imageidx-20230221085103.pdf

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Attached to
SHIPPING AND STORAG Federal contract opportunity
Solicitation number
SPRPA123RKJ24
Issued by
Defense Logistics Agency Aviation

About this file

This solicitation is for the procurement of shipping containers and related storage services. The Defense Logistics Agency Aviation seeks to acquire one sample unit for first article testing within 120 calendar days of award, with additional units to be delivered within 180 days for testing and evaluation at specified Navy facilities. Offerors must provide certifications of previous production experience or be prepared to undergo first article testing at an estimated cost of $15,000. The solicitation sets aside this requirement for small businesses and requires subcontracting plans. Packaging must meet MIL-STD-2073 standards.

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Text version

FCL

01/11/99

D REDRAWN & ADDED -2 01/02/02 DPB/FCL

ZONE REV DESCRIPTION

REVISIONS

DATE APPROVED

ARE IN INCHES

SPECIFIED DIMS

UNLESS OTHERWISE

USED ON

APPLICATION

NEXT ASSEMBLY

REVSIZE

DATE

DATE

DATE

DATEAPPROVED BY

GOV'T APVD BY

CHECKED BY

DRAWN BY

DATE:

CONTRACT NUMBER

SHEET:WEIGHT:SCALE:

CAGE CODE DWG NO.

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

B 05259

TOLERANCES ON:

.01 - .03RBREAK EDGES:

-.001 +.007

±.010 ±.015

HOLE SIZES:

BEND R .00 TO .09:

.091 AND ABOVE:

FRACTIONS: 1/16

ANGLES: 1°

DECIMALS:

.XX

.XXX

.X ±

.1

.06

.015

"DISTRIBUTION STATEMENT A

APPROVED FOR PUBLIC RELEASE; DISTRIBUTION IS UNLIMITED"

FCL

JNB

STD-147 D

LOCATING PIN

CAGE

CODE

QTY

REQ'D

PART NO.

IDENTIFY NUMBER

DATA: SPECIFICATION

NOTES, VENDORSNO.

ITEM

LENGTH

OD/ID

WIDTH

GAUGE

THICK

MATERIAL

NOMENCLATURE

OR DESCRIPTION

PARTS LIST

CAD MAINTAINED, CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

SEE NOTES 1 & 22.0.50 DIAASTM A108LOCATING PINSTD-147-11

SEE NOTE 12.0.50 DIA304 SSLOCATING PINSTD-147-22

.43

.382X

1.00

FLAT SURFACE

2 SIDES

.25

2.00

.375-16 UNC-2A

.50O STK

15°

NOTES:

1. RECOMMENDED HARDWARE TO BE ONE (1)

.38 PLAIN WASHER & ONE (1) .375-16 NUT-FLEXLOC.

2. CAD PLATE PER AMS-QQ-P-416, TYPE II, CLASS .

MIN. THREAD RELIEF REQUIRED

8 7

A

B

C

D

APPROVED FOR PUBLIC RELEASE; DISTRIBUTION IS UNLIMITED"

"DISTRIBUTION STATEMENT A

CAD MAINTAINED, CHANGES SHALL BE

INCORPORATED BY THE DESIGN ACTIVITY.

ADHESIVE, ARMSTRONG CORK CO.

ITEM 6 WAS #D-218

JBS

KA1

3M

SEE NOTES 2&8

SEE NOTES 2&8

SEE NOTE 8

SEE NOTE 1

AL 5052-H38

AL 5052-H38

NEOPRENE/MIL-PRF-6855

REQUEST

UPDATED PER CUSTOMER

FCL

JA2

H

ADDED NOTE 2. 4

FCLB2

D4 .12D FOR LANYARD USE FCL

CORRECTED LOCATION OF

G

.25

.25

.12 DIA THRU

.25

.25

2.86

(1.46)

12.68

11.74

1.46 2.86

11.740

12.68

2.13 2.70

10.68

10.50

.XXX±.030

.XX ± .06

FCL

FCL

JNB

AVDEL CORP.

