Attachments.pdf

CONTRACT DATA REQUIREMENTS LIST Form Approved (1 Data Item) 0MB No. 0704-0188 for this collection of information is estimated to average 110 hours per response, including the time for maintaining the data needed, and completing and reviewing the collection of information. Send comme your to be

A. CONTRACT UNE ITEM NO. B. EXHIBDT

A

C. CATEGORY:

TOP TM OTHER

NDTI

D. SYSTEM/ITEM (A1O-18-020)

SUPPORT, STRUCTURAL

E. CONTRACT/PR NO.

FD2020-19-00123

F. CONTRACTOR

1. DATA ITEM NO.

AOO 1

2. TITLE OF DATA ITEM

Test/Inspection Report

3. SUBTITLE

4. AUTHORITY (Data Acquisition Document No.)

DI-NDTI-80809B/T

5. CONTRACT REFERENCE

CLIN for Data

6. REQUIRING OFFICE

416 SCMS/GUEAB

7. DO 250 REQ

i-sr's

LJLJ

9. 01ST STATEMENT

REQUIRED

10. FREQUENCY

('5mm ff?

tJi1iV1E

12. DATE OF FIRST SUBMISSION

i..T I A 1N/t,

14. DISTRIBUTION

a. ADDRESSEE

b. COPIES

8. APP CODE

A

11. AS OF DATE

N/A

13. DATE OF SUBSEQUENT

SUBMISSION

N/A

Dr ft Final

Peg

Repro

16. REMARKS

NSN: 1560-00-605-4570FJ

NOTE: Changes to office symbols and/or e-mail addresses, when necessary shall be made by letter through the CO/ACO without further revision to this CDRL.

1. BLK 4: Contractor's format is acceptable. Paragraph 10.2 of DI-NDTI-80809B is clarified as follows:

a. All dimensions and tolerances specified on the manufacturing data shall be listed in one column, with the actual corresponding reading obtained from the inspection of the part listed in another column.

b. Materials utilized in the manufacture of "First Article" item shall be identified and certified along with a copy ofmaterial purchase requests as conforming to applicable data requirements.

c. Material processing, including finish requirements (plating, heat treatment, welding, inspecting, anodize, painting, etc.) utilized in the manufacture of "First Article't item shall be identified and certified as conforming to applicable requirements. A copy of the purchase order certifying the process accomplished at other than contractor facility shall be included.

d. Other requirements as called out on Engineering Data Requirements.

2. BLK 9: The Distribution Statement, Export Control Warning and Destruction Notice shall be placed on the first sheet of each document and be located in a conspicuous location.

a. DISTRIBUTION STATEMENT "B": Distribution authorized to U.S.

Government agencies only (Test & Evaluation) (23 Oct 2018). Other requests for this document shall be referred to (416 SCMS/GUEAB, Hill AFB, UT 84056-5826).

EXPORT CONTROL WARNING: All technical documents/data (printed, digital/electronic) that are determined to contain export-controlled technical data, shall be marked with the following statement:

SEE BLK 16

15.TOTAL 0 1 0

G. PREPARED BY L

Nila Dagsen (Contractor Dataer)

H. DATE

23 Oct 2018

I. APPRO,VY / __-

Ryan ongineer)

J.DATE

23 Oct 2018

17, PRICE GROUP

NSP

15, ESTIMATED

TOTAL PRICE

0.00

DD FORM 1423-1, FEB 2001 PREVIOUS EDITION MAY BE USED. Page 1 of 2 Pages

CONTRACT DATA REQUIREMENTS LIST

(1 Data Item)

A. CONTRACT LINE ITEM NO. B. EXHIBIT C. CATEGORY:

I A TDP TM OTHER

NDT

[bYSTEM/ITEM (A1O-18-020) E. CONTRACT/PR NO. F. CONTRACTOR

I SUPPORT, STRUCTURAL FD2020- 19-00123

16. REMARKS (Continued)

b. EXPORT CONTROL WARNiNG: This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.) or the Export Administration Act of 1979 (Title 50, U.S.C., App. 2401 et seq.), as amended. Violations of these export laws are subject to severe criminal penalties. Disseminate lAW provisions of DoD Directive 5230.25.

c. DESTRUCTION NOTICE: For classified documents, follow the procedures, in DoD 5220.22-M, National Industrial Security Program Operating Manual (NISPOM), Section 5-705, or DoD 5200.1-R, Information Security Program Chapter VI. For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document.

3. BLKs 10, 11, 12,13,14:

a. For Contractor Testing - submit lAW the current delivery schedule.

b. For Government Testing - Report to assist in 'First Article" testing by the Air Force shall be submitted concurrently with the "First Article' item either in the packaging of the shipping container or separately if the report will not fit within the container packaging unfolded. When shipped in the "First Article" container, the report shall be enclosed in a paper or plastic envelop.

c. SHIP TO: FB2029 Non-Accountable Bay Transportation Officer Bldg. 849 West Hill AFB, UT 84056-5999

MARK FOR: 809 MXSS/MXDEB

7278 4th Street (Bldg. 100, Bay D) Hill AFB, UT 84056-5205

NOTE: If report is shipped separate from First Article item, send report to "MARK FOR" address listed above.

d. Contractor shall deliver a Test Report via e-mail to the following e-mail address: ryan.moore.18us.af.mil

DD FORM 1423-1, FEB 2001 Page 2 of 2 Pages

ENGINEERING DATA LIST

DATE:

18 JAN 2018

REVISION: 10 *HISTORY*

CAGE:

98747

PAGE:

NSN:

1560006054570FJ

DATA TECH:

Tilton, Richard J

END ITEM:

A-10 AIRCRAFT

ORGANIZATION/OFFICE SYMBOL:

429 SCMS GUMACB/

MANUFACTURER NAME:

OGDEN AIR LOGISTICS CENTER

REFERENCE NUMBER:

162D611621-1003A

NOUN:

SUPPORT,STRUCTURAL

LINE/

SUB CAGE

ENG DRAWING NUM/ ACCOMP

DOC NUM REV

NR

SHEETS

FURN

CODE

DIST

CODE NOUN REMARKS

L 98747 162D611621-1003A_01 R ASSY-TRUNNION

(CONFIGURATION ITEM)(3D

MODEL)

