Revised_Drawings.pdf

1.650 REF

3.725 REF

108.000+ .000 .125

10.000 -.020 2X

20.000 -.020 2X

30.000 -.020 2X

40.000 -.020 2X

50.000 -.020 2X

60.000 -.020 2X

70.000 -.020 2X

5.375+ .000 .063 2X

1.650 REF

3.725 REF

88.000+ .000 .125

5.375+ .000 .063 2X

10.000 -.020 2X

20.000 -.020 2X

30.000 -.020 2X

40.000 -.020 2X

50.000 -.020 2X

60.000 -.020 2X

70.000 -.020 2X

80.000 -.020 2X

90.000 -.020 2X

54.000 REF

1.375 REF

1.375 REF

44.000 REF

A

A

B

I

I

EE

D

D

C

TOP TOP

TOP TOP

TOP TOP

TOPTOP

INBD

INBD

INBD

INBD

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.

4 3 22

4a 4a 4a 4a 4a

4a

4b 4b

4b

REFERENCE: ASSEMBLE

WITH IDENTIFIER LINE

ON THE INWARD SIDE

OF THE EXTRUSION

GMAW or GTAW, 4 PLACES

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

PALLET ASSEMBLY,

CARGO - HCU-6A/E

NEXT GENERATION

PROJECT ENGINEER

x

.010

.03 x x x

4/12/2019 x

4/11/2019 x x

M. HORAN

20199342698752 1/6 1 OF 2x x

K. BRANTLEY1°

AFMC Form 1656, 20150401

WT.

UNIT

THIRD ANGLE PROJECTION

U.S. AIR FORCE

_+.X

DO NOT SCALE DRAWING

_+.XX

+.XXX

QUANTITY REQUIRED PER SUFFIX (DASH) NUMBER

DIMENSIONS AND SURFACE

TEXTURE DESIGNATIONS APPLY

BEFORE PLATING OR FINISH

COATINGS

USED ONNEXT ASSY

APPROVEDDATE

PARTS LIST

ZONENOMENCLATURE CAGE CODE IDENTIFYING NO. MATERIAL / SPECIFICATION NO.

FIND

REVISION HISTORY

REV DESCRIPTIONSH

REV

OF SHEETS

REV STATUS

R E

V S

H D

W G

N O

C

F

G

H

A

D

E

8 7

CAGE CODE

CURRENT

APPLICATION

PARTS LIST

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

ASSEMBLY 98752 201993426

EDGE RAIL

INTERMEDIATE PANEL

CENTER PANEL (DOUBLE CLOSED)

TIE-DOWN RING ASSEMBLY

SIDE PANEL

CENTER PANEL (OPEN,CLOSED)

201993428-01

201993427

20199343098752

98752

98752

98752

98752

98752

9K475RIVET, BLIND 7

201993428-02

201993429

201993431

BOM-R10-8

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 201993432 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

INTERMEDIATE PANEL MATING JOINT AND COMPLY WITH OVERALL PALLET DIMENSION

REQUIREMENTS.

12. ORIENTATIONS OF INTERMEDIATE AND CENTER 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 CENTER PANEL MACHINED TO CREATE TOP AND BOTTOM SKIN EXTENSIONS THAT MATE WITH INBD SIDE OF MATING AS EXTRUDED CENTER PANEL. MANUFACTURER SHALL MACHINE AS

NECESSARY TO ACCOMMODATE EXTRUSION VARIATIONS AND COMPLY WITH OVERALL PALLET

DIMENSION REQUIREMENTS.

14. INBD SIDE OF INTERMEDIATE PANEL TOP AND BOTTOM SKINS SHALL BE TRIMMED TO FIT

EXTRUDED CENTER PANEL MATING JOINT AND COMPLY WITH OVERALL PALLET DIMENSION

REQUIREMENTS.

15. MANUFACTURER SHALL MACHINE TOP AND BOTTOM SKINS AND RIBS TO MATE ENDS OF SIDE, INTERMEDIATE, AND CENTER PANELS WITH EDGE RAILS AND PREPARE THEM FOR FRICTION STIR

WELDING, SEQUENCE AT MANUFACTURER'S DISCRETION.

16. 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.

17. 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.

18. THIS DRAWING (201993426.SLDDRW) IS BASED ON A 3D MODEL

(CARGO PALLET ASSEMBLY(201993426.SLDASM)).