CARR LANE

CARR LANE

CAMLOC

CAMLOC

CAMLOC

CAMLOC

8.00.06 D

11.12 12.68 12.03 15.50

2.86 2.86 10.50 14.53

.187

.125

.090

.090

SS

AL 6061-T6

19738 99862 99862

71286 71286 71286 71286 76381

RIVET1693-0410

FERRULECL-4-F

LANYARDCL-2-C

RET. RINGR4T102

GROMMET40G1-1192

RECEPTACLE244-16B-R82

STUD4002-14-W72

ADHESIVE13576AR

GASKETSTD-225-551

PLATESTD-225-441

BRACKETSTD-225-331

HOUSINGSTD-225-221

ASSEMBLYSTD-225-11

.38 R. TYP

.09

2 PL

.09

.62±.01

.12 .187

4 PLS

.132

.138

DIA THRU.50

1.15

1.00±.01

12.12

7 8 9 10

12.03

.78 TYP

.47

SCALE 2/1

SECTION A-A

.010 REF

.625 REF

32 PL

.09

A

A

+.010

-.000

.625 DIA X 140° CSK, TYP

.625 DIA X .010 DP C'BORE

.500 DIA THRU .12 DIA THRU

.47

ZONE LTR DESCRIPTION DATE APPROVED

REVISIONS

6 5 4 3 2 1

D

C

B

A

123456

CONTAINER RESEARCH

GLEN RIDDLE,PENNSLYVANIA

CORPORATION

CONTAINER RESEARCH

D

CODE IDENT NO.

PARTS LIST

SIZEMATERIAL

GUAGE OD/ID

THICK WIDTH

ZONE

NOTES,VENDOR

DATA:SPECIFICATIONLG

DRAWING NO.SIZE

SCALE:

CONTRACT NO.

DATE

DR BY

CHK BY

APPD

APPD

APPD

FRACTIONS DECIMALS ANGLES

TOLERANCES ON:

DIMENSIONS ARE IN INCHES

UNLESS OTHERWISE SPECIFIED

APPLICATION

NEXT ASS'Y USED ON

MATERIAL

OR DESCRIPTION

NOMENCLATURE

IDENTIFYING NUMBER

PART OR

IDENT

CODE

FIND NO.

ITEM OR

REQ'D

QTY

WT. SHEET

LOG COMPARTMENT

(ALUM FLAT)

STD-225 K

1/2

01/11/99

05259

2X

2X

2 PLS

4 PLS

2 PLS

2 PLS

2 PLS

ROTATED 90 CWv

TO ASTM B-209.

BOTH ALUMINUM ALLOYS 6061-T6 & 5052-H38 SHALL CONFORM8.

ALTERNATE MATERIAL: 6061-T6 CONFORMING TO ASTM B-209.2.

APPLY ITEM 5 TO ITEM 4 WITH ITEM 6.1.

3. WELDING

WELDING AND WELD INSPECTION SHALL BE IN ACCORDANCE

WITH MIL-W-22248, CLASS 4, EXCEPT THAT:

(1) VISUAL INSPECTION SHALL INCLUDE 5X (5 POWER)

MAGNIFICATION WHEN A SUSPECT CONDITION IS TO BE

EXAMINED BEYOND THE CAPABILITY OF NORMAL VISION.

(2) CRITICAL AND MAJOR WELDS MAY BE SUBJECTED TO

FURTHER NON-DESTRUCTIVE TESTING (SUCH AS DYE

PENETRANT INSPECTION) AS PRESCRIBED BY THE BUYING

ACTIVITY.

PROPER CONTROLS SHALL BE USED TO PREVENT MELT THROUGH

OR BURN THROUGH. WELDER QUALIFICATION SHALL BE TO

AWS D17.1. FILLER FOR WELDING 6061 ALLOY SHALL BE

4043. FILLER FOR WELDING 5052 ALLOY SHALL BE 5356.

4. CLEANING

PARTS TO BE WELDED SHALL BE CHEMICALLY CLEANED TO

REMOVE SURFACE SOILS SUCH AS OILS, WAXES, GREASE, INKS,

ETC, PER MIL-DTL-5541, EXCEPT THAT UNINHIBITED ALKALINE SOLUTIONS

SHALL NOT BE USED.

5. DEOXIDIZING

THE CLEANED PARTS SHALL BE CHEMICALLY DEOXIDIZED NO

MORE THEN 10 DAYS PRIOR TO WELDING TO REMOVE THICK

SURFACE OXIDE FILMS. (IF THE MATERIAL OR WORK IS EXPOSED

TO AN OUTDOOR ENVIRONMENT, THIS TIME LIMIT SHALL BE

REDUCED TO A MAXIMUM OF 3 DAYS, TO ACCOUNT FOR

ATMOSPHERIC EFFECTS). MECHANICAL CLEANING METHODS SHALL

BE APPLIED JUST PRIOR TO THE ACTUAL START OF WELDING,

TO REMOVE ANY REOXIDATION OR RESIDUAL THIN OXIDE FILMS.