L 98747 TPR_162D611621-1003A_01 R ASSY-TRUNNION

(CONFIGURATION ITEM)(3D

MODEL)

L 98747 162D611621-2003A_01 R FITTING-TRUNNION (3D

MODEL)

L 98747 TPR_162D611621-2003A_01 R FITTING-TRUNNION

L 98747 162D637002-2001_02 R BUSHING (3D MODEL)

L 98747 TPR_162D637002-2001_02 R BUSHING

L 98747 162D611621-5001_02 R FORGING LANDING GEAR

TRUNION FITTING (3D MODEL)

L 98747 TPR_162D611621-5001_02 R FORGING - LANDING GEAR

TRUNION FITTING

L 77751 160C637001 H S BUSHING Tilton, Richard J 18 JAN 2018

(-1)

NAME: DATE:

L 76301 ST3M738 H S NUT SELF-LOCKING & NON

LOCKING BARREL

Tilton, Richard J 18 JAN 2018

(-10)

NAME: DATE:

L 98747 162S900701_03 R MATERIAL SUBSTITUTIONS Tilton, Richard J 18 JAN 2018

THIS SPECIFICATION IS AVAILABLE FROM THE TEAMCENTER REPOSITORY.

CONTACT THE APPROPRIATE A-10 DATA CONTROL ORGANIZATION

THROUGH THE GOVERNMENT PROCURING AGENCY FOR THE APPLICABLE

FILES.

NAME: DATE:

L 98747 162S900702_10 R PART SUBSTITUTION Tilton, Richard J 18 JAN 2018

THIS SPECIFICATION IS AVAILABLE FROM THE TEAMCENTER REPOSITORY.

CONTACT THE APPROPRIATE A-10 DATA CONTROL ORGANIZATION

THROUGH THE GOVERNMENT PROCURING AGENCY FOR THE APPLICABLE

FILES.

NAME: DATE:

L 77751 G-F101 C S DEBURRING & BLENDING OF

METALS

L 77751 G-J301 A S ETCH, PRIOR TO PENETRANT

INSPECTION

Tilton, Richard J 18 JAN 2018

WITH AM-1

NAME: DATE:

C - CLASSIFIED DOCUMENT.

S - FURNISHED WITH SOLICITATION.

M - STABLE BASE DRAWING REQUIRED; FURNISHED WITH

CONTRACT AWARD.

X - DATA SUPPLIED (NOT IN JEDMICS).

R - FURNISHED BY PCO UPON REQUEST.

P - PARTIAL DOCUMENT FURNISHED.

V - VENDOR DRAWING; (NOT PROVIDED).

G - GOV'T DOCUMENT.

O - OTHERS, CONTRACTOR MUST ACQUIRE.

A- DATA NOT AVAILABLE.

FURNISHED METHOD CODE LEGEND:

Page 1 of 2EDL Version 10Generated by PRPS using Jasper Reports on 06 Nov 2018

ENGINEERING DATA LIST

18 JAN 2018

REVISION: 10 *HISTORY*

CAGE:

98747

PAGE:

NSN:

1560006054570FJ

DATA TECH:

Tilton, Richard J

END ITEM:

A-10 AIRCRAFT

ORGANIZATION/OFFICE SYMBOL:

429 SCMS GUMACB/

MANUFACTURER NAME:

OGDEN AIR LOGISTICS CENTER

REFERENCE NUMBER:

162D611621-1003A

NOUN:

SUPPORT,STRUCTURAL

LINE/

SUB CAGE

ENG DRAWING NUM/ ACCOMP

DOC NUM REV

NR

SHEETS

FURN

CODE

DIST

CODE NOUN REMARKS

L 77751 G-R301 D S CHEMICAL CLEANING OF

METAL

Tilton, Richard J 18 JAN 2018

WITH AT-1

NAME: DATE:

L 77751 G-R302 A S PROCESS FORSOLVENT

CLEANING OF METALS

Tilton, Richard J 18 JAN 2018

WITH AT-1

NAME: DATE:

L 77751 M-40 E S INSPECTION OF HOLES,

FATIGUE/FRAC CRITICAL

PARTS

L 77751 SM160M1000 D S FATIGUE & FRACTURE,

CRITERIA & CONTROL OF

L 77751 Z-P401 D S PAINT-POLYURETHANE

APPLICATION OF

Tilton, Richard J 18 JAN 2018

WITH 15C0901-H

NAME: DATE:

L 26512 Z-P801 B S STORAGE, HANDLING,

SHIPPING

Tilton, Richard J 18 JAN 2018

WITH AT-1

NAME: DATE:

L 77751 Z-R701 C S MARKINGS & IDENTIFICATION

REQUIREMENTS

Tilton, Richard J 18 JAN 2018

WITH AT-1

NAME: DATE:

L 77751 Z-R901 F S GENERAL FINISH

SPECIFICATIONS, A-10

L 98747 HILL AFB FORM 462 X ENGINEERING DATA

REQUIREMENTS

STANDARD ENGINEERING TEXT

Tilton, Richard J 18 JAN 2018

ALL LINE ITEMS WITH FURNISH CODE "R" ARE LOCATED IN TEAM CENTER REPOSITORY AND CAN BE OBTAINED BY CONTACTING THE APPROPRIATE A-10 DATA CONTROL ORGINIZATION

THROUGH THE GOVERNMENT PROCURING AGENCY.

THE A-10 ENGINEERING NOTES ARE LISTED ON HILL AIR FORCE BASE FORM 462 (ATTACHMENT A).

RELEASE OF THIS DATA TO A FOREIGN OWNED, CONTROLLED OR INFLUENCED COMPANY IS DEPENDENT UPON THE APPROVAL OF THE FOREIGN DISCLOSURE OFFICE.

NAME: DATE:

C - CLASSIFIED DOCUMENT.

S - FURNISHED WITH SOLICITATION.

M - STABLE BASE DRAWING REQUIRED; FURNISHED WITH

CONTRACT AWARD.

X - DATA SUPPLIED (NOT IN JEDMICS).

R - FURNISHED BY PCO UPON REQUEST.

P - PARTIAL DOCUMENT FURNISHED.

V - VENDOR DRAWING; (NOT PROVIDED).

G - GOV'T DOCUMENT.

O - OTHERS, CONTRACTOR MUST ACQUIRE.

A- DATA NOT AVAILABLE.

