Tab_12_SPE4AX-15-R-0005_Aircraft_Assembly_PID_Pack_Info.TXT

*** LTC PID Packaging Consolidated Text *** PLEASE SEE GLOSSARY AT THE END OF THE DOCUMENT FOR FULL TEXT OF THE ITEM DESCRIPTION

AND PACKAGING REFERENCE NUMBERS CALLED OUT FOR EACH NSN.

NSN:002148546

SUPPORT, STRUCTURAL

THE FOLLOWING EXCEPTIONS TO DWG: 9-25283 APPLY:

DWG: 9-25283(-8), E.O.# R 83C0001 & 2004C0091, NOTES:1-14

REFERENCE NUMBER:ZD004

1.,,PART MARKING PER MIL-STD-130, METHOD PER THE DRAWING REQUIREMENTS

AND BAC 5307. MARKING MUST INCLUDE NATIONAL STOCK NUMBER, PART NUMBER,

CURRENT DESIGN AUTHORITY CODE (98748), ACTUAL MANUFACTURER'S CAGE CODE

(-----), DATE OF MANUFACTURE, AND "FOR MILITARY USE ONLY". PARTS WILL

NOT BE MARKED WITH THE ORIGINAL DESIGN AUTHORITY (BOEING) CAGE CODE.

2.,,DELETE REFERENCE TO D2-5000 AND BAC 5005.

3.,,SURFACE TEXTURE PER ASME B46.1 IN LIEU OF BACD 2097.

4.,,DIMENSIONS AND TOLERANCES PER ASME Y14.5.

5.,,7075 ALUMINUM ALLOY FORGING PER SAE AMS-QQ-A-367 ALUMINUM ALLOY

FORGINGS IN LIEU OF QQ-A-367.

6.,,INSPECT FOR MECHANICAL PROPERTIES PER BMS 7-186 IN LIEU OF BAC

D-10875.

7.,,OPTIONAL TO OMIT RAISED LETTERING. OMIT REFERENCE TO THE WORD

"BOEING".

8.,,OPTIONAL TO PENETRANT INSPECT PER ASTM E1417 IN LIEU OF BAC 5423.

9.,,FINISH CODE F-2.10 DEFINED: APPLY NO FINISH, EXCEPT THAT TEMPORARY

PROTECTION MAY BE APPLIED FOR TRANSPORTATION, HANDLING, AND STORAGE.

10.,,FINISH CODE F-2.30 DEFINED: CHEMICAL TREAT ACCORDING TO

MIL-DTL-5541, CLASS 1A OR ANODIZE ACCORDING TO MIL-A-8625, TYPE I OR IC

(PREFERRED), CLASS 1. APPLY MIL-PRF-23377, TYPE I, CLASS C2 PRIMER TO A

DRY FILM THICKNESS OF 0.0003 TO 0.0005 INCH ACCORDING TO THE

MANUFACTURERS APPLICATION INSTRUCTIONS AND MIL-F-18264.

11.,,DELETE REFERENCE TO ".203 (.228/.203) DIA HOLE (2 PLACES) MX839.

12.,,SHOT PEEN PER SAE AMS 2430. THE LENGTH OF MACHINED PART MUST BE

PARALLEL TO THE LONGITUDINAL GRAIIN DIRECTION OF THE FORGED BILLET.

13.,,WHEN X'ED BELOW OR LISTED IN THESE NOTES, DEFINITIONS APPLICABLE TO

THIS PRODUCT ARE OR HAVE:

(A) ENGINEERING CRITICAL IN APPLICATION: An item, which requires special manufacturing processes, controls, and testing of material or end items.

Because of its use or application, failure to maintain the highest reliability of such an item could be catastrophic resulting in loss of life or serious injury, loss of a weapon system or extensive secondary damage, with direct impact on the capability to respond to a national emergency or to achieve wartime sustainability.

(B) CRITICAL CHARACTERISTICS: Characteristics which, when defective, are likely to result in hazardous or unsafe conditions for individuals using, maintaining or depending upon the product; or, are likely to prevent performance of the tactical function of a major end item such as an aircraft, missile, space vehicle, engine or a major part thereof.

(Derived from MIL-STD-1916).

(C) MAJOR CHARACTERISTICS: Characteristics (other than critical or minor), which, when defective, are likely to result in failure or to reduce the usability of the product or a major end item for its intended purpose. (Derived from MIL-STD-1916).

(D) MINOR CHARACTERISTICS: All characteristics not designated as critical or major but for which full conformity is required

(E) COMPLEX: Items having quality characteristics not wholly visible (hidden characteristics), in the end product for which contractual conformance must be established progressively through precise measurements, tests or controls applied during purchasing, manufacturing, performance, assembly and functional operation either as an individual item or in conjunction with other items [FAR SUBPART 46.203(b)].

(F). COMMERCIAL: Described in commercial catalogs, drawings or industrial standards [FAR SUBPART 46.203(a), (1)].

THIS PRODUCT HAS BEEN DETERMINED TO BE OR CONTAINS (AS X'ED BELOW):

__X__,, Engineering critical in application.

______ Critical characteristics.

__X___ Major characteristics.

__X___ Minor characteristics, all except critical and major.

______ Complex.

______ Available as a commercial product.

14.,,When materials, processes or components are to be obtained from directed sources as indicated herein or in the specifications, alternate sources may only be utilized upon prior approval by the contracting officer of this procuring activity as a deviation.

Bidders shall notify this procuring activity at the time of quotation of any drawing, specification or standard which is of more current data revision than those shown on the data listing or in these engineering notes. Determination of acceptability of the more currently dated data will be made by the responsible engineering office of this procuring activity.

Lower tier specifications listed in or referenced by first tier specifications may not be shown on the data lists or engineering notes accompanying this contract but are nonetheless required by this contract for compliance. Exceptions would occur only when such lower tier requirements have been specifically waived or substitute specifications/requirements are designated herein.

Reports, process sheets, inspection methods sheets and all other documents required by specifications imposed by this contract for contractor compliance which were previously required to be submitted to a prime design contractor shall be held at that facility for review by government personnel.

When prime design source specifications require or provide for participation by that prime source quality, manufacturing, laboratory or engineering support services, these requirements or provisions do not apply when the contract was issued by this procuring activity. For these services or direction pertaining thereto, contact the cognizant government contract administration office or this procuring activity for assistance.

