Drawings.pdf

88.000+ .000 .125

5.375+ .000 .063 2X

5.375+ .000 .063 2X

70.000 -.020 2X

60.000 -.020 2X

50.000 -.020 2X

40.000 -.020 2X

30.000 -.020 2X

20.000 -.020 2X

10.000 -.020 2X

108.000+ .000 .125

90.000 -.020 2X

70.000 -.020 2X

80.000 -.020 2X

60.000 -.020 2X

50.000 -.020 2X

40.000 -.020 2X

30.000 -.020 2X

20.000 -.020 2X

10.000 -.020 2X

3.725 REF

1.650 REF

1.650 REF

3.725 REF

1.375 REF

1.375 REF

44.000 REF

54.000REF

A

A

B

C

D

D

EE

I

I

4a

TOP

TOP

TOP

INBD

INBD

3 1 2 2 3

4a 4a 4a

4b

4b 4b

4a

REFERENCE: EXTRUSION PAINTED

MARKINGS FOR MANUFACTURING

ORIENTATION.

AS AN ALTERNATIVE TO THE SHOWN

MARKINGS AND MARKING SYSTEM,

ALTERNATIVE MANUFACTURING

ORIENTATION MARKINGS ARE

PERMITTED AT THE DISCRETION OF

THE MANUFACTURER. THESE

MARKINGS DO NOT NEED TO BE

REMOVED PRIOR TO DELIVERY.

INBD

INBD

TOP

REFERENCE: DASHED LINES ARE INK

MARKINGS FROM THE MIDDLE

PANEL EXTRUSION DRAWING

(201642456).

GMAW or GTAW, 4 PLACES

BY THE GOVERNMENT DESIGN ACTIVITY.

MAINTAINED BY A CAD SYSTEM. CHANGES

SHALL ONLY BE INCORPORATED AS DIRECTED

THIS DRAWING HAS BEEN GENERATED AND IS

NEXT GENERATION

CARGO - HCU-6A/E

PALLET ASSEMBLY,

PROJECT ENGINEER

FA8519-14-C-0004

.010

.03 06 JUL 2016

N. NGUYEN

D. BOWMAN

20164245598752

1/6 1 OF 2T. CAPELLE

G. MARTIN

K. VEHORN1°

THIRD ANGLE PROJECTION

U.S. AIR FORCE

_+.X

DO NOT SCALE DRAWING

_+.XX

.XXX

DIMENSIONS AND SURFACE

TEXTURE DESIGNATIONS APPLY

BEFORE PLATING OR FINISH

COATINGS

USED ONNEXT ASSY

APPROVEDDATE

REVISION HISTORY

REV DESCRIPTION

REV STATUS

OF SHEETS

R E

V S

H D

W G

N O

C

F

G

H

A

D

E

CAGE CODE

CURRENT

APPLICATION

TITLE

E

DWG NO.

SHEET

CAGE CODESIZE

SCALE

CHECKER

AF RELEASE

AF AUTHENTICATION

CONTRACT NO.

ENGINEERING APPROVAL

DATEDRAFTER

ANGLESDECIMALSFRACTIONS

DIMENSIONS ARE IN INCHES -TOLERANCES ON:

UNLESS OTHERWISE SPECIFIED

FINISH

TREATMENT

6 5 4 3 2 1

B

C

8 7 6 5 4 3 2 1

F

G

H

A

D

E

HCU-6A/E

NOTES:

1. INTERPRET THIS DRAWING IAW ASME Y14.100-2013.

2. NOTCH WITHOUT HOLES OR TIE-DOWN RING ASSEMBLY.

3. ASSEMBLY AND MACHINING SEQUENCE AT MANUFACTURER'S DISCRETION TO ACHIEVE FINAL

GEOMETRY.

4. WELD LINE:

a. FULL PENETRATION FRICTION STIR WELDING IAW ANSI STD AWS D17.3:2010 CLASS B (DYE

PENETRANT INSPECTION NOT REQUIRED, CERTIFIED WELD INSPECTOR NOT REQUIRED FOR

PRODUCTION WELDS).

b. GAS METAL ARC WELDING (GMAW) OR GAS TUNGSTEN ARC WELDING (GTAW) IAW ANSI STD AWS D1.2. V-GROOVE DEPTH TO 65% OF THICKNESS TO ACHIEVE FULL DEPTH PENETRATION. USE

5356 WIRE.

c. VENDOR TO MACHINE FACING SURFACE AT WELD LINES TO ACHIEVE "AS-WELDED"

DIMENSIONS. SEE NOTES 11-14.

d. FRICTION STIR WELD PIN EXTRACTION HOLE TO BE REMOVED WITH TAB OR FILLED AS PART

OF GMAW OR GTAW WELDS.

e. FRICTION STIR WELD FLASHING THAT IS SHARP OR ABRASIVE SHALL BE POLISHED/REMOVED

WITH A BUFFING WHEEL OR SIMILAR SYSTEM.

f. AFTER CLEANUP, GMAW OR GTAW WELDS SHALL NOT STAND ABOVE THE TOP OR BOTTOM

SURFACES OF THE PALLET BY MORE THAN 0.020, OR ABOVE THE SURFACES AT THE VERTICAL

CORNERS BY MORE THAN 0.060.

g. TOP SURFACE SHOWN - CONTINUOUS WELDS ON TOP AND BOTTOM SURFACES AT ALL

EXTRUSION MATING LINES/JOINTS, AND AROUND CORNERS AT "PICTURE FRAME" JOINTS.