FURNISHED METHOD CODE LEGEND:

Page 2 of 2EDL Version 10Generated by PRPS using Jasper Reports on 06 Nov 2018

REV: ENGINEERING DATA REQUIREMENTS

(ATTACHMENT “A”)

NOTE: MILITARY SPECIFICATIONS / STANDARDS WILL NOT BE FURNISHED IN THE BID SET.

1. THE FOLLOWING INSTRUCTIONS ARE FURNISHED FOR THE MANUFACTURE OF:

ASSY - TRUNNION, MLG, CWP (A-10)

2. PART NUMBER:

162D611621-1003

3. NATIONAL STOCK NUMBER:

1560-00-605-4570

PREPARED BY:

Ryan Moore

OFFICE SYMBOL:

GUEAB

20180118

HILL AFB FORM 462 Page 1 of 6

Distribution Statement: D: Distribution authorized to Department of Defense and U.S. DOD contractors only, for administrative and operational use. Date of determination is 7 March 2016. Refer other requests for this document to OO-ALC/508 ACSS/SU, Hill AFB, UT, 84056.

Destruction Notice: For classified document, follow the procedures in DOD 5220.22M, Industrial Security Manual, Section 11-19 or DOD

5200.1 R, Information Security Program Regulation, Chapter IX. For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document.

WARNING - the documents listed on this document and the associated Engineering Data List (EDL) contain technical data whose export is restrictive by the Arms Export Control act (Title 22, U.S.C., section 2751, et seq.), or the export administration act of 1979, as amended, title 50 U.S.C, Append 2401 et seq. Violators of these export laws are subject to severe criminal penalties.

4. THE TECHNICAL DATA PACKAGE (162D611621-1003) WAS DEVELOPED AND INTENDED TO BE PROVIDED IN SIEMENS NX FORMAT AS A MODEL BASED DEFINITION (MBD) DATASET IAW ASME Y14.41-2003 AND SHALL SERVE AS THE ENGINEERING BASELINE FOR THIS ACQUISITION. THIS INCLUDES 3-D MODELS AND EMBEDDED PRODUCTION AND MANUFACTURING INFORMATION (PMI) LAYERS. SOME OF THE REQUIRED PMI DATA FIELDS NEEDED FOR MANUFACTURING ARE OUTPUT IN A HUMAN READABLE FORMAT THAT THE GOVERNMENT WILL PROVIDE AS A “PART REPORT.” THE ASSOCIATED NX MODELS MAY BE AVAILABLE IN IGES/STEP FILE FORMAT;

REQUESTS FOR 3-D MODELS SHALL BE DIRECTED TO THE PCO.

5. THE PRIME CONTRACTOR MAY USE A TRANSLATOR TO CONVERT BETWEEN NX AND IGES/STEP IN SUPPORT OF THEIR SUBCONTRACTORS; HOWEVER, THE PRIME CONTRACTOR SHALL DEMONSTRATE THE TRANSLATION

PROCESS TO THE GOVERNMENT AND OBTAIN GOVERNMENT AUTHORIZATION TO PROCEED BEFORE

MANUFACTURING TO THE CONVERTED 3-D SOLID MODEL. FOR A TRANSLATOR TO BE AUTHORIZED, THE CONTRACTOR MUST SHOW THAT THE DELIVERED 3-D SOLID MODEL CONTAINS ALL OF THE NECESSARY INFORMATION REQUIRED TO ACCURATELY PRODUCE PARTS AS DEFINED IN THE ORIGINAL NX MODEL. THE 3-D MODELS SHALL DEFINE PRODUCT CONFIGURATION PER ASME Y14.41 MODEL ONLY (AKA “MODEL BASED

DEFINITION”) IN LIEU OF DRAWINGS.

6. THE CONTRACTOR IS RESPONSIBLE TO COMPLETELY RESEARCH ALL MANUALS, SPECIFICATIONS, AND

STANDARDS AND FULLY UNDERSTAND THE REQUIREMENTS NECESSARY FOR THE MANUFACTURE OF

COMPONENT PARTS AND ASSEMBLIES. ALL DEVIATIONS, MINOR AND MAJOR, FROM THE ENGINEERING DRAWING PACKAGE SHALL BE SUBMITTED TO THE PROPER A-10 ENGINEERING ORGANIZATION FOR COORDINATION AND

APPROVAL VIA DOD REQUEST FOR VARIANCE FORM DD1694 SUBMITTED THROUGH THE PCO.

7. WHEN MILITARY DOCUMENTS LISTED IN THE ENGINEERING DRAWING ARE CANCELLED THEY SHALL BE REPLACED BY THE INDUSTRY EQUIVALENT DOCUMENT SPECIFIED ON THE MILITARY DOCUMENT’S CANCELLATION NOTICE. THIS APPLIES TO THE ORIGINAL AIRCRAFT MANUFACTURER’S SPECIFICATIONS THAT ARE CITED IN THE DRAWING, AS WELL. THE CHARACTERISTICS OF TYPE, GRADE, CLASS, ETC. SPECIFIED IN THE CANCELLED MILITARY DOCUMENT SHALL BE MAINTAINED OR EXCEED THOSE CHARACTERISTICS WHEN APPLYING THE INDUSTRY EQUIVALENT DOCUMENT(S). WHEN THERE IS NO LISTED REPLACEMENT THE CONTRACTOR SHALL REQUEST AND RECOMMEND A SUBSTITUTE DOCUMENT FOR COORDINATION AND APPROVAL BY THE PROPER A-10 ENGINEERING ORGANIZATION VIA DOD REQUEST FOR VARIANCE FORM DD1694

SUBMITTED THROUGH THE PCO.

HILL AFB FORM 462 Page 2 of 6

8. USE OF ANY PROCESS OR MANUFACTURING TECHNIQUE WHICH CREATES A NET EDGE ON A METALLIC PART BY RELYING ON HEAT AT OR ABOVE THE PARTS MELTING POINT TO PRODUCE THE CUT IS NOT GENERALLY AUTHORIZED (I.E. LASER CUTTING, ELECTRICAL DISCHARGE MACHINE (EDM), PLASMA CUTTING, ETC.) WITHOUT PRIOR A-10 SYSTEM PROGRAM OFFICE APPROVAL. LIKEWISE, OTHER NON-HEAT GENERATING CUTTING PROCESSES INVOLVING HIGH PRESSURE FLUIDS AND SLURRIES (I.E., WATER JET) ARE ALSO NOT CURRENTLY APPROVED FOR USE IN THE PRODUCTION OF A-10 PARTS. ONLY THOSE PROCESSES CONTROLLED BY A-10 APPROVED PROGRAM SPECIFICATIONS AND A-10 DRAWINGS ARE PERMITTED TO BE USED IN THE MANUFACTURE

OF A-10 PARTS AND ASSEMBLIES.

