4892_-_Engineering_Data.pdf

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:

SPEED BRAKE ASSEMBLY - UPPER (A-10)

2. PART NUMBER:

160D712150-3

3. NATIONAL STOCK NUMBER:

1560-00-588-4892FJ

PREPARED BY:

RYAN MOORE

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

20190619

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4. THE FOLLOWING SPECIFICATIONS/STANDARDS, ETC. WILL BE USED IN LIEU OF THE DATA INDICATED. THE SUPERSEDED DATA

WILL NOT BE FURNISHED UNLESS SO INDICATED.

A. REFERENCE DRAWING 160D712551 AND 160D712552; PER NOTE 7, MAGNETIC PARTICLE INSPECTION IAW ASTM E1444.

B. REFERENCE DRAWING 160D712551F; PER NOTE 6, ULTRASONIC INSPECT FORGING IAW AMS-STD-2154.

C. REFERENCE DRAWING 160D712551 AND 160D712552; PER NOTE 6, HEAT TREAT PER AMS 2759/2 EXCEPT THAT PARTIAL

DECARBURIZATION SHALL NOT EXCEED 0.003 INCHES IN LIEU OF MIL-H-6875 AND F-T101.

5. CONTRACTOR IS RESPONSIBLE TO COMPLETELY RESEARCH THESE MANUALS, SPECIFICATIONS, AND STANDARDS AND FULLY UNDERSTAND THE REQUIREMENTS NECESSARY FOR MANUFACTURE OF COMPONENT PARTS AND ASSEMBLIES. ALL DEVIATIONS, MINOR AND MAJOR, FROM THE ENGINEERING DRAWING PACKAGE SHALL BE SUBMITTED TO THE ENGINEERING ORGANIZATION

LISTED IN THE OFFICE SYMBOL BLOCK LOCATED AT THE BOTTOM OF THIS DOCUMENT.

6. 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. 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 FROM THE ENGINEERING ORGANIZATION LISTED IN THE OFFICE SYMBOL BLOCK OF THIS DOCUMENT BY CONTACTING THE GOVERNMENT CONTRACTING OFFICIAL.

7. USE OF NORTHROP GRUMMAN SPECIFICATION Z-R701 IN CONJUNCTION WITH MIL-STD-130 IS MANDATORY TO ENSURE THE

PROPER MARKING OF THE PARTS. (Z-R701 HAS UNLIMITED DATA RIGHTS IN JEDMICS)

8. "IUID" (ITEM UNIQUE IDENTIFIER) IS REQUIRED IAW MIL-STD-130. SPECIFIC INSTRUCTIONS FOR MARKING METHODS, LOCATION, CONTENT AND FORMAT SHALL BE SPECIFIED BY THE CONTRACTOR AND SUBMITTED TO THE GOVERNMENT FOR APPROVAL PRIOR TO CONTRACT DELIVERY. THE CONTRACTOR MUST DEMONSTRATE THE MARKING DOES NOT ADVERSELY AFFECT ITEM INTEGRITY OR PERFORMANCE AND WILL REMAIN READABLE AND ATTACHED THROUGHOUT THE USEABLE LIFE OF THE ITEM.

9. COORDINATED TOOLING IS REQUIRED FOR THE MANUFACTURE OF THIS PART. THE TOOLING LISTED IN ITEM 10 (SEE BELOW) WAS PREVIOUSLY USED AT HILL AIR FORCE BASE FOR REFURBISHMENT PURPOSES BUT THE AVAILABILITY AND CONDITION OF THIS TOOLING IS UNKNOWN. THE CONTRACTOR WILL NEED TO DEVELOP/MANUFACTURE ITS OWN TOOLING AS REQUIRED TO PRODUCE THIS ASSEMBLY. PRIOR TO TOOL DEVELOPMENT, THE CONTRACTOR SHALL ADVISE THE GOVERNMENT IN WRITING OF THEIR INTENT TO DEVELOP NEW TOOLING. THE CONTRACTOR SHALL NOT PROCEED TO DEVELOP NEW TOOLING WITHOUT THE EXPRESS CONSENT OF THE GOVERNMENT PROCURING AGENCY. THE CONTRACTOR MAY REQUEST TO INSPECT EXISTING TOOLING.

ARRANGEMENTS FOR TOOL INSPECTION (OF THE EXISTING GOVERNMENT TOOLING, IF REQUIRED) SHALL BE MADE BY CONTACTING THE APPROPRIATE CONTRACTING PERSONNEL AND THE ENGINEERING AUTHORITY LISTED AT THE BOTTOM OF THIS DOCUMENT.