5. MAXIMUM WEIGHT SHALL NOT EXCEED 300 LBS.

6. BREAK ALL SHARP EDGES APPROX .010R.

7. FLATNESS REQUIREMENTS: A STRAIGHT EDGE APPLIED TO ENTIRE LENGTH OR WIDTH ON TOP

AND BOTTOM SURFACE OF PALLET SHALL REVEAL NO GAP EXCEEDING .187 INCH AT ANY POINT.

8. COAT 1/2" OF RIVET SHANK WITH MIL-DTL-53022, TYPE IV EPOXY. DRIVE THE RIVET WHILE PRESERVATIVE IS WET, 66 PLACES. USE 201642460 ALTERED ITEM HUCK RIVET TOOL NOSE ASSEMBLY TO

ENSURE PROPER SWAGING OF RIVET HEADS.

9. AFTER THE RIVET IS DRIVEN THE HEAD AND PIN SHALL BE COATED WITH ONE COAT MIL-DTL-

53022, TYPE IV EPOXY, 66 PLACES.

10. IAW MIL-STD-130 EACH PALLET SHALL HAVE "PROPERTY OF US AIR FORCE RETURN TO NEAREST AIR FORCE BASE" CENTERED AND STENCILED IN 1.00-INCH HIGH LETTERS ON THE TOP OF THE

LOCKING LIPS ON EACH LONG SIDE PANEL EDGE. THE MARKINGS SHALL BE MADE WITH

MANUFACTURERS STANDARD COMMERCIAL PAINT CLOSEST TO COLOR NUMBER 17038 OF FED-STD-

595. FOUR IDENTIFICATION PLATES SHALL BE ATTACHED TO THE PALLET CONFORMING TO A-A-50271 AND MARKED IAW MIL-STD-130. THE IDENTIFICATION PLATES SHALL BE OF A SIZE AND SHAPE CONSISTENT WITH THE INFORMATION REQUIRED. ONE PLATE SHALL BE LOCATED ON EACH OF ALL FOUR SIDES OF THE PALLET ABOVE THE LOCKING LIPS. THE IDENTIFICATION PLATES SHALL CONTAIN

THE FOLLOWING INFORMATION:

MANUFACTURER'S FEDERAL SUPPLY CODE

MANUFACTURER'S SERIAL NUMBER

CONTRACT NUMBER

DATE OF MANUFACTURE

IN LIEU OF IDENTIFICATIONS PLATES, PALLETS MAY BE LASER ETCHED WITH THE REQUIRED

INFORMATION IN THE SPECIFIED LOCATIONS.

11. LENGTH OF SIDE PANEL TOP AND BOTTOM SKINS SHALL BE TRIMMED TO FIT EXTRUDED MIDDLE

PANEL MATING JOINT AND COMPLY WITH OVERALL PALLET DIMENSION REQUIREMENTS.

12. ORIENTATIONS OF MIDDLE PANELS ARE CRITICAL TO PERFORMANCE. MANUFACTURER SHALL VERIFY THE ORIENTATION OF PANELS TO ENSURE THICKER BOTTOM SKINS ARE LOCATED TOWARD THE

PALLET CENTERLINE PRIOR TO FRICTION STIR WELDING OF ASSEMBLY.

13. INBD SIDE OF MIDDLE PANEL MACHINED TO CREATE TOP AND BOTTOM SKIN EXTENSIONS THAT MATE WITH INBD SIDE OF MATING AS EXTRUDED MIDDLE PANEL. MANUFACTURER SHALL MACHINE AS

NECESSARY TO ACCOMMODATE EXTRUSION VARIATIONS AND COMPLY WITH OVERALL PALLET

DIMENSION REQUIREMENTS.

14. MANUFACTURER SHALL MACHINE TOP AND BOTTOM SKINS AND RIBS TO MATE ENDS OF SIDE AND MIDDLE PANELS WITH EDGE RAILS AND PREPARE THEM FOR FRICTION STIR WELDING, SEQUENCE

AT MANUFACTURER'S DISCRETION.

15. MANUFACTURER SHALL WORK WITH EXTRUDER TO DEVELOP ACCEPTABLE TOLERANCES TO

MEET AWS D17.3 REQUIREMENTS AT WELD LOCATIONS. SPECIFICALLY ALLOWABLE MISMATCH SHALL

BE ADDRESSED BY CONTROLLING TOLERANCES AT THESE LOCATIONS AS WELL WITH SECONDARY

MACHINING/TRIMMING OPERATIONS. EXTRUSIONS IN TOLERANCE WITH EXTRUSION DRAWINGS AND

ANSI H35.2 DO NOT GUARANTEE WELDABLE JOINTS WITHOUT ADDITIONAL MACHINING AND

PREPARATION.

16. WELD REPAIR ALLOWED TO RECOVER FROM INADVERTENT WELD PROCESS STOP OR VISUALLY

DETECTED FLAW. REPAIR TECHNIQUES ALLOWED ARE FSW AND GMAW/GTAW. THIS INCLUDES A

SINGLE PASS RE-WELD OF ANY JOINT WITH FSW OR GMAW/GTAW UTILIZING A QUALIFIED WORK PROCESS SPECIFICATION (WPS). THE DEVELOPMENT OF THE REPAIR PROCEDURES SHALL BE QUALIFIED

ACCORDING TO THE PERFORMANCE REQUIREMENTS OF AWS D17.3 FOR FSW AND AWS D1.2 FOR

GMAW/GTAW, TO THE EXTENT SPECIFIED IN THE RESULTS SECTION OF PROCESS QUALIFICATION RECORD (PQR). REPAIR CRITERIA SHALL BE IN ASSOCIATED MANUFACTURING PLAN OR SEPARATE REPAIR PROCEDURE. FOR GMAW/GTAW REPAIRS, DYE PENETRANT INSPECTION IS REQUIRED AFTER

REPAIR. REPAIR AREA SHALL BE GROUND AS NECESSARY TO MEET FLUSHNESS REQUIREMENTS.

