01-233-2213
Aircraft Former
34.500" overall length 6.750" overall width 1.250" material thickness opposite p/n -2019; nha 68A332000
01-233-2214
Aircraft Former
34.500" overall length 6.750" overall width 1.250" material thickness opposite p/n -2020; nha 68A332000
01-233-2215
Aircraft Former
2.500" overall length 2.500" overall width 0.063" material thickness opposite p/n -2031
01-233-2216
Aircraft Former
4.250" overall length 2.120" overall width 0.063" material thickness opposite p/n -2034
01-233-2217
Aircraft Former
4.250" overall length 2.120" overall width 0.063" material thickness opposite p/n -2033
01-233-2218
Aircraft Former
2.500" overall length 2.380" overall width 0.063" material thickness opposite p/n -2036
01-233-2219
Aircraft Former
2.500" overall length 2.380" overall width 0.063" material thickness opposite p/n -2035
01-233-2220
Aircraft Former
2.500" overall length 2.500" overall width 0.063" material thickness opposite p/n -2032
01-233-2221
Aircraft Former
01-233-2222
Aircraft Former
01-233-2223
Aircraft Former
01-233-2224
Aircraft Former
01-233-2225
Airfoil Rib
T4 clad
01-233-2228
Aircraft Skin
01-233-2229
Aircraft Skin
Used on F-15.
01-233-2230
Aircraft Skin
Used on F-15.
01-233-2231
Aircraft Stringer
01-233-2232
Aircraft Stringer
01-233-2613
Structural Aircraft Plate
Used on F-15. 28.600" overall length 21.000" overall width 0.125" material thickness 6al-6v-2sn, mms-1203
01-233-2614
Structural Aircraft Plate
Used on F-15. 28.6000" overall length 21.000" overall width 0.125" material thickness
01-233-2615
Structural Aircraft Plate
Used on F-15. 28.600" overall length 21.000" overall width 0.125" material thickness
01-233-2616
Structural Aircraft Plate
Used on F-15.
01-233-2617
Structural Aircraft Plate
01-233-2618
Structural Aircraft Plate
Used on F-15.
01-233-2620
Structural Component Air Support
01-233-2621
Structural Component Air Support
Used on f-15 acft. p/o former-side panel; fuselage station 661.270
01-233-2622
Structural Component Air Support
01-233-2623
Structural Component Air Support
01-233-2624
Structural Component Air Support
01-233-2625
Structural Component Air Support
01-233-2626
Structural Component Air Support
Used on f-15 acft. p/o former-side panel; fuselage station 661.270
01-233-2627
Structural Component Air Support
01-233-2628
Structural Component Air Support
01-233-2629
Structural Component Air Support
Used on f-15 acft. p/o former-side panel; fuselage station 661.270
01-233-2630
Structural Component Air Support
01-233-2631
Structural Component Air Support
Used on f-15 acft. p/o former-side panel; fuselage station 661.270
01-233-2632
Structural Component Air Support
01-233-2636
Aircraft Former
01-233-2637
Aircraft Former
01-233-2638
Aircraft Former
9.000" overall length 8.000" overall width 0.040" material thickness opposite p/n -37r
01-233-2639
Aircraft Former
01-233-2640
Aircraft Former
01-233-2641
Aircraft Former
01-233-2642
Aircraft Former
01-233-3097
Structural Aircraft Plate
Used on b-1 se 30 in ejector. ejector side plate; ti
01-233-3591
Structural Component Air Support
01-233-3621
Structural Component Air Bracket
Used on sentry f22 aircraft. bracket assembly
01-233-3635
Aircraft Strut
Used on sentry f22 aircraft.
01-233-3681
Structural Component Air Bracket
Used on sentry f22 aircraft. bracket assembly
