformity are proprietary and pending registration with the United States Patent Office under the terms of USCC 1051 et.al (Trademark Act of 1946, Lanham Act). RULES AND REGULATIONS OF USAGE 1. Use of the appropriate Mark is delegated, in writing, to companies that have been

awarded a Program Certificate of Accreditation/Conformance or to companies and/or their products and/or processes listed on the PRI Qualified Products List (QPL).

2. When using the Mark of Conformity, the company shall be responsible for ensuring

the audit program (i.e., Heat Treating, Nondestructive Testing, Chemical Processing) or QPL standard/specification (i.e., AMS-S-8802, AS1339) is clearly identified along with the Mark.

3. The Mark of Conformity may be used on company letterhead, fax cover sheets,

business cards and other business stationary. The Mark of Conformity may be used in advertising such as web site, flyers, mailings, paid advertisements in magazines and trade publications, company promotional materials and company souvenirs.

4. When not in conflict with customer requirements, the Mark of Conformity may be

applied directly to products and/or their associated test reports for products/ processes that are listed in the PRI QPL.

5. Neither the Mark of Conformity, nor the Program Certificate nor the Program Name

shall be used in such a manner that confusion arises between certified and non-certified products, processes, or services to which the accreditation, qualification, or approval applies.

6. In every case, the Supplier shall take sufficient care in publications and advertising so

that no confusion arises about the scope of accreditation, qualification, or approval as it applies to products, process, and services.

7. The Mark of Conformity is not to be transferred from one entity to another.

Companies with multiple facilities or locations must indicate which facility or location is accredited, qualified or approved. Companies must ensure that when advertising accreditation, qualification or approval, the specific locations are identified and that no confusion arises in statements and/or promotional literature that indicate all or multiple facility accreditation, qualification or approval.


8. The Program accreditation or PRI QPL listing is valid through the expiration date indicated on the Certificate of Accreditation or formal qualification / approval letter. If the accreditation, qualification or approval is suspended, revoked for cause, or is not renewed, the Supplier is responsible to immediately cease using the Mark of Conformity, Program Certificate and/or Program Name, distributing literature or other materials which carry the Mark of Conformity.

9. Camera-ready artwork of the Mark of Conformity will be issued concurrently with the PRI accreditation, qualification or approval certificate/notification. Electronic file is available upon request. Contact the commodity specific CSR via phone or email, contact information can be found using the ‘Contact Us’ link on eAuditNet or the PRI Website.

10. PRI may employ reasonable surveillance to ensure proper use of the Mark of

Conformity, Program Certificate and Program Name. Improper or misleading references to the program, the certificate or the Mark that are found on products in advertisements, brochures, or other publications, will be subject to corrective actions that could include legal actions, publication of the violation via the Qualified Manufacture List (QML), and/or the Qualified Products List (QPL), and suspension or revocation of accreditation, qualification, or approval.

11. When using the Mark of Conformity, it shall appear as follows: For PRI Nadcap Qualified Manufacturers:

+ (INSERT APPLICABLE PROCESS (ES) / PRODUCT HERE)

TITLES: Aerospace Quality Systems ISO/IEC 17025 Chemical Processing Materials Testing Laboratory Coatings Measurement and Inspection Composites Nonconventional Machining Conventional Machining as a Special Process Nondestructive Testing Elastomer Seals Non Metallic Materials Manufacturing Electronics Non Metallic Materials Testing Etch Sealants Fluid Distribution Systems Surface Enhancement Heat Treating Welding


For PRI Qualified Products:

(INSERT QPL NUMBER HERE) “QPL – Spec/Standard”, e.g., PRI-QPL-AS1339, PRI-QPL-AMS-S-8802NOTE: Font is recommended to be Univers and the type sizes are 16pt, 13pt, 12pt, 9 pt, and 7pt

For PRI Brake Lining Materials:

Doing Business with BoeingApproved Process Sources D1-4426

Doing Business with Boeing HomeClose

Approved Process Sources D1-4426

Boeing Approved Process Sources - Home

Nadcap Accreditation

Notes & Exceptions

Revision Summary

User Instructions & Requirements

Approved Sources Flow Chart

Approved Processors

Geographic APL

Process Code Listing

Specification Index Listing

Limitation Index

Boeing Contacts

Authorized Distributors of Aircraft Bearings

Authorized Distributors of Designated Fasteners

Document D1-4426 - Processes for BE10360948

Processor Approval Status Updated DailyRevision IN - December 01, 2014

Detail Information for Processor Code number: BE10360948Supplier Name: DCI AEROTECH DIV OF DETROIT CHROME INCAddress: 7515 LYNDON AVE,

City/town: DETROIT

Province/state: MI 48238-2481

Country: UNITED STATES

Area: MI

Contact Name: David Thompson

Title: QA Director

Phone: 602-431-4403

Fax: 602-431-4435

* An acronym in the "Nadcap Commodity" column only indicates that Nadcap accreditation may be required for this Process Code. It does not provide any indication of this company's actual Nadcap accreditation status.

Process Code

*NadcapCommodity

Limitation Codes Doc Notes Nomenclature Specification

Number

001 AQS None None

Boeing approved QMS as defined in D1-4426 Processor Requirements Sec 6.15.1

Quality System

350 CP None . Chromium- Plating QQ-C-320

350B CP None . Chromium Plating (Electrodeposited)

AMS-QQ-C-320

351 CP None Tank #1 OnlyHard Chromium Plating - Class 1 and 2

BAC 5709

353 CP None Tank #1 OnlyHard Chromium Plating - Class 4 (QPL)

BAC 5709

355 CP None None Copper Plating MIL-C-14550

366 CP None Classes 1 & 2 Electroless Nickel Coatings MIL-C-26074

802 MTL A3 Bend testing only

Mechanical Testing - Metallic

Mech. Testing

803 MTL A3 Microhardness only

Metallurgical Testing Met. Testing

809 CP A3 None Process Solution Control

Chem. Testing

810 CP A3 None Salt Spray Testing ASTM-B-117

Page 1 of 2D14426

12/10/2014file:///C:/Users/DAVE~1.THO/AppData/Local/Temp/9TN74FLN.htm

M325 CP None None Chemical Film - Aluminum (Immersion Application Only) (QPL)

HP4-57

M335 CP None None Silver Plating (QPL) HP4-17

M341 CP None None Cadmium Plating (QPL) HP4-11

M344 CP None NoneCadmium - Titanium Plating (QPL)

HP4-125

M347 CP None None Brush Plating (QPL) HP4-113

M400 NDT None None Magnetic Particle Inspection (QPL) HP6-5

Copyright ©2010 The Boeing Company - All rights reserved Security Agreement

Page 2 of 2D14426

12/10/2014file:///C:/Users/DAVE~1.THO/AppData/Local/Temp/9TN74FLN.htm

© 2013 MOOG INC. ALL RIGHTS RESERVED.

Find by Supplier Name:

Find by Approved Specification:

AMS 2417 AMS 2424 AMS 2649 AMS-A-8625AMS-QQ-P-416 ASTM 967 ASTM E1417 ASTM E1444EP3647 MIL-C-13924 MIL-DTL-16232 MIL-PRF-22750MIL-PRF-23377 MIL-STD-867 QQ-C-320 QQ-P-416SAE AMS 2404 SAE-AMS2418 SAE-AMS2485 SAE-AMS2649SAE-AMS-QQ-P-35 SAE-AMS-QQ-P-416 SAE-AMS-S-13165 SBC00SQR-1

Search for ASPSs

DETROIT CHROME INC.

DETROIT , MI

UNITED STATESPhone:Fax:Contact:Approved Specs

SUPPLIERS OVERVIEW

UNITED STATES

UNITED KINGDOM

GERMANY

INDIA

IRELAND

LUXEMBOURG

PHILIPPINES (BAGUIO)

ABOUT MOOG PRIVACY POLICY CONTACT US CAREERS

WORLDWIDELOCATIONS

Search this site

SUPPLIERS INVESTORS NEWS & EVENTS CONTACT US PARTNER LOGIN

HOME MARKETS PRODUCTS UNIQUE CAPABILITIESSERVICES ABOUT MOOG CAREERS

Hard Chrome

Thin Dense Chrome

Cadmium Electroless

Nickel Sulfamate

Nickel Gold Silver Copper Lead Tin Zinc Indium

Nadcap X X X X X X X X X X X X FAA Repair

Station X X X X X X X X X X X X

AAR Cargo X X X X X X X X X X X

Goodrich Cargo X X X X X X X X X X X X

Boeing X X X X

Curtiss Wright X X X X X

Eaton X X X X X X X X X X X X

GE Aircraft X X X* X X X X

Global Tooling X X Hamilton

Sundstrand X X X X X X X X X X X

Lockheed Martin X

Lycoming X X X

Moog X X X X X

Parker X X X X X

Rolls Royce CA X X X X X X X X

Rolls Royce UK X X X X X X X X

Rolls Royce US X X X X X X X X

Vickers X X X X X Williams

International X X X X X X X X X X X

PLATING APPROVALS

Page 1 of 4

DCI Aerotech 7515 Lyndon Ave.