The contractor is responsible for assuring that all dimensions, conditions, tests and test results identified in these engineering notes, applicable drawings, specifications and contract quality requirements are met by themselves and their suppliers. This requirement applies to all characteristics whether those characteristics have been specifically designed as being critical, major or are those minor characteristics not specifically designated as such.

PROCESS DATA REQUIREMENTS (X'ED WHEN APPLICABLE)

____Prior to beginning of manufacture, the contractor will notify the engineering office of this procuring activity of all manufacturing process and processing procedures intended for use in production of this product. Once these processes are established, no changes shall be made without prior approval of the engineering office of this procuring activity.

SERIALIZATION OF PARTS (X'ED WHEN APPLICABLE)

_____Serialization of each part/assembly (contract end item) is required.

REFERENCE NUMBER:ZD059

REFERENCE NUMBER:A0003

REFERENCE NUMBER:CS001

REFERENCE NUMBER:Q0106

CRITICAL APPLICATION ITEM

IAW BASIC DRAWING NR 81205 9-25283

REVISION NR E DTD 08/29/1960

PART PIECE NUMBER: 9-25283-8

IAW REFERENCE DRAWING NR 81205 BAC5423

REVISION NR W DTD 09/15/2005

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 9-25283

REVISION NR E DTD 12/08/2004

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5009

REVISION NR AA DTD 06/22/1993

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5009

REVISION NR AA DTD 12/05/2011

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BMS7-186M

REVISION NR M DTD 05/16/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5423

REVISION NR W DTD 09/02/1999

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5307

REVISION NR T DTD 05/28/2013

PART PIECE NUMBER:

PREP FOR DELIVERY

LINE ITEM 00001 TYPE OF COVERAGE: DLA DIRECT, CONUS

PKGING DATA-QUP:001

SHALL BE PACKAGED IN ACCORDANCE WITH HAZARDOUS

MATERIALS PACKAGING REQUIREMENTS.

PACKAGING: PACKAGING FOR HAZARDOUS MATERIALS

SHALL COMPLY WITH APPLICABLE REGULATIONS, I.E.,

TITLE 49 CODE OF FEDERAL REGULATIONS,

INTERNATIONAL CIVIL AVIATION ORGANIZATION (ICAO)

TECHNICAL INSTUCTIONS (EXCLUDING PARAGRAPH 1.4

OF CHAPTERS 1 AND 3), AND INTERNATIONAL MARITIME

DANGEROUS GOODS CODE (IMDG). BOTH ICAO AND IMDG

COMPLY WITH UNITED NATIONS (UN) RECOMMENDATIONS

ON TRANSPORT OF DANGEROUS GOODS. WHEN A);

CONTRACT/ORDER FOR HAZARDOUS MATERIALS REQUIRES

SHIPMENT THROUGH A MILITARY AERIAL PORT FOR

TRANSPORT VIA MILITARY AIRCRAFT, PACKAGING SHALL

COMPLY WITH DLAI 4145.3, PREPARING HAZARDOUS

MATERIALS FOR MILITARY AIR SHIPMENT.

LABELING AND MARKING: ALL INTERIOR AND EXTERIOR

CONTAINERS SHALL BE LABELED AND MARKED AS

SPECIFIED IN THE REFERENCED PRODUCT

SPECIFICATION, AND/OR AS SPECIFIED IN SECTION D

OF THE CONTRACT OR ORDER. IN ADDITION, ALL

LABELING AND MARKING SHALL COMPLY WITH THE

REQUIREMENTS OF MIL-STD-129, 49 CFR, 29 CFR,

AND, AS APPLICABLE, ICAO TECHNICAL INSTRUCTIONS,

IMDG ANNEX 1, AND/OR DLAI 4145.3.

CERTIFICATION: ALL PACKAGING PERFORMANCE TEST

REQUIREMENTS SHALL BE SUPPORTED BY CERTIFICATES

AND REPORTS ATTESTING TO DATE OF TESTING AND

DATA RESULTS OBTAINED FROM TESTING. THE

CONTRACTOR'S SIGNED CERTIFICATION THAT PACKAGE

CONFIGURATION MEETS 49 CFR, AND, AS APPLICABLE,

ICAO, IMDG AND/OR DLAI 4145.3 REQUIREMENTS,

SHALL BE INCLUDED ON THE DD FORM 250 (MATERIAL

INSPECTION AND RECEIVING REPORT), OR ANY

SUITABLE ALTERNATE COMMERCIAL PACKING LIST. ALL

CERTIFICATES/REPORTS SHALL BE AVAILABLE FOR

INSPECTION BY AUTHORIZED U. S. GOVERNMENT

REPRESENTATIVES FOR A PERIOD OF NOT LESS THAN 3

YEARS FROM THE DATE OF SHIPMENT.

IF THE MATERIAL IS NOT CONSIDERED HAZARDOUS,

IN ACCORDANCE WITH FED-STD-313, THE MATERIAL

SHALL BE COMMERCIALLY PACKAGED IN ACCORDANCE

WITH "ASTM D3951."

NSN:002499192

COVER,ACCESS

DRAWING EXCEPTIONS:

1. DOCUMENT 200415485 ENGINEERING NOTES 1,3,7 & 12 APPLY.

2.SPARES CONFIGURATION: PER DRAWING EXCEPT (38).196 DIA AND (2) .281 DIA

ATTACH HOLES OMITTED.

3.1/4" EXCESS TRIM ON ALL SIDES.

4.PER PROCESS SPEC: 68A900000 E0:2015C0002-R DATED:30 MARCH 2015.THIS EO

SPECIFIES THE PRIMER THAT IS APPROVED FOR USE ON ALL USAF F-15 AIRCRAFT

SPARED PARTS. THE ONLY PRIMERS CURRENTLY APPROVED FOR USE ON USAF

F-15C/D/E SPARED PARTS THAT ARE NOT FUEL WETTED ARE DEFT PPG 02GN084 AND

DEFT PPG 02GN093 NON-CHROME CORROSION INHIBITING POLYAMIDE PRIMERS. SEE

PARAGRAPH 3.6.9.1 OF THE FINISH SPEC FOR THE REQUIRED COATING FOR FUEL

WETTED PARTS.

