SOW_ATTACHMENT_A_Engineering_Data_Requirements.pdf

STATEMENT OF WORK

ATTACHMENT A

ENGINEERING DATA REQUIREMENTS

FOR

A-10 THUNDERBOLT ADVANCED WING

CONTINUATION KITTING (ATTACK)

18 May 2018

Prepared by:

AFLCMC/WWAE

Fighter/Bomber Directorate

Hill AFB, Utah 84056

REVISION CONTROL

Note: The portion of the text affected by the current revision is indicated by vertical black lines in the outer left hand margin.

Revision Date Description Pages Changed Initial 18 May 2018

Initial Release

ATTACHMENT A - ENGINEERING DATA REQUIREMENTS

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

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

ATTACK Assembly (Configuration Item)

2. PART NUMBER:

162D610010-1001

3. NATIONAL STOCK NUMBER:

PREPARED BY:

Casey Thurber

OFFICE SYMBOL:

AFLCLMC/WWAEC

DATE:

5/18/2018

HILL AFB FORM 462 Page 3 of 4

1. The final manufactured 162D610010-1001 wing assembly shall be per the TDP delivered with the RFP with the exceptions noted herein. These exceptions may be incorporated into the final 162D610010-1001 TDP that will include incorporated items from this attachment as well as a revised attachment A. This final TDP will be delivered at contract award. The delivered TDP along with this attachment constitute all the expected changes that will create the final 162D610010-1001 configuration. There may be minor changes in the TDP at time of award.

2. The following notes may include part numbers that represent the scope of the engineering change.

While considerable effort has been placed in identifying these applicable part numbers and assemblies, these lists may not be final and all-inclusive. The contractor may encounter differences between the provided lists and the TDP, in this situation the contractor shall contact A-10 SPO engineering to resolve any ambiguities.

3. Part Report Note GDT-27 will be removed from parts/assemblies that are not peripherally constrained at the next higher assembly. These parts/assemblies shall meet TDP requirements in an un-restrained and un-weighted condition.

The following part numbers indicate parts/assemblies affected by this change:

162D611512-1003 162D611512-1004

162D611512-2053 162D611512-2054

162D612512-1003 162D612512-1004

162D612512-2053 162D612512-2054

Note that next higher assemblies may have a change of part number only to maintain configuration control.

4. Design and installation of aluminum end caps/plugs on all hydraulic tube assemblies shall be per NAS 847 .

5. The inspection requirements of 160D900004 shall apply. Though part numbers referenced in the drawing, refer to legacy parts, all requirements shall be applicable for equivalent ATTACK parts.

6. Interchangeable items may require a refinement of assembly tolerances of non-specified Interchangeable features in order to ensure Interchangeable items can be assembled without a modification in order to meet the overarching Interchangeable requirement as defined in MIL-I-8500.

7. 162S900718, “Inspection of Composite Structure; S-F502 Supplement,” will be updated to allow for through transmission ultrasonics scanning speeds to be faster than six inches per second. Additionally, it will clarify rejection criteria.

ATTACHMENT A - ENGINEERING DATA REQUIREMENTS

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

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

ATTACK Assembly (Configuration Item)

2. PART NUMBER:

162D610010-1001

3. NATIONAL STOCK NUMBER:

PREPARED BY:

Casey Thurber

OFFICE SYMBOL:

AFLCLMC/WWAEC

DATE:

5/18/2018

HILL AFB FORM 462 Page 4 of 4

8. All holes common to Forward Attach Fitting 162D611604, Aft Attach Fitting 162D611605, Longerons 162D611635 shall have a 63 RHR or better surface finish through stack up.

9. The 162D711140-2003, 162D711180-2003, 162D711180-2004, 162D712140-2001, 162D712140-2002, 162D712151-2051, 162D712151-2052, 162D712171-2051, 162D712171-2052 and 162D611572-2021 PR’s will be updated to include an updated CORE 14 note.

10. The 162D611572-2021 PR will be updated to provide sources of supply for the Cruciform: Part shall be fabricated per P.S 14295. Approved source for fabrication is RMB Products, 1201 RMB Court, Fountain, CO 80817.

11. S-F502 will be updated from Revision K to include Kevlar in the scope, S-F501in the applicable documents and various clarifications in all sections to remove ambiguity and update materials and specifications that have become outdated.

12. Note 004556 will be corrected to call out Z-R901 instead of Z-P901.

13. Note 007344 will be corrected to call out drawing no. 162D641031-1003 instead of 162D641031-1001.

14. When Fairchild Quality Assurance Test Bulletin(QATB) documents are called out by part reports, specifications or other engineering, the following updated specs shall be used to satisfy the original QATB process requirements;

PW220T0040 in place of QATB M-40

PW220T0037 in place of QATB M-37

PW220T0036 in place of QATB M-36

PW220T0035 in place of QATB M-35

15. A working copy of specification A-F501_RevH is contained in the TDP, this revision is currently under review and it is the Government’s intent to have a final version at contract award. Minimal changes may be made to this revision before final signature.

16. The 162D712100-0001/0003 deceleron assembly will be updated to include a new anti-rotation pin design in the outboard leading edge fittings. The new design will replace the MS20392-13P21 pin and MS24665-86 cotter pin with NAS1160-08-8H shoulder bolt and safety wire.