Detroit, MI 48238

(313) 341-9478

Fax (313) 341-0315

AEROSPACE QUALITY SYSTEMS

CHEMICAL PROCESSING

NONDESTRUCTIVE TESTING

SURFACE ENHANCEMENT

DCI Aerotech A Division of Detroit Chrome

Special Process Approval*

Alloy Plating Approvals Page 2 of 4 DCI Aerotech

A Division of Detroit Chrome

Bronze

Nickel Cadmium Diffused

Ti-Cad Lead Indium

Diffused Lead Tin Zinc Nickel Shotpeen

Nadcap X X X X X X X FAA Repair Station

X X X X X X X

AAR Cargo

Goodrich Cargo X X X X X X X

Boeing

Curtiss Wright

Eaton X X X X X X X

GE Aircraft Hamilton Sundstrand

X X X

HR Textron

Lycoming

Moog X X

Parker X

Rolls Royce UK X

Rolls Royce US X

Vickers X Williams International

X X X X


Detroit, MI 48238

(313) 341-9478

Fax (313) 341-0315


CHEMICAL PROCESSING


SURFACE ENHANCEMENT

of 4 A Division of Detroit Chrome

DCI Aerotech Nondestructive Testing Approvals

Magnetic Particle

Inspection

Liquid Penetrant Inspection

Temper Etch Inspection

Pre-Penetrant

Etch Passivation

Nadcap X X X X X

FAA Repair Station X X X X

AAR Cargo X X X

Goodrich Cargo X X X X X

Curtiss Wright X X

Eaton X X X X X

GE Aircraft X* X*

Hamilton Sundstrand X X X X X

Moog X X X X

Lockheed Martin X

Lycoming X X X

Parker X X X

Rolls Royce UK X X

Rolls Royce US X

Siemens, FL X*

Vickers X X X

Williams International X X X X X


Detroit, MI 48238

(313) 341-9478

Fax (313) 341-0315

Approval Pending


CHEMICAL PROCESSING


SURFACE ENHANCEMENT

Special Process Approval*

Surface Coatings

Prime & Paint

Dry Film Lube

Enamel Coating

Chemical Conversion

Coating

Manganese Phosphate

Zinc Phosphate

Heavy Zinc Phosphate

Titanium Fluoride

Phosphate Black Oxide

Nadcap X X X X X X X X X FAA Repair Station

X X X X X X

AAR Cargo X X X X X

Goodrich Cargo X X X X X X X X X

Boeing

Curtiss Wright X

Eaton X X X X X X X X X

GE Aircraft X Hamilton Sundstrand

X X X

HR Textron

Lockheed Martin X

Moog X X

Rolls Royce CA X

Rolls Royce UK X X X X X

Rolls Royce US X

Vickers X X X Williams International

X X X X X X X X X

Page 4 of 4 A Division of Detroit Chrome

DCI Aerotech


Detroit, MI 48238

(313) 341-9478

Fax (313) 341-0315


CHEMICAL PROCESSING


SURFACE ENHANCEMENT

GE Transportation

Aviation

Special Process Certification

Supplier DETROIT CHROME ELECT FOB

AE Supplier Code T2986

Issue Date Sep-16-2015

Street Number 7515 LYNDON AVE

Street DETROIT, MI

City DETROIT

State MI

Country USA

Zip 48238

Attention THOMPSON, DAVID

Code - Name ofProcess

Category Supplier Tech. Rep. Specification Approvals

1 2

DB - Plating X Approved for Bronze Plating (DB09) per AMS-2429;

Chromium Plating (DB01) per AMS-2406, AMS 2460 (QQ-

C-320); Copper Plating (DB07) per AMS-2418; Nickel

Plating (DB02) per AMS 2403; Electroless-Nickel Plating

(DB03) per AMS-2404; Silver Plating (DB05) per AMS-

2410, 2412; QQ-S-365; S-414.

DK -

Stripping/Leeching

X Approved for Chemical Stripping or Leaching (DK00) per

P4-TE20, P4TF5, MIL-STD-871.

DO - Coating,

Black Oxide

X Approved for Black Oxide Conversion Coating (DO00) per

MIL-DTL-13924, AMS 2485, S-414.

Remarks: Certification issued in recognition of Nadcap accreditation.

This is to certify that a review has been completed of your technical resources and quality system controls used for the above named process(es) and

found them to be capable of satisfying the requirements of the above specifications, subject to the limitations in AE Quality Specification S-1000 for

Category I or II Suppliers.This a does not in itself constitute a waiver of specification requirements as to inspection, testing, maintenance of records,

and/or other provisions of the Purchase Order/Sub Contract, nor does it guarantee the acceptance of articles produced for the General Electric

Company. Requirements for the submission and qualification of individual parts/samples or other items as contained in specifications, engineering

drawings or Purchase Order will be completed as outlined. Inspection of the facilities for which this certification is granted may be conducted at any

time by an Aviation Representative to determine continued compliance with Aviation requirements.

The Certification shall expire at the end of Jul-31-2017 unless canceled by an Aviation representative.

Signature PLOUCHA, MICHAEL

One Neumann Way; MD J22

Source Code : T2986; Issue Date: Sep-16-2015;Page 1 of 2

Evendale, Ohio USA 45215-1988 Telephone: +1 513 243 6362

Unit SOURCING QUALITY

Title GET, AE Quality Auditor

One Neumann WayCincinnati,Ohio 45215Telephone

GT193 (1/10/00)

Source Code : T2986; Issue Date: Sep-16-2015;Page 2 of 2

GE Transportation

Aviation

Special Process Certification

Supplier DETROIT CHROME ELECT FOB

AE Supplier Code T2986

Issue Date May-02-2016

Street Number 7515 LYNDON AVE

Street DETROIT, MI

City DETROIT

State MI

Country USA

Zip 48238

Attention THOMPSON, DAVID

Code - Name ofProcess

Category Supplier Tech. Rep. Specification Approvals

1 2

AB - Inspection,

Magnetic Particle

X Approved for P3TF9, P3TF44, P3TF48, NAS410 Approved

Level III: Sheldon Emmanuel

Remarks: Certification issued in recognition of Nadcap accreditation.

Please note: Next Nadcap assessment must include GE supplemental questions.

Any changes in the listed approved Level III should be communicated immediately to GE-A, to the attention of Michael Dragon at

[email protected] or 513-552-4521.

This is to certify that a review has been completed of your technical resources and quality system controls used for the above named process(es) and

found them to be capable of satisfying the requirements of the above specifications, subject to the limitations in AE Quality Specification S-1000 for

Category I or II Suppliers.This a does not in itself constitute a waiver of specification requirements as to inspection, testing, maintenance of records,

and/or other provisions of the Purchase Order/Sub Contract, nor does it guarantee the acceptance of articles produced for the General Electric

Company. Requirements for the submission and qualification of individual parts/samples or other items as contained in specifications, engineering

drawings or Purchase Order will be completed as outlined. Inspection of the facilities for which this certification is granted may be conducted at any

time by an Aviation Representative to determine continued compliance with Aviation requirements.

The Certification shall expire at the end of Apr-30-2017 unless canceled by an Aviation representative.

Signature PLOUCHA, MICHAEL

One Neumann Way; MD J22 Evendale, Ohio USA 45215-1988 Telephone: +1 513 243 6362

Unit SOURCING QUALITY

Source Code : T2986; Issue Date: May-02-2016;Page 1 of 2

Title GET, AE Quality Auditor

One Neumann WayCincinnati,Ohio 45215Telephone

GT193 (1/10/00)

Source Code : T2986; Issue Date: May-02-2016;Page 2 of 2

SCOPE OF ACCREDITATIONChemical Processing

DCI Aerotech Div. of Detroit Chrome Inc7515 Lyndon Ave Detroit, MI 48238

This certificate expiration is updated based on periodic audits. The current expiration date and scope of accreditation are listed at: www.eAuditNet.com - Online QML (Qualified

Manufacturer Listing).