CRITICAL APPLICATION ITEM:

REFERENCE NUMBER:A0003

HIGHER LEVEL CONTRACT QUALITY REQUIREMENT (MANUFACTURERS)

REFERENCE NUMBER:ZD059

GOVERNMENT FIRST ARTICLE TESTING REQUIREMENTS:

REFERENCE NUMBER:ZD038

GOVERNMENT FIRST ARTICLE ADDRESS FOR

WARNER ROBBINS AFB QTY:2

SEND FIRST ARTICLE TEST SAMPLES TO:

DODAAC:FD2060

SPECIAL HANDLING UNIT, FAT

455 B:RRON ST. ROBINS AFB, GA 31098

FAT-DO NOT POST. BLDG #376

email: 782cbsg.fl5fat@robins.af.mil

<H>ENSURE THAT THE WORDS "FIRST ARTICLE" ARE MARKED IN RED ON THE

OUTSIDE OF THE BOX IN LARGE CONSPICUOUS LETTERS".</>

EXPORT CONTROL APPLIES:

REFERENCE NUMBER:CS001

SAMPLING:

IAW BASIC DRAWING NR 76301 68A230075

REVISION NR D DTD 06/06/1997

PART PIECE NUMBER: 68A230075-1005

IAW REFERENCE DRAWING NR 76301 68A900029

REVISION NR H DTD 10/08/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A900029

REVISION NR H DTD 07/16/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A230075

REVISION NR D DTD 06/24/1997

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 40M114

REVISION NR M DTD 07/25/2011

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A009998

REVISION NR C DTD 06/27/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-1

REVISION NR H DTD 04/30/2009

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-10

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-11

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-2

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-231

REVISION NR D DTD 05/11/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-232

REVISION NR D DTD 05/11/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-3

REVISION NR D DTD 05/20/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-4

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-5

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-6

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-7

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-8

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-9

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.15500

REVISION NR W1 DTD 03/16/1993

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.15500.4

REVISION NR A DTD 07/08/1998

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A900000

REVISION NR K DTD 05/21/2012

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.14007

REVISION NR AB DTD 12/14/2005

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.15500

REVISION NR W DTD 07/30/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-233

REVISION NR G DTD 08/29/1986

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-268

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-272

REVISION NR D DTD 05/20/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-276

REVISION NR D DTD 05/11/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A239998-277

REVISION NR D DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A009998

REVISION NR C DTD 10/15/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.19000

REVISION NR W1 DTD 06/14/1988

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.13201

REVISION NR AK DTD 01/20/2010

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.20006

REVISION NR 18 DTD 11/07/1994

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.20006

REVISION NR R DTD 02/06/2007

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.16001

REVISION NR CA DTD 11/07/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 98752 200415485

REVISION NR C DTD 09/05/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.19000

REVISION NR W DTD 01/23/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.16001

REVISION NR CA DTD 01/23/1995

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.13201

REVISION NR AK DTD 01/23/1991

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A900000

REVISION NR K DTD 03/30/2015

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 1MA100

REVISION NR AF DTD 08/30/2006

LINE ITEM 00003 TYPE OF COVERAGE: DLA DIRECT, CONUS

PKGING DATA-QUP:001

SHALL BE PACKAGED IN ACCORDANCE WITH HAZARDOUS

MATERIALS PACKAGING REQUIREMENTS.

PACKAGING: PACKAGING FOR HAZARDOUS MATERIALS

SHALL COMPLY WITH APPLICABLE REGULATIONS, I.E.,

TITLE 49 CODE OF FEDERAL REGULATIONS,

INTERNATIONAL CIVIL AVIATION ORGANIZATION (ICAO)

TECHNICAL INSTUCTIONS (EXCLUDING PARAGRAPH 1.4

OF CHAPTERS 1 AND 3), AND INTERNATIONAL MARITIME

DANGEROUS GOODS CODE (IMDG). BOTH ICAO AND IMDG

COMPLY WITH UNITED NATIONS (UN) RECOMMENDATIONS

ON TRANSPORT OF DANGEROUS GOODS. WHEN A);

CONTRACT/ORDER FOR HAZARDOUS MATERIALS REQUIRES

SHIPMENT THROUGH A MILITARY AERIAL PORT FOR

TRANSPORT VIA MILITARY AIRCRAFT, PACKAGING SHALL

COMPLY WITH DLAI 4145.3, PREPARING HAZARDOUS

MATERIALS FOR MILITARY AIR SHIPMENT.

LABELING AND MARKING: ALL INTERIOR AND EXTERIOR

CONTAINERS SHALL BE LABELED AND MARKED AS

SPECIFIED IN THE REFERENCED PRODUCT

SPECIFICATION, AND/OR AS SPECIFIED IN SECTION D

OF THE CONTRACT OR ORDER. IN ADDITION, ALL

LABELING AND MARKING SHALL COMPLY WITH THE

REQUIREMENTS OF MIL-STD-129, 49 CFR, 29 CFR,

AND, AS APPLICABLE, ICAO TECHNICAL INSTRUCTIONS,

IMDG ANNEX 1, AND/OR DLAI 4145.3.

CERTIFICATION: ALL PACKAGING PERFORMANCE TEST

REQUIREMENTS SHALL BE SUPPORTED BY CERTIFICATES

AND REPORTS ATTESTING TO DATE OF TESTING AND

DATA RESULTS OBTAINED FROM TESTING. THE

CONTRACTOR'S SIGNED CERTIFICATION THAT PACKAGE

CONFIGURATION MEETS 49 CFR, AND, AS APPLICABLE,

ICAO, IMDG AND/OR DLAI 4145.3 REQUIREMENTS,

SHALL BE INCLUDED ON THE DD FORM 250 (MATERIAL

INSPECTION AND RECEIVING REPORT), OR ANY

SUITABLE ALTERNATE COMMERCIAL PACKING LIST. ALL

CERTIFICATES/REPORTS SHALL BE AVAILABLE FOR

INSPECTION BY AUTHORIZED U. S. GOVERNMENT

REPRESENTATIVES FOR A PERIOD OF NOT LESS THAN 3

YEARS FROM THE DATE OF SHIPMENT.