.348+ .005

.002 TYP

DRILL THRU TO

MATCH ITEM 4

2.250 REF

.560+ .020

.005 TYP

.730+ .020 .005

1.625 REF

1.190 REF

SECTION A-A

SCALE 1 : 2

5 66X

4 22X

2.750+ .000

.003 TYP

R.12 TYP

DETAIL B

SCALE 1 : 2

125 TYP

125 TYP12

TY

P

.075

.080

.380+ .050 .000

SECTION I-I

SCALE 1 : 1

G H F I AJ

SECTION E-E

SCALE 1 : 4

.348+ .005

.002 TYP

DRILL THRU TO

MATCH ITEM 4

.560+ .020

.005 TYP

1.625±.020 TYP

1.375 TYP

SECTION D-D

SCALE 1 : 2 8

45°

1.650+ .030

.015 TYP

R.12 MAX TYP

DETAIL C

SCALE 1 : 2

4b

TYP

TY

P

.100 REF

.100 REF

.076 REF

.117 REF

DETAIL G

SCALE 1 : 1

TRIMMED SIDE PANEL

201993429

AS EXTRUDED, OUTBD

SIDE OF INTERMEDIATE PANEL

201993427

.100 REF

.100REF .100 REF

.132 REF

DETAIL H

SCALE 1 : 1

AS EXTRUDED, OUTBD

SIDE OF CENTER PANEL

201993428

.100 REF .100 REF

.100 REF .100 REF

DETAIL F

SCALE 1 : 1

.100 REF .100 REF

.100 REF .132 REF

DETAIL I

SCALE 1 : 1

.100 REF

.100 REF .076 REF

.117 REF

DETAIL AJ

SCALE 1 : 1

TIE-DOWN RING

ASSEMBLY 201642459-01

OMITTED FOR CLARITY

AS EXTRUDED, OUTBD

SIDE OF INTERMEDIATE PANEL

201993427

TRIMMED SIDE PANEL

201993429

TRIMMED INBD SIDE

OF INTERMEDIATE PANEL

201993427

MACHINED INBD

SIDE OF CENTER PANEL

201993428

AS EXTRUDED, INBD

SIDE OF CENTER PANEL

201993428

TRIMMED INBD SIDE

OF INTERMEDIATE PANEL

201993427

AS EXTRUDED, OUTBD

SIDE OF CENTER PANEL

201993428

BY THE GOVERNMENT DESIGN ACTIVITY.

MAINTAINED BY A CAD SYSTEM. CHANGES

SHALL ONLY BE INCORPORATED AS DIRECTED

THIS DRAWING HAS BEEN GENERATED AND IS

SEE SHT 1 FOR PARTLIST, NOTES AND REVISION STATUS

20199342698752

VARIOUS 2 OF 2

AFMC Form 1656, 20150401

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

6X .076

R.150 TYP

2X R.016

2.250+ .000 .060

.171

R.150 TYP

5X R6.034 R5.622

10X .081

9X .140 2X .090

2X .084

2X R.150

2X .100 (MEASURED AT

NOMINAL TRIM LINE)

6X 2.140

11x 10.3°

6X 2.200

.122 5X .117

14.500+ .200 .000

.030

14.250, NOMINAL TRIMLINE

LOCATION, SEE NEXT ASSEMBLY

A

+NOTE 7

- 0.000

REF: INTERMEDIATE PANEL TO CENTER

PANEL JOINT NEXT ASSY

INBDOUTBD

REF: INTERMEDIATE PANEL TO SIDE PANEL

JOINT NEXT ASSY

7X .060

4X R.075

2X R.179

2.050

2X 45.0°

2X 35.0°

2X R.016 2X R.032

2X R.016

2X .100±.007

1.582

2X .234 .319

.324

2X .238

2X .075

2X .184

DETAIL A

SCALE 2 : 1

UP

2.25 X 14.7 X 114, 6005A-T61, ASTM B221-14 6

120199342798752INTERMEDIATE 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

201993427

INTERMEDIATE PANEL

EXTRUSION-PALLET,

AIRBORNE CARGO

.005

.01

20199342798752

1/1 1 OF 1

1°

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

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

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

C6

201993426 HCU-6A/E

FIND

NO.

FIND

NO.

