Atch 2 201754322-37.pdf
PDF 300 KB Posted
- Attached to
- 15108 DCSA Sources Sought Synopsis
- Solicitation number
- 15108
About this file
This is a U.S. Air Force engineering drawing for a Wire Pass Through Cover, Consolidated Stack (Part Number 201754322-37, CAGE Code D, Revision 0.02).
The part is manufactured from aluminum alloy 6061-T6 and weighs 0.117 pounds. The component features dimensions of approximately 3.000 inches in length with multiple mounting holes (6 holes at 0.125 inches diameter through holes and 2 holes at 0.125 inches for full radial cuts). The drawing specifies a 3:1 scale and includes three sheets with isometric views, section details, and masking diagrams. Manufacturing requirements include chemical film finishing per MIL-DTL-5541 Type 1 Class 3, epoxy prime per MIL-DTL-53022 Type IV, and white polyurethane coating per MIL-PRF-85285 Type II Class H (Color #17925 per FED-STD-595). All fabrication must conform to MIL-HDBK-454 and MIL-STD-108 standards. The drawing was released on 3/17/2025 and is marked as preliminary. It is designed for the ATS Program Office and used on assembly 201754322-30. The document is distribution-controlled, authorized only to DOD and U.S. DOD contractors, and marked as export-controlled under the Arms Export Control Act.
View the file
Other files
| File | Type | Posted |
|---|---|---|
| 15108 DCSA RFI SSS.pdf | ||
| Atch 6 201754323-40.pdf | ||
| Atch 5 201754323-31.pdf | ||
| Atch 4 201754322-47.pdf | ||
| Atch 3 201754322-40.pdf | ||
| Atch 1 15108 DCSA Equipment List_Redacted.pdf |
On GovTribe
Work with this file
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
AL 6061-T6WIRE PASS THROUGH COVER, CONSOLIDATED STACK201754322-3798752
PARTS LIST
MATERIAL/SPECIFICATIONDESCRIPTIONPART NUMBERCAGEC
98752D 201754322-37 0.02
UNLESS OTHERWISE SPECIFIED
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONS DECIMALS ANGLES
± 1/32 .X ± .100
.XX ± .030
.XXX ± .010
± 2°
THIRD ANGLE PROJECTION
DRAFTER
CHECKER
PROJECT ENGINEER
ENGINEERING APPROVAL
A.F. AUTHENTICATION
RELEASE
J.GILLMOR
T.PRICE
T.PRICE
B.BINGHAM
E.MULLINAX
K.SIMPSON
516 MXDPAF
516 MXDPAF
516 MXDPAF
516 MXDPAF
AFLCMC/WNAEA
AFLCMC/WNAE
DATE
3/17/2025
3/17/2025
3/17/2025
3/17/2025
U.S. AIR FORCE
TITLE
WIRE PASS THROUGH COVER,
CONSOLIDATED STACK
SIZE CAGE CODE DWG NO. REV
SCALE WEIGHT SHEET
3:1 0.117 LBS 1 OF 3
INVENTOR
CAD PROG: VER:
COMPUTER DRAWING
FILE NAME:
201754322-37.idw
UNLESS OTHERWISE INDICATED:
-DRAWING WAS PREPARED IN ACCORDANCE
WITH ASME 14.100, APPX. B THRU. E
-INTERPRET DRAWINGS IN ACCORDANCE WITH
ASME Y14.5-2009
-REMOVE BURRS AND BREAK SHARP EDGES
DESIGNED FOR:
ATS PROGRAM OFFICE
NEXT ASSY
201754322-30 2020109112-10
USED ON
APPLICATION
A A
B B
C C
D D
REVISION HISTORY
REV DESCRIPTION DATE APPROVED
0.02 INITIAL RELEASE 3/17/2025 B.BINGHAM
NOTES:
FINISH: EXCEPT WHERE SPECIFIED.