IF THE MATERIAL IS NOT CONSIDERED HAZARDOUS,

IN ACCORDANCE WITH FED-STD-313, THE MATERIAL

NSN:002749846

COVER, ACCESS, AIRCRAFT

REFERENCE NUMBER:A0003

REFERENCE NUMBER:ZD071

REFERENCE NUMBER:ZD059

EXCEPTIONS TO DWG 68A480901:

1. FINISH: PER B/P

2. SPARES CONFIG: PER B/P EXCEPT ADD 1/4" EXCESS TRIM, AND (1) .500 DIA

HOLE OMITTED.

3.DRAWING NOTES 1, 3, 10, 11, AND 12 APPLY

REFERENCE NUMBER:ZD038

REFERENCE NUMBER:Q0070

INSPECTION REPORTS:

402 MXSG/MXRILM

ATTN: FIRST ARTICLE TEST LAB

450 THIRD ST. BLDG 323

ROBINS AFB, GA. 31098-1640

FIRST ARTICLE TEST SAMPLES SHALL BE SENT TO:

FD2060

DLA CENTRAL RECEIVING

DDWG ER

SPECIAL HANDLING, FIRST ARTICLE UNIT

455 BYRON STREET

WR-ALC

ROBINS AFB, GA 31098-1887

SAMPLING:

REFERENCE NUMBER:Q0106

EXPORT CONTROL:

REFERENCE NUMBER:CS001

CRITICAL APPLICATION ITEM

IAW BASIC DRAWING NR 76301 68A480901

REVISION NR B DTD 11/07/1980

PART PIECE NUMBER: 68A480901-2007

IAW REFERENCE DRAWING NR 76301 P.S.15500.4

REVISION NR A DTD 07/08/1998

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A900000

REVISION NR K DTD 05/21/2012

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A009995

REVISION NR P DTD 10/15/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A009995

REVISION NR P DTD 06/27/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.15500

REVISION NR W DTD 07/30/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-1

REVISION NR H DTD 04/30/2009

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-931

REVISION NR C DTD 05/14/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-932

REVISION NR C DTD 05/17/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-933

REVISION NR E DTD 05/12/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-934

REVISION NR C DTD 05/14/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-935

REVISION NR C DTD 05/14/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-936

REVISION NR C DTD 05/14/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-937

REVISION NR C DTD 05/14/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-938

REVISION NR C DTD 05/14/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-939

REVISION NR C DTD 05/14/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-945

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-946

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-947

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-948

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-949

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-950

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-951

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-952

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.20022

REVISION NR M DTD 04/21/1998

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-10

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-11

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-2

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-3

REVISION NR C DTD 05/19/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-4

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-5

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-6

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-7

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-8

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A339998-9

REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A480901

REVISION NR B DTD 05/13/1981

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A480901

REVISION NR B DTD 05/13/1981

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 ST3M454

REVISION NR AD DTD 06/19/2002

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.23041

REVISION NR V DTD 02/24/2009

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.23041

REVISION NR V1 DTD 06/05/1992

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.20006

REVISION NR R DTD 02/06/2007

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.16001

REVISION NR CA DTD 11/07/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.20022

REVISION NR M1 DTD 03/15/1988

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.16001

REVISION NR CA DTD 01/23/1995

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A900000

REVISION NR K DTD 07/22/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.20022

REVISION NR M DTD 08/14/2008

LINE ITEM 00005 TYPE OF COVERAGE: DLA DIRECT, CONUS

PKGING DATA-QUP:001

SHALL BE PACKAGED IN ACCORDANCE WITH HAZARDOUS

MATERIALS PACKAGING REQUIREMENTS.

PACKAGING: PACKAGING FOR HAZARDOUS MATERIALS

SHALL COMPLY WITH APPLICABLE REGULATIONS, I.E.,

TITLE 49 CODE OF FEDERAL REGULATIONS,

INTERNATIONAL CIVIL AVIATION ORGANIZATION (ICAO)

TECHNICAL INSTUCTIONS (EXCLUDING PARAGRAPH 1.4

OF CHAPTERS 1 AND 3), AND INTERNATIONAL MARITIME

DANGEROUS GOODS CODE (IMDG). BOTH ICAO AND IMDG

COMPLY WITH UNITED NATIONS (UN) RECOMMENDATIONS

ON TRANSPORT OF DANGEROUS GOODS. WHEN A);

CONTRACT/ORDER FOR HAZARDOUS MATERIALS REQUIRES

SHIPMENT THROUGH A MILITARY AERIAL PORT FOR

TRANSPORT VIA MILITARY AIRCRAFT, PACKAGING SHALL

COMPLY WITH DLAI 4145.3, PREPARING HAZARDOUS

MATERIALS FOR MILITARY AIR SHIPMENT.

LABELING AND MARKING: ALL INTERIOR AND EXTERIOR

CONTAINERS SHALL BE LABELED AND MARKED AS

SPECIFIED IN THE REFERENCED PRODUCT

SPECIFICATION, AND/OR AS SPECIFIED IN SECTION D

OF THE CONTRACT OR ORDER. IN ADDITION, ALL

LABELING AND MARKING SHALL COMPLY WITH THE

REQUIREMENTS OF MIL-STD-129, 49 CFR, 29 CFR,

AND, AS APPLICABLE, ICAO TECHNICAL INSTRUCTIONS,

IMDG ANNEX 1, AND/OR DLAI 4145.3.

CERTIFICATION: ALL PACKAGING PERFORMANCE TEST

REQUIREMENTS SHALL BE SUPPORTED BY CERTIFICATES

AND REPORTS ATTESTING TO DATE OF TESTING AND

DATA RESULTS OBTAINED FROM TESTING. THE

CONTRACTOR'S SIGNED CERTIFICATION THAT PACKAGE

CONFIGURATION MEETS 49 CFR, AND, AS APPLICABLE,

ICAO, IMDG AND/OR DLAI 4145.3 REQUIREMENTS,

SHALL BE INCLUDED ON THE DD FORM 250 (MATERIAL

INSPECTION AND RECEIVING REPORT), OR ANY

SUITABLE ALTERNATE COMMERCIAL PACKING LIST. ALL

CERTIFICATES/REPORTS SHALL BE AVAILABLE FOR

INSPECTION BY AUTHORIZED U. S. GOVERNMENT

REPRESENTATIVES FOR A PERIOD OF NOT LESS THAN 3

YEARS FROM THE DATE OF SHIPMENT.

