01-224-7141
Aircraft Skin
Used on xw-fms only. 0.090 by 8 by 15 qq-a-250/4-T62 aluminum alloy
01-224-7142
Aircraft Skin
Used on xw-fms only. 0.090 by 6 by 18 qq-a-250/4-T62 aluminum alloy
01-224-7801
Structural Component Air Support
Used on c-141 aircraft. fitting-WS77, inner wing, front beam, lower; matl 7075-f per qq-a-367; size 8.0X10.0X24.0; opposite -102; nha 3W29039-101
01-224-7802
Structural Component Air Support
Used on c-141 aircraft. fitting-WS77, inner wing, front beam, lower; matl 7075-f per qq-a-367; size 8.0X10.0X24.0; opposite -101; nha 3W29039-102
01-224-7803
Structural Component Air Support
Used on c-5 aircraft. fitting, attach-intercostal to frame, fus sta 1418.16 & 1488.16; matl 7075-T651 alum alloy per qq-a-250/12; size 2.0X2.0X5.0in; opposite -602a
01-224-7915
Radome
Used on f-5e aircraft.
01-224-8454
Aircraft Skin
Used on aircraft model av-8. aluminum alloy per qq-a-250/13, cond-o
01-224-8455
Aircraft Tip
Used on av8b attack aircraft. tip, wing
01-224-8456
Aircraft Tip
Used on av8b attack aircraft. tip, wing
01-224-8840
Structural Aircraft Plate
Used on acft model c/kc-135. nha 35-35423-502
01-224-8841
Structural Aircraft Plate
3.700" overall length 1.700" overall width 0.050" material thickness material per mms 1203 6al-6v-2sn
01-224-8842
Structural Aircraft Plate
7.100" overall length 3.800" overall width 0.056" material thickness
01-224-8844
Structural Component Air Support
Used on f-5e aircraft. bracket, hose support-right side, nose wheel steering; matl AND10134-1602 extr al 7075-6511 per qq-a-200/11
01-224-8845
Structural Component Air Support
Used on f-15 aircraft.
01-224-8846
Structural Component Air Support
Used on f-15 aircraft.
01-224-8847
Structural Component Air Support
Used on f-15 aircraft. material per mms-149 condition T851 2124-T851, 25.500 in. lg, 7.500 in. w, 1.750 in. thk
01-224-8848
Structural Component Air Support
Used on f-15 aircraft. material per mms-149 condition T851 2124-T851, 25.500 in. lg, 7.500 in. w, 1.750 in. thk
01-224-8849
Structural Component Air Support
Used on acft model f-15. titanium alloy per mil-t-9046 type 3 composition c anl, 1.900 in. lg, 1.650 in. w, 0.040 in. thk
01-224-8851
Structural Component Air Support
Used on acft model f-15. titanium alloy per mil-t-9046 type 3 composition c anl, 1.250 in. lg, 1.250 in. w, 0.032 in. thk
01-224-8855
Structural Aircraft Panel
C/o 1 panel, 3 rubber supports, 1 gap filler, dacron cloth, 2 ballards, rigid vinyl, 7 inserts, 1 bronze staple
01-224-8863
Aircraft Former
7.000" overall length 2.400" overall width 0.063" material thickness material per mms 1203 6al-6v-2sn
01-224-8864
Aircraft Former
7.000" overall length 2.050" overall width 0.063" material thickness material per mms 1203 6al-6v-2sn
01-224-8865
Aircraft Former
3.310" overall length 2.670" overall width 0.056" material thickness
01-224-8866
Aircraft Former
5.700" overall length 4.500" overall width 0.050" material thickness
01-224-8867
Aircraft Former
14.200" overall length 2.940" overall width 0.036" material thickness
01-224-8868
Aircraft Former
16.200" overall length 6.400" overall width 0.040" material thickness
01-224-8869
Aircraft Former
10.000" overall length 2.200" overall width 0.036" material thickness
01-224-8878
Aircraft Skin
Used on F-15. 55.000" overall length 30.200" overall width
01-224-8879
Aircraft Skin
Used on F-15. 55.000" overall length 30.200" overall width
01-225-1724
Access Aircraft Door
Used on acft model b-1b. c/o 1 closeout, 1 doubler, 2 rail plate, 2 skin, 1 core, 4 filler, misc hardware; located at YF1475 to YF1500.208
01-225-1725
Access Aircraft Door
Used on acft model b-1b. c/o 1 glass, 1 doubler, 2 rail plate, 2 skin, 1 core, 4 filler, misc hardware; located at YF1475 to YF1500.208
01-225-1771
Structural Aircraft Plate
Used on acft model b-1b. replaces -003; matl ST0160LB0014 steel plate per PH13-8M0 alloy; 4.12 in. lg, 3.25 in. wd, 0.187 in. thk; nha L3052985
01-225-1772
Structural Aircraft Plate
01-225-1773
Structural Aircraft Plate
01-225-1774
Structural Component Air Support
Used on c-5 aircraft. bracket assembly, stabilizer, flight station, stair ladder
01-225-1775
Structural Component Air Support
Used on acft model f-15. titanium alloy per mil-t-9046 type 3 cmpsnc anl, 2.000 in. lg, 1.500 in. w, 0.056 in. thk
01-225-1776
Structural Component Air Support
Used on acft model f-15. titanium alloy per mil-t-9046 type 3 cmpsnc anl, 2.000 in. lg, 1.500 in. w, 0.056 in. thk
01-225-1777
Structural Component Air Support
Used on acft model f-15. titanium alloy per mil-t-9046 type 3 cmpsnc anl condition a, 1.250 in. lg, 1.250 in. w, 0.056 in. thk
01-225-1778
Structural Component Air Support
Used on acft model f-15. titanium per mil-t-9046 type 3 comp c anl, 2.700 in. lg, 1.700 in. w, 0.040 in. thk
01-225-1779
Structural Component Air Support
Used on acft model f-15. titanium per mil-t-9046 type 3 composition c anl, 3.000 in. lg, 2.500 in. w, 0.040 in. thk
01-225-1780
Structural Component Air Support
Used on acft model f-15. titanium alloy per mil-t-9046 type 3 composition c anl, 3.690 in. lg, 3.560 in. w, 0.100 in. thk
01-225-1781
Structural Component Air Support
Used on acft model f-15. titanium alloy per mil-t-9046 type 3 composition c anl, 3.690 in. lg, 3.560 in. w, 0.100 in. thk
01-225-1784
Aircraft Former
2.900" overall length 1.500" overall width 0.045" material thickness
01-225-1785
Aircraft Former
2.900" overall length 1.500" overall width 0.045" material thickness
01-225-1786
Aircraft Former
24.000" overall length 1.350" overall width 0.032" material thickness
01-225-1787
Aircraft Former
5.000" overall length 2.700" overall width 0.050" material thickness
01-225-1788
Aircraft Former
4.000" overall length 2.500" overall width 0.063" material thickness
01-225-1789
Aircraft Former
5.900" overall length 3.100" overall width 0.050" material thickness
01-225-1790
Aircraft Former
14.500" overall length 2.400" overall width 0.045" material thickness