A. CHEM FILM PER MIL-DTL-5541, TYPE 1, CLASS 3
B. PRIME EXTERIOR ONLY WITH EPOXY PRIME PER MIL-DTL-53022, TYPE IV EXCEPT ON NOTED AREAS.
C. PAINT EXTERIOR ONLY WITH WHITE POLYURETHANE COATING PER MIL-PRF-85285, TYPE II, CLASS H COLOR # 17925 OF FED-STD-595.
1. IDENTIFY PART IN ACCORDANCE WITH MIL-STD-130. BAG AND TAG ALL ITEMS TOO SMALL TO IDENTIFY.
2. MASK FROM PRIMER AND PAINT.
3. ALL FABRICATION TO CONFORM TO MIL-HDBK-454 & MIL-STD-108.
4. AFTER FABRICATION, PARTS AND ASSEMBLED EQUIPMENT SHALL BE CLEANED OF SMUDGES; LOOSE, SPATTERED, OR EXCESS SOLDER; WELD METAL; METAL CHIPS AND MOLD
RELEASE AGENTS; OR ANY OTHER FOREIGN MATERIAL WHICH MIGHT DETRACT FROM THE INTENDED OPERATION, FUNCTION, OR APPEARANCE OF THE EQUIPMENT.
5. FOR DIMENSIONS NOT SHOWN REFER TO CAD DATA.
6. CAD DATA IS BASIC UNLESS OTHERWISE SPECIFIED 0.030.
PRELIMINARY
3/17/2025
DISTRIBUTION STATEMENT D
DESTRUCTION NOTICE
WARNING
DISTRIBUTION AUTHORIZED TO DOD AND U.S. DOD CONTRACTORS ONLY
FOR ADMINISTRATIVE OR OPERATIONAL USE. DATE OF DETERMINATION
IS . OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO THE
ATS PROGRAM OFFICE AFLCMC/WNA-ATS ROBINS A.F.B GA. 31098.
QUESTIONS CONCERNING TECHNICAL CONTENT SHALL BE REFERRED TO
309 SWEG/516 SWES/MXDPAF HILL A.F.B. UT. 84056
DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF
CONTENTS OR RECONSTRUCTION OF THE DOCUMENTS.
EXPORT CONTROLLED. THIS DOCUMENT CONTAINS TECHNICAL
DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT
CONTROL ACT (TITLE 22, U.S.C.2751 ET SEQ.) OR THE EXPORT
ADMINISTRATION ACT OF 1979, AS AMENDED, TITLE 50, U.S.C.,APP.
2401 ET SEQ. VIOLATION OF THESE EXPORT-CONTROL LAWS IS
SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF
THIS DOCUMENT IS CONTROLLED UNDER DoD DIRECTIVE 5230.25.
ALL SHEETS ARE THE
SAME REVISION STATUS
-37 WIRE PASS THROUGH COVER
TOP ISOMETRIC
SCALE 3 : 1
BOTTOM ISOMETRIC
SECTION A-A
SECTION B-B
TOP ISOMETRIC
A
A
B B
SIZE
DWG NO REV
SCALE
SHEET
OF
CAGE CODE
98752
D
0.02
201754322-37
J.GILLMOR
DRAWN:
CHECKED:
T.PRICE
3:1
A A
B B
C C
D D
.750
1.3751.375
1.250
3.000
6X .125
.001
.004+
THRU
.250 X 82°
R.0304X WIRE EDGE SMOOTHING
(R.125)
1.00
(.625)
1.000
.000
.015+
(.500)
.125
.015
.000+
2X
.375
B
C
A
.375
R.1254X
.005 A B C
D
.000 A B
.005 A B
.250 1.00 TO CAVITY
.004
.9375.010
.375 BETWEEN RADIAL CUTS
.000 B
.000 B
1.75
.250
.1252X FULL RADIAL CUTS
.250
(.1875)
TOP ISOMETRIC
SCALE 3 : 1
-37 MASK SHADED AREAS
SIZE
DWG NO REV
SCALE
SHEET
OF
CAGE CODE
98752
D
0.02
201754322-37
J.GILLMOR
DRAWN:
CHECKED:
T.PRICE
3:1
A A
B B
C C
D D
File details come from the government source that posted it. Updated .