IF THE MATERIAL IS NOT CONSIDERED HAZARDOUS,

IN ACCORDANCE WITH FED-STD-313, THE MATERIAL

NSN:002838343

FAIRING,AIRCRAFT

DRAWING EXCEPTIONS:

1. DOCUMENT 200415485 NOTES 1,3,10,11 & 12 APPLY.

2. OMIT ALL "MATE WITH" HOLES.

3. FINISH: NO PAINT REQUIRED.

REFERENCE NUMBER:ZD059

REFERENCE NUMBER:ZD038

REFERENCE NUMBER:Q0070

FAT ADDRESS:

SEND FIRST ARTICLE TEST SAMPLES TO:

DODAAC:FD2060

SPECIAL HANDLING UNIT, FAT

455 BYRON ST. ROBINS AFB, GA 31098

FAT-DO NOT POST. BLDG #376

email: 782cbsg.fl5fat@robins.af.mil

EXPORT CONTROL APPLIES

REFERENCE NUMBER:CS001

SAMPLING:

REFERENCE NUMBER:Q0106

MYLAR INFO:

REFERENCE NUMBER:ZD057

CRITICAL APPLICATION ITEM

IAW BASIC DRAWING NR 76301 68A335100

REVISION NR V DTD 06/20/2014

PART PIECE NUMBER: 68A335100-2153

IAW REFERENCE DRAWING NR 76301 40M114

REVISION NR M DTD 07/25/2011

PART PIECE NUMBER:

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REVISION NR C DTD 06/27/2008

PART PIECE NUMBER:

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REVISION NR K DTD 05/21/2012

PART PIECE NUMBER:

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REVISION NR AA DTD 06/19/1998

PART PIECE NUMBER:

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REVISION NR V DTD 10/23/2000

PART PIECE NUMBER:

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REVISION NR M DTD 04/21/1998

PART PIECE NUMBER:

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REVISION NR C DTD 10/15/2008

PART PIECE NUMBER:

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REVISION NR V1 DTD 05/23/1991

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REVISION NR C DTD 05/08/1971

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 09/14/1988

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REVISION NR C DTD 05/08/1971

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REVISION NR C DTD 05/08/1971

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REVISION NR C DTD 05/19/1971

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REVISION NR C DTD 05/08/1971

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REVISION NR C DTD 05/08/1971

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REVISION NR C DTD 05/08/1971

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REVISION NR C DTD 05/08/1971

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REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

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REVISION NR C DTD 05/08/1971

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.20006

REVISION NR R DTD 02/06/2007

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.16001

REVISION NR CA DTD 11/07/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A335100/3

REVISION NR K DTD 10/10/2014

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A335100/4

REVISION NR W DTD 05/19/2015

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 98752 200415485

REVISION NR C DTD 09/05/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A335100/5

REVISION NR P DTD 10/10/2014

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.20022

REVISION NR M1 DTD 03/15/1988

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.19000

REVISION NR W DTD 01/23/2008

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 P.S.16001

REVISION NR CA DTD 01/23/1995

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A900000

REVISION NR K DTD 03/30/2015

PART PIECE NUMBER:

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REVISION NR T DTD 10/10/2014

PART PIECE NUMBER:

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REVISION NR W DTD 01/21/2015

PART PIECE NUMBER:

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REVISION NR W DTD 03/20/2015

PART PIECE NUMBER:

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REVISION NR W DTD 03/20/2015

LINE ITEM 00007 TYPE OF COVERAGE: DLA DIRECT, CONUS

PKGING DATA-QUP:001

SHALL BE PACKAGED IN ACCORDANCE WITH HAZARDOUS

MATERIALS PACKAGING REQUIREMENTS.

PACKAGING: PACKAGING FOR HAZARDOUS MATERIALS

SHALL COMPLY WITH APPLICABLE REGULATIONS, I.E.,

TITLE 49 CODE OF FEDERAL REGULATIONS,

INTERNATIONAL CIVIL AVIATION ORGANIZATION (ICAO)

TECHNICAL INSTUCTIONS (EXCLUDING PARAGRAPH 1.4

OF CHAPTERS 1 AND 3), AND INTERNATIONAL MARITIME

DANGEROUS GOODS CODE (IMDG). BOTH ICAO AND IMDG

COMPLY WITH UNITED NATIONS (UN) RECOMMENDATIONS

ON TRANSPORT OF DANGEROUS GOODS. WHEN A);

CONTRACT/ORDER FOR HAZARDOUS MATERIALS REQUIRES

SHIPMENT THROUGH A MILITARY AERIAL PORT FOR

TRANSPORT VIA MILITARY AIRCRAFT, PACKAGING SHALL

COMPLY WITH DLAI 4145.3, PREPARING HAZARDOUS

MATERIALS FOR MILITARY AIR SHIPMENT.

LABELING AND MARKING: ALL INTERIOR AND EXTERIOR

CONTAINERS SHALL BE LABELED AND MARKED AS

SPECIFIED IN THE REFERENCED PRODUCT

SPECIFICATION, AND/OR AS SPECIFIED IN SECTION D

OF THE CONTRACT OR ORDER. IN ADDITION, ALL

LABELING AND MARKING SHALL COMPLY WITH THE

REQUIREMENTS OF MIL-STD-129, 49 CFR, 29 CFR,

AND, AS APPLICABLE, ICAO TECHNICAL INSTRUCTIONS,

IMDG ANNEX 1, AND/OR DLAI 4145.3.

CERTIFICATION: ALL PACKAGING PERFORMANCE TEST

REQUIREMENTS SHALL BE SUPPORTED BY CERTIFICATES

AND REPORTS ATTESTING TO DATE OF TESTING AND

DATA RESULTS OBTAINED FROM TESTING. THE

CONTRACTOR'S SIGNED CERTIFICATION THAT PACKAGE

CONFIGURATION MEETS 49 CFR, AND, AS APPLICABLE,

ICAO, IMDG AND/OR DLAI 4145.3 REQUIREMENTS,

SHALL BE INCLUDED ON THE DD FORM 250 (MATERIAL

INSPECTION AND RECEIVING REPORT), OR ANY

SUITABLE ALTERNATE COMMERCIAL PACKING LIST. ALL

CERTIFICATES/REPORTS SHALL BE AVAILABLE FOR

INSPECTION BY AUTHORIZED U. S. GOVERNMENT

REPRESENTATIVES FOR A PERIOD OF NOT LESS THAN 3

YEARS FROM THE DATE OF SHIPMENT.

