Attachment_7_HEDS_Dome_Scaffolding_Machine_Drawings.pdf
PDF 7 MB Posted
- Attached to
- HEDS Dome Scaffolding Federal contract opportunity
- Solicitation number
- FA8224-16-R-0058
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Attachment 7 - HEDS Dome Scaffolding Machine Drawings
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| FA8224-16-R-0058-0002_2nd_PoP_Extension.pdf | ||
| FA8224-16-R-0058-0001_PoP_Extension.pdf | ||
| Attachment_6_Scaffold_Equipment_Delivery_List.xlsx | XLSX spreadsheet | |
| Attachment_3_HEDS_Dome_Scaffold_Model_File_Locations.pdf | ||
| FA8224-16-R-0058.pdf | ||
| Attachment_5_Fans.pdf | ||
| Attachment_8_-_GFP_Equipment.pdf | ||
| Attachment_4_HEDS_Dome_Scaffolding_Images.pdf | ||
| HEDS_Scaffolding_PWS_12_Apr_16.docx | DOCX document | |
| CDRLs.pdf |
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Text version
Attachment 4 HEDS Dome Scaffolding Machine Drawings
Note: This file contains machine drawings generated from the SolidWorks model of the scaffolding for parts that require machining. Most parts do not require machining they are simply extruded aluminum cut to length. These have names that match the parts names referenced from the parts list.
3.000
0.750
2.289 1.997
0.919 1.419
1.822
0.585
0.915
0.330
35.907°
0.655 2.155
2.810
0.750
2.250
3.000
0.330 THRU
X4
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 1 MIRROR BRACKET
DOME SCAFFOLD
1:1.25 1OF 1
7 CLASSIFICATION UNCLASSIFIED
APRIL 30, 2012
1.405 .705
.330 THRU
3.000
.920
2.420
1.405
.700
3.000
.750
2.250
.330 THRU
(2 X)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
ANGLE BRACKET 1 POINT 4
INCHES LONG 1 SLOT
DOME SCAFFOLD
1:1.25 1OF 1
SEPTEMBER 27, 2010
2.810
.660 2.150
.330 THRU .330 THRU1.500
.725
1.085
2.810
.660 2.150
3.000
.750
2.000
.330 THRU
(4 X)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
ANGLE BRACKET 2 POINT 81
INCHES LONG TWO SLOTS
DOME SCAFFOLD
1:1 1OF 1
SEPTEMBER 27, 2010
2.810
.350
.750
2.250
2.650
.330 THRU
.330 THRU
3.000
.750
2.250
2.810
.350 2.650
.330 THRU
.330 THRU
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
ANGLE BRACKET 2 POINT
81 INCHES LONG 4 SLOTS
DOME SCAFFOLD
1:1.5 1OF 1
SEPTEMBER 24, 2010
.750
2.250
.330 THRU
.330 THRU
4.300
.350 3.950
3.000
.750
2.250
4.300
.350 3.950
.330 THRU
.330 THRU
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
ANGLE BRACKET 4 POINT 3
INCHES LONG 4 SLOTS
DOME SCAFFOLD
1:1.75 1OF 1
.500 2.750
2.650
3.580
.750 .750
2.038
4.086
1.500
4.232
4.852
.982
4.250
1.168
65.59°
R.500 65.59°
1.500
122.79°
122.79°
4.8834 x .328 .250
*3.000
*3.000
.25
BLACK ANODIZE
NOTES:
*INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
(21/64" DRILL)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 1 BRACKET 1
DOME SCAFFOLD
1:2 1OF 1
SEPTEMBER 1, 2010
1.500
.750 .750
1.645 3.467
.500
2.500
3.890
4.716
114.41°
114.41°
R.500 3.612
4.232
1.500
4 x .328 .250
*3.000
*3.000
.250
BLACK ANODIZE
NOTES:
* INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
(21/64" DRILL)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 1 BRACKET 2