FIND

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

K. BRANTLEY

PROJECT ENGINEER

REV STATUS

OF SHEETS

REV

SH DESCRIPTIONREV

REVISION HISTORY

DATE APPROVEDNOTES:

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 114 INCHES WITH SQUARE ENDS UNLESS A DIFFERENT DIMENSION IS REQUESTED

BY THE FRICTION STIR WELD/ASSEMBLY CONTRACTOR.

5. 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 201993426 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.

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

7. MAXIMUM WEIGHT NOT TO EXCEED 4.50 LBS/FT UNLESS APPROVED BY MANUFACTURER OF PALLET.

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

9. THIS DRAWING (201993427.SLDDRW) IS BASED ON A 3D MODEL (INTERMEDIATE PANEL EXTRUSION (201993427.SLDPRT)).

M. HORAN

4/11/2019

4/12/2019

2.250+ .000 .060

5X .076 .100 4X R.016

4X R.075

4X 45°

.131

2X .087

R5.122

.090

R.150 TYP

R.150 TYP

5X 10.3°

2X .090

R4.902

2X .090

2X .093 2X .101 2X .101 2X .100

R4.802 R4.182 R4.182 R3.395

2X .090 2X .090 2X .090 2X .089 6X 12.8°

14.500+ .000 .060

6X 2.140

2X .100 (MEASURED AT

NOMINAL TRIM LINE)

6X 2.200

.030

.132 .137 .141 .157 .157 .167

14.000, NOMINAL TRIM LINE

LOCATION, SEE NEXT ASSEMBLY

A

8X .060

REF: APPROX PALLET

CENTER NEXT ASSY

R.150 4X .100±.007

4X 35.0°

4X R.179

2.050

4X R.032

4X R.016

4X R.075

1.579

2X .236 2X .347

2X .184

1.300

2X .209

2X .105

DETATIL A

SCALE 2 : 1

UP

INBDOUTBD

REF: CENTER PANEL TO CENTER

PANEL (MACHINED) JOINT NEXT ASSYREF: CENTER PANEL TO INTERMEDIATE

PANEL JOINT NEXT ASSY

+NOTE 7

- 0.010

2.25 X 14.9 X 114, 6005A-T61, ASTM B221-14 6 120199342898752CENTER 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

201993428

CENTER PANEL EXTRUSION-

PALLET,

AIRBORNE CARGO

PROJECT ENGINEER

.005

.01

20199342898752

1/1 1 OF 1

K. BRANTLEY1°

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

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

TITLE

D

DWG NO.

SHEETWEIGHT

CAGE CODESIZE

SCALE

CHECKER

AF RELEASE

CONTRACT NO.

ENGINEERING APPROVAL

DATEDRAFTER

ANGLESDECIMALSFRACTIONS

DIMENSIONS ARE IN INCHES -TOLERANCES ON:

UNLESS OTHERWISE SPECIFIED

FINISH

TREATMENT

C6

201993426 HCU-6A/E

FIND

NO.

FIND

NO.

FIND

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

AF AUTHENTICATION

REV STATUS

OF SHEETS

REV

SH DESCRIPTIONREV

REVISION HISTORY

DATE APPROVED

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 114 INCHES WITH SQUARE ENDS UNLESS A DIFFERENT DIMENSION IS

REQUESTED BY THE FRICTION STIR WELD/ASSEMBLY CONTRACTOR.

5. 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 201993426 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.

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

7. MAXIMUM WEIGHT NOT TO EXCEED 5.20 LBS/FT UNLESS APPROVED BY MANUFACTURER OF PALLET.

8. SURFACE MUST BE 0.007 OF SHELF HEIGHT.

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

10. THIS DRAWING (201993428.SLDDRW) IS BASED ON A 3D MODEL (CENTER PANEL EXTRUSION (201993428.SLDPRT)).

M. HORAN

4/11/2019

4X .100 .076

2X .100±.007 (MEASURED AT

NOMINAL TRIM LINE)