6. CHEMICAL TREATMENT

AN ACID DEOXIDIZING TREATMENT SHALL BE APPLIED BY EITHER

IMMERSION OR BRUSHING/WIPING. DEOXIDIZERS ACCEPTABLE FOR

USE SHALL INCLUDE NITRIC ACID, SULFURIC CHROMIC, PHOSPHORIC

CHROMIC, OR EQUIVALENT SOLUTIONS. SODIUM HYDROXIDE SOLUTIONS

SHALL NOT BE USED. CARE SHALL BE TAKEN TO ASSURE 100

SOLUTION COVERAGE OF THE AREA TO BE WELDED. TO ALLOW

AN ADEQUATELY SIZED DEOXIDIZED AREA FOR GOOD WELDING,

THE SOLUTION SHALL BE APPLIED TO AN AREA EXTENDING AT

LEAST 2 INCHES FROM THE WELD SITE, OR ENDING AT ANY

CLOSER ADJACENT EDGE.

7. MECHANICAL MEANS

IMMEDIATELY PRIOR TO WELDING, MECHANICAL CLEANING METHODS

SHALL BE APPLIED TO THE WELD AREAS PREVIOUSLY CHEMICALLY

TREATED TO ASSURE REMOVAL OF RESIDUAL OR REFORMED OXIDES,

IF ANY. ACCEPTABLE METHODS OF MECHANICAL CLEANING INCLUDE

STAINLESS STEEL WIRE BRUSHING, SCRAPING, FILING, OR SANDING.

HOWEVER, ABRASIVES CONTAINING IRON AND ITS OXIDES, STEEL

WOOL AND WIRE, AND COPPER ALLOY BASE WIRE, WHICH MAY

BECOME EMBEDDED WITH GALVANICALLY ACTIVE METALS AND

ACCELERATE CORROSION OF ALUMINUM ALLOYS, SHALL NOT BE

USED. MECHANICAL METHODS SHALL BE VIGOROUS ENOUGH TO

ADEQUATELY REMOVE ANY RESIDUAL OXIDE FILMS, BUT GENTLE

ENOUGH TO AVOID FORMING AN EXCESSIVELY ROUGH SURFACE IN

THE COMPARATIVELY SOFT METAL UNDERNEATH.

NOTES:

H

NAME PLATE

BRACKET

04/07/97

STD-265

5.124.00 SEE NOTE 2ALUM 5052-H38NAME PLATE BRACKETSTD-265-1

FSCM

NO.

QTY

REQ'D

PART NO.

IDENTIFY NUMBER

DATA: SPECIFICTION

NOTES, VENDORSNO.

ITEM

LENGTH

OD/ID

WIDTH

GAUGE

THICK

MATERIAL

NOMENCLATURE

OR DESCRIPTION

PARTS LIST

H REDRAWN ON SOLID EDGE 02/01/00

ZONE REV DESCRIPTION

REVISIONS

DATE APPROVED

CAD MAINTAINED, CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

ARE IN INCHES

SPECIFIED DIMS

UNLESS OTHERWISE

USED ON

APPLICATION

NEXT ASSEMBLY

REVSIZE

DATE

DATE

DATE

DATEAPPROVED BY

GOV'T APVD BY

CHECKED BY

DRAWN BY

DATE:

CONTRACT NUMBER

SHEET:WEIGHT:SCALE:

FSCM NO. DWG NO.

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

C 05259

TOLERANCES ON:

.01 - .03RBREAK EDGES:

-.001 +.007

±.010 ±.015

HOLE SIZES:

BEND R .00 TO .09:

.091 AND ABOVE:

FRACTIONS: 1/16

.X

ANGLES: 2°

DECIMALS:

.XX

.XXX

.1

.06

.015

APPROVED FOR PUBLIC RELEASE; DISTRIBUTION IS UNLIMITED"

"DISTRIBUTION STATEMENT A

A

B

C

D D

C

A

4 3 2 1

4 3 2 1

A

B

2 5.124.00.063 SEE NOTE 2ALUM 6061-T6NAME PLATE BRACKETSTD-265-2

.063

4.50

4.00

.502X

R .252X

.06 STK

NOTES:

1. CENTER NAME PLATE ON BRACKET.

LINE DRILL HOLES USING ∅.1285 (#30) DRILL.

2. BOTH ALUMINUM ALLOYS 6061-T6 AND

5052-H38 SHALL CONFORM TO ASTM B209.

SEE NOTE 1

O .1284X THRU

SEE NOTE 1

1 OF 11/1

IDENTIFY NUMBER

PART NO.QTY

REQ'D NO.