IF THE MATERIAL IS NOT CONSIDERED HAZARDOUS,

IN ACCORDANCE WITH FED-STD-313, THE MATERIAL

NSN:003390119

SUPPORT,STRUCTURAL

SEE BIDSET FOR ENGINEERING INSTRUCTIONS

FOR THIS NSN.

"The First Article offered must be manufactured at the facilities in which that item is to be produced under the contract, or if the First Article is a component not manufactured by the contractor, such component must be manufactured at the facilities in which the component is to be produced for the contract. A certification to this effect must accompany each First Article which is offered."

Performance or other characteristics which the First Articles must meet are DEFINED BY ENGINEERING DWG: DOCUMENTED IN FIRST ARTICLE INSPECTION

(TEST) REPORT.

The detailed technical requirements for First Article approval tests are contained in ENGINEERING DWG AND GOVERNMENT EVALUATION.

TEST REPORT REQUIRED.

First Articles will be installed on aircraft/equipment to determine proper fit/function. Approved article will remain on the aircraft/equipment and will not be forwarded to USAF Supply, but will be considered part of the contract quantity.

CERTIFICATE OF COMPLIANCE & MATERIAL CERTIFICATION REQUIRED.

JUSTIFICATION STATEMENT: FIRST ARTICLE IS REQUIRED IN LIEU OF INITIAL

PRODUCTION EVALUATION TO VERIFY CONTRACTOR CAPABILITY TO SUCCESSFULLY

MANUFACTURE REMAINING PRODUCTION QUANTITY.

INCLUDE REQUIREMENTS OF FAR 52.209-9018.

CONTRACTOR SHALL MAINTAIN ONE OF THE FOLLOWING QUALITY SYSTEMS AND

PROVIDE CURRENT THIRD PARTY REGISTRAR CERTIFICATE.

ISO9001:2000,AS9100,NATO AQAP 2070 OR EQUIVALENT.

ALL SPECIAL PROCESSES SHALL BE PERFORMED BY ORGANIZATIONS MAINTAINING

NADCAP APPROVAL FOR RELEVANT SPECIAL PROCESS.

REMINDER: Per DFAR 246.202-4 Higher-level Contract Quality Requirements.

(1) Higher-level contract quality requirements are used in ADDITION to a standard inspection requirement.

(2) Higher-level contract quality requirements, including non-government quality system standards adopted to meet DoD needs, are listed in the DoD Index of Specifications and Standards.

Contractor's notification to ACO and 424 SCMS/GUEA of test time and location due 30 days prior to start of testing.

***** NOTE: ENSURE THE WORDS"FIRST ARTICLES" & DON'T STOCK,OR

ISSUE ARE MARKED ON THE OUTSIDE OF THE BOX,IN LARGE RED CONSPICUOUS

LETTERS**** .

FIRST ARTICLE TESTING INSTRUCTIONS

1. THE CRITICAL NATURE OF THE PART REQUIRES A FIRST ARTICLE FROM A

CONTRACTOR WHO HAS NEVER PRODUCED THE ITEM OR HAS NOT PRODUCED THE ITEM

FOR AN EXTENDED PERIOD OF TIME.

2. A VENDOR WILL NORMALLY BE ALLOWED ONLY ONE ATTEMPT TO RECEIVE FULL OR

CONDITIONAL APPROVAL.

FAILURE TO RECEIVE APPROVAL OF FIRST ARTICLE INSPECTION WILL, AT THE

DISCRETION OF THE GOVERNMENT, RESULT IN TERMINATION OF THE CONTRACT. IT

MAY ALSO RESULT IN SUBSEQUENT REMOVAL OF THE VENDOR AS AN APPROVED

SOURCE (IF THE ITEM IS CODED AMSC "C").

3. THE CONTRACTOR SHALL PRODUCE A REPORT ON THE SUBJECT ITEM WITH ALL

DIMENSIONS AND TOLERANCES SPECIFIED ON THE MANUFACTURING DATA LISTED IN

ONE COLUMN AND THE ACTUAL CORRESPONDING READING OBTAINED FROM THE

INSPECTION OF THE PART LISTED IN ANOTHER COLUMN.

4. MATERIALS UTILIZED IN THE MANUFACTURE OF FIRST ARTICLE ITEMS SHALL BE

IDENTIFIED AND CERTIFIED ALONG WITH A COPY OF MATERIAL PURCHASE REQUESTS

AS CONFIRMING TO APPLICABLE DATA REQUIREMENTS.

5. MATERIAL PROCESSING, INCLUDING FINISH REQUIREMENTS (PLATING, CASTING,

FORGING, HEAT TREATMENT, WELDING, INSPECTION, ANODIZE, PAINTING, ETC.)

UTILIZED IN THE MANUFACTURE OF FIRST ARTICLE ITEMS SHALL BE IDENTIFIED

AND CERTIFIED ALONG WITH A COPY OF MATERIAL PURCHASE REQUESTS AS

CONFIRMING TO APPLICABLE DATA REQUIREMENTS. A COPY OF THE PURCHASE ORDER

CERTIFYING THE PROCESS ACCOMPLISHED AT OTHER THAN CONTRACTOR FACILITY

SHALL BE INCLUDED.