In recognition of the successful completion of the PRI evaluation process, accreditation is granted to this facility to perform the following:

AC7108 Rev D - Nadcap Audit Criteria for Chemical Processing Alloy Plating – AMS 2415 Alloy Plating – AMS 2416 Alloy Plating – AMS 2417 Alloy Plating – AMS-P-81728 Alloy Plating – MIL-P-81728 Alloy Plating – MIL-STD-1500 Alloy Plating – Other Alpha Case Removal (This addresses the removal process only and not the evaluation process) Anodizing – Other Brush Plating – Other Cadmium Plating – AMS 2400 Cadmium Plating – AMS 2401 Cadmium Plating – AMS 2419 Cadmium Plating – AMS-QQ-P-416 Cadmium Plating – MIL-STD-870 Cadmium Plating – Other Cadmium Plating – QQ-P-416 Chemical Cleaning – ASTM B600 Chemical Cleaning – Acid Cleaning (If Titanium Acid Cleaning is also carried out then please check “Chemical Cleaning – Titanium Cleaning – Acid” also) Chemical Cleaning – Alkaline Cleaning (If Titanium Alkaline Cleaning is also carried out then please check “Chemical Cleaning – Titanium Cleaning – Alkaline” also) Chemical Cleaning – Emulsion Cleaning Chemical Cleaning – Other

Americas+ 1 724 772 1616

Asia + 86 10 6461 9807

Europe+44 870 350 5011

www.pri-network.comP110190

Administered by PRI

Chemical Cleaning – Semi-Aqueous Cleaning Chemical Cleaning – Solvent Cleaning Chemical Cleaning – Titanium Cleaning – Alkaline Chromium Plating – AMS 2406 Chromium Plating – AMS 2438 Chromium Plating – AMS 2460 Chromium Plating – ASTM B 650 Chromium Plating – MIL-STD-1501 Chromium Plating – Other Chromium Plating –AMS-QQ-C-320 Chromium Plating –QQ-C-320 Conversion/Phosphate Coatings – AMS 2480 Conversion/Phosphate Coatings – AMS 2481 Conversion/Phosphate Coatings – AMS 2485 Conversion/Phosphate Coatings – AMS 2486 Conversion/Phosphate Coatings – DOD-P-16232 Conversion/Phosphate Coatings – MIL-C-13924 Conversion/Phosphate Coatings – MIL-C-5541 Conversion/Phosphate Coatings – MIL-DTL-13924 Conversion/Phosphate Coatings – MIL-DTL-16232 Conversion/Phosphate Coatings – MIL-DTL-5541 Conversion/Phosphate Coatings – Other Conversion/Phosphate Coatings – TT-C-490 Copper Plating – AMS 2418 Copper Plating – MIL-C-14550 Copper Plating – Other Electroless Plating Nickel – AMS 2404 Electroless Plating Nickel – AMS 2405 Electroless Plating Nickel – AMS-C-26074 Electroless Plating Nickel – MIL-C-26074 Electroless Plating Nickel – Other Electropolishing – Other Etch (AC7108/2 MUST ALSO BE SELECTED) Gold Plating – AMS 2422 Gold Plating – AMS 2425 Gold Plating – MIL-G-45204 Gold Plating – Other Gold Plating-ASTM B 488 Lead Plating – AMS 2414 Lead Plating – MIL-L-13808 Lead Plating – Other Nickel Plating – AMS 2403

Americas+ 1 724 772 1616

Asia + 86 10 6461 9807

Europe+44 870 350 5011


Administered by PRI

Nickel Plating – AMS 2423 Nickel Plating – AMS 2424 Nickel Plating – AMS-QQ-N-290 Nickel Plating – Other Nickel Plating – QQ-N-290 Paint/Dry Film (AC7108/1 MUST ALSO BE SELECTED) Silver Plating – AMS 2410 Silver Plating – AMS 2411 Silver Plating – AMS 2412 Silver Plating – ASTM B 700 Silver Plating – Other Silver Plating – QQ-S-365 Surface Treatment/Passivation – ASTM A 380 Surface Treatment/Passivation – ASTM A 967 Surface Treatment/Passivation – Other Surface Treatment/Passivation – QQ-P-35 Surface Treatment/Passivation– AMS-2700 Surface Treatment/Passivation– AMS-QQ-P-35 TESTING PERFORMED INTERNALLY IN SUPPORT OF CHEMICAL PROCESSING IN THE SCOPE OF THE AUDIT. (DO NOT CHECK TESTS THAT ARE OUTSOURCED.) B10 Adhesion Tape Testing B11 Adhesion Scratch and Chisel Testing B12 Adhesion Bend Testing (Metallic Coatings) B13 Coating Weight Testing B16 Thickness Verification of Magnetic, Eddy Current and XRF Machines B18 Adhesion Testing Heat and Quench B20 Porosity B21 Other Test Method B3 Metallography Testing B4 Microhardness Testing B5 Corrosion/Salt Spray Testing B6 Water Immersion/High Humidity Testing B7 Heat Resistance Testing Solution Analysis Tin Plating – AMS 2408 Tin Plating – AMS 2409 Tin Plating – ASTM B 339 Tin Plating – ASTM B 545 Tin Plating – MIL-T-10727 Tin Plating – Other Zinc Plating – AMS 2402

Americas+ 1 724 772 1616

Asia + 86 10 6461 9807

Europe+44 870 350 5011


Administered by PRI

Zinc Plating – AMS 2420 Zinc Plating – ASTM B 633 Zinc Plating – Other Zinc Plating – QQ-Z-325 AC7108/1 Rev A - Nadcap Audit Criteria for Painting & Dry Film Coatings (1) DOD-P-15328 Dry Film Coatings - Other MIL-C-22750 MIL-C-46168 MIL-C-53039 MIL-C-8514 MIL-C-85285 MIL-DTL-53022 MIL-DTL-53030 MIL-DTL-53039 MIL-L-46010 MIL-P-23377 MIL-PRF-22750 MIL-PRF-23377 MIL-PRF-85285 MIL-PRF-85582 Paint - Other Paint/Dry Film Coatings-Other AC7108/2 Rev B - Nadcap Audit Criteria for Etch Processes (Blue Etch Anodize, Local, Macrostructure, Nital, Pre-Penetrant, Temper) AMS 2643 AMS 2649 Etching - Other Local (Swab) Etch MIL-STD-867 Macrostructure Etch Nital Etch Pre-Penetrant Etch Solution Analysis Performed On Site in Support of Etch Processes Temper Etch

Americas+ 1 724 772 1616

Asia + 86 10 6461 9807

Europe+44 870 350 5011


Administered by PRI


NonDestructive Testing

DCI Aerotech Div. of Detroit Chrome Inc7515 Lyndon Ave Detroit, MI 48238

This certificate expiration is updated based on periodic audits. The current expiration date and scope of accreditation are listed at: www.eAuditNet.com - Online QML (Qualified

Manufacturer Listing).

In recognition of the successful completion of the PRI evaluation process, accreditation is granted to this facility to perform the following:

AC7114 Rev E - Nadcap Audit Criteria for NonDestructive Testing (NDT) Suppliers Accreditation Program AC7114/1 Rev E - Nadcap Audit Criteria for NonDestructive Testing Facility Penetrant Survey AC7114/2 Rev E - Nadcap Audit Criteria for NonDestructive Testing Magnetic Particle Survey

Americas+ 1 724 772 1616

Asia + 86 10 6461 9807

Europe+44 870 350 5011


Administered by PRI



DCI Aerotech Div. of Detroit Chrome Inc 7515 Lyndon Ave Detroit, MI 48238

This certificate expiration is updated based on periodic audits. The current expiration date and scopeof accreditation are listed at: www.eAuditNet.com - Online QML (Qualified Manufacturer Listing).

