462.pdf

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T-38 Wing Acquisition
Solicitation number
FA8208-19-R-0001
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This document contains engineering data requirements for the manufacture of a wing assembly for the T-38 aircraft. Specifications for the component include using MIL-STD-130 for marking, ASME B46.1 for surface roughness measurements, and ASME Y14.5 for geometric dimensioning and tolerancing, in lieu of other standards. Straightening of castings shall be per MA-82 instead of MA-37, and screw and pipe thread tolerances per FH-32 instead of FH-32.1.

The related federal contract opportunity notice is a pre-solicitation for the T-38 wing acquisition by the Department of the Air Force Materiel Command Lifecycle Management Center at Hill Air Force Base. The solicitation for the acquisition will be posted at a later date, and the contracting officer is now Leslie Trice.

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Engineering Data Requirements Attachment "A"

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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:

WING ASSEMBLY, AIRCRAFT T-38

2. PART NUMBER:

2-23000-33

3. NATIONAL STOCK NUMBER:

1560-01-527-3968 XE

PREPARED BY:

EZEKIEL SMITH

OFFICE SYMBOL:

416 SCMS/GUEAB

DATE:

10/17/2018

HILL AFB FORM 462 Page 1 of 1

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SUPERSEDED DATA WILL NOT BE FURNISHED UNLESS SO INDICATED.

5. MARKING PER MIL-STD-130 IN LIEU OF IM-8, IM-23, IM-24 AND IM-25.

6. SURFACE ROUGHNESS PER ASME B46.1 IN LIEU OF MIL-STD-10.

7. GEOMETRIC DIMENSIONING AND TOLERANCING PER ASME Y14.5 IN LIEU OF 20Y201.

8. STRAIGHTENING OF CASTINGS PER MA-82 IN LIEU OF MA-37.

9. TOLERANCE FOR SCREW AND PIPE THREADS PER FH-32 IN LIEU OF FH-32.1.

File details come from the government source that posted it. Updated .