REFERENCE NUMBER:ZD038

COPY OF ORDER/CONTRACT TO BE PROVIDED

SEND TEST REPORT, & EXHIBIT TO:

DDOO-SOP (FIRST ARTICLES)

BLDG 18 DOOR 16 (405) 739-7667

8080 PERIMETER RD

TINKER AFB OK 73145-8000

DODAAC: FY2303

MARK FOR: FIRST ARTICLES

ATTN: DDOO-SOP

REFERENCE NUMBER:Q0070

REFERENCE NUMBER:ZD004

REFERENCE NUMBER:CS001

IAW BASIC DRAWING NR 81205 9-58914

REVISION NR B DTD 08/20/2001

PART PIECE NUMBER: 9-58914-3

IAW REFERENCE DRAWING NR 81205 BAC5300

REVISION NR M DTD 09/09/2011

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5300

REVISION NR M DTD 10/31/1999

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5300-1

REVISION NR F DTD 04/09/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5300-2

REVISION NR G DTD 10/09/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5300-1

REVISION NR F DTD 09/01/2006

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5300-2

REVISION NR G DTD 09/01/2006

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 81205 BAC5307

REVISION NR R DTD 04/08/2010

LINE ITEM 00009 TYPE OF COVERAGE: DLA DIRECT, CONUS

PKGING DATA-QUP:001

SHALL BE PACKAGED IN ACCORDANCE WITH HAZARDOUS

MATERIALS PACKAGING REQUIREMENTS.

PACKAGING: PACKAGING FOR HAZARDOUS MATERIALS

SHALL COMPLY WITH APPLICABLE REGULATIONS, I.E.,

TITLE 49 CODE OF FEDERAL REGULATIONS,

INTERNATIONAL CIVIL AVIATION ORGANIZATION (ICAO)

TECHNICAL INSTUCTIONS (EXCLUDING PARAGRAPH 1.4

OF CHAPTERS 1 AND 3), AND INTERNATIONAL MARITIME

DANGEROUS GOODS CODE (IMDG). BOTH ICAO AND IMDG

COMPLY WITH UNITED NATIONS (UN) RECOMMENDATIONS

ON TRANSPORT OF DANGEROUS GOODS. WHEN A);

CONTRACT/ORDER FOR HAZARDOUS MATERIALS REQUIRES

SHIPMENT THROUGH A MILITARY AERIAL PORT FOR

TRANSPORT VIA MILITARY AIRCRAFT, PACKAGING SHALL

COMPLY WITH DLAI 4145.3, PREPARING HAZARDOUS

MATERIALS FOR MILITARY AIR SHIPMENT.

LABELING AND MARKING: ALL INTERIOR AND EXTERIOR

CONTAINERS SHALL BE LABELED AND MARKED AS

SPECIFIED IN THE REFERENCED PRODUCT

SPECIFICATION, AND/OR AS SPECIFIED IN SECTION D

OF THE CONTRACT OR ORDER. IN ADDITION, ALL

LABELING AND MARKING SHALL COMPLY WITH THE

REQUIREMENTS OF MIL-STD-129, 49 CFR, 29 CFR,

AND, AS APPLICABLE, ICAO TECHNICAL INSTRUCTIONS,

IMDG ANNEX 1, AND/OR DLAI 4145.3.

CERTIFICATION: ALL PACKAGING PERFORMANCE TEST

REQUIREMENTS SHALL BE SUPPORTED BY CERTIFICATES

AND REPORTS ATTESTING TO DATE OF TESTING AND

DATA RESULTS OBTAINED FROM TESTING. THE

CONTRACTOR'S SIGNED CERTIFICATION THAT PACKAGE

CONFIGURATION MEETS 49 CFR, AND, AS APPLICABLE,

ICAO, IMDG AND/OR DLAI 4145.3 REQUIREMENTS,

SHALL BE INCLUDED ON THE DD FORM 250 (MATERIAL

INSPECTION AND RECEIVING REPORT), OR ANY

SUITABLE ALTERNATE COMMERCIAL PACKING LIST. ALL

CERTIFICATES/REPORTS SHALL BE AVAILABLE FOR

INSPECTION BY AUTHORIZED U. S. GOVERNMENT

REPRESENTATIVES FOR A PERIOD OF NOT LESS THAN 3

YEARS FROM THE DATE OF SHIPMENT.

IF THE MATERIAL IS NOT CONSIDERED HAZARDOUS,

IN ACCORDANCE WITH FED-STD-313, THE MATERIAL

NSN:003617241

SKIN, AIRCRAFT

REFERENCE NUMBER:ZD071

REFERENCE NUMBER:ZD059

REFERENCE NUMBER:ZD038

REFERENCE NUMBER:Q0070

FAT ADDRESS:

SEND FIRST ARTICLE TEST SAMPLES TO:

DODAAC FS2060

SPECIAL HANDLING UNIT, FIRST ARTICLE UNIT

455 BYRON STREET

ROBINS AFB, GA 31098-1887

MARK FOR: FIRST ARTICLE INSPECTION AND TEST.

DO NOT POST.

DWG EXCEPTIONS & ENGINEERING NOTES:

1. DOCUMENT 200415485 NOTES 1,3,10,11 & 12 APPLY.

2. FINISH: WHEN THE BLUEPRINT CALLS OUT ALUMINUM ALLOYS 2XXX -7XXX, USE

MIL-DTL-5541 FOR SURFACE PREPARATION (CHROMATE CONVERSION), FOLLOWED BY

2 COATS MIL-PRF-23377, TYPE I, CLS C2 (EPOXY PRIMER) FOR NON-FUEL WETTED

SURFACES AND SAE AMS-C-27725 (POLYURETHANE PRIMER) FOR FUEL WETTED

SURFACES. ALL OTHER SURFACE COATINGS WILL BE PER BLUEPRINT.

3. OMIT "MATE WITH" HOLES.

4. SUPPLY PART WITH .250" EXCESS TRIM ON ALL SIDES.

REFERENCE NUMBER:Q0106

EXPORT CONTROL APPLIES:

REFERENCE NUMBER:CS001

CRITICAL APPLICATION ITEM

IAW BASIC DRAWING NR 76301 68A327180

REVISION NR B DTD 08/06/1984

PART PIECE NUMBER: 68A327180-2008

IAW REFERENCE DRAWING NR 76301 68A900001

REVISION NR P DTD 04/03/2013

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 40M114

REVISION NR M DTD 07/25/2011

PART PIECE NUMBER:

IAW REFERENCE DRAWING NR 76301 68A009998

REVISION NR C DTD 06/27/2008

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LINE ITEM 00011 TYPE OF COVERAGE: DLA DIRECT, CONUS

PKGING DATA - MIL-STD-2073-1D, 15 DEC 1999

QUP:001 PRES MTHD:10 CLNG/DRY:1 PRESV MAT:XX

WRAP MAT:XX CUSH/DUNN MAT:XX CUSH/DUNN THKNESS:X

UNIT CONT:D3 OPI:M

INTRMDTE CONT:XX INTRMDTE CONT QTY:AAA

PACK CODE:U

MARKING SHALL BE IN ACCORDANCE WITH MIL-STD-129.