DOME SCAFFOLD
1:2 1OF 1
0.747
1.653
3.736 4.035
4.407
104.335°
104.335°
R0.300
1.500
4.346
3.816
2.650 0.500
4 x 0.313 THRU ALL
4.165
5.196
0.250
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 1 MIRRORS R2 BRACKET 5
DOME SCAFFOLD
1:1.5 1OF 1
MARCH 20, 2012
3.527
6.279
0.500 2.500
3.940 5.421
1.500
3.378
0.750 1.288
2.477
4 x 0.313 THRU ALL
141.252°
141.252°
0.250
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 1 MIRRORS R2 BRACKET 5
DOME SCAFFOLD
1:1.5 1OF 1
MARCH 20, 2012
.750 .750.500
1.500
1.543
2.749
.622
2.789 3.119
105.29°
R.500
2.500
1.025
1.500
2.500
3.429 3.034
142.65°
142.65°
4 x .328 THRU ALL
*2.000
*2.000
.250
BLACK ANODIZE
(21/64" DRILL)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 2 BRACKET 1
DOME SCAFFOLD
1:1.5 1OF 1
SEPTEMBER 2, 2010
1.939
3.627
.9311.171
3.500
3.500
1.500
R.500
127.36°
127.36°
74.71°
4.307
3.912
.500 2.250
3.158
2.696
4 x .328 .250
*2.500
*2.500
.250
BLACK ANODIZE
(21/64" DRILL)
NOTES:
* INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 2 BRACKET 2
DOME SCAFFOLD
1:1.5 1OF 1
1.418
3.011
.425
3.157
3.777
.500 2.000
3.286 4.009
R.500 114.41°
147.21°
147.21°
1.500
3.000
.784
4 x .328 THRU ALL 3.000
*2.500
*2.500
.250
BLACK ANDODIZE
(21/64" DRILL)
NOTES:
* INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 3 BRACKET 1
DOME SCAFFOLD
1:1.5 1OF 1
.500 2.500
1.582
3.176
3.786
3.063
4.250
4.882
2.173
3.539
.982
3.321
3.941
1.168
65.59°
R.500
122.80°
122.80°
3.250
4 x .328 .250
*3.000
*2.000
.250
BLACK ANODIZE
(21/64" DRILL)
NOTES:
* INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 3 BRACKET 2
DOME SCAFFOLD
1:1.5 1OF 1
1.176
2.528
.626
115.63°
3.303
2.654
1.500
2.
1.175147.82°
147.82°
R.500
3.250 4.244
5.218
.500 2.250
3.676
4.325
4 x .328 THRU ALL
3.000
2.
(21/64" DRILL)
.250
BLACK ANODIZE
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 4 BRACKET 1
DOME SCAFFOLD
1:1.5 1OF 1
SEPTEMBER 3, 2010
1.824
3.177
1.022
3.9523.303
.500 2.500
4.250
3.676 3.027
4.893
3.487
R.500 64.37°
1.207122.19°
122.19°
3.250
4 x .33 THRU ALL
2.13
*3.000
*2.000
.250
BLACK ANODIZE
(21/64" DRILL)
NOTES:
* DENOTES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 4 BRACKET 2
DOME SCAFFOLD
1:1.5 1OF 1
SEPTEMBER 3, 2010
1.214
2.601
2.778 3.349
.466
3.500
2.500
.838
1.500
112.39°
R.500
146.20°
146.20°
4.196
5.149 4 x .328 THRU ALL
3.693
4.265
.500 2.500
*3.000
*2.000
.250
BLACK ANODIZE
(21/64" DRILL)
NOTES:
* INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGED .01"2.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 5 MIRROR 1 BRACKET 1
DOME SCAFFOLD
1:1.5 1OF 1
SEPTEMBER 7, 2010
1.555
3.173
1.147
3.349
3.921
.500 2.500
1.500
1.380
3.000
4.000
3.789
3.122
67.61° R.500
123.81°
123.81°
4 x .328 THRU ALL 4.768
*3.000
*2.000
.250
BLACK ANODIZE
(21/64" DRILL)
NOTES:
* DENOTES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 5 MIRROR 1 BRACKET 2
DOME SCAFFOLD
1:1.5 1OF 1
1.437
.684
3.048
3.215 3.801
.500 2.250
3.788
4.472
2.750
1.500
3.250
4.283 5.358
3.977
113°
R.500
146.50°
146.50°
1.24
4 x .328 THRU ALL
*3.000
*2.500
