01-225-7897
Aircraft Window Panel
Zu/a: window assembly, camera; c/o: optical glass per mil-g-174, borosilicate crown type bk-7, 517642 or equivlent, grade nh-2a, fine annealed; finished glass plate shall have a mininum of 37percent tansmission betweem 400 & 750 nanometers
01-225-7911
Structural Aircraft Plate
Aluminum alloy, qq-a-250/8, 5052 H32; 5.797 in. lg, 5.350 in. wd, 0.090 in. thk, 4.750 in. dia aperature; nutplate in ea corner
01-225-8060
Access Aircraft Cover
01-225-8161
Structural Aircraft Plate
7.300" overall length 3.250" overall width 0.056" material thickness
01-225-8162
Structural Aircraft Plate
26.500" overall length 8.100" overall width 0.080" material thickness material per mms-1203
01-225-8163
Structural Aircraft Plate
26.500" overall length 8.100" overall width 0.080" material thickness material per mms-1203
01-225-8166
Structural Aircraft Panel
Used on acft model e-3a.
01-225-8168
Structural Aircraft Panel
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket, 1 ident plate, 4 grommet; located at yan 47.217 to yan 83.00
01-225-8169
Structural Aircraft Panel
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket, 1 ident plate, 4 grommet; located at yan 47.217 to yan 83.00
01-225-8170
Structural Aircraft Panel
Used on acft model b-1b. consists of 2 facesheet, 1 batt blanket, 1 ident plate, 11 grommet; located at yan 47.217 to yan 83.00
01-225-8171
Structural Aircraft Panel
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket, 1 ident plate, 2 grommet; located at yan 47.217 to yan 83.00
01-225-8172
Structural Aircraft Panel
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket, 1 ident plate, 9 grommet; located at yan 47.217 to yan 83.00
01-225-8173
Structural Aircraft Panel
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket, 1 ident plate, 9 grommet; located at yan 47.217 to yan 83.00
01-225-8174
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 outer face sheet, 1 inner face sheet, 1 batt insulation, 1 ident plate, 6 grommet; located at yan 25.936 to yan 47.216
01-225-8175
Structural Aircraft Panel
Used on acft model b-1b. consists of 1 batt insulation, 2 facesheet, 1 ident plate, 5 grommet; located at yan 25.936 to yan 47.216
01-225-8176
Structural Aircraft Panel
Used on acft model b-1b. consist of outer face sheet 1, 1 inner facesheet, 1 batt insulation, 1 ident plate, 3 grommet; located at yan 25.936 to yan 47.216
01-225-8177
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 batt insulation, 1 outer facesheet, 1 facesheet, 1 ident plate, 11 grommet; located at yan 25.936 to yan 47.216
01-225-8184
Aircraft Former
01-225-8262
Access Aircraft Cover
01-225-8263
Access Aircraft Cover
01-225-8264
Access Aircraft Door
01-226-0910
Access Aircraft Door
Used on acft model b-1b. c/o 1 closeout, 1 glass, 1 doubler, 2 skin, 1 core, 4 filler, misc hardware; located at YF1450 to YF1475
01-226-1089
Aircraft Fairing
35.000" overall length 10.000" overall width 0.063" material thickness part of crown installtion-landing gear fairing
01-226-1111
Inner Wing Section
01-226-2625
Access Aircraft Door
Used on f-15 aircraft.