In recognition of the successful completion of the PRI evaluation process, accreditation is granted to

this facility to perform the following: AC7126 Rev B - Nadcap Audit Criteria for Conventional Machining as a Special Process(Holemaking, Broaching, Turning, Milling, Grinding, Edge Treatment) AC7126/5 Rev A - Nadcap Audit Criteria for Grinding General Grinding Grinding of Coatings

t-frm-17 17-Jun-10

U.S. Department

of Transportation

Federal Aviation

Administration Operations Specifications

001 Issuance and Applicability 002 Definitions and Abbreviations 003 Ratings and Limitations

004 S��m�ry of Special Authorizations andL1m1tat10ns

007 Designated Persons

449 Antidrug and Alcohol Misuse PreventionProgram

DCI AEROTECH DIVISION OF DETROIT CHROME INC

Table of Contents

Part A

HQ CONTROL DATE

01/31/2012 01/12/2012 01/30/2004

09/23/1998

12/19/2006

07/17/2009

Part A-1

EFFECTIVE

DATE 06/19/2013 06/19/2013 09/03/2008

09/03/2008

09/03/2008

06/19/2013

AMENDMENT NUMBER

I

1

0

0

0

Certificate No.: D77R737Y

U.S. Departmentof TransportationFederal AviationAdministration Operations Specihcations

4001 . Issuance and Apnlicability HQ Control. 0ll3ll20l2HQ Revision: 05d

a. These operations specifications are issued to DCI AEROTECH DIVISION OF DETROITCHROME INC, a Repair Station located in the United States, pursuant to 14 CFR Part 145,

$ 145.53. The repair station certificate holder shall conduct operations in accordance with 14 CFRPafi 145 and these operations specifications.

The certificate holder's address:

Fixed Location:7515 Lyndon AveDetroit, Michigan 48238

b. The holder of these operations specifications is the holder of certificate number D77P.737Y andshall hereafter be referred to as the "certificate holder".

c. These operations specifications are issued as part ofthis repair station cerlificate and arein effect as ofthe date approval is effective. This certificate and these operations specificationsshall remain in effect until the certihcate for a repair station that is located in the United States issurrendered, suspended, or revoked.

d. U.S./EC Aviation Safety Agreement Repair Station/lvfaintenance Organization Approvals notauthorized.

e. The certificate holder is authorized to use only the business name which appears on thecertificate to conduct the operations described in subparagraph a.

Delegated authorities: None

DCI AEROTECH DIVISION 4001-1 CertificateNo.: D77R737YOF DETROIT CHROME INC Amdt. No: 1

U.S. Departmentof ïransportationFederal AviationAdministration Operations Specifications

1. Issued by the Federal Aviation Administration.2. These Operations Specifications are approved by direction of the Administrator.

Digitally signed by James Gotha, Principal Maintenance Inspector (GL23)[] EFFECTIVE DATE: 6119/2013, [2] AMENDMENT#: IDATE: 2013.06.18 06:28:48 -05:00

3. I hereby accept and receive the Operations Specifications in this paragraph.

-DThompson, David R.,

DCI AEROTECH DIVISIONOF DETROIT CHROME INC

4001-2Amdt. No: 1

Certificate No. : D77R737Y

U.S. Departmentof ÏransportationFederal AviationAdministration Operations Specifications

4002 . Definitions and Abbreviations HQ Control2 0lll2l20l2HQ Revision: 05b

Unless otherwise defined in these operations specifications, all words, phrases, definitions, andabbreviations have identical meanings to those used in 14 CFR and 49 U.S.C., as cited in Public Law103-272, as amended. Additionally, the defrnitions listed below are applicable to operationsconducted in accordance with these operations specifications.

BASA The Bilateral Aviation Safety Agreement (BASA) is an executiveagreement concluded between the United States and a foreign countryfor the purpose of promoting aviation safety; also known as anAgreement for the Promotion of Aviation Safety.

Certificate Holder In these operations specifications, the term "certificate holder" means

the holder ofthe repair station certificate described in these operationsspecifications in Part A paragraph A00l and any ofits officers,employees, or agents used in the conduct of operations under thiscertificate.

CFR Code of Federal Regulations

Class rating As used with respect to the certification, ratings, privileges, and

limitation of aircraft within a category having similar operatingcharacteristics.

EASA European Aviation Safety Agency

EASA Accountable The manager who has corporate authority for ensuring that allManager maintenance required by the customer can be financed and carried out

to the standard required by the EASA full-member Authority.

Exemption An authorization that permits an alternate means of compliance with aspecific CFR. The exemption must meet the procedural requirementsof 14 CFR Part I L

FAA Accountable A person designated by the certificated repair station who isManager responsible for and has authority over all repair station operations that

are conducted under 14 CFR Part 145, including ensuring that the

repair station's personnel follow the regulations and serving as theprimary contact with the FAA.

Geographic An approval provided to a repair station located outside the UnitedAuthorization States to perform maintenance support under contract for a U.S. air

carrier (or an operator of U.S.- registered aircraft under 14 CFRParT 129) at a location other than the repair station facility. Ageographic authorization is issued by the FAA to respond to a U.S. aircarrier's or Part 129 foreign operator's need for ma-intenance at astation where the frequency and scope of that maintenance does not

DCI AEROTECH DIVISION 4002-1 Certificate No.: D77R737YOF DETROIT CHROME INC Amdt. No: 1

U,S. Departmentof TransportationFederal AviationAdministration Operations Specihcations

Limited Rating

Limited Ratings -Specialized Services

Line Maintenance

MAG

Maintenance

U.S./EC AviationSafety Agreement,Annex 2,Maintenance

MIP

MOE

PreventiveMaintenance

QCM

Repair Station locatedin the United States

Repair Station locatedoutside the UnitedStates

RSM

warrant permanently staffing and equipping the station for itsaccomplishment.

A rating issued to repair stations for the performance of maintenanceon particular makes and models of airframes, powerplants, propellers,radios, instruments, accessories, and/or parts.

Rating issued for a special maintenance function when the function isperformed in accordance with a specification approved by theAdministrator.

Any unscheduled maintenance resulting from unforeseen events, orscheduled checks where certain servicing and./or inspections do notrequire specialized training, equipment, or facilities.

The Maintenance Amex Guidance (MAG) defines the process thatthe FAA and EASA undertake in the inspection, findings ofcompliance certification, and monitoring of repair stations, as well as

theirjoint cooperation in quality assurance and standardization activitiesin support of the Agreement, Amex 2, Maintenance.

The inspection, overhaul, repair, preservation, and replacement ofparts, but excludes preventive maintenance.

Annex 2 covers the reciprocal acceptance offindings ofcompliance,approvals, documentation and technical assistance regarding approvalsand the monitoring of repair stations/maintenance organizations.

Maintenance Implementation Procedures (MIP) are procedures forimplementing the provisions of a BASA that apply to maintenance.

A maintenance organizatron exposition (MOE) pertains to EASAmember countries that use an MOE in place of a Repair StationManual (RSM) and a Quality Control Manual (QCM).

As defined in 14 CFR part I and part 43 appendix A, subparagraph(c).

Quality Control Manual

A certificated repair station located in the United States.

A certihcated repair station located outside of the United States.

Repair Station Manual

DCI AEROTECHDIVISIONOF DETROIT CHROME INC

1i002-2Amdt. No: 1


U.S. Departmentof TransportationFederal AviationAdministration Operations Specifi cations

1. Issued by the Federal Aviation Administration.2. These Operations Specihcations are approved by direction of the Administrator.

Digitally signed by James Gotha, Principal Maintenance Inspector (GL23)[1] EFFECTIVE DATE: 611912013, [2] AMENDMENT#: IDATE: 2013.06.18 06:28:50 -05:00

accept and receive the Operations Speciflrcations in this paragraph.

¿4-/JThompson, David fy Assurance Director Date

DCI AEROTECH DIVISIONOF DETROIT CHROME INC

11002-3

Amdt. No: ICertificate No.: D77R737Y

U.S. Departmentof Transportation

Federal AviationAdministration

Operations Specifications

4003. Rati¡ss and Limitations

The Certificate Holder is authorized the following Ratings and./or Limitations:

Class Ratings

None Authorized

Manufacturer Make / ModelFrom t}re accepted capability F¡omthe accepted Capability

lis! as amended. List, as amended.

0l/30/04010

LimitationsUse the methods, techniques, and

practices prescribed in the currentmanufactu¡ers maintenancemanual or inst¡uctions fo¡continued airworthiness, or othermethods, techniques, andpractices acceptable to theAd¡ninistrator.

Same as abovg and ASTM-E-7444, as amended.

Same as above, and ASTM-E-1417, as amended,

Same æ above, and MIL-STD-867,as amcnded.

HQ Control:IIQ Revision:

Limited Ratinss

RatinsNondestructive

lnspection, Testingand Processing

Magnetic ParticleInspection

Fluo¡escent Penetantlnspection

NitaÌ Etch Inspection

F¡om tåe acceptedCapability Lisl as

amended.From the accepted

Capability Lis! asamended.

From the acceptedCapability List, as

amendcd.