17. THIS DRAWING (201642455_1.SLDDRW AND 201642455_2.SLDDRW) IS BASED ON A 3D MODEL

(CARGO PALLET ASSEMBLY(201642455-10).SLDASM).

1201642458-0198752EDGE RAIL2

ACCORDANCE WITH PROVISIONS OF DOD DIRECTIVE 5230-25.

EXPORT CONTROL NOTICE DISTRIBUTION STATEMENT C NOTICE DESTRUCTION NOTICE

WARNING -THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE

EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT

(TITLE 22, U.S.C. SEC 2751 ET SEQ.) OR THE EXPORT

ADMINISTRATION ACT OF 1979 (TITLE 50, U.S.C., APP 2401 ET

SEQ.), AS AMENDED. VIOLATIONS OF THESE EXPORT LAWS ARE

SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE IN

DISTRIBUTION STATEMENT C. DISTRIBUTION AUTHORIZED TO U.S.

REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO

AFLCMC/WNZEB, ROBINS AFB, GA 31098.

DESTRUCTION NOTICE-FOR CLASSIFIED DOCUMENTS, FOLLOW

THE PROCEDURES IN DoD 5220.22-M, INDUSTRIAL SECURITY

MANUAL, CHAPTER 5, SECTION PARAGRAPHS 700 THROUGH 711

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.

WT.

UNIT

QUANTITY REQUIRED PER SUFFIX (DASH) NUMBER PARTS LIST

ZONENOMENCLATURE CAGE CODE IDENTIFYING NO. MATERIAL / SPECIFICATION NO.

FIND

PARTS LIST

201642456-01 298752MIDDLE PANEL2

4201642459-1098752TIE-DOWN RING ASSEMBLY22

BOM-R10-89K475RIVET, BLIND66

3201642457-0198752SIDE PANEL2

201642455-10ASSEMBLY 98752

52G7

2G7

1H6 1H4 1H5 1H4 1H5 1C6

GOVERNMENT AGENCIES AND THEIR CONTRACTORS (FOR THEIR

ADMINISTRATIVE OR OPERATIONAL USE; 2014-MAY-23). OTHER

C. HERNANDEZ

06 JUL 2016

06 JUL 2016

06 JUL 2016

06 JUL 2016

06 JUL 2016

K.VEHORN29 AUG 2018

CHANGES TO NOTES 4 AND 10, CHANGES TO ORIENTATION

MARKINGS, ADDED NOTES 15 AND 16, TIE-DOWN RING CORRECTION

OF DASH NO IN PARTS LIST, CHANGED FIRST AND CENTER POCKET

DIMENSIONS, AND DRAWING TITLE MODIFIED FROM HCU-6E TO

HCU-6A/E.

2 K.VEHORN

SECTION H (ZONE F7) DEPTH OF RELIEF CUT CHANGED FROM 0.250

TO 0.380 +0.050/-0.000.

29 AUG 2018

A

A

SHEET

B

K.VEHORN16 JAN 2019

ADDED NOTE LEADERS IN ZONE F6, C6-7, C4-5, AND C2-3.

B2

R.12 MAX TYP

45°

1.650+ .030

.015 TYP

DETAIL C

SCALE 1 : 2

4b

TYP

TIE-DOWN RING

ASSEMBLY 201642459-01

OMITTED FOR CLARITY

TY

P

.348+ .005

.002 TYP

DRILL THRU TO

MATCH ITEM 4

1.190 REF

1.625 REF

.730+ .020 .005

.560+ .020

.005 TYP

2.100 REF

VIEW A-A

SCALE 1 : 2

5 66X

4 22X

1.650+ .030

.015 TYP

R.12 TYP

2.750+ .000

.030 TYP

DETAIL B

SCALE 1 : 2

TY

P

125 TYP

125 TYP

.348+ .005

.002 TYP

DRILL THRU TO

MATCH ITEM 4

.560+ .020

.005 TYP

1.375 TYP

1.625 .020 TYP

VIEW D-D

SCALE 1 : 2

FG H

SECTION E-E

SCALE 1 : 4

UP

.076 REF

.117 REF

DETAIL G

SCALE 1 : 1

TRIMMED SIDE PANEL

201642457-01

AS EXTRUDED, OUTBD

SIDE OF MIDDLE PANEL

201642456-01

.100 REF .100 REF

.100 REF

.090 REF .090 REF

.162 REF .162 REF

DETAIL F

SCALE 1 : 1

AS EXTRUDED, INBD SIDE

OF MIDDLE PANEL

201642456-01

MACHINED INBD SIDE

OF MIDDLE PANEL

201642456-01

.076 REF

.117 REF

DETAIL H

SCALE 1 : 1

TRIMMED SIDE PANEL

201642457-01

AS EXTRUDED OUTBD

SIDE OF MIDDLE PANEL

201642456-01

.075

.380+ .050 .000

.080

SECTION I-I

SCALE 1 : 1

BY THE GOVERNMENT DESIGN ACTIVITY.