9. FORGING REQUIREMENTS: IF THE FORGING SOURCE(S) IS KNOWN, THE CONTRACTOR MAY PROCURE FORGINGS FROM SOURCES PRE-APPROVED BY THE PROPER A-10 ENGINEERING ORGANIZATION TO BUILD THE 162D611621-5001 FORGING. IF FORGINGS ARE PROCURED FROM TOOLING APPROVED BY A-10 ENGINEERING, ORIGINAL CERTIFIED FORGING PROCEDURES AND DIES/TOOLING OR EQUIVALENT (E.G., REFURBISHED/RESUNK BY APPROVED FORGING SOURCE AND HAVING THE SAME DIE NUMBER DESIGNATION) SHALL BE USED. NEW TOOLING AT AN EXISTING SOURCE MUST BE QUALIFIED PRIOR TO CONTRACT AWARD, THE DETAILED PART BIDDER SHALL PROVIDE VERIFICATION (E.G., FORGING QUOTE) TO THE GOVERNMENT THAT THE CERTIFIED DIES AND PROCEDURES ARE AVAILABLE FOR THEIR USE IN THE EVENT THEY ARE THE SUCCESSFUL BIDDER.

10. IF THE FORGING SOURCE IS LISTED AS UNKNOWN OR THE CONTRACTOR WISHES TO DEVELOP ADDITIONAL SOURCES OR NEW TOOLING AT AN EXISTING FORGING SOURCE, THE CONTRACTOR SHALL ADVISE THE GOVERNMENT IN WRITING OF THEIR INTENT TO PROCURE NEW FORGING DIES AND THE PROPOSED FORGING SOURCE PRIOR TO CONTRACT AWARD. THE CONTRACTOR SHALL NOT PROCEED TO OBTAIN NEW DIES WITHOUT THE EXPRESS CONSENT OF THE GOVERNMENT PROCURING AGENCY. THE GOVERNMENT SHALL HAVE UNLIMITED USE OF THE DIES DEVELOPED UNDER THIS CONTRACT. THE CONTRACTOR SHALL INFORM THE FORGING HOUSE IN WRITING, AT THE SAME TIME THE ORDER FOR THE DIES IS PLACED, THAT THE GOVERNMENT HAS UNLIMITED USE RIGHT OF THE DIES AND FORWARD A COPY OF THIS LETTER TO THE GOVERNMENT CONTRACTING OFFICER.

11. PRIOR TO PRODUCTION, FORGING LOT QUALIFICATION SHALL BE ACCOMPLISHED AS SPECIFIED ON THE 162D611621-5001 PART REPORT. THE PRIME CONTRACTOR SHALL ASSURE THAT THIS HAS BEEN ACCOMPLISHED BY THE FORGING SOURCE AND RETAIN IN THEIR RECORDS FOR NO LESS THAN 10 YEARS. THE A-10 ENGINEERING

ORGANIZATION RESERVES THE RIGHT TO REVIEW THIS DOCUMENTATION AS NEEDED.

12. THE TRUNNION ASSEMBLY IS AN INTERCHANGEABLE ITEM IN ACCORDANCE WITH MIL-I-8500 AS DEFINED BY THE TECH DATA PACKAGE. INTERCHANGEABILITY, IN ACCORDANCE WITH MIL-I-8500, TO INCLUDE, ENHANCED WING ASSEMBLY (EWA) AND LEGACY WING COMPONENTS/ASSEMBLIES, SHALL BE PROVEN PRIOR TO FIRST ARTICLE ACCEPTANCE VIA FIRST ARTICLE DEMONSTRATION (FAD) EFFORT. THE CONTRACTOR SHALL BE RESPONSIBLE TO DEFINE THE METHOD OF CONTROLLING INDIVIDUAL INTERCHANGEABLE FEATURES, THROUGH THE USE OF TOOLING AND/OR OTHER MEANS AND SHALL SUBMIT A REPORT TO THE GOVERNMENT

REGARDING COMPLIANCE PLANS/PROCESSES WITH THESE REQUIREMENTS.

13. THIS PART IS CLASSIFIED AS A CRITICAL SAFETY ITEM (CSI) AND SHALL BE MANAGED IN ACCORDANCE WITH AFI 20-106. THE CRITICAL PROCESSES AND CHARACTERISTICS ARE IDENTIFIED FOR THE PART/ASSEMBLY AS DETAILED BELOW. THE METHOD OF OVERSIGHT SHALL BE COMMENSURATE WITH DCMA CSI MANAGEMENT

POLICY.

ATTRIBUTES/DATA LISTED IN THE FOLLOWING TABLES WITHIN BRACKETS (E.G. [FEATURE 1] OR [MINIMUM TORQUE]) CAN BE FOUND IN THE ASSOCIATED PART REPORT. REFERENCE ASSOCIATED PART REPORT(S) FOR CLARIFICATION. IF ANY DISCREPANCIES BETWEEN THE DATA IN THE TABLES BELOW AND THE ASSOCIATED

PART REPORT ARE IDENTIFIED, THE DATA IN THE PART REPORT SHALL TAKE PRECEDENCE.

HILL AFB FORM 462 Page 3 of 6

(13 cont’d)

Part Number 162D611621-1003

Description ASSY - TRUNNION, MLG, CWP (CONFIGURATION ITEM)

Critical Characteristic 1 MISC-01/01-Storage, Handling, Shipping; Storage, handling and shipping shall be in accordance with Z-P801.

Critical Characteristic 2 MACH-21/01-Deburr; Deburr part per P.S. 20024 or alternatively per G-F101.

Critical Characteristic 3 MACH-13/01-Local Surface Roughness; Maximum surface roughness of indicated area(s) to be [roughness] micro-inches Ra per ASME B46.1 (1995).

Critical Characteristic 4 BUSH-02/01-Bushing and Bearing Ream; Ream indicated hole(s) to dimensions shown in MBD dataset.