10. TOOL LISTING IS AS FOLLOWS:

TOOL LOCATION BOX NUMBER

160D712150-001/ASF UNKNOWN N/A

160D712151-001/BAJ UNKNOWN N/A

11. THE CONTRACTOR SHOULD WORK THROUGH THE GOVERNMENT PROCURING AGENCY TO CONTACT THE ENGINEERING ORGANIZATION LISTED IN THE OFFICE SYMBOL BLOCK LOCATED AT THE BOTTOM OF THIS DOCUMENT IN ORDER TO MAKE SURE ANY NEWLY DEVELOPED TOOLING AND FIXTURES WILL PRODUCE AN ACCEPTABLE PART THAT WILL FIT ON THE AIRCRAFT. THIS WILL MAKE SURE CHANGES AND CHECKS ARE DONE EARLY TO PREVENT FAILURE OF THE FIRST ARTICLE.

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12. THE FORGING SHALL BE PROCURED FROM SOURCES, USING THE ORIGINAL CERTIFIED FORGING PROCEDURES AND

DIES/TOOLING.

A. PRIOR TO CONTRACT AWARD, THE DETAILED PART BIDDER SHALL PROVIDE CERTIFICATION FROM THE FORGING SOURCE, TO THE GOVERNMENT THAT THE CERTIFIED DIES AND PROCEDURES ARE AVAILABLE AND THE FORGING SOURCE HAS AN AGREEMENT WITH THE DETAILED PART BIDDER TO PROVIDE FORGINGS FOR THEIR USE IN THE EVENT THEY ARE THE

SUCCESSFUL BIDDER.

B. PRIOR TO PRODUCTION, FORGING LOT QUALIFICATION SHALL BE ACCOMPLISHED AS SPECIFIED ON THE FORGING DRAWING AND SAE AMS-F-7190 FOR STEEL FORGINGS AND SAE AMS-A-22771 FOR ALUMINUM FORGINGS. THE DETAILED PART CONTRACTOR SHALL ASSURE THAT THIS HAS BEEN ACCOMPLISHED BY THE FORGING SOURCE AND SHALL SUBMIT

CERTIFIED DOCUMENTATION OF ACCOMPLISHMENT TO THE GOVERNMENT.

C. PRIOR TO CONTRACT AWARD, THE CONTRACTOR SHALL ADVISE THE GOVERNMENT IN WRITING OF THEIR INTENT TO PROCURE NEW FORGING DIES AND THE PROPOSED FORGING SOURCE. 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 RIGHTS OF THE DIES AND FORWARD A COPY OF THIS LETTER TO THE GOVERNMENT CONTRACTING OFFICER.

13. FORGING SOURCE, CONTROL OF FORGING DIES, AND THE LOCATION OF THE DIES:

A. FORGING DRAWING: 1600712551F-11 (DIE IS LISTED AT W. PAT CROW UNDER PIN 160D712551F-15)

B. DIE NUMBER: 2881

C. CONTROL AND LOCATION OF FORGING DIES:

W. PAT CROW, INC.

200 LUXTON STREET

P.O. BOX 1720

FT. WORTH, TX 76104

PHONE, (817) 536-2861 EXT 280

POC: YESENIA LOPEZ

CAGE: 94790

14. PER DRAWING 160D712551F NOTE 9, THE -13F AND THE -15F ARE ALTERNATE MATERIALS FOR THE MANUFACTURE OF

160D712551F-11. DIE #2881 IS FOR PART NUMBER 160D712551F-15.

15. IN LIEU OF 160J900001, FINAL TOP COAT FINISH PER Z-R901, CODE ZC (FED-STD-595, COLOR 36320), OVER MIL-PRF-23377 TYPE II (LOW INFRARED REFLECTIVE) PRIMER. DO NOT FINISH SPECIFIC SURFACE WHICH WILL AFFECT THE ASSEMBLY, FIT, OR FUNCTION OF THE ITEM; SUCH AS THREADS, ASSEMBLY HOLES, HOLES, NUT PLATES, CONTROL CABLES, AND SEALS. (SPECIFIC EXAMPLES:

HINGE PIN HOLES AND MATING FACES OF HINGE TANGS, ATTACH FITTING BEARINGS/BUSHINGS, AUXILIARY FITTING

BUSHINGS/LINERS, RUB BLOCKS, RUB STRIPS, IDENTITY PLATE, OR MONOBALLS)

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16. DECELERON/SPEED BRAKE TRIM TAB FITTING (160D712555-X) AND TRIM TAB HINGE (160D712150-11) RELATIONSHIP DEFINITION