MAINTAINED BY A CAD SYSTEM. CHANGES

SHALL ONLY BE INCORPORATED AS DIRECTED

THIS DRAWING HAS BEEN GENERATED AND IS

2016425598752

VARIOUS 2 OF 2

R E

V S

H D

W G

N O

C

F

G

H

A

D

E

8 7

E

DWG NO.

SHEET

CAGE CODESIZE

SCALE

6 5 4 3 2 1

B

C

8 7 6 5 4 3 2 1

F

G

H

A

D

E

SEE SHT 1 FOR PARTLIST, NOTES AND REVISION STATUS

B

4X .144

2.100±.034

9X .076 .100

.172 .140

R6.034 13X 10.3°

2X .140

R6.034

2X .090

R5.622

2X .081 2X .081

2X .090 2X .090 2X .090 2X .090 2X .090 2X .090 2X 12.8° 2X 12.8°

2X .084 2X .087 2X .090 2X .093 2X .101 2X .101

R5.362 R5.122 R4.902 R4.802 R4.182 R4.182

9X 2.140

2X .081

4X 35°

4X R.016

22.060+ .000 .125

2X .100 2X .100

11X .060

2X 12.8° R3.395

.100

.295 .089

4X R.179

R.016 TYP

1.900 .024

.841

4X 45°

.090

4X R.075 R.150 TYP

R.150 TYP

2.200

4X R.075

.100

.660 .117 .117 .122 .127 .132 .137 .141 .157 .157 .162

.660 .680 .680 .680 .680 .680 .680 .680

2.260

.030

.698

4X .200

4X .170

9X 2.200

2X .210

REF: MIDDLE PANEL TO MIDDLE

PANEL (MACHINED) JOINT NEXT ASSY

REF: MIDDLE PANEL TO SIDE PANEL

JOINT NEXT ASSY

REF: APPROX PALLET

CENTER NEXT ASSY

OUTBD

INBD

+NOTE 13

- 0.010

UP

+NOTE 12

- 0.000

+NOTE 12

- 0.005

+NOTE 13

- 0.010

2.1 X 22.5 X 114, 6005A-T61, ASTM B221-14 11

1201642456-0198752MIDDLE PANEL EXTRUSION1

ACCORDANCE WITH PROVISIONS OF DOD DIRECTIVE 5230-25.

EXPORT CONTROL NOTICE DISTRIBUTION STATEMENT C NOTICE DESTRUCTION NOTICE

WARNING -THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE

EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT

(TITLE 22, U.S.C. SEC 2751 ET SEQ.) OR THE EXPORT

ADMINISTRATION ACT OF 1979 (TITLE 50, U.S.C., APP 2401 ET

SEQ.), AS AMENDED. VIOLATIONS OF THESE EXPORT LAWS ARE

SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE IN

DISTRIBUTION STATEMENT C. DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS (FOR THEIR

ADMINISTRATIVE OR OPERATIONAL USE; 2014-MAY-23). OTHER

REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO

AFLCMC/WNZEB, ROBINS AFB, GA 31098.

DESTRUCTION NOTICE-FOR CLASSIFIED DOCUMENTS, FOLLOW

THE PROCEDURES IN DoD 5220.22-M, INDUSTRIAL SECURITY

MANUAL, CHAPTER 5, SECTION PARAGRAPHS 700 THROUGH 711

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.

BY THE GOVERNMENT DESIGN ACTIVITY.

MAINTAINED BY A CAD SYSTEM. CHANGES

SHALL ONLY BE INCORPORATED AS DIRECTED

THIS DRAWING HAS BEEN GENERATED AND IS

201642456

MIDDLE PANEL EXTRUSION-

PALLET,

AIRBORNE CARGO

PROJECT ENGINEER

FA8519-14-C-0004

.005

.01

20164245698752

1/1 1 OF 1

06 JUL 2016

G. MARTIN

K. VEHORN1°

WT.

UNIT

NO.

THIRD ANGLE PROJECTION

U.S. AIR FORCE

_+.X

DO NOT SCALE DRAWING

_+.XX

.XXX

QUANTITY REQUIRED PER SUFFIX (DASH) NUMBER

USED ON NEXT ASSY

APPLICATION

APPROVEDDATEREV DESCRIPTION

PARTS LIST

ZONENOMENCLATURE CAGE CODE IDENTIFYING NO. MATERIAL / SPECIFICATION

SHDWG NO.

18 57 6 4 3 1

8 57 6 4 3 2 1

D

C

B

A

D

C

B

A

CAGE CODE

CURRENT

REVISION HISTORY

TITLE

D

DWG NO.

SHEETWEIGHT

CAGE CODESIZE

SCALE

CHECKER

AF RELEASE

AF AUTHENTICATION

CONTRACT NO.

ENGINEERING APPROVAL

DATEDRAFTER

ANGLESDECIMALSFRACTIONS

DIMENSIONS ARE IN INCHES -TOLERANCES ON:

UNLESS OTHERWISE SPECIFIED

FINISH

TREATMENT

SHEET

REV STATUS

OF SHEETS

B5

201642455 HCU-6A/E

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100-2013.