Critical Characteristic 5

ID-02/03-I only; This part/assembly is interchangeable in accordance with MIL-I-8500D and is controlled through control media. The interchangeable features of this part/assembly are: [feature1] [feature2] [feature3] [feature4] [feature5] [feature6] Mark part/assembly using P.S. 16001 rubber stamp or stencil methods only or alternatively Z-R701, code RS or ST with the following:

"INTERCHANGEABLE - DO NOT ALTER".

Critical Characteristic 6

BUSH-01/01-Press Fit Bushing Installation; Install indicated press fit bushing(s) and/or bearing(s) by applying MIL-PRF-23377, Type I, Class C primer to the outer diameter of the bushing or bearing and while primer is still wet, using a hydraulic/mechanical press, press bushing or bearing into hole until it is properly seated .

Subsequent to bushing or bearing installation apply AMS-S-8802 sealant to both ends of the bushing or bearing plus 0.12 to 0.25 inches of the surrounding housing surface, covering the interface. Care shall be taken to prevent application of sealant to any part of the bushing or bearing which may interfere with its function.

Critical Characteristic 7

018035 - Install indicated press fit bushing(s) by applying MIL-PRF-23377, Type I, Class C primer on the outer diameter of the bushing, and while primer is still wet, press bushing into hole using hydraulic/mechanical press until bushing is fully seated. No gap is permitted under the bushing flange. To aid bushing installation, it is optional to use one of the following methods to cold shrink bushing(s) prior to installation: (a) place in liquid nitrogen until the resultant bubbling of the liquid nitrogen stops, (b) place in bath of dry ice and isopropyl or methyl alcohol mixture until the resultant bubbling of the bath stops, or (c) chill in a 0 degrees Fahrenheit or lower freezer for a minimum of 8 hours. When the cold shrink method is used, apply primer to the non-chilled mating surfaces of the hole and install the bushing(s) while primer is still wet.

Critical Characteristic 8 018015 - To meet the noted dimension, the entire surface of each applicable flat bushing flange shall be faced after installation of bushings per Note #9. It is permissible to pre-machine bushing face(s), provided requirements of this note are met.

HILL AFB FORM 462 Page 4 of 6

Part Number 162D611621-2003

Description FITTING - TRUNNION, LANDING GEAR

Critical Characteristic 1 CRIT-01/01-Class 1A; This is a Fatigue and Fracture Critical part, Class 1A, in accordance with SM160M1000.

Critical Characteristic 2 MISC-01/01-Storage, Handling, Shipping; Storage, handling and shipping shall be in accordance with Z-P801.

Critical Characteristic 3

NDT-02/01-Penetrant; Prior to shot peening, penetrant inspect per ASTM E1417. Pre- penetrant etch per P.S.

12050 or G-J301 to remove 0.0002 to 0.0005 inches from each surface prior to penetrant inspection. Relevant linear indications are unacceptable. Linear indications are those indications in which the length is more than three times the width. Evaluate all rounded penetrant indications 0.016 inch diameter and larger under visible light and accept any rounded voids up to 0.005 inch diameter. Reject two or more voids in the range of

0.005 to

0.009 inch diameter which are located with 0.25 inch edge to edge or any single void with a diameter of 0.010 inch diameter or larger.

Critical Characteristic 4 NDT-19/01-Hole Inspection - A2; Inspect [feature description] to quality level A2 in accordance with QATB M- 40.

Critical Characteristic 5 MACH-19/01-Roughness - Surface Specific; Unless otherwise noted, maximum surface finish of [feature(s)] to be [roughness] micro-inches Ra per ASME B46.1 (1995).

Critical Characteristic 6 MACH-08/01-Break Edges; Prior to shot peening, unless otherwise noted, break all sharp edges [lower] to [upper] inches per P.S. 20024 or alternatively per G-F101.

Critical Characteristic 7 SP-13/01-Sat Peen Variable-Omit Holes; Shot peen all surfaces, except holes, per AMS 2430 to provide 200% coverage, using an Almen intensity of [intensity] and a shot size of [lower limit] to [upper limit]. Holes present in the part at the time of shot peening shall be suitably plugged/masked to prevent peening and damage of the holes.

Critical Characteristic 8 FIN-09/01-Sulf Anodize; Sulfuric acid anodize per MIL-A-8625, Type II, Class 1.

Critical Characteristic 9

MACH-11/01-Mismatch; Unless otherwise specified, general surface mismatch shall not exceed [general mismatch] inches. Mismatch within 0.060 inches of the tangency of intersecting features (such as the intersection of a corner radius and the side of a stiffener) shall not exceed [feature mismatch] inches, except that mismatch at intersections of equal height flanges and stiffeners shall not exceed [height mismatch] inches. The fillet radius associated with any surface mismatch shall be [minimum fillet] inches minimum.

Critical Characteristic 10

GDT-02/01-Restraint; The part shall be capable of being brought to the datum simulators by applying up to five pounds of force within any twelve-inch interval or an equivalent force within a smaller interval (e.g., half the allowed force at six-inch intervals, one quarter of the allowed force at three-inch intervals). Any number of allowed force units may be applied as long as the equivalent forces and intervals are maintained.

Critical Characteristic 11 MACH-01/01-Roughness; Unless otherwise noted, maximum surface roughness of part to be 125 micro-inches Ra per ASME B46.1 (1995).

Critical Characteristic 12 MACH-09/01-Blend; All corner radii intersecting plane surfaces shall blend smoothly from [lower] to [upper] corner radius.

HILL AFB FORM 462 Page 5 of 6

Critical Characteristic 13 GEN-09/01-Material Sub; Material substitution permissible per 162S900701.

Critical Characteristic 14

ID-02/03-I only; This part/assembly is interchangeable in accordance with MIL-I-8500D and is controlled through control media. The interchangeable features of this part/assembly are: [feature1] [feature2] [feature3] [feature4] [feature5] [feature6] Mark part/assembly using P.S. 16001 rubber stamp or stencil methods only or alternatively Z-R701, code RS or ST with the following:

"INTERCHANGEABLE - DO NOT ALTER".

Part Number 162D611621-5001

Description FORGING -LANDING GEAR TRUNNION FITTING

Critical Characteristic 1 CRIT-01/01-Class 1A; This is a Fatigue and Fracture Critical part, Class 1A, in accordance with SM160M1000.