From the accepted CapabilityList as amended.

F¡om the accepted CapabilityList, as amended.

From the accepted CapabilityLisq as amended.

Limited Ratines - Soecialized Services

RatinqChemical Cleaning

Alloy Plating

Brush Plating

Snecifications

MIL-S-5002, SPOP 2l I, and PWA-83-a3, all as amendod

AMS-24 I 5, AMS-241ó, AMS-24 17,MIL-P-81728, MIL-S1D-1500,Hr'-G- I, AMS-2429, BPS-4525,PS-172, TAP.PS-920, TAP.PS-809, EPS-3647, and VS-l-3-1-19,all as amended.

MIL-STD-8ó5, as amended.

LimitationsUse the methods, techniques, and practices

prescribed in the cu¡rent manufacturersmainfs¡anç. manual or Instructions forContinued Airworthiness, or other methods,techniques, and practices acceptable to theAdministator.

Use the methods, techniques, and practicesprescribed in the current manufacturcrsmai¡tenance manual or Instructions forContinued Airworthiness, or other metbods,techniques, and practices acceptable to theAdminisüator.

Use the methods, techniques, and practìcesprescribed in the cunent manufacture¡smaintenance ma¡ual or Instructions forContinued Airworthiness, or other methods,techniques, and practices acceptable to theAdministrator.

Print Date: 9/312008DCI AEROTECH DIVTSION OF DETROIT CHROME INC

4003-l Cerrificare No.: D77R737Y

U.S. Departmentof TransportationFederal AviationAdministralion


Limited Ratines - Snecialized Servicea

RatinsCadmium Plating

Chromium Plating

Conversi onÆhosphate Coatings

Copper Plating

ElecÍoless Plating-Nickel

Gold Plating

Lead Plating

Niokel Plating

Painting/Dry Film Coating

Soecilications

AMS-QQ-P-4 I 6, AMS-2400, AMS-2401, MIL-STD-870, and QQ-P-416, all as amended.

AMS-2460, AMS-QQ-C-320, AMS-2406, AN[S-2438, ASTM-B-6 50,MIL-STD-1501, QQ-C-320,BAC-5709, HS-246, BPS-45 I 7,BPP-320, BPP-3 20.2, BPP-320. 4,TSBS-5702355, and TSBS-05-000084, all as amended.

MILDTL- 1 3 92 4, MTL.DTL-I 6232,MILDTL-5s4 1, AMS-2480,AMS-2481, AMS-2485, AMS-2486, MIL-C-13924, DOD-P-I 6232, MtL- C-5 5 4 1, TT-C-490,a¡d BPP-F-340.6, all as irmended.

AMS-2418, MIL-C-14550, andRPS-29?, all as amended.

AMS.C.26O74, AMS-2404, AMS.2405, and MIL -C-26O7 4, all as

amended.

AMS-2422, ANIS-2425, and MIL-G-45204, all as amended.

AMS-2414 and MIL-L-I3808, all as

amended.

AMS-QQ-N-290, AMS-2403,4M5.2423, AMS -2424, MIL-STD-868, QQ-N-290, and SPOP-26, all as amended.

DOD-P 15328, MIL-DTL-53022,MIL-L-4601 0, MLL-P -2337 7,MIL-PRF-23377, MIL-PRF-460 r 0, WA-PD -3 65, TT -P -664,TT-P-1757, AMS-3136,P50T154, and TT-P-636, all as

amended.


prescribed in the cunent manufacturersmaintenance manual or Insüuctions fo¡Continued Airworthiness, or other methods,techniques, and practices acceptable to theAdministrator.

Use the methods, techniques, and practicesprescribed in the cur¡ent ma¡ufactu¡ersmaintenance manual or lnstructions forContinued Airworthiness, or ofher methods,techniques, and practices acceptable to theAdministator.

Use the methods, techniques, and practicesprescribed in tle current manufacturersmaintenalce manua'l or Instructions forContinued Airworthiness, or other mcthods,tcchniques, and practices acceptable to theAdminisnator.

Use the methods, techniques, and practicesprescribed in the cunent manufacturersmaintenance manual or Instuctions forContinued Airworthiness, or other metlods,techniques, ald practices acceptable to theAdministrator.

Use tle methods, techniques, and practicesprescribed in the cu¡rent manufacturersmainlenance ma¡rual o¡ Instructions forContinued Airworthiness, or other methods,techniques, and praclices acceptable to theAdministrator.

Use the methods, techniques, and practicesprescribed in the current manufacturersmaintenance manual or Inskuctions forContinued Airworthiness, or othe¡ methods,techniques, and practices acceptable to theAdministrator,

Use the methods, techniques, and practicesprescribed in the current manufacture¡smaintenance ma¡ual or lnstructions fo¡Continued Airworthiness, or other methods,techniques, and practices acceptable to theAdministrator.

Use the methods, techliques, and practicesprescribed in the current manufacfursrsmaintenance manual or lnstructions forContinued Airworthiness, or othsr methods,techniques, and practices acceptable to theAdminishator.

Use the methods, techniques, and practicesprescribed in the cunent manufactulersmaintenance manual or lnstructions fo¡Continued Airworthiness, or other metlods,techniques, and practiccs acceptable to theAdministrator.

Print Date: 9/3/2008DCI AEROTECH DIVISION OF DETROIT CHROME INC

A003-2 Certificate No.: D77R737Y

U.S. Deparlmentof lransporletionFederal AviationAdministration


Limited Ratinss - Specialized Se¡vices

RatineSilver Plating

S urface Treatmenl/Passivation

f in Plating

Zinc Plating

Stripping

Snecifications

^MS-2410, AMS-241 l, AMS-241 2,

ASTM-B-700, QQ-S-365, andRPS-168, all as amended.

AMS-QQ-P-3 5, ASTM-A-967,ASTM-A-380, QQ-P-35, AMS-27 00, BAC-5625, and EPS-11250, all as amended.

ASTM-8.339, AMS-2408, AMS-2409, ASTM-B-545, and MIL-T-10721, all as amended.

AMS-2402, AMS-2420, ASTM.B-633, and QQ-Z-325, all as

amended,

MIL-STD-871, as amended.


prescribed in the current ma¡rufacturersmaintenance manual or Instuctions forContinued Airworthiness, o¡ other methods,techniques, and practices acceptable to theAdminist¡ato¡.

Use the methods, techaiques, and practices

prescrihed ìn the cur¡ent manufacfurersmaintenance manual or lnshuctions forContinued Äirworthiness, or other methods,techniques, and practices acceptable to theAdministato¡.

Use the methods, techniques, and practicesprescribed in the current manufacturersrnaintenance manual or Insûuctions forContinued Airworthiness, or other methods,techniques, and practices acceptable to theAdminishator.

Use fhe methods, techniques, and practices

prescribed in the current ma¡rufacturersmaintena¡lce manual or Instructions forContinued Airworthiness, or other methods,kchniques, and practices acceptable to theAdminist¡ator.

Use the methods, tecbniques, and practicesprescribed in the current manufactu¡ersmaintenance manual or Instuctions forContinued Ai¡worthiness, or other methods,tccbniques, and practices acceptable to theAdministato¡.

Supportlssued by tbe Federal Aviation Administration,

are approved by direction of the Adminisfrator,

EmèïSon, Eric E. Maintenance Inspector

4.5.

Date Approval is effective: 913/08I hgreby accept and receivc the Operations Specifications in this paragraph.

Assurance Director

GL23

Amendment Number: 0

Print Date: 9/3/2008 4003-3DCI AEROTECH DIVISION OF

Certifïcate No.: D77R737YDETROIT CHROME INC

U,S Dopartmentof TransporlalionFederal AviationAdministration


4004, Summary of Special Authorizations and Limitations HQ Control: 9/2311998HQ Revision: 010

ReferenceParagraDhs

^449

a. The certificate holder, in accordance with the reference paragraphs, is authorized to:

Conduct operations choosing to have an antidrug and alcohol misuse preventionprogram.

b. The certilicate holder is not autho¡ized and shall not:

Use Exemptions. 4005

Use an approved electronic recordkeeping system, electronic/digital signature, and,/or A025electronic media.

Perform maintenance with NAA ratings where the scope of work is authorized by a 4060BASA/MIP,

Perform work, incìuding continuous operations, at additional locations other than at its 4101primary fixed location.

Perforur maintenance in accordance with foreign repair station geographic 8050authorizations.

Perform work, excluding continuous operations, at additional locations other than at its Dl00primary Fixed Location.