2. EXTRUSION TOLERANCES PER ANSI H35.2 EXCEPT AS NOTED.

3. DELETED.

4. DELETED.

5. BLENDING OF SKINS SHALL BE SMOOTH WITHOUT HARMFUL DISCONTINUITIES, THERE SHALL BE NO

THINNING OF WEBS OR SKINS AT TANGENT POINT RADII.

6. EXTRUDER SHALL FURNISH LENGTHS OF 114 INCHES WITH SQUARE ENDS UNLESS A DIFFERENT

DIMENSION IS REQUESTED BY THE FRICTION STIR WELD/ASSEMBLY CONTRACTOR.

7. DELETED.

8. EXTRUDER SHALL MARK TOP OF EXTRUSION ALONG TRIM LINE WITH A DASHED LINE AND THE WORDS "TOP INBD" AT BOTH ENDS OF THE TRIM LINE WITH AN ARROW POINTING TO THE EDGE USING INDELIBLE INK (REF 20164255 SHT 1) IN LIEU OF THE SHOWN MARKINGS AND MARKING SYSTEM.

ALTERNATIVE MANUFACTURING ORIENTATION MARKINGS ARE PERMITTED AT THE DISCRETION OF THE

MANUFACTURER. THESE MARKINGS DO NOT NEED TO BE REMOVED PRIOR TO DELIVERY.

9. DELETED.

10. DELETED.

11. AS AN ALTERNATE, 6061-T6, ASTM B221-14 MAY BE USED.

12. MAXIMUM WEIGHT NOT TO EXCEED 7.75 LBS/FT UNLESS APPROVED BY MANUFACTURER OF PALLET.

13. SURFACE MUST BE 0.007 OF SHELF HEIGHT.

14. UNLESS OTHERWISE NOTED ALL THICKNESS TOLERANCES SHALL BE (+NOTE 12/-0.010).

15. THIS DRAWING (201642456.SLDDRW) IS BASED ON A 3D MODEL (MIDDLE PANEL EXTRUSION

(201642456-01).SLDPRT).

N. NGUYEN

C. HERNANDEZ

D. BOWMAN

06 JUL 2016

06 JUL 2016

06 JUL 2016

06 JUL 2016

06 JUL 2016

FIND

NO.

FIND

NO.

FIND

T. CAPELLE

EXTRUSION PARAMETERS

BOW: .0125 IN/FT STRAIGHTNESS: .0125 IN/FT

FLATNESS: .014 IN/IN TWIST: .25 DEG/FT, 3 DEG MAX

ANGULARITY: ± 1.5 DEG

A

DELETED NOTES 7, 9, AND 10. CHANGED NOTE

8, EXTRUSION GEOMETRY, AND MODIFIED

NEXT HIGHER ASSY TO HCU-6A/E.

29 AUG 2018 K. VEHORN1

K. VEHORN16 JAN 2019EXTRUSION GEOMETRY CHANGES AND ADDED

NOTE 12, 13, AND 14. DELETED NOTES 3 AND 4. B1

8X .090 8X .140

4X R6.042 R4.182 3X R5.252 2X 12.8°

4X .065

4X .060 R.150 TYP

4X 2.135 2.138 3X 2.140

6X 10°

6X .091 2X .101

8X 10°

8X .081

2.100

.034 AT BASE

.054 AT TIPS

4X .100 4X .076

2X .100 .014

R.150 TYP

4X .680 4X .660

3X .135 .157

4X .117

21.920, NOMINAL TRIM LINE

LOCATION, SEE NEXT ASSEMBLY

22.212+ .200 .000

2.200 TYP

A

INBD

OUTBD

+NOTE 9

- 0.000+NOTE 9

- 0.000

1.830 .024

.250 .038

R.367

R.625

R.563

.100 1°

18°

.875±.018

R.125

17°

4X R.075 4X R.075

2°

.125

R.125

R.187

.188

R.134 R.150

R.125

R.125

3°

R.118

37°

R.150 .070

.088

1.116

1.713

3.500

83°

.302

.147

.503

.195

.175 .153

.120

.181 .107

.044

.034

.435

DETAIL A

SCALE 2 : 1

TAPER FROM .070 to .088

UP

2.1 X 22 X 114, 6005A-T61, ASTM B221-14 8 1201642457-0198752SIDE PANEL EXTRUSION1

ACCORDANCE WITH PROVISIONS OF DOD DIRECTIVE 5230-25.

EXPORT CONTROL NOTICE DISTRIBUTION STATEMENT C NOTICE DESTRUCTION NOTICE

WARNING -THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE

EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT

(TITLE 22, U.S.C. SEC 2751 ET SEQ.) OR THE EXPORT

ADMINISTRATION ACT OF 1979 (TITLE 50, U.S.C., APP 2401 ET

SEQ.), AS AMENDED. VIOLATIONS OF THESE EXPORT LAWS ARE

SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE IN

DISTRIBUTION STATEMENT C. DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS (FOR THEIR

ADMINISTRATIVE OR OPERATIONAL USE; 2014-MAY-23). OTHER

REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO

AFLCMC/WNZEB, ROBINS AFB, GA 31098.

DESTRUCTION NOTICE-FOR CLASSIFIED DOCUMENTS, FOLLOW

THE PROCEDURES IN DoD 5220.22-M, INDUSTRIAL SECURITY

MANUAL, CHAPTER 5, SECTION PARAGRAPHS 700 THROUGH 711

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.

BY THE GOVERNMENT DESIGN ACTIVITY.

