01-073-2098
Aircraft Stiffener
01-073-2099
Aircraft Stiffener
01-073-2100
Aircraft Stiffener
01-073-2101
Aircraft Stiffener
01-073-2102
Aircraft Stiffener
01-073-2103
Structural Component Air Bracket
3.000" overall length 2.000" overall width 0.050" material thickness
01-073-2104
Structural Aircraft Plate
01-073-2105
Structural Aircraft Plate
01-073-2106
Structural Component Air Support
01-073-2107
Structural Component Aircraf Web
14.000" overall length 8.000" overall width 0.072" material thickness
01-073-2195
Aircraft Strut
C/o 1 strut, 2 sleeve, 1 pin, 1 eye, 1 nut, wire rope a/r
01-073-2285
Structural Aircraft Plate
Used on acft model f4c. titanium alloy per mil-t-9046 type 111, comp a, annealed, do not use cadmium plated tools on this item, stock size 0.032 in.thick, 5.20 in.wide, 10.00 in.length;
01-073-2286
Structural Aircraft Plate
17.150" overall length 6.520" overall width 0.250" material thickness shot peen per mil-s-13165, magnetic inspect per mil-i-6868, heat treatment 125000-145000 psi per mil-h-6875, cad. plate per qq-p-416, type ii, class 2 followed by 2 coats of epoxy primer mil-p-23377, and one coat polyurethane paint mil-c-83286
01-073-2287
Structural Aircraft Plate
17.150" overall length 6.520" overall width 0.250" material thickness shot peen per mil-s-13165, magnetic inspect per mil-i-6868, heat treatment 125000-145000 psi per mil-h-6875, cad. plate per qq-p-416, type ii, class 2 followed by 2 coats epoxy primer per mil-p-23377, one coat polyurethane paint per mil-c-83286
01-073-2288
Structural Aircraft Plate
17.150" overall length 6.520" overall width 0.250" material thickness shot peen per mil-s-13165, magnetic inspect per mil-i-6868, heat treatment 125000-145000 psi per mil-h-6875, cad. plate per qq-p-416, type ii, class 2 followed by 2 coats epoxy primer per mil-p-23377, one coat polyurethane paint per mil-c-83286
01-073-2289
Structural Aircraft Plate
17.150" overall length 6.520" overall width 0.520" material thickness shot peen per mil-s-13165, magnetic inspect per mil-i-6868, heat treatment 125000-145000 psi per mil-h-6875, cad. plate per qq-p-416, type ii, class 2 followed by 2 coats epoxy primer per mil-p-23377, one coat polyurethane paint per mil-c-83286
01-073-2290
Structural Aircraft Plate
4.860" overall length 2.720" overall width 2.720" material thickness 6hheat treatment 125000-140000 psi per mil-h-6875; shot peen per mil-s-13165; magnetic inspect per mil-i-6868; cad. plate per qq-p-416, type ii, class 2, followed by 2 coats epoxy primer per mil-p-23377, and one coat polyurethane paint per mil-c-83286
01-073-2291
Structural Aircraft Plate
4.860" overall length 2.720" overall width 0.125" material thickness 5heat treatment 125000-140000 psi per mil-h-6875; shot peen per mil-s-13165; magnetic inspect per mil-i-6868; cad. plate per qq-p-416, type ii, class 2, followed by 2 coats epoxy primer per mil-p-23377, and one coat polyurethane paint per mil-c-83286
01-073-2294
Structural Component Air Support
Used on acft model 1f4c. alum alloy 7075-0 per qq-a-250/13 cond 0, stock size 0.050 in.thick, 4.70 in.wide, 5.00 in.length, used on canted rib assy, inboard leading edge flap bl S9.56
01-073-2295
Structural Component Air Support
Used on acft model 1f4c. alum clad 7178-0 per qq-a-250/15 cond 0. stock size 0.063 in.thick, 7.52 in.wide, 11.24 in.length
01-073-2309
Airfoil Rib
0.032" material thickness cond 0; br 06, max flg 1.97 in.
01-073-2311
Airfoil Rib
8.250" overall length 3.550" overall width 0.025" material thickness
01-073-2312
Aircraft Skin
Used on F-4. part of pneumatic starter pan assembly
01-073-2313
Aircraft Tip
Used on T-38. c/o name plate, pn ms 27253F1, equip instl, pn 2-60021-506, wing tip panel, pn 3-21200-504
01-073-2707
Aircraft Rudder
01-073-3917
Structural Aircraft Plate
Used on acft model f4c.
01-073-3918
Aircraft Fairing
10.290" overall length 5.600" overall width 0.032" material thickness
01-073-3919
Structural Component Air Support
Used on acft model f4c. alum 2024-0 per qq-a-250/5 cond 0, stock size 0.063 in.thick, 6.24 in.wide, 10.11 in.length, used on seat rail assy, aft cockpit
01-073-3920
Structural Component Air Support
Used on acft model f4e. nickel chromium alloy per mil-n-7786, stock size 0.040 in.thick, 2.40 in.wide, 18.80 in.length;
01-073-3932
Aircraft Skin
Used on F-16.
01-073-3933
Aircraft Skin
Used on acft model f4e. alum clad 7075-T6 per qq-a-250/13 cond T6, stock size 0.063 in.thick, 2.85 in.wide, 63.25 in.length
01-073-3934
Aircraft Skin
34.400" overall length 4.800" overall width
01-073-4196
Structural Aircraft Panel
Used on F-16.
01-073-4856
Aircraft Fairing
Used on helicopter,attack,model ah-1s.
01-073-6187
Access Aircraft Cover
01-073-6265
Aircraft Stiffener
Temper T6
01-073-6266
Aircraft Stiffener
5.000" overall length 5.000" overall width 0.050" material thickness matl: PH15-7mo cres ams 5520 annealed
01-073-6267
Aircraft Stiffener
5.000" overall length 5.000" overall width 0.050" material thickness matl: PH15-7mo cres ams 5520 annealed
01-073-6268
Aircraft Stiffener
5.000" overall length 5.000" overall width 0.050" material thickness matl: PH15-7mo cres AMS5520 annealed
01-073-6269
Aircraft Stiffener
5.000" overall length 5.000" overall width 0.050" material thickness matl: PH15-7mo AMS5520 annelaed
01-073-6270
Aircraft Stiffener
5.000" overall length 5.000" overall width 0.050" material thickness matl: PH15-7mo cres ams 5520 annealed
01-073-6271
Aircraft Stiffener
5.000" overall length 5.000" overall width 0.050" material thickness matl: PH15-7mo cres AMS5520 annealed
01-073-6272
Structural Component Air Support
7.000" overall length 2.000" overall width 0.070" material thickness
01-073-6273
Structural Component Air Support
7.000" overall length 2.000" overall width 0.070" material thickness
01-073-6275
Aircraft Stiffener
01-073-6276
Aircraft Stiffener
Stock LS30033-1 x 3.000
01-073-6278
Aircraft Stiffener
01-073-6279
Aircraft Stiffener
01-073-6295
Access Aircraft Door
Used on F-16. video tape crtg