01-226-2709
Fluid Aircraft Manifold
01-226-2733
Structural Aircraft Plate
Used on acft model e-3a. consist of 2 end panel, 1 door, 4facesheet, 1 seal, 1 trim, 1 inbd panel, 2 end panel assy, 1 inbd panel assy, 1 stiffener, 1 stop plate, 1 guide plate, 1 shroud instrument pml, 1 latch assy, misc hardware; located at sta 540 l.h; nha 204-40501
01-226-2735
Structural Component Air Support
14.000" overall length 8.000" overall width 1.750" material thickness
01-226-2736
Structural Component Air Support
14.000" overall length 8.000" overall width 1.750" material thickness
01-226-2737
Structural Component Air Support
Used on f-15 aircraft. 2124-T851 per mms-149 cond t-851; 14.70 in. lg, 6.75 in. wd, 4.00 in. thk; opposite p/n -2014; nha 68A324587; located on fs 512.175
01-226-2738
Structural Component Air Support
Used on f-15 aircraft. 2124-T851 per mms-149 cond t-851; 14.70 in. lg, 6.75 in. wd, 4.00 in. thk; opposite -2013; nha 68A324587; located on fs 512.175
01-226-2743
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 end panel assy, 2 facesheet, 1 seal, 1 inbd panel assy, 1 stiffener, misc hardware; located at sta 742 l.h; nha 204-40501
01-226-2744
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 inbd panel assy, 2 facesheet, 1 seal, 1 end panel assy, 1 tie clip, 1 stiffener, misc hardware; located at sta 742 r.h; nha 204-40501
01-226-2745
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 side panel assy, 1 side panel, 2 facesheet, 1 seal, 1 inbd panel assy, 1 inbd panel, 2 stiffener, misc hardware; located at sta 800 l.h; nha 204-40501
01-226-2746
Structural Aircraft Panel
Consist of 1 step panel, 1 facesheet, 1 seal, 1 air return grille, 2 insert; nha 204-40501
01-226-2747
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 inbd panel assy, 1 inbd panel, 1 end panel assy, 1 end panel, 2 facesheet, 1 seal, 2 stiffener, misc hardware; located at sta 96011
01-226-2748
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 inbd panel assy, 1 inbd panel, 2 facesheet, 2 foil, 1 seal, 1 end panel assy, 1 end panel, 2 stiffener, misc hardware; located at sta 1085 l.h; nha 204-40501
01-226-2749
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 inbd panel assy, 1 inbd panel, 2 face sheet, 1 seal, 1 end panel assy, 1 end panel, 2 stiffener, 1 tie clip, misc hardware; located at sta 1082.9 r.h; nha 204-40501
01-226-2750
Structural Aircraft Panel
01-226-2751
Structural Aircraft Panel
01-226-2763
Aircraft Skin
Used on F-15.
01-226-2764
Aircraft Skin
Used on F-15. 29.310" overall length 7.300" overall width
01-226-2765
Aircraft Skin
Used on F-15.
01-226-3676
Access Aircraft Door
Used on acft model e-3a. nha 204-40501
01-226-3846
Structural Aircraft Plate
Used on acft model e-3a. consist of 1 end panel assy, 1 end panel, 2 facesheet, 2 seal, 2 trim, 1 inbd panel assy, 1 inbd panel, 1 stiffener, 1 air return grille, misc hardware; located at sta 690 l.h; nha 204-40501
01-226-3847
Structural Aircraft Plate
Used on acft model e-3a. consist of 1 aft panel assy, 1 aft panel, 1 outbd panel assy, 1 outbd panel, 1 inbd panel assy, 1 inbd panel, 4 facesheet, 1 seal, 1 fwd panel assy, 1 fwd panel, 2 bracket, 5 angle, 3 tie clip, 4 stiffener, misc hardware; located at sta 791 r.h; nha 204-40501
01-226-3863
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 end panel, 1 inbd panel assy, 1 inbd panel, 2 facesheet, 1 seal, 1 end panel assy, 2 stiffener, 1 tie clip, misc hardware; located at sta 1152.5 l.h; nha 204-40501
01-226-3865
Structural Aircraft Panel
Used on acft model e-3a. consist of 2 facesheet, 1 seal, 1 inbd panel assy, 1 inbd panel, 1 end panel assy, 1 end panel, 2 stiffener, 1 doubler, misc hardware; located at sta 516 l.h; nha 204-40501
01-226-3867
Structural Aircraft Panel
Used on acft model e-3a. consist of 3 facesheet, 1 inbd panel assy, 1 inbd panel, 2 bottom panel, 2 bottom panel assy, 1 doubler, 1 sirqud assy, 2 grommet, misc hardware; nha 204-40501; located at sta 460 l.h