FIGURE 1: RELATIONSHIP DEFINITION BETWEEN CENTER POINT OF SPHERICAL BEARING (PART OF TRIM TAB FITTING

160D712555-X) AND FACE OF TANG ON TRIM TAB HINGE HALF (160D712150-11)

THE RELATIONSHIP DEFINITION BETWEEN THE CENTER POINT OF THE SPHERICAL BEARING (P/N MS14103-4; PART OF TRIM TAB FITTING 160D712555-X) AND THE INBOARD FACE OF THE FIRST TANG ON THE TRIM TAB HINGE HALF (160D712150-11) ALONG THE TRIM TAB HINGE CENTER LINE (CL) SHALL BE DEFINED BY THE NOMINAL ENGINEERING DEFINITION AND FURTHER CONTROLLED BY THE

DIMENSIONAL RELATIONSHIP IN FIGURE 1.

160D712555-X

(TRIM TAB FITTING)

160D712543

(PART OF TRIM TAB)

160D712150-11

(TRIM TAB HINGE)

FWD

IB

W.S. 199.00

1.523” +/- 0.005

IMAGE FROM DRAWING 160D712150 (SHEET 2, ZONE C9), DETAIL F

(LH SHOWN, RH OPPOSITE)

TRIM TAB HINGE CL

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17. SPEED BRAKE MAIN HINGE LINE CONTROL

ASSEMBLY TOOL METHOD REQUIREMENTS:

A. ESTABLISH REPRESENTATIVE CENTER POINT OF IB MAIN ATTACH/ACTUATOR FITTING (P/N 160D712551-X) SPHERICAL

BEARING (P/N MS14103-14) ON SPEED BRAKE ASSEMBLY FIXTURE DETAIL.

B. ESTABLISH REPRESENTATIVE CENTER POINT OF OB MAIN ATTACH/ACTUATOR FITTING (P/N 160D712552-X) SPHERICAL

BEARING (P/N MS14103-14) ON SPEED BRAKE ASSEMBLY FIXTURE DETAIL.

C. UTILIZING THE CENTER POINTS DEFINED IN STEP 1 AND STEP 2; IDENTIFY THE APPARENT SPEED BRAKE MAIN HINGE CENTER LINE (CL), OR DATUM ‘A’, BY CREATING A STRAIGHT LINE BETWEEN THESE TWO CENTER POINTS AND EXTENDING

THAT LINE IN THE IB/OB DIRECTION TO THE EXTENTS OF THE PART/TOOL.

D. LOCATE ASSEMBLY FIXTURE DETAIL(S) USED TO DEFINE THE LOCATION OF THE IB AUXILIARY FITTING (P/N 160D712553-X) SO THAT THE CENTER POINT OF THE ASSEMBLY FIXTURE DETAIL BUSHINGS (AND REPRESENTATIVE CENTER POINT OF THE

IB AUXILIARY FITTING BUSHING) ARE WITHIN THE TOLERANCE DEFINED IN FIGURE 2.

FIGURE 2: EXAMPLE ASSEMBLY FIXTURE MAIN HINGE LINE TOLERANCE

(LH SHOWN, RH OPPOSITE)

NOTE: THE ABOVE SPEED BRAKE MAIN HINGE LINE CONTROL IS AN EXAMPLE OF A SINGLE METHOD TO CONTROL THE

SPEED BRAKE MAIN HINGE LINE.

PART METHOD REQUIREMENTS:

IF THE CONTRACTOR CHOOSES TO LOCATE THE SPEED BRAKE MAIN ATTACH FITTINGS (P/N 160D712551-X AND 160D712552-X) AND SPEED BRAKE AUXILIARY FITTINGS (P/N 160D712553-X AND 160D712554-X) UTILIZING AN ALTERNATE METHOD OTHER THAN THE TOOL METHOD REQUIREMENT ABOVE, THE RESULTANT SPEED BRAKE MAIN HINGE LINE [AS DEFINED BY DRAWING REQUIREMENTS, THE CENTER POINT OF THE SPHERICAL BEARINGS (P/N MS14103-14) ON THE IB/OB MAIN ATTACH/ACTUATOR FITTINGS (160D712551-X AND 160D712552-X), AND CENTER POINT OF THE BUSHING (P/N S5003-6-500) ON THE IB AUXILIARY FITTING BUSHING (P/N 160D712553- X)] SHALL BE HELD TO A POSITIONAL TOLERANCE OF 0.010” IN RELATION TO THE APPARENT HINGE LINE CREATED BY THE CENTER

POINTS OF THESE FITTING BUSHINGS/BEARINGS.