MAINTAINED BY A CAD SYSTEM. CHANGES

SHALL ONLY BE INCORPORATED AS DIRECTED

THIS DRAWING HAS BEEN GENERATED AND IS

201642457

AIRBORNE CARGO

PALLET,

SIDE PANEL EXTRUSION-

PROJECT ENGINEER

FA8519-14-C-0004

.005

.01

201642457

1/1 1 OF 1

06 JUL 2016

G. MARTIN

K. VEHORN 1°

WT.

UNIT

NO.

FIND

NO.

THIRD ANGLE PROJECTION

U.S. AIR FORCE

_+.X

DO NOT SCALE DRAWING

.XX

.XXX

QUANTITY REQUIRED PER SUFFIX (DASH) NUMBER

USED ONNEXT ASSY

APPLICATION

APPROVEDDATEREV DESCRIPTION

PARTS LIST

ZONENOMENCLATURE CAGE CODE IDENTIFYING NO. MATERIAL / SPECIFICATION NO.

SHDWG NO.

18 57 6 4 3 1

8 57 6 4 3 2 1

D

C

B

A

D

C

B

A

CAGE CODE

CURRENT

REVISION HISTORY

TITLE

D

DWG NO.

SHEETWEIGHT

CAGE CODESIZE

SCALE

CHECKER

AF RELEASE

AF AUTHENTICATION

CONTRACT NO.

ENGINEERING APPROVAL

DATEDRAFTER

ANGLESDECIMALSFRACTIONS

DIMENSIONS ARE IN INCHES -TOLERANCES ON:

UNLESS OTHERWISE SPECIFIED

FINISH

TREATMENT

SHEET

REV STATUS

OF SHEETS

B6

EXTRUSION PARAMETERS

BOW: .0125 IN/FT STRAIGHTNESS: .0125 IN/FT

FLATNESS: .014 IN/IN TWIST: .25 DEG/FT, 3 DEG MAX

ANGULARITY: ± 1.5 DEG

201642455 HCU-6A/E

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100-2013.

2. EXTRUSION TOLERANCES PER ANSI H35.2, EXCEPT AS NOTED.

3. DELETED.

4. DELETED.

5. BLENDING OF SKINS SHALL BE SMOOTH WITHOUT HARMFUL DISCONTINUITIES,

THERE SHALL BE NO THINNING OF WEBS OR SKINS AT TANGENT POINT RADII.

6. EXTRUDER SHALL FURNISH LENGTHS OF 114 INCHES WITH SQUARE ENDS UNLESS A

DIFFERENT DIMENSION IS REQUESTED BY THE FRICTION STIR WELD/ASSEMBLY

CONTRACTOR.

7. DELETED.

8. AS AN ALTERNATE, 6061-T61, ASTM B221-14, MAY BE USED.

9. MAXIMUM WEIGHT NOT TO EXCEED 8.3 LBS/FT UNLESS APPROVED BY

MANUFACTURER OF PALLET.

10. UNLESS OTHERWISE NOTED ALL THICKNESS TOLERANCES SHALL BE (+NOTE 9/-

0.010).

11. THIS DRAWING (201642457.SLDDRW) IS BASED ON A 3D MODEL (SIDE PANEL

EXTRUSION (201642457-01).SLDPRT).

T. CAPELLE

N. NGUYEN

C. HERNANDEZ

D. BOWMAN

06 JUL 2016

06 JUL 2016

06 JUL 2016

06 JUL 2016

06 JUL 2016

98752

K. VEHORN29 AUG 2018

DELETED NOTE 7, MADE EXTRUSION

GEOMETRY CHANGES, AND CHANGED

NEXT HIGHER ASSY TO HCU-6A/E.

A1

K. VEHORN16 JAN 2019

EXTRUSION GEOMETRY CHANGES AND

ADDED NOTE 9 AND 10. DELETED NOTES 3

AND 4.

B1

3.500 .034

1.830 .024

.225

R.592

R.375

.125

R.367

.875 .018

18°

.100±.010 2°

2X R.125

2X 61°

.075±.006

.080±.006

2X .375+ .000 .050

2X 35°

2X .037

3°

R.125

R.125

37°

2.100 .034 .090

2X .250

R.125

R.135

4X R.156

3°

2X R.125

14°

R.187

.188

6X R.125

.200 .010

.205 .010

3°

1.712

.136

.488

.213

.128 .201 2X .136

.199

.594 .397

1.210 .323

.045

2X .124

1.250

+NOTE 7

- 0.035

UP

+NOTE 7

- 0.013

+NOTE 7

- 0.005

2.1 x 3.9 x 92, 6005A-T61, ASTM B221-14 6 1201642458-0198752EDGE RAIL EXTRUSION1

ACCORDANCE WITH PROVISIONS OF DOD DIRECTIVE 5230-25.

EXPORT CONTROL NOTICE DISTRIBUTION STATEMENT C NOTICE DESTRUCTION NOTICE

WARNING -THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE

EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT

(TITLE 22, U.S.C. SEC 2751 ET SEQ.) OR THE EXPORT

ADMINISTRATION ACT OF 1979 (TITLE 50, U.S.C., APP 2401 ET

SEQ.), AS AMENDED. VIOLATIONS OF THESE EXPORT LAWS ARE

SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE IN

DISTRIBUTION STATEMENT C. DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS (FOR THEIR

ADMINISTRATIVE OR OPERATIONAL USE; 2014-MAY-23). OTHER

REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO

AFLCMC/WNZEB, ROBINS AFB, GA 31098.