Perform line maintenance for cert. holders çonducling operations under Parts 12l and Dl07135 and for foreign carriers/persons operating U.S. registered aircraft in commoncaniage under Part 129, apart from Dl00 which authorizes that work away fromstation.

tE

lssued by the Federal Aviation Admjnistration.

ifications are approved bv direction of the Administrator.,t-----..

Principal Maintenance lnspector

4. Date Approval is effective: 9/3108acc€pt and receive the Operations Specifications in this paragraph

Assurance Director

GL23

Amendment Number: 0

Date: 9/3/08

merson, Eric


A004-t Certificate No.: D77R737Y

U.S. Departmentof Transportation

Federal AviationAdmin¡stration

Operations Specifi cations

4007. I)esisnatedPersons HQ Control: 12119106

HQ Revision: 030

a. The personnel listed in the following table are designated to officially apply for and receive operationsspecifications for the certificate holder indicated below.

tions

b. The following personnel listed in Table 2 are designated by the certihcate holder to receiveInformation for Operators (INFO) m€ssages for the certificate holder as indicated below. A receipt for theinformation by an operator or person is not required.

'able I - Des Persons to lbr and Receive AuthorlzaTitle Name Parts Authorized

QualiE Assurance Director ThomDson, David R AFAA Accountable Manager, 145 iPresident

Nichols, Ronald N, Sr. A

Vice President of Operations Nichols, Bruce A AC'hief lnspector / AerospaceProduction Manace¡

Nguyen, Vinh Quoc A

Table 2 - to Receive INFOName Emsil Addrcss Telephone No. Type of Informatioo to

Receive

David R. Thomnson davet(Edetroitchrome. com 313-341-9478 ALL

l. lssued by the Federal Aviation Administration.2. Support3,,-These C

.SÄí'-I9Emèrson. Er

are approved by direction of the Adminisüator,

mE-rson, Eric E. Principal Maintenançe lnspector GL23

4, Date Approval is effective: 9/3/08 AmendmentNumber: 0

5 accept and receive the Operations Specifications in this paragraph.

Assurance Director Date: 9/3/08


4007-t Certificate No.: D77R737Y

U.S. Departmentof TransportationFederal AviationAdministration Operations Speciflrcations

^449 . Antidrus and Alcohol Misuse Prevention Prosram HQ Control: 0711712009

HQ Revision: 00a

a. The Part 145 repair station certificate holder has elected to implement an Antidrug andAlcohol Misuse Prevention Program, because the certificate holder performssafety-sensitive fl¡nctions for a 14 CFR Part l2I, and 135 certificate holder and/or for a14 CFR Part 9l operator conducting operations under Section 9I.147 .

b. The certificate holder certifies that it will comply with the requirements of 14 CFR Part 120and 49 CFR Part 40 for its Antidrug and Alcohol Misuse Prevention Program.

c. Antidrug and Alcohol Misuse Prevention Program records are maintained and available forinspection by the FAA's Drug Abatement Compliance and Enforcement Inspectors at thelocation listed in Table 1 below:

Table 1

Location & Telephone of Antidrug and Alcohol MisusePrevention Prosram Records:

felephone Number: A1(3r3)34r-9478Address: 7515 Lvndon St.

Address: N/ACity: Detroit

State: MIZip code: 48238

d. Limitations and Provrsrons.

(1) Antidrug and Alcohol Misuse Prevention Program inspections and enforcement activitywill be conducted by the Drug Abatement Division. Questions regarding theseprograms should be directed to the Drug Abatement Division.

(2) The certificate holder is responsible for updating this operations speciltcation when anyof the following changes occur:

(a) Location or phone number where the Antidrug and Alcohol Misuse PreventionProgram Records are kept.

(b) If the certificate holder's number of safety-sensitive employees goes to 50 andabove, or falls below 50 safety-sensitive employees.

(3) The certif,rcate holder with 50 or more employees performing a safety-sensitivefunction on January I of the calendar year must submit an annual report to the DrugAbatement Division of the FAA.

(4) The certificate holder with fewer than 50 employees performing a safety-sensitivefunction on January 1 of any calendar year must submit an annual report upon requestof the Administrator, as specified in the regulations.

The certificate holder has fewer than 50 safety-sensitive employees.

DCI AEROTECH DIVISION A449-I Certificate No.: D77R737YOF DETROIT CHROME INC Amdt. No: 1

U.S. Departmentof TransportationFederal AviationAdministration Operations Specifications

1. Issued by the Federal Aviation Administration.2. These Operations Specifications are approved by direction of the Administrator.

Digitally signed by Principal Maintenance Inspector (GL23)[] EFFECTIVE D 13, [2] AMENDMENT #: 1

DATE:2013.06.18 00

accept and receive the Specifications in this paragraph.

ø1t7Date

DCI AEROTECH DTVISIONOF DETROIT CHROME INC

1'449-2Amdt. No: I


Rolls-Royce

Rolls-Royce CorporationPO Box 420lndianapolis, lN 46206-0420USA

roval

ls an approved supplier for the

Scope of approval:

Rolls-Royce Corporation Sub Tier Supplier

specified

AMS 2410, AMS 24I I,

AMS 2485

a

a

a

a

a

a

a

a

a

a

a

Cert¡fi

USA

AMS-QQ-C-320, AMS-QQ-N-2eO, AMS-QQ-P-35, A

AMS 2400, AMS 2403, AMS 2404, AMS 2405, AMS

AMS2412, AMS 2416, AMS 24I8, AMS 2424, AMS

ASTM A 360, ASTM B 633, ASTM B 650

MIL- C- | 3 9 24, li{tL- C-2607 4

RPS 168, RPS 297, RPS 66IlI5, RPS 661/2, RRPS 66119

EPS 316, EIS 15IO

RRPs8003-142, tA3, tD4

RRP58004

NOTE: RPS 278 (removal of white layer) is not approved for

number:108670r.içÉqe date: 10-03-2014 Rolls-Royce

This certificate supersedes all previous approvalsubject to the terms on the back hereof.

Certificateof

Approval

This is to certify that

Rolls-Royce Canada Limited

9500 Côte-de-LiesseLachine, Québec, H8T 1A2Tel: (514) 636-0964Fax: (514) 828-1763

Scope of approval:

DCI Aerotech

Approval number: 216521

AMS-QQ-C-320, AMS-QQ-N-290, AMS-QQ-P-35, AMS-QQ-P-416, AMS-QQ-Z-325, AMS2400, AMS2403, AMS2404, AMS2405, AMS2406, AMS2410, AMS2411, AMS2412, AMS2416, AMS2418, AMS2424, AMS2438, AMS2485, ASTMA380, ASTMB633, ASTMB650, EDS1306, MIL_C_13924, MIL_C_26074, MSRR9274, RPS168, RPS278, RPS297, RPS661/15, RPS661/2, RPS661/9, RRQ, RRU2, RRU6

Issue date: January 22, 2008Expiry date: Unlimited

Manager, Supplier Quality, Rolls-Royce Canada

Andrew Robinson

Category: Process shop

We confirm that your Quality Assurance Controls meet the general requirements of Rolls-Royce Canada Limited, as specified in RR9000:SABRe. The approval Scope defined is only valid whilst Quality Systems Approval to an appropriate internationally recognized standard is maintained. Your attention is drawn to the need for you to notify Rolls-Royce Canada Limited of management and organisational changes and any change of status of your Quality Systems Approval, in accordance with RR9000:SABRe. Approvals granted are dependent upon the agreed standards being maintained by you and may be revoked at any time by Rolls-Royce Canada Limited, without notice and liability. Nothing in this approval shall prejudice any rights or remedies which Rolls-Royce Canada Limited may have, whether now or in the future in respect of goods which fail to meet contract requirements.