.250
BLACK ANODIZE
(21/64" DRILL)
NOTES:
* INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2. 1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 5 MIRROR 2 BRACKET 1
DOME SCAFFOLD
1:1.5 1OF 1
4.000
.750 1.166
1.793
3.634
3.801
4.387
.500 2.500
3.690
2.909
2.023
4.771
3.404
4 x .328 THRU ALL
.250
BLACK ANODIZE
(21/64" DRILL)
NOTES:
* INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2. 1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 5 MIRROR 2 BRACKET 2
DOME SCAFFOLD
1:1.5 1OF 1
1.4312
4.6073
3.5214
1.9949
4 x 0.2010 THRU ALL
1/4-20 UNC THRU ALL
4.2188
0.9368
1.0256
2.6889
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BAND 2 MIRROR JOINING PLATE
DOME SCAFFOLD
1:1.5 1OF 1
MARCH 12, 2012
2.000 - .000 +.005
A
A
1.098
1.654
2.211
2.718
.325
25.67°
.503 1.660
2.818
1.276 25.67°
R.500
3.325
.531 .313 3 x .323 THRUB
B
(3X NEARSIDE, 3X FARSIDE)
BLACK ANODIZE
.531 2.413 4 x .323 THRU ALL
.750
1.500
1.500
.750
2.042
25.67°
.750
.600*
SECTION A-A
.050 45° X
SECTION B-B
(2 PLACES)
NOTES:
*INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CENTER BRACKET ANGLE 1
DOME SCAFFOLD
VAR 1OF 1
AUGUST 31, 2010
89.41° ±.25°
.050 45° X
(4X .388)
1.250 2X .749 - .005
+.000
1.999 - .005 +.000.501
3.000
1.281
.5 9°
A A
(2 PLACES)
5/16-18 UNC .630
3 x .257 .800
.380
.3801.2841.284
BLACK ANODIZE
3.330
5/16-18 UNC .630
3 x .257 .800
.380
.380 1.284 1.284
.531 .913 4 x .323 THRU ALL
.880
1.500
.795 1.500
SECTION A-A
NOTES:
TAP DRILL ON 5/16-18 TAPPED HOLES CAN BE THRU ALL.1.
BREAK ALL SHARP EDGES .01"2.
IF ANGLE (89.41) PRESENTS DIFFICULTY, PLEASE CALL TO DISCUSS.3.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CENTER BRACKET ANGLE 2
DOME SCAFFOLD
VAR 1OF 1
65.000
0.750 32.500
64.247
47.500
0.750
46.750
0.635 X 100°
6 x 0.332 THRU ALL
0.750
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
POWDER COAT BLACK
BLACK
CARBON STEEL
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
BASEPLATE
F16 COCKPIT STAND
1:3.15 1OF 1
MARCH 1, 2011
.700
.100
R.250
1.500
4.500
1.500
7.000
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
FILE LOCATION:
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
JOANN LUU
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= +- 0.15
.XXX= +- 0.005
.XXXX= +- 0.002
FRACTION= +- 1/32
ANGLES= +- 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # NUMBER
COCKPIT STAND
EXTRUSION 1
F16 COCKPIT STAND
1:2 1OF 1
ALUMINUM
BLACK
BLACK ANODIZATION
7.000
R.250
.700
.100
1.050
.750 (4X)
.750
.260 (4X)
5/16" TAP DRILL SIZE F
3.000
3.000
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
FILE LOCATION:
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
JOANN LUU
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= +- 0.15
.XXX= +- 0.005
.XXXX= +- 0.002
FRACTION= +- 1/32
ANGLES= +- 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # NUMBER
COCKPIT STAND
EXTRUSION 2
F16 COCKPIT STAND
1:2 1OF 1
ALUMINUM
1.309
.100
1.500
R.500
4.500
1.500
4.000
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
FILE LOCATION:
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