Critical Characteristic 2 FORG-02/01-Grain Flow; Primary grain flow shall be as shown in the MBD dataset.

Critical Characteristic 3 FORG-03/01-Grain Flow; First article grain flow verification shall be accomplished by sectioning and etching per AMS 2375 at locations as shown in the MBD dataset. Grain flow shall conform to the general shape of the forging and shall have no re-entrant flow lines.

Critical Characteristic 4

FORG-04/01-FA Tensile; First article tensile property verification shall consist of testing specimen numbers [number1] thru [number2] in accordance with ASTM E8. Sample orientation and location, within the forging, shall be as shown in the MBD dataset. Specimen geometry shall be in accordance with ASTM E8 using a minimum gage diameter of 0.25 inches.

Critical Characteristic 5 FORG-06/01-Tensile; Recurring lot tensile property verification shall consist of testing specimen number [number1] in accordance with ASTM E8. Sample orientation and location, within the forging prolongation, shall be as shown in the MBD dataset. Specimen geometry shall be in accordance with ASTM E8 using a minimum gage diameter of 0.25 inches. Testing frequency shall be a minimum one specimen for every [number 2] forgings, or portion thereof, per forging lot.

Critical Characteristic 6 NDT-07/01-Sonic Inspect; Ultrasonically inspect finished forging per AMS-STD-2154, Class A.

Critical Characteristic 7 FORG-09/01-Tensile Req'ts; Minimum acceptance criteria for tensile specimen [number 1] shall be:

Specimen Orientation: [orientation 1] Ultimate Tensile Strength: [number 2] ksi Tensile Yield Strength:

[number 3] ksi Elongation: [number 4]%

Critical Characteristic 8 FORG-09/01-Tensile Req'ts; Minimum acceptance criteria for tensile specimen [number 1] shall be:

Specimen Orientation: [orientation 1] Ultimate Tensile Strength: [number 2] ksi Tensile Yield Strength:

[number 3] ksi Elongation: [number 4]%

Critical Characteristic 9 FORG-09/01-Tensile Req'ts; Minimum acceptance criteria for tensile specimen [number 1] shall be:

Specimen Orientation: [orientation 1] Ultimate Tensile Strength: [number 2] ksi Tensile Yield Strength:

[number 3] ksi Elongation: [number 4]%

Critical Characteristic 10 FORG-09/01-Tensile Req'ts; Minimum acceptance criteria for tensile specimen [number 1] shall be:

Specimen Orientation: [orientation 1] Ultimate Tensile Strength: [number 2] ksi Tensile Yield Strength:

[number 3] ksi Elongation: [number 4]%

Critical Characteristic 11 FORG-09/01-Tensile Req'ts; Minimum acceptance criteria for tensile specimen [number 1] shall be:

Specimen Orientation: [orientation 1] Ultimate Tensile Strength: [number 2] ksi Tensile Yield Strength:

[number 3] ksi Elongation: [number 4]%

Critical Characteristic 12 FORG-09/01-Tensile Req'ts; Minimum acceptance criteria for tensile specimen [number 1] shall be:

Specimen Orientation: [orientation 1] Ultimate Tensile Strength: [number 2] ksi Tensile Yield Strength:

[number 3] ksi Elongation: [number 4]%

HILL AFB FORM 462 Page 6 of 6

Critical Characteristic 13 FORG-09/01-Tensile Req'ts; Minimum acceptance criteria for tensile specimen [number 1] shall be:

Specimen Orientation: [orientation 1] Ultimate Tensile Strength: [number 2] ksi Tensile Yield Strength:

[number 3] ksi Elongation: [number 4]%

Critical Characteristic 14 FORG-09/01-Tensile Req'ts; Minimum acceptance criteria for tensile specimen [number 1] shall be:

Specimen Orientation: [orientation 1] Ultimate Tensile Strength: [number 2] ksi Tensile Yield Strength:

[number 3] ksi Elongation: [number 4]%

Critical Characteristic 15 FORG-09/01-Tensile Req'ts; Minimum acceptance criteria for tensile specimen [number 1] shall be:

Specimen Orientation: [orientation 1] Ultimate Tensile Strength: [number 2] ksi Tensile Yield Strength:

[number 3] ksi Elongation: [number 4]%

Critical Characteristic 16 FORG-12/01-Flash; Flash extension tolerance is [dimension 1] inches maximum.

Critical Characteristic 17 FORG-01/01-First Art; Forging first article approval and production control shall be in accordance with AMS 2375.

Critical Characteristic 18 MISC-01/01-Storage, Handling, Shipping; Storage, handling and shipping shall be in accordance -P801.

406 SCMS/GULAA-Hill October1, 2015

Statement Of Work (SOW) for Packaging & Preservation

ASSIST Documents for Specifications Listed in the GSA Index of Federal Specifications, Standards and Commercial Item Descriptions The contractor shall use the public ASSIST Quick Search website to access specification, standards, data item descriptions documents listed in this contract solicitation:

http://quicksearch.dla.mil

PRESERVATION, PACKAGING & MARKING REQUIREMENTS

The contractor shall develop, implement and maintain the preservation, packaging and packing of all items to be delivered under the terms of this contract. Packaging procedures will be established in accordance with AFMCI 24-

201, specifically Paragraph 3.7 and MIL-STD-2073-1, Standard Practice for Military Packaging (current revision);

Packaging requirements are identified in the AFMC Form 158, Packaging Requirements submitted by the responsible packaging specialist. All “markings and labeling” of shipments shall conform to MIL-STD 129, DoD Standard

Practice, Military Marking for Shipment and Storage (current revision)

INTERNATIONAL STANDARDS FOR PHYTOSANITARY MEASURES (ISPM NO. 15)

REQUIREMENTS

The contractor shall use the wood packaging material regulation for international trade which describes phytosanitary

(including treatments) that have been approved for wood packaging material and provides for the approval of new or revised treatments. Use the latest revision of (ISPM No. 15), and the following statement complies with the United

Nations-implemented restrictions on wood packaging material (WPM). “This requirement is specifically concerned with invasive species such as pinewood nematode. WPM is defined as wood pallets, skids, load boards, pallet collars, wooden boxes, reels, dunnage, crates, frames, and cleats. The statement below cites the requirements in detail and covers lumber for building containers and pallets used for deliveries resulting in worldwide shipments (direct vendor deliveries, Air Logistics complex (ALC), Container Consolidation Points (CCP), Aerial Ports, Water Ports, or other

DoD installations.):

ELECTROSTATIC MATERIAL (When Applicable) The Contractor shall apply provisions of MIL-STD-1686 (current revision) when identifying all solid state devices and modules containing diodes, translators, integrated circuits and/or other microelectronic components sensitive to electrostatic forces. All such items shall be packaged IAW MIL_STD 2073-1 using electrostatic free barrier materials and shall clearly bear “Electrostatic Sensitive Device” labels IAW MIL-STD 129, Department of Defense Standard

Practice Military Marking for Shipment and Storage.