- E 0

is an approved supplier for the scope specified

Energy Business

Parker Aerospace approvals DCI AEROTECH 7515 LYNDON,, ..........SURVEYED ON (8/5/2015) DETROIT, MI 48238 313-341 9478 29 processes found

Process Code Status Specification NADCAP AA10 All NADCAP CHROME PLATING C002 All AMS 2406'N' CHROME PLATING C003 All AMS 2460'A' CADMIUM PLATING D001 All AMS-QQ-P-416'D' Type I

CADMIUM PLATING D002 All AMS-QQ-P-416'D' Type II

CADMIUM PLATING D003 All AMS-QQ-P-416'D' Type

III

SURFACE TREATMENTS E023 All MIL-DTL-13924'D, NT1'

DALIC PLATING F010 All MIL-STD-865'D' NT1 MISC PLATING G015 All AMS 2410'K' MISC PLATING G032 All AMS 2418'H' MISC PLATING G067 All BPS4525'H' HEAT TREAT H009 All AMS 2759/9'D' HEAT TREAT H033 All AMS 2759/11'05 R14' HEAT TREAT H080 All BPS4620'U' NDT N010 All ASTM E1417/E1417M'13' NDT N027 All ASTM E1444/E1444M'12'

NDT N090 View Limitations

BPS4110'W'

PASSIVATION P002 All AMS 2700'E' Type 2 PASSIVATION P006 All AMS 2700'E' Type 6 PASSIVATION P007 All AMS 2700'E' Type 7 PASSIVATION P008 All AMS 2700'E' Type 8 PASSIVATION P015 All AMS-QQ-P-35'98' Type II PASSIVATION P016 All AMS-QQ-P-35'98' Type VI

PASSIVATION P017 All AMS-QQ-P-35'98' Type VII

PASSIVATION P018 All AMS-QQ-P-35'98' Type VIII

PRIORTY PROCESS PP20 All BPS4127'C'CHROME

PRIORTY PROCESS PP60 All BPS 4127'C' MISC PLATING

PAINT R010 All MIL-DTL-18264'E'

MISC PROCESS X035

View Limitations

BPS4776'G'

Power, Controls & Sensing Systems

UTC Aerospace Systems

One Hamilton Road

Windsor Locks, CT 06096, USA

+1 860 654 2432 Fax: +1 860 660 1436

[email protected]

www.utcaerospacesystems.com

Sergey Yesilevich

Sr. Analyst- Special Processes & NDT

Page | 1

Hamilton Sundstrand

February 11, 2016

DCI AEROTECH 7515 Lyndon Avenue Detroit, MI 48238 United States Attention: Dave Thompson, - Quality Assurance Director Bill Knapp, - Sales Director

SAP Vendor Number: 1119753.

Subject: UTC Aerospace Systems (UTAS) Approved Special Process Accreditation

Dear Mr. Thompson and Mr. Knapp,

UTC Aerospace Systems (Hamilton Sundstrand), a division of United Technologies Corporation (UTC), is pleased to inform you that your facility has recently been granted authorization to perform certain manufacturing special processes in accordance with applicable process specifications. This accreditation status is extended until your next onsite review, which will be scheduled no later than FEBRUARY 11, 2020 (4 YEARS FROM DATE).

After successfully completing a recent survey at your company, UTC Aerospace Systems (Hamilton Sundstrand) is pleased to classify you as an accredited supplier for the applicable processes listed on the attached Hamilton Sundstrand Report # 70 and any equipment/processing limitations.

At this time we would also like to make reference to the Nadcap accreditation program. UTC Aerospace Systems (Hamilton Sundstrand) as well as United Technologies Corporation has set an expectation that all special processing facilities maintain Nadcap accreditation for required special processes. Special processing supplier’s participation in this program is an expectation of UTC Aerospace Systems (Hamilton Sundstrand) and is strongly recommended going forward.

As such, we rely heavily on the integrity with which your system is implemented. Your effort and responsiveness to the importance of providing goods or services on schedule, at a competitive price, and compliant to our quality requirements are essential to the maintenance of your accreditation status and our combined competitive position.

Our sincere congratulations are extended to you and your personnel and our expectations are for your continued success.

Very Truly Yours,

Sergey Yesilevich

Sergey Yesilevich

Supplier Quality & Development - Special Processes 860-654-2432 / [email protected] UTC Aerospace Systems United Technologies Corporation



One Hamilton Road


+1 860 654 2432 Fax: +1 860 660 1436

[email protected]


Sergey Yesilevich


Page | 2

Hamilton Sundstrand

Enclosure: Special Process Approvals (Report 70) / Limitations Vendor Number Specification Qualification Spec/Qual Description Name

119753 QQ-P-35 PASSIVATION TREATMENT FOR CRES. DCI AEROTECH DETROIT CHROME INC

119753 QQ-C-320 CL2 RC40 AND OVER CHROME PLATE DCI AEROTECH DETROIT CHROME INC

119753 QQ-C-320 CL2 UP TO RC40 CHROME PLATE DCI AEROTECH DETROIT CHROME INC

119753 AMS-QQ-P-416 COATING, CADMIUM (ELECTRODEPOSITED) DCI AEROTECH DETROIT CHROME INC

119753 PN14.10 PASSIVATION DCI AEROTECH DETROIT CHROME INC

119753 ES9-27 TEMPER ETCH INSPECTION DCI AEROTECH DETROIT CHROME INC

119753 AMS 2418 TYPE 1 COPPER PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2417 TY2 ZINC-NICKEL ALLOY PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2417 TY1 ZINC-NICKEL ALLOY PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 201 ELECTROLESS NICKEL PLATE DCI AEROTECH DETROIT CHROME INC

119753 HS 201 RC40 AND OVER

ELECTROLESS NICKEL PLATE DCI AEROTECH DETROIT CHROME INC

119753 HS 201 UP TO RC40 ELECTROLESS NICKEL PLATE DCI AEROTECH DETROIT CHROME INC

119753 QQ-Z-325 ZINC PLATING DCI AEROTECH DETROIT CHROME INC

119753 ASTM B633 ZINC PLATING DCI AEROTECH DETROIT CHROME INC

119753 CP13.15-02-01 PLATING, BRONZE, ELECTRODEPOSITED DCI AEROTECH DETROIT CHROME INC

119753 PN13.08-02 CADMIUM-TITANIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 MIL-STD-1500 CADMIUM-TITANIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 MIL-STD-1500 TYPE I CD-TI PLATING, LOW EMBRITTLEMENT DCI AEROTECH DETROIT CHROME INC

119753 MIL-STD-1500 TYPE II CD-TI PLATING, LOW EMBRITTLEMENT DCI AEROTECH DETROIT CHROME INC

119753 PN09.0000-SR-5

STRESS / EMBRITTLEMENT RELIEVE DCI AEROTECH DETROIT CHROME INC

119753 AMS-C-26074 CL1 GRB RC40 AND OVER

ELECTROLESS NICKEL PLATE DCI AEROTECH DETROIT CHROME INC

119753 PN13.12-03 PLATING, ELECTROLESS NICKEL DCI AEROTECH DETROIT CHROME INC



One Hamilton Road


+1 860 654 2432 Fax: +1 860 660 1436

[email protected]


Sergey Yesilevich


Page | 3

Hamilton Sundstrand

119753 AMS 2700 Passivation of Corrosion Resistance Alloy DCI AEROTECH DETROIT CHROME INC

119753 HS 178 CATA PASSIVATION REQUIREMENT DCI AEROTECH DETROIT CHROME INC

119753 ASTM B700

SILVER, ELECTRODEPOSITED COATINGS DCI AEROTECH DETROIT CHROME INC

119753 ASTM A380 PASSIVATION DCI AEROTECH DETROIT CHROME INC

119753 HS 74 CL1 TY1 OVER RC46 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 74 CL1 TY1 RC40 TO RC46 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 74 CL1 TY1 UP TO RC40 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC



















One Hamilton Road


+1 860 654 2432 Fax: +1 860 660 1436

[email protected]


Sergey Yesilevich


Page | 4

Hamilton Sundstrand



119753 PN13.08 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2411

SILVER PLATING, FOR HIGH TEMPERATURE APPLICATIONS DCI AEROTECH DETROIT CHROME INC

119753 HS 519 GRA RC40 AND OVER SILVER PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 519 GRB RC40 AND OVER SILVER PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 519 TY1 GRB UP TO RC40 SILVER PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 519 UP TO RC40 SILVER PLATING DCI AEROTECH DETROIT CHROME INC

119753 PN13.14 SILVER PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 332 PRECISION CHROMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 PN13.06 CHROMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 PN13.12 PLATING, NICKEL (ELECTRODEPOSITED) DCI AEROTECH DETROIT CHROME INC

119753 AMS 2402 ZINC PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 447

INSPECTION - PENETRANT METHODS OF DCI AEROTECH DETROIT CHROME INC

119753 PN16.03

PENETRANT INSPECTION AND CLASSIFICATION DCI AEROTECH DETROIT CHROME INC

119753 PN16.04

MAGNETIC PARTICLE INSPECTION AND CLASSIF DCI AEROTECH DETROIT CHROME INC

119753 HS 31 INSPECTION, MAGNETIC PARTICLE DCI AEROTECH DETROIT CHROME INC

119753 ASTM E 1417 DYE PENETRANT INSPECTION DCI AEROTECH DETROIT CHROME INC

119753 ASTM E 1444

Standard Practice of Magnetic Particle Examination DCI AEROTECH DETROIT CHROME INC

