imageidx-20230221085103.pdf
PDF 24 MB Posted
- 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.
View the file
On GovTribe
Work with this file on GovTribe
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
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 .