DESTRUCTION NOTICE-FOR CLASSIFIED DOCUMENTS, FOLLOW

THE PROCEDURES IN DoD 5220.22-M, INDUSTRIAL SECURITY

MANUAL, CHAPTER 5, SECTION PARAGRAPHS 700 THROUGH 711

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.

BY THE GOVERNMENT DESIGN ACTIVITY.

MAINTAINED BY A CAD SYSTEM. CHANGES

SHALL ONLY BE INCORPORATED AS DIRECTED

THIS DRAWING HAS BEEN GENERATED AND IS

201642458

EDGE RAIL EXTRUSION-

PALLET,

AIRBORNE CARGO

PROJECT ENGINEER

FA8519-14-C-0004

.005

.01

20164245898752

2/1 1 OF 1

06 JUL 2016

G. MARTIN

K. VEHORN1°

WT.

UNIT

NO.

FIND

NO.

FIND

THIRD ANGLE PROJECTION

U.S. AIR FORCE

_+.X

DO NOT SCALE DRAWING

_+.XX

.XXX

QUANTITY REQUIRED PER SUFFIX (DASH) NUMBER

USED ON NEXT ASSY

APPLICATION

APPROVEDDATEREV DESCRIPTION

PARTS LIST

ZONENOMENCLATURE CAGE CODE IDENTIFYING NO. MATERIAL / SPECIFICATION NO.

FIND

SHDWG NO.

18 57 6 4 3 1

8 57 6 4 3 2 1

D

C

B

A

D

C

B

A

CAGE CODE

CURRENT

REVISION HISTORY

TITLE

D

DWG NO.

SHEETWEIGHT

CAGE CODESIZE

SCALE

CHECKER

AF RELEASE

AF AUTHENTICATION

CONTRACT NO.

ENGINEERING APPROVAL

DATEDRAFTER

ANGLESDECIMALSFRACTIONS

DIMENSIONS ARE IN INCHES -TOLERANCES ON:

UNLESS OTHERWISE SPECIFIED

FINISH

TREATMENT

SHEET

REV STATUS

OF SHEETS

B4

201642455 HCU-6A/E

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100-2013.

2. EXTRUSION TOLERANCES PER ANSI H35.2, EXCEPT AS NOTED.

3. BLENDING OF SKINS SHALL BE SMOOTH WITHOUT HARMFUL DISCONTINUITIES, THERE SHALL BE

NO THINNING OF WEBS OR SKINS AT TANGENT POINT RADII.

4. EXTRUDER SHALL FURNISH LENGTHS OF 92 INCHES WITH SQUARE ENDS UNLESS A DIFFERENT

DIMENSION IS REQUESTED BY THE FRICTION STIR WELD/ASSEMBLY CONTRACTOR.

5. DELETED.

6. AS AN ALTERNATE, 6061-T61, ASTM B221-14, MAY BE USED.

7. MAXIMUM WEIGHT NOT TO EXCEED 2.5 LBS/FT UNLESS APPROVED BY MANUFACTURER OF

PALLET.

8. UNLESS OTHERWISE NOTED ALL THICKNESS TOLERANCES SHALL BE (+NOTE 7/-0.010).

9. THIS DRAWING (201642458.SLDDRW) IS BASED ON A 3D MODEL (EDGE RAIL EXTRUSION

(201642458-01).SLDPRT).

T. CAPELLE

N. NGUYEN

C. HERNANDEZ

D. BOWMAN

06 JUL 2016

06 JUL 2016

EXTRUSION PARAMETERS

BOW: .0125 IN/FT STRAIGHTNESS: .0125 IN/FT

FLATNESS: .014 IN/IN TWIST: .25 DEG/FT, 3 DEG MAX

ANGULARITY: ± 1.5 DEG

06 JUL 2016

06 JUL 2016

06 JUL 2016

K. VEHORN29 AUG 2018

DELETED NOTE 5, MADE EXTRUSION

GEOMETRY CHANGES, AND CHANGED

NEXT HIGHER ASSY TO HCU-6A/E.

A1

K. VEHORN16 JAN 2019EXTRUSION GEOMETRY CHANGES AND

ADDED NOTE 7 AND 8.B1

0.50

0.06 0.00

2.25

R0.63

3X 0.25

3X 0.348 0.005 0.002

R0.325

(OPPOSING SIDE)

0.35

0.04 0.00

0.682

MIN TRIM

2X R0.11

2X R0.06 70° 60°

3.932

1.625 0.010

1.210

0.456

R0.156 4 PLACES

(OPPOSING SIDE)

60° 3X

30°

10 4 PLCS

4X R 0.120 SPHERICAL 4X R 0.04

R 0.046 ENTIRE EDGE

3 PLCS

3X 0.25

2X 0.187

7° TYP

SEE NOTE 6

4X R0.09

0.775

0.452

A

A

5 3 PLCS

0.312 0.10

0.134

(0.000) NO GAP

AT WELD LOCATIONS

SEE NOTE 10

R0.25

R0.31

0.05 0.01 GAP

AFTER FORMING

R0.04 TYP

(BRACKET,

FORGING) 2.10

0.02 0.05

0.25

0.04 0.00

SECTION A-A

201642459-1098752ASSEMBLY

DISTRIBUTION STATEMENT C NOTICE DESTRUCTION NOTICE

DISTRIBUTION STATEMENT C. DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS (FOR THEIR

ADMINISTRATIVE OR OPERATIONAL USE; 2014-MAY-23). OTHER

REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO

AFLCMC/WNZEB, ROBINS AFB, GA 31098.