JOANN LUU
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= +- 0.15
.XXX= +- 0.005
.XXXX= +- 0.002
FRACTION= +- 1/32
ANGLES= +- 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # NUMBER
COCKPIT STAND
EXTRUSION 3
F16 COCKPIT STAND
1:2 1OF 1
ALUMINUM
2.250 2.250
1.189
2.541
.297
1.598
2.057
3.408
4.301
.500
.500
2.500
2.500
4.301 3.000
4.426
3.776
7.004 6.228
5.578
5.703
1.334
R.500
154.302°
167.151°
167.151°
3.000
8 x .328 THRU ALL
*3.000
*3.000.250
BLACK ANODIZE
(21/64" DRILL)
NOTES:
* DENOTES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2. 1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION BRACKET 1
DOME SCAFFOLD
1:1.5 1OF 1
6.521
.750 .750
2.250 2.250
.520 .520
2.480 2.480
.500
.500
1.500 2.831
4.495
2.250 3.774
5.437
8 x .328 THRU ALL
.250
BLACK ANODIZE
NOTES:
1. BREAK ALL SHARP EDGES .01"
(21/64" DRILL)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION BRACKET 4
DOME SCAFFOLD
1:1.5 1OF 1
129.554
1.610
33.610
41.317 46.017
64.027
13.157 27.835
28.260 37.460
38.210
64.798 92.133
91.383 95.983
101.333
101.718 116.433
127.233
.750
1.600
9.500
13.875
24.645
25.555
27.745
23.895
26.995
14 X .34375 THRU ALL
42.555°
1.000
(11/32" DRILL)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION MEZZANINE 1
DOME SCAFFOLD
1:15 1OF 1
NOVEMBER 3, 2010
14 x 0.34375 THRU ALL
66.870
4.600
62.270 61.246
39.500
6.958
34.800
58.620
50.668 49.818
48.318 47.196
37.168
29.661 19.590
18.520 17.018
16.168
51.418
15.4188.250
33.216
43.140
1.600 3.000
0.750
12.145
18.031
27.134
33.986
35.400
40.040
42.390
64.552°
(11/32" DRILL)
1.000
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION MEZZANINE 2
DOME SCAFFOLD
1:10 1OF 1
NOVEMBER 3, 2010
16.250
5/16-18 UNC 0.625
5/16-18 UNC 0.625
5/16-18 UNC 0.625
5/16-18 UNC 0.625
BLACK ANODIZE
NOTES:
1) 6 INCH BY 3 INCH FRACTIONAL EXTRUSION
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 1
DOME SCAFFOLD
1:3 1OF 1
154.511
144.931
A B
51.43°
DETAIL A
SCALE 1 : 3
51.43°
DETAIL B
SCALE 1 : 3
NOTES:
1) 6 INCH BY 3 INCH FRACTIONAL EXTRUSION
NOTES:
1) 6 INCH BY 3 INCH FRACTIONAL EXTRUSION
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 2
DOME SCAFFOLD
1:17 1OF 1
153.475
143.893
A B
51.44°
DETAIL A
SCALE 1 : 3
51.44°
DETAIL B
SCALE 1 : 3
NOTES:
1) 6 INCH BY 3 INCH FRACTIONAL EXTRUSION
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 3
DOME SCAFFOLD
1:17 1OF 1
190.773
188.031C D
77.15°
DETAIL C
SCALE 1 : 3
77.15°
DETAIL D
SCALE 1 : 3
NOTES:
1) 6 INCH BY 3 INCH FRACTIONAL EXTRUSION
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 4
DOME SCAFFOLD
1:17 1OF 1
186.790
184.047C D
77.14°
DETAIL C
SCALE 1 : 3
77.14°
DETAIL D
SCALE 1 : 3
NOTES:
1) 6 BY 3 INCH FRACTIONAL EXTRUSION 1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 5
DOME SCAFFOLD
1:20 1OF 1
28.335
26.889
64.27°
NOTES:
1) 3 BY 3 INCH FRACTIONAL EXTRUSION 1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 6
DOME SCAFFOLD
1:3 1OF 1
20.095
21.539
64.29°
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 7
DOME SCAFFOLD
1:3 1OF 1
115.000
114.311
