01-217-4916
Structural Aircraft Plate
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13, T6; matl 0.040 in. thk by 3.172 in. w by 3.531 in. lg
01-217-4917
Structural Aircraft Plate
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13, T6; matl 0.040 in. thk by 3.172 in. w by 3.297 in. lg
01-217-4918
Structural Aircraft Plate
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13, to; matl 0.032 in. thk by 7.594 in. w by 9.703 in. lg
01-217-4920
Structural Component Air Support
Used on mcdonnell p/n 53-111002-1 door assy. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250-13 to; channel cross section; matl 0.063 in. thk by 5.500 in. w by 5.625 in. lg; left hand appl
01-217-4921
Structural Component Air Support
Used on mcdonnell p/n 53-111002-2 door assy. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250-13 to; channel cross section; matl 0.063 in. thk by 5.500 in. w by 5.625 in. lg; right
01-217-4922
Structural Component Air Support
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/05, T3; matl 0.063 in. thk by 1.375 in. w by 1.594 in. lg
01-217-4923
Structural Component Air Support
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250113, to; matl 0.040 in. thk by 3.547 in. w by 62.703 in. lg
01-217-4924
Structural Component Air Support
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13, to; matl 0.040 in. thk by 3.141 in. w by 16.266 in. lg
01-217-4925
Structural Component Air Support
11.055" overall length 3.083" overall width 0.312" material thickness
01-217-6171
Structural Aircraft Plate
Used on mcdonnell p/n 32-33203-309 support assy. type/model designation:f-4e/gy/ aluminum alloy 7178 qq-a-250/5, to; matl 0.040 in. thk by 2.562 in. w by 4.453 in. lg
01-217-6172
Structural Aircraft Plate
Used on 1560-01-086-0653. type/model designation:f-4e/gy/ titanium alloy uns R56080 mil-t-9046 type 3 comp a; matl 0.050 in. thk by 1.453 in. w by 2.359 in. lg; rivet hole 0.191 in. min
01-217-6173
Structural Aircraft Plate
01-217-6174
Structural Aircraft Plate
01-217-6175
Structural Aircraft Plate
01-217-6176
Structural Aircraft Plate
01-217-6177
Structural Aircraft Plate
01-217-6178
Structural Aircraft Plate
01-217-6179
Structural Aircraft Plate
Used on 1560-00-451-4355. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/4, T3; matl 0.016 in. thk by 1.656 in. w by 6.047 in. lg; 2 rivet holes 0.196 in. min 0.202 in. max dia; right appl
01-217-6180
Structural Aircraft Plate
demensions 0.025" thick, 5.500" wide, 7.500" long; aluminum alloy 2024; qq-a-250/5
01-217-6182
Structural Component Air Support
Type/model designation:f-4e/gy/ titanium alloy uns R56080 ams 4908; matl 0.063 in. thk by 3.797 in. w by 13.297 in. lg; l cross section; right appl
01-217-6183
Structural Component Air Support
Type/model designation:f-4e/gy/ titanium alloy uns R56080 ams 4908; matl 0.063 in. thk by 3.797 in. w by 13.297 in. lg; l cross section; left appl
01-217-6184
Structural Component Air Support
Used on mcdonnell p/n 32-33143-2 deflector assy,jet blast. type/model designation:f-4e/gy/ cres uns S30200 mil-s-5059 cond a; matl 0.016 in. thk by 2.047 in. w by 7.297 in. lg; l cross section; left appl
01-217-6185
Structural Component Air Support
Used on mcdonnell p/n 32-33143-1 deflector assy,jet blast. type/model designation:f-4e/gy/ cres uns S30200 mil-s-5059 cond a; matl 0.016 in. thk by 2.609 in. w by 7.297 in. lg; l cross section; right appl
01-217-6186
Structural Component Air Support
Used on mcdonnell p/n 32-33143-2 deflector assy,jet blast. type/model designation:f-4e/gy/ cres uns S30200 mil-s-5059 cond a; matl 0.016 in. thk by 2.609 in. w by 7.297 in. lg; l cross section; left appl
01-217-6187
Structural Component Air Support
Used on mcdonnell p/n 32-33143-1 deflector assy,jet blast. type/model designation:f-4e/gy/ cres uns S30200 mil-s-5059 cond a; matl 0.016 in. thk by 2.047 in. w by 7.297 in. lg; l cross section, right appl
01-217-6188
Structural Component Air Support
Used on 1560-01-086-0653. type/model designation:f-4e/gy/ titanium alloy uns R56080 mil-t-9046 type 3 comp a; matl 0.050 in. thk by 2.422 in. w by 12.734 in. lg; u cross section; lower appl
01-217-6189
Structural Component Air Support
Used on 1560-01-086-0653. type/model designation:f-4e/gy/ titanium alloy uns R56080 mil-t-9046 type 3 comp a; matl 0.050 in. thk by 2.500 in. w by 12.656 in. lg; u cross section; upper appl
01-217-6190
Structural Component Air Support
01-217-6191
Structural Component Air Support
01-217-6192
Structural Component Air Support
01-217-6204
Aircraft Skin
01-217-6469
Aircraft Former
01-217-6576
Stiffener Aircraft Rib
01-217-6582
Structural Aircraft Plate
01-217-6583
Structural Aircraft Plate
01-217-6584
Structural Aircraft Plate
01-217-6585
Structural Aircraft Plate
01-217-6586
Structural Aircraft Plate
01-217-6587
Structural Aircraft Plate
01-217-6590
Structural Component Air Support
Used on t-38 aircraft. matl A356-T6 aluminum
01-217-6591
Structural Component Air Support
Used on t-38 aircraft. matl A356-T6 aluminum
01-217-6592
Structural Component Air Support
Used on c-130 acft. aluminum alloy 2024-T3 clad per qq-a-362; righthand; p/o lower firewall
01-217-6600
Structural Aircraft Panel
Used on acft model b-52g/h. al alloy clad sheet 2024-T3 per qq-a-362; finish f-2.116; 31.30 in. lg, 23.30 in. w, 0.032 in. thk; nha 5-47348
01-217-6611
Aircraft Former
7.000" overall length 2.000" overall width 0.032" material thickness
01-217-6615
Aircraft Skin
Used on F-111. 67.000" overall length 22.000" overall width fms 1053 type 1
01-217-6616
Aircraft Skin
Used on F-111. 67.000" overall length 22.000" overall width fms 1053 type 1
01-217-6786
Fluid Aircraft Manifold
01-217-7488
Aircraft Pylon
Explosive cartridges 650 gal fueltank
01-217-7914
Structural Aircraft Plate
Used on c-5 aircraft. matl 7075-0 per qq-a-250/12; heat treat T6; size .250X8.0X14.0; part of -105c & -105d bulkhead assembly-aft ramp station 158.68