119753 MIL-STD-1907

INSPECTION, PENETRANT & MAG PARTICLE DCI AEROTECH DETROIT CHROME INC

119753 MIL-STD-1949 MAGNETIC PARTICLE INSPECTION (SUPERCEDED BY ASTM-E1444)

119753 PN16.05

TEMPER ETCH INSPECTION AND CLASSIFICATIO DCI AEROTECH DETROIT CHROME INC

119753 PN13.02 BLACK OXIDE DCI AEROTECH DETROIT CHROME INC



One Hamilton Road


+1 860 654 2432 Fax: +1 860 660 1436

[email protected]


Sergey Yesilevich


Page | 5

Hamilton Sundstrand

119753 HS 826 BLACK OXIDE DCI AEROTECH DETROIT CHROME INC

119753 MIL-C-13924 BLACK OXIDE (ALL CLASSES) DCI AEROTECH DETROIT CHROME INC

119753 AMS 2405 PLATING, ELECTROLESS NICKEL DCI AEROTECH DETROIT CHROME INC

119753 PN14.16-03 DRY FILM LUBRICANT DCI AEROTECH DETROIT CHROME INC

119753 HS 248 TYA1 SOLID DRY FILM LUBE COATING DCI AEROTECH DETROIT CHROME INC



119753 AMS 2410 RC40 AND OVER SILVER PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2410 UP TO RC40 SILVER PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2404 RC40 AND OVER NICKEL PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2404 UP TO RC40 NICKEL PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2400 RC40 TO RC46 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 760 PICKLING, CRES PROCESS, FOR DCI AEROTECH DETROIT CHROME INC

119753 PN14.30 SHOTPEEN DCI AEROTECH DETROIT CHROME INC

119753 AMS 2430 SHOT PEENING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2432 SHOTPEENING, COMPUTER MONITORED DCI AEROTECH DETROIT CHROME INC

119753 AMS-S-13165 SHOT PEENING DCI AEROTECH DETROIT CHROME INC

119753 MIL-S-13165 SHOT PEENING DCI AEROTECH DETROIT CHROME INC

119753 HS 67 SHOT PEENING CONTROL DCI AEROTECH DETROIT CHROME INC

119753 HS 2062 GLASS BEAD PEENING DCI AEROTECH DETROIT CHROME INC

119753 MIL-C-14550 COPPER PLATING DCI AEROTECH DETROIT CHROME INC

119753 PN13.19 COPPER PLATING DCI AEROTECH DETROIT CHROME INC

119753 PN13.15 PLATING, BRONZE DCI AEROTECH DETROIT CHROME INC

119753 AMS 2485 BLACK OXIDE DCI AEROTECH DETROIT CHROME INC

119753 MIL-C-13924 CL1 BLACK OXIDE COAT (LOW ALLOY STEEL) DCI AEROTECH DETROIT CHROME INC

119753 AMS 2759/9 HYDROGEN EMBRITTLEMENT RELIEF DCI AEROTECH DETROIT CHROME INC

119753 PN14.50-03 WHITE LAYER REMOVAL FROM NITRIDED STEELS DCI AEROTECH DETROIT CHROME INC

119753 AMS 2415 UP TO RC40 LEAD AND INDIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 7725 INSPECTION, ETCH PRIOR TO PENETRANT DCI AEROTECH DETROIT CHROME INC



One Hamilton Road


+1 860 654 2432 Fax: +1 860 660 1436

[email protected]


Sergey Yesilevich


Page | 6

Hamilton Sundstrand

119753 AMS 2419 CADMIUM-TITANIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2438 CHROMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 TT-C-490 PHOSPHATE, ZINC, TYPE I DCI AEROTECH DETROIT CHROME INC

119753 AMS 2400 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2403 NICKEL PLATING - GENERAL PURPOSE DCI AEROTECH DETROIT CHROME INC

119753 AMS 2404 Electroless Nickel Plating DCI AEROTECH DETROIT CHROME INC

119753 AMS 2406 CHROMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2410 SILVER PLATING, NICKEL STRIKE, HIGH BAKE DCI AEROTECH DETROIT CHROME INC

119753 AMS 2412 SILVER PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2418 COPPER PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2429 PLATING, BRONZE DCI AEROTECH DETROIT CHROME INC

119753 P1 LEAD INDIUM PLATING OF BEARINGS DCI AEROTECH DETROIT CHROME INC

119753 P142 CHROMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 246 UP TO RC40 CHROME PLATE DCI AEROTECH DETROIT CHROME INC

119753 ASTM B700 TYPE 1 GRADE A CLASS N

ELECTRODEPOSITED COATINGS OF SILVER DCI AEROTECH DETROIT CHROME INC

119753 ASTM B700 TYPE 1 GRADE A CLASS S

ELECTRODEPOSITED COATINGS OF SILVER DCI AEROTECH DETROIT CHROME INC

119753 MIL-I-6868 MAGNETIC PARTICLE INSPECTION (SUPERCEDED BY MIL-STD-1949)

119753 MIL-STD-867 TEMPER ETCH INSPECTION DCI AEROTECH DETROIT CHROME INC

119753 QQ-Z-325 TY1 ZINC PLATE DCI AEROTECH DETROIT CHROME INC

119753 QQ-Z-325 TY2 ZINC PLATE DCI AEROTECH DETROIT CHROME INC

119753 HS 7725 TY2 INSPECTION, ETCH PRIOR TO PENETRANT DCI AEROTECH DETROIT CHROME INC

119753 AMS 2412 UP TO RC40

SILVER PLATING,COPPER STRIKE DCI AEROTECH DETROIT CHROME INC

119753 AMS 2412 RC40 AND OVER

SILVER PLATE,COPPER STRIKE DCI AEROTECH DETROIT CHROME INC

119753 HS 7725 TY1 PRE-PENETRANT ETCH DCI AEROTECH DETROIT CHROME INC

119753 QQ-S-365 SILVER PLATING DCI AEROTECH DETROIT CHROME INC

119753 PN15.66

CHEMICAL STRIPPING OF INORGANIC COATINGS DCI AEROTECH DETROIT CHROME INC

119753 AMS 2460 CL2 RC40 AND OVER CHROMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2460 CL2 UP TO RC40 CHROMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2401 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC



One Hamilton Road


+1 860 654 2432 Fax: +1 860 660 1436

[email protected]


Sergey Yesilevich


Page | 7

Hamilton Sundstrand

119753 AMS 2401 UP TO RC40 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2401 RC40 AND OVER CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2418 TYPE 2 MASKANT PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2400 UP TO RC40 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 AMS 2405 UP TO RC33 NICKEL PLATING DCI AEROTECH DETROIT CHROME INC

119753 HS 246 CHROME PLATE (ALL HARDNESS LEVELS) DCI AEROTECH DETROIT CHROME INC

119753 AMS 2429 MASKANT PLATING, BRONZE DCI AEROTECH DETROIT CHROME INC

119753 QQ-C-320 CHROMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 QQ-N-290 NICKEL PLATING DCI AEROTECH DETROIT CHROME INC

119753 QQ-P-416 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 QQ-P-416 CL1 TY1 RC40 AND OVER CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC

119753 QQ-P-416 CL1 TY1 UP TO RC40 CADMIUM PLATING DCI AEROTECH DETROIT CHROME INC





119753 MIL-DTL-16232 PHOSPHATE COATING, TYPE M OR Z DCI AEROTECH DETROIT CHROME INC

119753 MIL-DTL-16232 TYPE Z CLASS 2

PHOSPHATE COATING, HEAVY, MANGANESE OR ZINC BASE DCI AEROTECH DETROIT CHROME INC

119753 MIL-DTL-16232 TYPE Z CLASS 3

PHOSPHATE COATING, HEAVY, MANGANESE OR ZINC BASE DCI AEROTECH DETROIT CHROME INC

119753 SUPPLIER NADCAP ID Supplier Nadcap Identification Number DCI AEROTECH DETROIT CHROME INC

119753 NADCAP CP Nadcap Accreditation - Chemical Processing DCI AEROTECH DETROIT CHROME INC

119753 NADCAP NDT Nadcap Accreditation - Non-Destructive Testing DCI AEROTECH DETROIT CHROME INC

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