A
77.06°
DETAIL A
SCALE 1 : 2
B
5/16-18 UNC 0.625
DETAIL B
SCALE 1 : 2
(4 PLACES)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 8
DOME SCAFFOLD
1:13 1OF 1
SEPTEMBER 28, 2010
25.88°
20.000
13.816
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 9
DOME SCAFFOLD
1:2 1OF 1
SEPTEMBER 28, 2010
97.385
96.696
A
B .531 1.587
2 x .323 THRU ALL
.531 1.396 2 x .323 THRU ALL
DETAIL B
SCALE 1 : 2
77.06°
25.88° 25.88°
1.587 1.396
DETAIL A
SCALE 1 : 2
C
.750
2.250
.750
2.250 DETAIL C
SCALE 1 : 2
SEE DETAIL A AND C FOR
MORE INFORMATION
SEE DETAIL A AND C FOR
MORE INFORMATION
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 10
DOME SCAFFOLD
1:10 1OF 1
SEPTEMBER 29, 2010
107.860
107.171
A
77.06°
25.88° 25.88°
1.587 1.396
DETAIL A
SCALE 1 : 2
B
.531 1.587 2 x .323 THRU ALL
.531 1.396 2 x .323 THRU ALL
DETAIL B
SCALE 1 : 2
SEE DETAIL A AND C FOR
MORE INFORMATION
SEE DETAIL A AND C FOR
MORE INFORMATION
C .750
2.250
.750
2.250
DETAIL C
SCALE 1 : 2
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 11
DOME SCAFFOLD
1:10 1OF 1
SEPTEMBER 29, 2010
129.7400
126.8447 A B
64.2400°
DETAIL A
64.2400°
DETAIL B
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 12
DOME SCAFFOLD
1:13 1OF 1
FEBRUARY 1, 2011
75.834
72.939
A B
64.240°
DETAIL A
64.240°
DETAIL B
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
CONSTRUCTION SCAFFOLD
EXTRUSION 13
DOME SCAFFOLD
1:8 1OF 1
FEBRUARY 1, 2011
0.386 THRU ALL
2.998
0.700
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
JOINING PLATE SHOULDER BOLT
DOME SCAFFOLD
1:2 1OF 1
MARCH 1, 2011
.600
1/4-20 UNC THRU
.201 THRU
3.000
.350
.270 1.000
4.020
6.000
5.550
.250
.270
1.100
1.259 1.384
45.00°
.170 THRU
.250
3.770
1.502 - .000 +.002.800
2.636 A
.010
0.05 X 45
45.00°
DETAIL A
SCALE 5 : 1
(2 PLACES)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
NAVITAR BRACKET 2
DOME SCAFFOLD
1:2 1OF 1
OCTOBER 29, 2010
3.776
5.500
6.420
1.250 .469
6.881 6.750
10.000
4.000
11.620
14.120
16.620
8.000
3.509
4.491
11.069
17.171
17.500
5/16-18 UNC THRU ALL
4 x .257 THRU ALL
3 x .266 THRU ALL
2 x .31250 - .0005 +.0000
THRU ALL3/8-24 UNF THRU ALL
.332 THRU ALL
.982
6.102
(PRESS FIT TO DOWEL PIN.
MCMASTER CARR PART
NUMBER 90145A580)
.500
A .250
DETAIL A
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
NAVITAR BRACKET 3
DOME SCAFFOLD
1:3.15 1OF 1
NOVEMBER 2, 2010
.4375 - .0005 +.0000
.7000
.700 .159
.388 THRU
.4375 - .0005 +.0000
.7000
.500
3.000
5.500
.729
.750
.440
1.458 - .002 +.000
45° 45°
.880
* 1.500 - .002 +.000
B
1.458 - .002 +.000
.900 .160
6.000
3.000
.388 THRU
.729
45°
.03 X 45
DETAIL B
SCALE 10 : 1
NOTES:
1) * INDICATES DIMENSION TO THEORETICAL SHARP
(PRESS FIT TO SLEEVE
BEARING. MCMASTER
CARR PART NUMBER
6381K444)
(PRESS FIT TO SLEEVE
BEARING. MCMASTER
CARR PART NUMBER
6381K444)
NOTES:
1) REAM ID OF SLEEVE BEARINGS (MCMASTER CARR PART # 6381K444)
FOR SLIP FIT OF DOWEL PIN (MCMASTER CARR PART #90145A580)
(2 PLACES)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
NAVITAR BRACKET 4
DOME SCAFFOLD
1:1.25 1OF 1
NOVEMBER 1, 2010
BEFORE MACHINE OPERATION
0.