REUSABLE CONTAINERS

The contractor shall safeguard all received reusable shipping containers that meet the requirements of the AFMC

Form 158 and are suitable for return shipment of serviceable assets. The contractor shall dispose of and replace unserviceable containers with new containers that meet requirements of the AFMC Form 158. Contact the

Administering Contracting Office (ACO) for disposition and replacement when Long Life Reusable Containers

(LLRC) are received in an unserviceable condition.

SOW for Packaging & Preservation Standards (Cont.) October 1, 2015

REPORTING DISCREPANCIES

The contractor shall use Web Supply Discrepancy Report (WebSDR) to submit/reply to an Supply Discrepancy

Report (SDR), when improperly packed assets are received/shipped in other than the contracted packaging requirements (coded data or Special Packaging Instructions (SPI) drawings) from Department of Defense (DoD) components/ or contractor activities.

The contractor shall request for a WebSDR account via the following URL:

https://www.transactionservices.dla.mil/daashome

(See Defense Logistics Management (DLM) 4000.25-M, Volume 2, Supply Standard and Procedures, Chapter 17, Supply Discrepancy Reporting, http://www2.dla.mil/j-6/dlmso/elibrary/manuals/dlm/dlm_pubs.asp ).

Exceptions when no damage has occurred are as follows:

- Items packaged before the current SPI date.

- An alternate pack may be used, provided the prime Air Force Sustainment Complex, Packaging office at the Air

Logistics Complex (ALC) approves and issues a waiver, deviation number, which would be annotated on the exterior container on the lower right hand portion of the identification side of the container.

- In accordance with Technical Order (T.O.) 00-85B-3, How to Package Air Force Spares, the contractor may substitute the next larger size fast pack, of the type I or type II to ship transportation priorities 1 and 2 shipments as long as there is no decrease in any of the container dimensions without the requirement of a waiver deviation. T.O.

00-85-3, can be access via the website: http://www.tinker.af.mil/shared/media/document/AFD-061220-059.pdf

HAZARDOUS MATERIALS (When Applicable) The contractor shall ensure Hazardous shipments comply with International Civil Aviation Organization (ICAO), U.S.

Code of Federal Regulations (CFR) Title 49, International Air Transport Association (IATA) Dangerous Goods

Regulation, International Maritime Dangerous Goods Code (IMDG, Annex 1), and AFMAN24-204_IP, Preparing

Hazardous Materials for Military Air Shipments. Packaging shall meet “DOT specification or a United Nation (UN) specification ” manufactured in accordance with 49 CFR, Part 178 and the final packages assembled IAW 49 CFR, Parts 100-185 as applicable. A Competent Authority Approval (CAA) shall be acquired from the responsible

Associate Administrator or other designated Department official to perform a function requiring prior consent under the Hazardous Material Regulation (HMR). Packages(s) shall be marked IAW MIL-STD-129, DoD Standard

Practice, and Military Marking for Shipment and Storage. If a symbol is used to represent the manufacturer or the approval agency certifying compliance with 49 CFR 178, subparts L and M, the symbol must be registered with the

U.S. Department of Transportation. A copy of the Contractor’s Test Report and signed certification that the package configuration meets both CFR and UN requirements shall be made available to the procuring contract office, as required, prior to acceptance or shipment of any portion of the product IAW Contract Data Requirements List

(CDRL) (Reference AFMC Form 158). Safety Data Sheets (SDS) are required for known hazardous items and applicable items shown in FED-STD-313, Tables I and II. The SDS shall have any applicable identification number, such as National Stock Number or Special Item Number. A copy of the SDS shall be mailed or e-mailed no later than

“FIVE” days prior to contractual delivery of items:

AFMC

406 SCMS/GULAA

Attn: Michael S, Merrill

Packaging Specialist

E-mail: michael.merrill.4@us.af.mil

DSN # 777-1460

https://www.transactionservices.dla.mil/daashome http://www2.dla.mil/j-6/dlmso/elibrary/manuals/dlm/dlm_pubs.asp http://www.tinker.af.mil/shared/media/document/AFD-061220-059.pdf

SOW for Packaging & Preservation (Cont) October 1, 2015

APPLICABLE GOVERNMENT PACKAGING DOCUMENTS

NOTE: “UTILIZE THE MOST RECENT POLICY”

AFI 24-203, Preparation and Movement of Air Force Cargo

AFMAN 24-204_IP, Preparing Hazardous Materials for Military Air Shipments

AFMCI 24-201, AFMC Packaging and Materials, Handling Policies and Procedures

DLMS 4000.25-M, Defense Logistics Management Systems (DLMS), Volume 2, Supply

Standards and Procedures, Chapter 17, Supply Discrepancy Reporting

DoD 4140.01-M-1, Compliance for Defense Packaging: Phytosanitary Requirements for

Wood Packaging Material (WPM)

DOT Title 29, Occupational Safety and Health Administration, Labor

DOT Title 49, Code of Federal Regulations (49 CFR), Transportation

International Civil Aviation Organization (ICAO) Technical Instructions

International Air Transport Association (IATA) Dangerous Goods Regulation

International Maritime Dangerous Goods (IMDG) Code

ISPM No. 15, International Standard Phytosanitary Measure

Note: Marking Requirements can be found in the American standards committee, incorporated wood packaging material enforcement regulations dated November 11, 2005 and IPSM 15 No. 15.

