01-232-9353
Longeron
Used on F-15.
01-232-9417
Fuel Aircraft Tank
Used on 230-gallon external fuel tank;ov-10 aircraft.
01-233-0037
Fuselage Section
01-233-0038
Fuselage Section
01-233-0039
Fuselage Section
01-233-0040
Fuselage Section
01-233-0246
Structural Aircraft Plate
Used on F-15.
01-233-0247
Structural Aircraft Plate
Used on F-15.
01-233-0248
Structural Aircraft Plate
Used on F-15.
01-233-0249
Structural Component Air Support
Used on f-15 acft. clip p/o former, side panel; fuselage station
01-233-0250
Structural Component Air Support
Used on f-15 acft. clip p/o former, sidepanel; fuselage station 702.900
01-233-0251
Structural Component Air Support
Used on f-15 acft. clip p/o former, sidepanel; fuselage station 702.900
01-233-0252
Structural Component Air Support
Used on f-15 acft. clip p/o former, sidepanel; fuselage station 702.900
01-233-0253
Structural Component Air Support
Used on f-15 acft. clip p/o former, side panel; fuselage station 702.900
01-233-0254
Structural Component Air Support
Used on f-15 acft. clip p/o former, side panel; fuselage 702.900
01-233-0255
Structural Component Air Support
Used on f-15 acft. clip p/o former, side panel; fuselage 702.900
01-233-0256
Structural Component Air Support
Used on f-15 acft. clip p/o former, side panel; fuselage station 702.900
01-233-0257
Structural Component Air Support
Used on f-15 acft. angle p/o former, side panel; fuselage station 702.900
01-233-0260
Structural Aircraft Panel
Part of -101a shelf instl-heat exchanger support, wing to fus fairing; opposite -240a; eff on 0008 & up
01-233-0268
Aircraft Former
30.950" overall length 3.920" overall width 1.250" material thickness nha 68A332000; opposite p/n -2018
01-233-0269
Aircraft Former
30.950" overall length 3.920" overall width 1.250" material thickness opposite p/n -2017; nha 68A332000
01-233-0270
Aircraft Former
20.000" overall length 4.000" overall width 0.050" material thickness 6al-6v-2sn per mms-1203
01-233-0271
Aircraft Former
20.750" overall length 2.060" overall width 0.036" material thickness
01-233-0272
Aircraft Former
21.000" overall length 4.000" overall width 0.050" material thickness
01-233-0273
Aircraft Former
21.000" overall length 4.000" overall width 0.050" material thickness
01-233-0274
Aircraft Former
6.200" overall length 1.140" overall width 0.036" material thickness
01-233-0275
Aircraft Former
21.000" overall length 4.000" overall width 0.050" material thickness
01-233-0276
Aircraft Former
Opposite p/n -2008; nha 68A333001
01-233-0277
Aircraft Former
Side panel
01-233-0974
Aircraft Former
01-233-1943
Structural Aircraft Plate
CF1018 steel bar qq-s-634; 6.000 in. l. x 3.000 in. w. x 1.000 in h; six holes evenly spaced; 3 0.750 in. dia. along length; three 0.410 in.dia.w/counterbore of 0.875 in. dia. x 0.500 in.dp. on opposite side
01-233-2099
Access Aircraft Cover
Used on acft model a-10a.
01-233-2174
Structural Aircraft Plate
Used on F-15.
01-233-2175
Structural Aircraft Plate
01-233-2176
Structural Aircraft Plate
48.770" overall length 2.070" overall width 0.080" material thickness NHA68A333001
01-233-2177
Structural Aircraft Plate
01-233-2178
Structural Aircraft Plate
Used on C-130. T6 clad
01-233-2179
Structural Aircraft Plate
01-233-2180
Structural Aircraft Plate
01-233-2193
Structural Component Air Support
01-233-2194
Structural Component Air Support
Used on f-15 acft. angle p/o former, side panel; fuselage station 702.900
01-233-2195
Structural Component Air Support
Used on f-15e aircraft. matl/size IMT360A01-10039X4.38; opposite -2003; located-fs 661.270; nha 68A331011; eff on 2 & up
01-233-2197
Structural Component Air Support
01-233-2198
Structural Component Air Support
01-233-2199
Structural Component Air Support
01-233-2200
Structural Component Air Support
01-233-2201
Structural Component Air Support
Used on f-15 acft. titanium; angle p/o former empennage support beam; fuselage station 721.830
01-233-2202
Structural Component Air Support
Used on f-15 acft. titanium; angle p/o former empennage support beam; fuselage station 721.830
01-233-2203
Structural Component Air Support
01-233-2204
Structural Component Air Support