AFTER MACHINE OPERATION
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
PIVOT NUB NO GUIDE
DOME SCAFFOLD
1:1 1OF 1
0.431
3.954 4.014
0.743
1.829 2.026
4 x 0.266 1.000
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
PROJECTOR MOUNT SHIM
DOME SCAFFOLD
1:2 1OF 1
MARCH 12, 2012
2.000 - .000 +.005
A
A
3.000
23.490° 1.091
1.591
2.092
2.592
.299
23.49°
.496 1.647
2.799
3.299
R.500
.531 .313 3 x .323 THRU
1.288
B
B
.750
1.500
1.500
.531 2.213 4 x .323 THRU ALL
.750
BLACK ANODIZE
1.904 23.49°
.750
.600*
SECTION A-A
.050 45.00° X
SECTION B-B
(2 PLACES)
(3X NEARSIDE, 3X FARSIDE)
NOTES:
* INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
RIGHT BRACKET ANGLE 1
DOME SCAFFOLD
VAR 1OF 1
4X .388
1.250 2X .7499 - .0050
+.0000
1.829
3.000
.501 1.999 - .005 +.000
79.08°
.050 45° X
11°
A
A
(2 PLACES) 5/16-18 UNC .625
3 x .257 .792
1.254 1.256 .380
.3
5/16-18 UNC .625
3 x .257 .792
3.270
.380 1.256 1.254
.3
BLACK ANODIZE
.531 1.413 4 x .323 THRU ALL
.905
1.500
.880
1.500
SECTION A-A
NOTES:
TAP DRILL ON 5/16-18 TAPPED HOLES CAN BE THRU ALL.1.
BREAK ALL SHARP EDGES .01"2.
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
RIGHT BRACKET ANGLE 2
DOME SCAFFOLD
VAR 1OF 1
.250
BLACK ANODIZE
3.000
.750
2.250 .500
.500
.750
2.250 2.750
2.750
4.750
5.250
.750
2.250
5.939 6.287
7.636 9.211
5.857 6.981
8.556
154.12°
1.002
1.657
2.421 3.006
3.770
2.461
4.500
3.000
R.500
154.12°
12 x .328 THRU ALL
*5.250
*3.811
NOTES:
* INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
(21/64" DRILL)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
UPRIGHT BRACKET 1
DOME SCAFFOLD
VAR 1OF 1
2.250
.750
2.250
1.031
2.708 3.253
.750
1.904
.750 .750
2.854
4.204
2.250 2.250
3.804
5.154
.500
.500
2.250
2.586 3.681
3.701
4.826
5.481 5.880
6.786
7.440 8.380
8.881
8.744
9.399
10.153 10.880
6.047
R.500
154.12°
11.800
6.721
90°
64.12°
17 x .328 THRU ALL
*2.586
*6.981 .25
BLACK ANODIZE
NOTES:
*INDICATES DIMENSION TO THEORETICAL SHARP1.
BREAK ALL SHARP EDGES .01"2.
(21/64" DRILL)
1 DIMENSIONS
2 MATERIALS
3 COLOR
4 FINISH
5 INSPECTION
6 DESIGNED BY
QUALITY REQUIREMENTS TOLERANCES UOS
INCHES UOS; BEFORE FINISH
BLACK ANODIZATION
BLACK
ALUMINUM 6061
MATT FISHER
THIS DOCUMENT AND DATA ARE ISSUED IN STRICT
CONFIDENCE AND ARE NOT TO BE REPRODUCED
IN WHOLE OR IN PART WITHOUT WRITTEN PERMISSION.
COPYRIGHT UNITED STATES AIR FORCE.
HEDS
519 MXDEC
.XX= 0.15
.XXX= 0.005
.XXXX= 0.002
FRACTION= 1/32
ANGLES= 0.5 deg
INTERPRET PER ASME
Y14.5 M -1994
PART DESCRIPTION:
PROJECT NAME:
SCALE SHEET # DATE:
UPRIGHT BRACKET 2
DOME SCAFFOLD
VAR 1OF 1
| 662026_2_81_4_holes_2_slots_1_angled |
| Sheet1 |
| Drawing View5 |
| Drawing View6 |
| Drawing View7 |
| Drawing View8 |
| angle_bracket_1_point_4_inches_long_1_slot |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Drawing View4 |
| Drawing View5 |
| angle_bracket_2_point_81_inches_long_2_slots |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Drawing View4 |
| Drawing View5 |
| angle_bracket_2_point_81_inches_long_4_slots |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Drawing View4 |
| Drawing View5 |
| angle_bracket_4_point_3_inches_long_4_slots |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Drawing View4 |
| Drawing View5 |
| band_1_bracket_1 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_1_bracket_2 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_1_rev_2_bracket_5 |
| Sheet1 |
| Drawing View3 |
| Drawing View4 |
| Drawing View5 |
| band_1_rev_2_bracket_6 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| band_2_bracket_1 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_2_bracket_2 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_3_bracket_1 |
| Sheet1 |
| Drawing View9 |
| Drawing View10 |
| band_3_bracket_2 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_4_bracket_1 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_4_bracket_2 |
| Sheet1 |
| Drawing View3 |
| Drawing View4 |