6X 10.3°

2X .101 2X .081

3X R5.252 R4.182 R6.042

8X .090 2X .140

R.150 TYP

R.150 TYP

5X .065

6X .091

2.123 4X 2.135

2X 12.8° 2X 10.3°

2.250+ .000 .060

2.200 TYP

3X .135 .157 .117

15.750+ .200 .000

15.500 NOMINAL TRIMLINE

LOCATION, SEE NEXT ASSEMBLY

A

+NOTE 6

- 0.000

OUTBD

UP

INBD

REF: SIDE PANEL TO INTERMEDIATE PANEL

JOINT NEXT ASSY

R.150 3°

R.118

R.125

37°

R.125

R.367

R.625

R.563 4X R.075

2°

.125 R.134

R.150

4X R.075

.188

R.125

.875±.018

17° R.187 18°

.175 R.125

.250±.038

1.830±.024

.090

1° .100

.265

.291

.453 .276

.195

.147

83°

.302

1.116

1.713

.435

.503

.045

3.500

DETAIL A

SCALE 2 : 1

2.25 X 15.75 X 114, 6005A-T61, ASTM B221-14 5 120199342998752SIDE 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

201993429

SIDE PANEL EXTRUSION-

PALLET,

AIRBORNE CARGO

PROJECT ENGINEER

X

.005

.01

20199342998752

1/1 1 OF 1X

X

X

4/12/2019

X

4/11/2019

X

X

X

M. HORAN

X

K. BRANTLEY1°

AFMC Form 1655, 20150330

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

SH

REV

OF SHEETS

REV STATUS

201993426 HCU-6A/E

C6

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 114 INCHES WITH SQUARE ENDS UNLESS A DIFFERENT DIMENSION IS

REQUESTED BY THE FRICTION STIR WELD/ASSEMBLY CONTRACTOR.

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

6. MAXIMUM WEIGHT NOT TO EXCEED 5.85 LBS/FT UNLESS APPROVED BY MANUFACTURER OF PALLET.

7. UNLESS OTHERWISE NOTED ALL THICKNESS TOLERANCES SHALL BE (+NOTE 6/- 0.010).

8. THIS DRAWING (201993429.SLDDRW) IS BASED ON A 3D MODEL (SIDE PANEL EXTRUSION (201993429.SLDPRT)).

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°

2.250+ .000 .060 .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

2X .264

2X .241

.561

.095

3°

1.712

.136

.488

.128 .201

.199

.594 .397

1.210 .323

1.250

+NOTE 6

- 0.035

UP

+NOTE 6

- 0.013

+NOTE 6

- 0.005

2.25 x 3.9 x 92, 6005A-T61, ASTM B221-14 5 120199343098752EDGE 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

201993430

EDGE RAIL EXTRUSION-

PALLET,

AIRBORNE CARGO

PROJECT ENGINEER

.005

.01

20199343098752

2/1 1 OF 1

4/11/2019K. BRANTLEY1°

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 AUTHENTICATION

CONTRACT NO.

ENGINEERING APPROVAL

DATEDRAFTER

ANGLESDECIMALSFRACTIONS

DIMENSIONS ARE IN INCHES -TOLERANCES ON:

UNLESS OTHERWISE SPECIFIED

FINISH

TREATMENT

SHEET

REV STATUS

OF SHEETS

B4

201993426 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. AS AN ALTERNATE, 6061-T61, ASTM B221-14, MAY BE USED.

6. MAXIMUM WEIGHT NOT TO EXCEED 2.1 LBS/FT UNLESS APPROVED BY MANUFACTURER OF PALLET.

7. UNLESS OTHERWISE NOTED ALL THICKNESS TOLERANCES SHALL BE (+NOTE 6/-0.010).

8. THIS DRAWING (201993430.SLDDRW) IS BASED ON A 3D MODEL (EDGE RAIL EXTRUSION (201993430).SLDPRT)).

M. HORAN

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

AF RELEASE

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°

8 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 8

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

20199343298752ASSEMBLY

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

201993432

PROJECT ENGINEER

.010

.04

20199343298752

2/1 1 OF 1

4/11/2019K. BRANTLEY1°

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

201993426 HCU-6A/E

SEE NOTE 9.

1B4201993432-0198752

RING

2C4AMS-SAE6370/STL 4130201993432-02987521 BRACKET, FORGING

AMS-SAE6345/STL SHEET 4130

M. HORAN

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

0.093

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

9. HEAT TREAT ASSEMBLY TO 160,000-180,000 PSI PER SAE-AMS-H-6875. 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.

10. 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.

11. THIS DRAWING (201993432.SLDDRW) IS BASED ON A 3D MODEL (TIE-DOWN RING

ASSEMBLY (201993432).SLDASM).

4/12/2019

+_ TIE-DOWN RING ASSEMBLY -

PALLET,

AIRBORNE CARGO

SEE NOTE 10.