DESTRUCTION NOTICE-FOR CLASSIFIED DOCUMENTS, FOLLOW

THE PROCEDURES IN DoD 5220.22-M, INDUSTRIAL SECURITY

MANUAL, CHAPTER 5, SECTION PARAGRAPHS 700 THROUGH 711

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.

BY THE GOVERNMENT DESIGN ACTIVITY.

MAINTAINED BY A CAD SYSTEM. CHANGES

SHALL ONLY BE INCORPORATED AS DIRECTED

THIS DRAWING HAS BEEN GENERATED AND IS

201642459

PROJECT ENGINEER

FA8519-14-C-0004

.010

.04

20164245998752

2/1 1 OF 1

06 JUL 2016

G. MARTIN

K. VEHORN1°

WT. NO.

FIND

THIRD ANGLE PROJECTION

U.S. AIR FORCE

.X

DO NOT SCALE DRAWING

_+.XX

.XXX

QUANTITY REQUIRED PER SUFFIX (DASH) NUMBER

USED ONNEXT ASSY

APPLICATION

APPROVEDDATEREV DESCRIPTION

PARTS LIST

ZONENOMENCLATURE CAGE CODE IDENTIFYING NO. MATERIAL / SPECIFICATION

SHDWG NO.

18 57 6 4 3 1

8 57 6 4 3 2 1

D

C

B

A

D

C

B

A

CAGE CODE

CURRENT

REVISION HISTORY

TITLE

D

DWG NO.

SHEETWEIGHT

CAGE CODESIZE

SCALE

CHECKER

AF RELEASE

AF AUTHENTICATION

CONTRACT NO.

ENGINEERING APPROVAL

DATEDRAFTER

ANGLESDECIMALSFRACTIONS

DIMENSIONS ARE IN INCHES -TOLERANCES ON:

UNLESS OTHERWISE SPECIFIED

FINISH

TREATMENT

SHEET

REV STATUS

OF SHEETS

201642455 HCU-6A/E

SEE NOTE 11.

1B4201642459-0198752

RING

2C4AMS-SAE6370/STL 4130201642459-03987521 BRACKET, FORGING

AMS-SAE6345/STL SHEET 4130

T. CAPELLE

N. NGUYEN

C. HERNANDEZ

D. BOWMAN

ACCORDANCE WITH PROVISIONS OF DOD DIRECTIVE 5230-25.

EXPORT CONTROL NOTICE

WARNING -THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE

EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT

(TITLE 22, U.S.C. SEC 2751 ET SEQ.) OR THE EXPORT

ADMINISTRATION ACT OF 1979 (TITLE 50, U.S.C., APP 2401 ET

SEQ.), AS AMENDED. VIOLATIONS OF THESE EXPORT LAWS ARE

SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE IN

UNIT

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100-2013.

2. BREAK ALL SHARP EDGES APPROXIMATELY .010R.

3. ASSEMBLIES SHALL BE FUNCTIONALLY AND DIMENSIONALLY INTERCHANGEABLE.

4. RING CAPACITY 7500 LBS IN ANY DIRECTION WITHIN FREEDOM OF MOVEMENT.

5. DIRECTION OF PIERCING.

6. MAXIMUM DRAFT ANGLE 7° 1°.

7. DELETED.

8. UNLESS OTHERWISE SPECIFIED, CORNER RADII TO 0.046 AND FILLET RADII TO

0.093.

9. DELETED.

10. SPOT WELD IN APPROXIMATE LOCATIONS ON MIDDLE WIDTH OF RING.

11. HEAT TREAT ASSEMBLY TO 160,000-180,000 PSI PER MIL-H-6875H. NOTE: DUE TO

HEAT AFFECTED ZONES FROM SPOT WELDING, FINAL HEAT TREATED ASSEMBLY MUST

HAVE C33-C37 (150,000-170,000 PSI) MINIMUM HARDNESS VALUES NEAR SPOT WELD

LOCATIONS.

12. ZINC ALLOY THERMO-DIFFUSION COAT IAW ASTM A1059, CLASS 40.

COMMERCIAL PRODUCT ARMORGALV 3000. PROCESS AT MAXIMUM TEMPERATURE OF

310°C (590°F) TO PREVENT DEGRADATION OF THE HEAT-TREATED STRENGTH VALUES.

13. THIS DRAWING (201642459.SLDDRW) IS BASED ON A 3D MODEL (TIE-DOWN RING

ASSEMBLY (201642459-10).SLDASM).

06 JUL 2016

06 JUL 2016

06 JUL 2016

06 JUL 2016

06 JUL 2016

A

TIE-DOWN RING ASSEMBLY -

PALLET,

AIRBORNE CARGO

CHANGED NOTE 7, DELETED NOTE 9 AND ADDED NOTES

10 AND 11, GEOMETRIC CHANGES TO BOTH RING AND

BRACKET, CHANGED MATERIAL FINISH, AND CHANGED

NEXT HIGHER ASSY TO HCU-6A/E.

29 AUG 20181 K.VEHORN

K.VEHORN16 JAN 2019

CHANGED MATERIAL TREATMENT (NOTE 11) AND FINISH

(NOTE 12), DELETED NOTE 7, AND DECREASED

TOLERANCE OF SPOT WELD LOCATIONS (ZONE B2). B1

SEE NOTE 12.