| band_5_mirror_1_bracket_1 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_5_mirror_1_bracket_2 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_5_mirror_2_bracket_1 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_5_mirror_2_bracket_2 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| band_two_mirror_joining_plate |
| Sheet1 |
| Drawing View1 |
| center_bracket_angle_1 |
| Sheet1 |
| Drawing View4 |
| Drawing View5 |
| Drawing View7 |
| Drawing View9 |
| Section View A-A |
| Section View B-B |
| center_bracket_angle_2 |
| Sheet1 |
| Drawing View6 |
| Drawing View7 |
| Drawing View8 |
| Drawing View9 |
| Section View A-A |
| cockpit_stand_baseplate |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| cockpit_stand_extrusion_1 |
| Sheet1 |
| Drawing View4 |
| Drawing View5 |
| Drawing View6 |
| Drawing View7 |
| cockpit_stand_extrusion_2 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Drawing View4 |
| cockpit_stand_extrusion_3 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Drawing View4 |
| construction_bracket_1 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| construction_bracket_4 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| construction_mezzanine_1 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| construction_mezzanine_2 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| construction_scaffold_extrusion_1 |
| Sheet1 |
| Drawing View2 |
| Drawing View3 |
| construction_scaffold_extrusion_2 |
| Sheet1 |
| Drawing View1 |
| Detail View A (1 : 3) |
| Detail View B (1 : 3) |
| construction_scaffold_extrusion_3 |
| Sheet1 |
| Drawing View1 |
| Detail View A (1 : 3) |
| Detail View B (1 : 3) |
| construction_scaffold_extrusion_4 |
| Sheet1 |
| Drawing View4 |
| Detail View C (1 : 3) |
| Detail View D (1 : 3) |
| construction_scaffold_extrusion_5 |
| Sheet1 |
| Drawing View4 |
| Detail View C (1 : 3) |
| Detail View D (1 : 3) |
| construction_scaffold_extrusion_6 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| construction_scaffold_extrusion_7 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| construction_scaffold_extrusion_8 |
| Sheet1 |
| Drawing View1 |
| Detail View A (1 : 2) |
| Drawing View5 |
| Detail View B (1 : 2) |
| construction_scaffold_extrusion_9 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| construction_scaffold_extrusion_10 |
| Sheet1 |
| Drawing View1 |
| Drawing View6 |
| Detail View B (1 : 2) |
| Detail View A (1 : 2) |
| Drawing View9 |
| Detail View C (1 : 2) |
| construction_scaffold_extrusion_11 |
| Sheet1 |
| Drawing View1 |
| Detail View A (1 : 2) |
| Drawing View3 |
| Detail View B (1 : 2) |
| Drawing View5 |
| Detail View C (1 : 2) |
| construction_scaffold_extrusion_12 |
| Sheet1 |
| Drawing View2 |
| Detail View A (1 : 1) |
| Detail View B (1 : 1) |
| construction_scaffold_extrusion_13 |
| Sheet1 |
| Drawing View1 |
| Detail View A (1 : 1) |
| Detail View B (1 : 1) |
| joining_plate_shoulder_bolt |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| navitar_bracket_2 |
| Sheet1 |
| Drawing View5 |
| Drawing View6 |
| Drawing View7 |
| Drawing View11 |
| Detail View A (5 : 1) |
| navitar_bracket_3 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Detail View A (1 : 1) |
| navitar_bracket_4 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Detail View B (10 : 1) |
| Drawing View6 |
| Drawing View7 |
| pivot_nub_no_guide |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Drawing View4 |
| projector_mount_shim |
| Sheet1 |
| Drawing View1 |
| right_bracket_angle_1 |
| Sheet1 |
| Drawing View14 |
| Drawing View15 |
| Drawing View16 |
| Drawing View23 |
| Section View A-A |
| Section View B-B |
| right_bracket_angle_2 |
| Sheet1 |
| Drawing View1 |
| Drawing View2 |
| Drawing View3 |
| Drawing View17 |
| Section View A-A |
| upright_bracket_angle_1 |
| Sheet1 |
| Drawing View2 |
| Drawing View4 |
| upright_bracket_angle_2 |
| Sheet1 |
| Drawing View3 |
| Drawing View4 |
Blank Page
File details come from the government source that posted it. Updated .