MIL-STD-2073-1, Standard Practice, for Military Packaging

MIL-STD-129, Department of Defense Standard Practice Military Marking for Shipment and Storage

MANUFACTURING QUALIFICATION REQUIREMENTS

NSN: 1560-00-605-4570

P/N: 162D611621-1003 Noun: FITTING – TRUNNION, LANDING GEAR Application: A-10

16 Jan 2018 Section C 1/3

SECTION C:

1. QUALIFICATION REQUIREMENTS THAT MUST BE SATISFIED TO BECOME A QUALIFIED SOURCE

a. Prequalification Notice/Sources Sought: The offeror shall notify the appropriate government Small Business Office or, if responding to a solicitation, the contracting officer in the appropriate government contracting office, of intent to qualify as a source for this FITTING – TRUNNION, LANDING GEAR. The offeror shall prepare a Source Approval Request (SAR) in accordance with AFMCI 23-113 and submit to 416th SCMS/GUEAB for their review and approval.

b. Facilities, Testing, and Inspection Capabilities: The offeror must certify to the government that they have, or have access to, the required facilities and equipment to manufacture, inspect, test, package, and store the item. The offeror shall make their facilities, equipment, tooling, and personnel available for evaluation and inspection by the government.

c. Data Verification: The offeror must verify that he has a complete data package. This verification must include a complete list of all procedures, drawings, 3D CAD models and specifications, including change notices, in the offeror’s possession. The offeror may also be required to produce copies of all applicable procedures, drawings, or specifications.

d. Manufacture/Process Verification: The offeror must manufacture this item to conform to the government requirements as prescribed within the ESA-approved engineering/technical data package. The offeror must show compliance with Unique Identification (UID) requirements in accordance with DFARS 211.274 as prescribed within the ESA-approved engineering/technical data package. The offeror must provide, at their own expense, data showing the results of all quality, performance, and environmental evaluations conducted by the offeror to show compliance with the government requirements as prescribed by 416 SCMS/GUEAB. The offeror shall also identify its sources for materials and its standards for internally used processes. This item is classified as a Critical Safety Item (CSI) and must be managed as such. The offeror must also provide evidence in the form of a management process in which they will manage Critical Safety Items (CSIs) and all of the critical characteristics and critical safety processes.

e. Test and Evaluation and/or Verification: The offeror, at their own expense, shall prepare and submit to 416 SCMS/GUEAB for their prior approval, a qualification test plan/procedure detailing how they intend to verify compliance with all performance, environmental, mechanical, and quality assurance requirements identified by the complete engineering Technical Data Package. After completion of the approved qualification testing, the offeror shall be required to submit a complete test report of the results to 416 SCMS/GUEAB for their review and approval prior to the contract award. The government retains the right to exercise the option to inspect the testing processes, including on-site witnessing of any or all documented testing. To allow accomplishing this, the offeror shall notify the government at least 30 days in advance of the occurrence of any testing that will be used as a basis for qualification. The offeror’s facilities shall be made available for government inspection during these tests.

P/N: 162D611621-1003

16 Jan 2018 Section C 2/3

f. Qualification Article Verification: The offeror must provide, at their own expense, a pre-contract award qualification article for evaluation by the government. This article must comply with all of the requirements of the complete engineering Technical Data Package. This article shall be subjected to a form, fit, and function evaluation to demonstrate compatibility with the weapon system and to evaluate the manufacturing capability of the offeror. Offerors will be notified whether or not their qualification article passed or failed the required qualification testing within 90 days of submitting a product for qualification testing. Note that successful completion of the qualification testing does not guarantee any contract award. If the offeror is deemed qualified and awarded the contract, a post-contract award first article exhibit may be required to verify production capability.

g. Qualification Requirement Cost Estimate: Estimated likely costs for testing and evaluation, which will be incurred by the potential offering party to become qualified: $1,750.

h. Qualification Time Completion Estimate: It is the estimate of the engineering support activity that completion of this qualification effort should require 120 days. This is based on complexity of the FITTING – TRUNNION, LANDING GEAR and other factors.

i. Qualification Time Limitation: An offeror may not be denied the opportunity to submit and have considered an offer for a contract if the offeror can demonstrate to the satisfaction of the contracting officer that the offeror (or its product) meets these standards for qualification or can meet them before the date specified for award of the contract. The award will not be delayed to provide the vendor with an opportunity to demonstrate its ability to meet the standards specified in this qualification requirement.

j. Evaluation of Proposals Not Previously Qualified: The offeror must be fully qualified in order to be eligible for a contract award. Therefore, the offeror must fulfill all of the requirements stated, in writing, in the qualification requirement before the date specified for award of the contract. Once all requirements are met, the offeror will be listed as an approved source for this item. Approval, however, does not guarantee subsequent contract award.

P/N: 162D611621-1003

16 Jan 2018 Section C 3/3

2. SOURCE QUALIFICATION WAIVER REQUIREMENTS

Sources who meet any of the following source Qualification Waiver Criteria (QWC) may apply for a waiver of all or part of the qualification requirements. If a waiver is granted and the offeror is awarded a contract, the offeror may still be required to provide a post-contract award first article exhibit to verify production capability:

a. QWC1: The potential source submits written certification that the articles have been supplied to the government or original equipment manufacturer (e.g., DD Form 250, Material Inspection and Receiving Report, Purchase Order invoice, etc).

b. QWC2: The potential source is qualified on the right-hand article and requests to be qualified on the left-hand article. If the right-and left-hand articles are mirror images of each other, then approval can generally be given.

c. QWC3: A source qualified to provide an assembly is usually qualified to provide subassemblies, major components, and items of that assembly.

d. QWC4: A source qualified to provide earlier dash numbers of a basic P/N may be qualified to provide other dash numbers of that same basic P/N, provided there is no increase in complexity, criticality, or other relevant requirements.

e. QWC5: A source qualified to provide a similar or like item can be qualified to provide the required item. However, for approval, the engineering authority must verify that there is no increase in complexity, criticality, or other requirements over that of the similar item. At a minimum, the source shall provide a complete set of drawings for the similar item and written proof, such as purchase orders, shipping documents, etc., to show that the similar item was provided to the original equipment manufacturer or DoD.

f. QWC6: A source previously qualified to provide an item, but which has been purchased, sold, merged, absorbed, reformed, split, etc., may qualify if it can be established that the qualification is currently with the requester and that the requester has the same or equivalent facilities, tooling, equipment, personnel, and utilizes the original forging, castings, etc., in the manufacturing process.