ITEM CODE

IDENT OR DESCRIPTION

NOMENCLATURE

MATERIAL

GAUGE

THICK

OD/ID

WIDTH

LENGTH

NOTES, VENDORS

DATA: SPECIFICATION

PARTS LIST

C 1. REDRAWN IN SOLID EDGE GC8/8/07

DATEDESCRIPTIONREVZONE APPROVED

REVISIONS

D

1345678

12345678

A

B

C

D

C

B

A

DATE:

DRAWN BY

CHECKED BY

APPROVED BY

GOV'T APVD BY DATE

DATE

DATE

DATE

CONTRACT NUMBER

WEIGHT:SCALE:

SIZE

D

CODE IDENT NO.

05259

DWG NO. REV

SHEET:

GLEN RIDDLE, PENNSYLVANIACORPORATION

CONTAINER RESEARCH

SPECIFIED DIMENSIONS

UNLESS OTHERWISE

ARE IN INCHES

NEXT ASSEMBLY USED ON

APPLICATION .01-.03R

±.015

±.010

- .001 +.007

.091 AND ABOVE:

BEND RADII .00 TO .09:

HOLE SIZES:

BREAK EDGES:

TOLERANCES ON:

1/16

2°

.X

.XX

.XXX

± .015

.06

.1

FRACTIONS:

ANGLES:

DECIMALS:

GC 06/10

DPB

8/11/2010

SEALING FLANGE

13D097 C

EXTRUSIONS

8/11/2010

06/10

DETAIL A

15°2X

3.53

2.03

.25 +.00 -.01

5.94

R .13 R .50

R .09

R .09

.33

2.31

.31

1.21

.66

.63 +.01 -.00

.12

.19

45°

.25

4.20

5.73 6.11

7.43

R .132X

.35

1.78

.49

.38

1.70

R .19

R .25

18°

.3752X

R .096X

.2772X

.833

.394

.89

3.02 3.15 .185

45°

R .38

.25

.60.640

1.46

3.87

4.73

.496

FULL RADIUS

1.13

1.442

2.38

30° 15°R .281

.120

.140

.120

.3302X

30°2X

.38

FULL RADIUS 2X

.23

.26 +.015 -.000

.38

.75

1.37

.19

.18

.16

.76

.07

.38

.13

1.27

R .31

.80 1.19

1.73

.92 4.21

1.25

.42

2.35

2.75

20°

.31

.31

3.30

5.50

.12

.20

.40 1.30

1.01

30°

.20

1.08

R .05

R .12

15°

R .12

.62 +.000 -.015

.20

R 2.67

.70

55°

R .125

R .50

.75

20°

14.12

FULL RADIUS

ALL EDGES AND CORNERS TO BE BROKEN BY

A .01 RADIUS, UNLESS OTHERWISE SPECIFIED

.13 X 45v CHAMFER

.13 X 45v CHAMFER

ALL EDGES AND CORNERS TO BE BROKEN BY

A .03 RADIUS, UNLESS OTHERWISE SPECIFIED

1 1 13D097-1 COVER EXTRUSION AL 6061-T6 2.86 LBS/FT; ASTM-B241

1 2 13D097-2 BASE EXTRUSION AL 6061-T6 6.97 LBS/FT ASTM-B241

1 3 13D097-3 MK-45 EXTRUSION AL 6061-T6 3.48 LBS/FT; ASTM-B241

1 4 13D097-4 TEE BASE EXTRUSION AL 6061-T6 2.90 LBS/FT ASTM-B241

CAD MAINTAINED, CHANGES SHALL BE INCORPORATED BY THE DESIGN ACTIVITY.

NOTES:

1. IDENTIFY IN ACCORDANCE WITH MIL-STD-130

2. TOLERANCE PER ANSI H35.2

7°10°

A

7.12

STD-147 05259 D 0001 0001
STD-225 05259 K 0001 0001
STD-245 05259 G 0001 0001
STD-251 05259 D 0001 0001
STD-265 05259 H 0001 0001
STD-295 05259 M 0001 0001
STD-295 05259 M 0002 0001
STD-295 05259 M 0003 0001
STD-295 05259 M 0004 0001
STD-359 05259 E 0001 0001
13C057 05259 J 0001 0001
13C058 05259 U 0001 0001
13C058 05259 U 0002 0001
13C058 05259 U 0003 0001
13C058 05259 U 0004 0001
13D097 05259 C 0001 0001
13D097 05259 C 0001 0000
17D043 05259 AN 0001 0001
17D043 05259 AN 0002 0001
17D058 05259 AA 0001 0001
17D058 05259 AA 0002 0001
17D058 05259 AA 0003 0001
20D004 05259 B 0001 0001
583D006 05259 0001 0001
583D006 80132 1N CN01.1 0001
583D006 80132 1N CN01.2 0001
583C010 05259 0001 0001
583C010 05259 0002 0001

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