SPECIAL MARKING CODE:00 -00 No special marking

PALLETIZATION SHALL BE IN ACCORDANCE WITH MD00100452 REV B DATED JULY 01, 2008

NSN:007779173

BRIDGE ASSEMBLY,FAN

THE FOLLOWING EXCEPTIONS TO DWG:35-10738 APPLY:

DWG:35-10738(-2),NOTES:1-15,& 17

DWG:39-10776(-503),NOTES:1-3,& 16

BACD2032(-1-23),NO NOTES

1. PART MARKING PER MIL-STD-130, METHOD PER THE DRAWING REQUIREMENTS AND

BAC 5307. MARKING MUST INCLUDE NATIONAL STOCK NUMBER, PART NUMBER,

CURRENT DESIGN AUTHORITY CODE (98748), ACTUAL MANUFACTURER#S CAGE CODE

(-----), DATE OF MANUFACTURE, AND #FOR MILITARY USE ONLY#. PARTS WILL

NOT BE MARKED WITH THE ORIGINAL DESIGN AUTHORITY (BOEING) CAGE CODE.

2. DIMENSIONING AND TOLERANCING PER ASME Y14.5.

3. DISREGARD REFERENCE TO MATERIAL SUBSTITUTION DOCUMENT BAC 5005.

4. PART TO BE FURNISHED WITHOUT RIVET OR FASTENER HOLES.

5. USE ALUMINUM ALLOY ALCLAD 2024 PER AMS-QQ-A-250 AMD AMS-QQ-A-250/5 IN

LIEU OF QQ-A-362.

6. HEAT TREAT ALUMINUM ALLOY PER AMS 2770 AND AMS 2772 IN LIEU OF

BAC5602 AND MIL-H-6088.

7. HEAT TREAT ALUMINUM ALLOY 2024 PLATE/SHEET TO T42 TEMPER IN LIEU OF

T4.

8. DISREGARD REFERENCE TO #LOCATE TO MATCH 35-8275, 35-10235 &

35-12542#.

9. FINISH CODE F-2.115 / F-2.30 DEFINED: CHEMICAL TREAT ACCORDING TO

MIL-DTL-5541, CLASS 1A OR ANODIZE ACCORDING TO MIL-A-8625, TYPE I OR IC

(PREFERRED), CLASS 1. APPLY MIL-PRF-23377, TYPE I, CLASS C2 PRIMER TO A

DRY FILM THICKNESS OF 0.0003 TO 0.0005 INCH ACCORDING TO THE

MANUFACTURERS APPLICATION INSTRUCTIONS AND MIL-F-18264.

10. USE EXTRUDED ALUMINUM ALLOY 2024 BAR, ROD, SHAPES PER AMS-QQ-A-200

AND AMS-QQ-A-200/3 IN LIEU OF QQ-A-267.

11. USE AMS 10134-1005 EXTRUDED ALUMINUM ANGLE IN LIEU OF AND10134-1005.

12. USE MS21075 NUT PLATE PER NASM21075 IN LIEU OF NAS1068, BAC N10FM.

13. USE MS20470 UNIVERSAL HEAD RIVETS PER NASM20470 IN LIEU OF AN470.

14. USE WASHER NAS1149D0463K IN LIEU OF AN960PD416.

15. DISREGARD REFERENCE TO "THE INTERCHANGEABILITY REQUIREMENTS OF THIS

DRAWING ARE CONTROLLED BY BOEING MASTER GAGES".

16. USE ASTM D4066 NYLON INJECTION & EXTRUSION MATERIALS IN LIEU

OF MIL-P-20693 MOLDING PLASTIC, POLYAMIDE (NYLON), RIGID.

17. WHEN X'ED BELOW OR LISTED IN THESE NOTES, DEFINITIONS APPLICABLE TO

THIS PRODUCT ARE OR HAVE:

(A) ENGINEERING CRITICAL IN APPLICATION: An item, which requires special manufacturing processes, controls, and testing of material or end items.

Because of its use or application, failure to maintain the highest reliability of such an item could be catastrophic resulting in loss of life or serious injury, loss of a weapon system or extensive secondary damage, with direct impact on the capability to respond to a national emergency or to achieve wartime sustainability.

(B) CRITICAL CHARACTERISTICS: Characteristics which, when defective, are likely to result in hazardous or unsafe conditions for individuals using, maintaining or depending upon the product; or, are likely to prevent performance of the tactical function of a major end item such as an aircraft, missile, space vehicle, engine or a major part thereof.

(Derived from MIL-STD-1916).

(C) MAJOR CHARACTERISTICS: Characteristics (other than critical or minor), which, when defective, are likely to result in failure or to reduce the usability of the product or a major end item for its intended purpose. (Derived from MIL-STD-1916).

(D) MINOR CHARACTERISTICS: All characteristics not designated as critical or major but for which full conformity is required

(E) COMPLEX: Items having quality characteristics not wholly visible (hidden characteristics), in the end product for which contractual conformance must be established progressively through precise measurements, tests or controls applied during purchasing, manufacturing, performance, assembly and functional operation either as an individual item or in conjunction with other items [FAR SUBPART 46.203(b)].

(F). COMMERCIAL: Described in commercial catalogs, drawings or industrial standards [FAR SUBPART 46.203(a), (1)].

THIS PRODUCT HAS BEEN DETERMINED TO BE OR CONTAINS (AS X'ED BELOW):

______ Engineering critical in application ______ Critical characteristics ______ Major characteristics ____X_ Minor characteristics, all except critical and major ______ Complex ______ Available as a commercial product When materials, processes or components are to be obtained from directed sources as indicated herein or in the specifications, the contracting officer of this procuring activity may only utilize alternate sources as a deviation upon prior approval.

Bidders shall notify this procuring activity at the time of quotation of any drawing, specification or standard which is of more current data revision than those shown on the data listing or in these engineering notes.