Engineering_Instructions.pdf

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

DATE:

20210603

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 3 June 2021. Refer other requests for this document to OO-ALC/416 SCMS/GUEAB, 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.

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

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

DATE:

20210603

HILL AFB FORM 462 Page 2 of 6

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.

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

DATE:

20210603

HILL AFB FORM 462 Page 3 of 6

(13 cont’d)

Part Number 162D6116211003

Description ASSY TRUNNION, MLG, CWP (CONFIGURATION ITEM)

Critical Characteristic 1 MISC01/01Storage, Handling, Shipping; Storage, handling and shipping shall be in accordance with ZP801.

Critical Characteristic 2 MACH21/01Deburr; Deburr part per P.S. 20024 or alternatively per GF101.

Critical Characteristic 3 MACH13/01Local Surface Roughness; Maximum surface roughness of indicated area(s) to be [roughness] microinches Ra per ASME B46.1 (1995).

Critical Characteristic 4 BUSH02/01Bushing and Bearing Ream; Ream indicated hole(s) to dimensions shown in MBD dataset.

Critical Characteristic 5

ID02/03I only; This part/assembly is interchangeable in accordance with MILI8500D 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 ZR701, code RS or ST with the following:

"INTERCHANGEABLE DO NOT ALTER".

Critical Characteristic 6

BUSH01/01Press Fit Bushing Installation; Install indicated press fit bushing(s) and/or bearing(s) by applying MILPRF23377, 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 AMSS8802 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 MILPRF23377, 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 nonchilled 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 premachine bushing face(s), provided requirements of this note are met.

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

DATE:

20210603

HILL AFB FORM 462 Page 4 of 6

Part Number 162D6116212003

Description FITTING TRUNNION, LANDING GEAR

Critical Characteristic 1 CRIT01/01Class 1A; This is a Fatigue and Fracture Critical part, Class 1A, in accordance with SM160M1000.

Critical Characteristic 2 MISC01/01Storage, Handling, Shipping; Storage, handling and shipping shall be in accordance with ZP801.

Critical Characteristic 3

NDT02/01Penetrant; Prior to shot peening, penetrant inspect per ASTM E1417. Pre penetrant etch per P.S.

12050 or GJ301 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 NDT19/01Hole Inspection A2; Inspect [feature description] to quality level A2 in accordance with QATB M 40.

Critical Characteristic 5 MACH19/01Roughness Surface Specific; Unless otherwise noted, maximum surface finish of [feature(s)] to be [roughness] microinches Ra per ASME B46.1 (1995).

Critical Characteristic 6 MACH08/01Break Edges; Prior to shot peening, unless otherwise noted, break all sharp edges [lower] to [upper] inches per P.S. 20024 or alternatively per GF101.

Critical Characteristic 7 SP13/01Sat Peen VariableOmit 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 FIN09/01Sulf Anodize; Sulfuric acid anodize per MILA8625, Type II, Class 1.

Critical Characteristic 9

MACH11/01Mismatch; 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

GDT02/01Restraint; The part shall be capable of being brought to the datum simulators by applying up to five pounds of force within any twelveinch interval or an equivalent force within a smaller interval (e.g., half the allowed force at sixinch intervals, one quarter of the allowed force at threeinch intervals). Any number of allowed force units may be applied as long as the equivalent forces and intervals are maintained.

Critical Characteristic 11 MACH01/01Roughness; Unless otherwise noted, maximum surface roughness of part to be 125 micro inches Ra per ASME B46.1 (1995).

Critical Characteristic 12 MACH09/01Blend; All corner radii intersecting plane surfaces shall blend smoothly from [lower] to [upper] corner radius.

Critical Characteristic 13 GEN09/01Material Sub; Material substitution permissible per 162S900701.

Critical Characteristic 14

ID02/03I only; This part/assembly is interchangeable in accordance with MILI8500D 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 ZR701, code RS or ST with the following:

"INTERCHANGEABLE DO NOT ALTER".

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

DATE:

20210603

HILL AFB FORM 462 Page 5 of 6

Part Number 162D6116215001

Description FORGING LANDING GEAR TRUNNION FITTING

Critical Characteristic 1 CRIT01/01Class 1A; This is a Fatigue and Fracture Critical part, Class 1A, in accordance with SM160M1000.

Critical Characteristic 2 FORG02/01Grain Flow; Primary grain flow shall be as shown in the MBD dataset.

Critical Characteristic 3 FORG03/01Grain 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 reentrant flow lines.

Critical Characteristic 4

FORG04/01FA 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 FORG06/01Tensile; 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 NDT07/01Sonic Inspect; Ultrasonically inspect finished forging per AMSSTD2154, Class A.

Critical Characteristic 7 FORG09/01Tensile 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 FORG09/01Tensile 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 FORG09/01Tensile 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 FORG09/01Tensile 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 FORG09/01Tensile 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 FORG09/01Tensile 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 13 FORG09/01Tensile 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 FORG09/01Tensile 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 FORG09/01Tensile 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 FORG12/01Flash; Flash extension tolerance is [dimension 1] inches maximum.

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

DATE:

20210603

HILL AFB FORM 462 Page 6 of 6

Critical Characteristic 17 FORG01/01First Art; Forging first article approval and production control shall be in accordance with AMS 2375.

Critical Characteristic 18 MISC01/01Storage, Handling, Shipping; Storage, handling and shipping shall be in accordance P801.

14. DOCUMENT QATB M-40 WILL NOT BE SUPPLIED. WHERE REFERENCED IN THE TECHNICAL DATA PACKAGE, PW220T0040 SHALL BE USED IN LIEU OF QATB M-40.