01-245-4937
Structural Component Air Support
Used on f-15 acft. channel; titanium alloy per mil-t-9046 type 3 comp c annealed; u/o keel structure, center-fuselage station 712.310 to 749.000
01-245-4938
Structural Component Air Support
Used on f-15 acft. channel; titanium alloy per mil-t-9046 type 3 comp c annealed; u/o keel structure, center-fuselage station 712.310 to 749.000
01-245-4939
Structural Component Air Support
Used on f-15 acft. channel; titanium alloy per mil-t-9046 type 3 comp c annealed; u/o keel structure, center-fuselage station 712.310 to 749.000
01-245-4941
Structural Component Air Support
Used on f-15 acft.
01-245-4942
Structural Component Air Support
Used on f-15 acft.
01-245-4943
Structural Component Air Support
Used on f-15 acft. u/o sill-lower outboard empennage support beam canted, fuselage station 672.680
01-245-4944
Structural Component Air Support
Used on f-15 acft. u/o sill-lower outboard empennage support beam canted, fuselage station 672.680
01-245-4945
Structural Component Air Support
Used on f-15 acft. aluminum alloy 7075-T7351; fitting support-lower, ics, left hand forward, buttock line 14.600
01-245-4947
Structural Aircraft Panel
Used on keel structure, center fuselage
01-245-4948
Structural Aircraft Panel
Used on keel structure, center fuselage
01-245-4959
Aircraft Former
69.000" overall length 14.000" overall width 0.562" material thickness
01-245-4962
Aircraft Skin
Used on A-10. 26.500" overall length 20.500" overall width inner skin
01-245-4963
Aircraft Skin
Used on A-10. 26.500" overall length 20.500" overall width inner skin
01-245-4964
Aircraft Skin
22.500" overall length 16.500" overall width outer skin
01-245-4965
Aircraft Skin
Used on A-10. 22.500" overall length 16.500" overall width outer skin
01-245-4966
Aircraft Skin
Used on F-15.
01-245-4967
Aircraft Skin
Used on F-15.
01-245-4968
Aircraft Skin
Used on F-15.
01-245-4969
Aircraft Skin
Used on F-15.
01-245-4970
Aircraft Skin
Used on F-15.
01-245-4972
Aircraft Stringer
51.500" overall length 2.800" overall width 0.071" material thickness opposite -2100; part of -1013
01-245-4973
Aircraft Stringer
51.500" overall length 2.800" overall width 0.071" material thickness opposite -2099; part of -1014
01-245-5151
Structural Aircraft Plate
Used on F-15.
01-245-5152
Structural Aircraft Plate
Used on F-15.
01-245-5153
Structural Aircraft Plate
Used on F-15.
01-245-5154
Structural Aircraft Plate
Used on F-15.
01-245-5155
Structural Component Air Support
Used on f-15 aircraft. clip; size .045X2.23X2.73; used on -1005 former-emp support beam, fus STA693.50
01-245-5156
Structural Component Air Support
Used on f-15 aircraft. size .050X4.20X22.50; part of -1006 former-emp support beam fus sta 693.50
01-245-5157
Structural Component Air Support
Used on f-15 aircraft. clip; size .045X2.23X3.35; part of -1006 former-emp support beam fus sta 693.50
01-245-5158
Structural Component Air Support
Used on f-15 aircraft. size .050X4.20X22.50; part of -1005 former-emp support beam fus sta 693.50
01-245-5159
Structural Component Air Support
Used on f-15 aircraft. clip; size .045X2.23X3.35; part of -1005 former-emp support beam fus sta 693.50
01-245-5160
Structural Component Air Support
Used on f-15 aircraft. 2.730" overall length 2.230" overall width clip
01-245-5161
Structural Component Air Support
C/o 1 fitting, 1 bearing, 1 lube fitting; opposite -1001
01-245-5162
Structural Component Air Support
C/o 1 fitting, 1 bearing, 1 lube fitting; opp -1002
01-245-5164
Structural Component Air Support
Used on f-15 acft. tinanium alloy per mil-t-9046 type 3 comp c annealed; p/o keel structure, aft fuselage-fuselage station 626.900 to 712.310
01-245-5165
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o keel structure, aft fuselage-fuselage station 626.900 to 712.310
01-245-5166
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o keel structure, aft fuselage-fuselage station 626.900 to 712.310
01-245-5167
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o keel structure, aft fuselage-fuselage station 626.900 to 712.310
01-245-5168
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o keel structure, aft fuselage-fuselage station 626.900 to 712.310
01-245-5169
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o keel structure, aft fuselage, fuselage station 626.900 to 712.310
01-245-5170
Structural Component Air Support
Used on f-15 acft.
01-245-5179
Aircraft Skin
Used on F-15.
01-245-5180
Aircraft Skin
Used on F-15.
01-245-5181
Aircraft Skin
Used on F-15.
01-245-5182
Aircraft Skin
Used on F-15.
01-245-7359
Structural Aircraft Plate
Used on F-15. 16.050" overall length 1.710" overall width 0.081" material thickness stiffener; opposite -2099
01-245-7360
Structural Aircraft Plate
Used on F-15. 16.050" overall length 1.710" overall width 0.080" material thickness stiffener; opposite -2097
01-245-7374
Aircraft Former
Nuclear hardness critical item
01-245-7377
Aircraft Stringer
18.000" overall length 3.500" overall width 0.080" material thickness opposite -2102; part of -1013
01-245-7644
Structural Component Air Support
Aluminum alloy 2024-0 qq-a-25015 cond 0, matl 0.160 in. thk by 1.672 in. by 10.250 in. lg
