01-498-5913
Structural Aircraft Plate
Used on f-22 raptor. plate assy consists of pn 5HW82495-163 plate, MS20427M4-7 rivets (2) , MS20427M4-8 rivets (2) ,
01-498-5914
Structural Aircraft Plate
Used on f-22 raptor. plate assy consists of pn 5HW82495-165 plate, MS20427M4-6 rivets (2) , MS20427M4-7 rivets (2) , NS203203F5-2 nutplate (1)
01-498-5917
Structural Aircraft Plate
Used on f-22 raptor. plate assy consists of 5HW82495-167 plate (1) , MS20427M4-6 rivets (4) , NS203214F8-1 nutplate (2)
01-498-5918
Structural Aircraft Plate
Used on f-22 raptor. plate assy consists of 5HW82495-169 plate (1) , MS20427M3-6 rivets (2) , MS20427M4-6 rivets (2) , NS203214F8-1 nutplate (2)
01-498-5922
Structural Aircraft Plate
Used on f-22 raptor. plate assy consists of 5HW82495-173 plate (1) , MS20427M4-6 rivets (4) , NS203203F5-2 nutplate (2)
01-498-5923
Structural Aircraft Plate
Used on f-22 raptor. plate assy consists of 5HW82495-175 plate (1) , MS20427M4-6 rivets (4) , NS203214F8-1 nutplate (2)
01-498-5928
Structural Aircraft Plate
Used on f-22 raptor. plate assy consists of 5HW82495-181 plate (1) , MS20427M4-7 rivet (1) , MS20427M4-6 rivet (1) , MS20427M4-8 rivet (2) , NS203214F8-1 nutplate (2)
01-498-5929
Structural Aircraft Plate
Used on f-22a raptor. plate assembly, wing joint consists of 1 5HW82495-179 plate; 1 MS20427M4-5 rivet; 2 MS20427M4-7 rivets; 2 MS20427M4-8 rivets; 1 MS20427M4-9 rivet; 3 NS203214F8-1 nutplates
01-498-5932
Structural Aircraft Plate
Used on f-22a raptor. plate assembly, wing joint consists of 1 5HW82495-185 plate; 8 MS20427M4-5 rivets; 4 NS203214F8-1 nutplates
01-498-5935
Structural Aircraft Plate
Used on f-22a raptor. plate assembly, wing joint consists of 1 5HW82495-197 plate; 4 MS20427M4-6 rivets; 2 NS203214F8-1 nutplates
01-498-5937
Structural Aircraft Plate
Used on f-22a raptor. plate assembly, wing joint consists of 1 5HW82495-187 plate; 4 MS20427M3-6 rivets; 4 MS20427M4-5 rivets; 2 NS203203F4-2 nutplates; 2 NS203203F5-2 nutplates
01-498-5938
Structural Aircraft Plate
Used on f-22a raptor. plate assembly, wing joint consists of 1 5HW82495-191 plate; 4 MS20427M4-5 rivets; 2 NS203203F5-2 nutplates
01-498-5940
Structural Component Air Fitting
Used on f/a-22 raptor. fitting-actuator 3 & 4, leading edge, wing box
01-498-5946
Structural Component Air Fitting
Used on f-22 raptor. 5.000" overall length 4.000" overall width fitting assembly fracture/durability critical item; c/o: -115 fitting, 4065-090 bushing (4) , 4065-091 bushing (2) ; dim. are stock material; m/o 62222 sta titanium plate
01-498-5947
Aircraft Fairing
Used on f-22 raptor. t-beam, fairing-splice - wheel well opposite 5HW82492-102
01-498-5948
Structural Component Air Fitting
Used on f-22 raptor. 4.000" overall length 6.000" overall width fitting assembly fracture/durablilty critical item; dim. are stock material; 6-2222 sta titanium plate; c/o -113 fitting, 4065-088 bushing; -101 opposite -102
01-498-5949
Structural Aircraft Plate
Used on f-22 raptor. 3.503" overall length 1.500" overall width plate assembly consists of -153 plate, MS20427M4-6 rivet (2) , MS20427M4-7 rivet (2) , NS203214F8-1 nutplate (2) , ga-.250, al-6al-4v, te cond a, code ab-1
01-498-5951
Structural Aircraft Plate
Used on f/a-22 raptor. 3.503" overall length plate assembly consists of -155 plate, MS20427M3-6 rivet (2) , MS20427M3-7 rivet (2) , NS203214F8-1 nutplate (2) , ga -.250, al-6al-4v, te-cond a, ma-T1
01-498-5952
Structural Component Air Fitting
Used on f/a-22 raptor. fitting-actuator no.1, leading edge, wing box
01-498-5954
Structural Aircraft Plate
Used on f-22 raptor. 3.503" overall length 1.500" overall width plate assembly consists of -101 plate, MS20427M4-6 rivet (2) , MS20427M4-7 rivet (2) , NS203214F8-1 nutplate (2) , ga -.375, al-6al-4v, te-cond a, cond ab-1
01-498-5956
Structural Aircraft Plate
Used on f-22 raptor. 1.847" overall length 1.018" overall width plate assembly consists of -171 plate, MS20427M3-6 rivet (4) , NS203203F4-2 nutplate (2) , ga -.080, al-6al-4v, te cond a, ma-T1
01-498-5959
Structural Aircraft Plate
Used on f-22 raptor. 5.500" overall length 1.500" overall width plate assembly consists of -177 plate, MS20427M4-6 rivet (6) , NS203214F8-1 nutplate (3) , ga -.375, al-6al-4v, te cond a, cond ab-1
01-498-5961
Structural Aircraft Plate
Used on f-22 raptor. 3.682" overall length 1.500" overall width plate assembly consists of -183 plate, MS20427M4-6 rivet (4) , NS203214F8-1 nutplate (2) , ga -.080, al-6al-4v, te cond a, ma-T1
01-498-5964
Structural Aircraft Plate
Used on f-22 raptor. 2.464" overall length 1.100" overall width plate assembly consists of -189 plate, MS20427M4-6 rivet (4) , NS203203F6-2 nutplate (2) , ga-.080, al-6al-4v, te cond a, ma-T1
01-498-5965
Structural Aircraft Plate
Used on f-22 raptor. 3.879" overall length 2.969" overall width plate assembly consists of -193 plate, MS20427M4-6 rivet (8) , NS203203F6-2 nutplate (2) , NS203214F8-1 nutplate (2) , ga -.250, al-6al-4v, te cond a, ma-T1
01-498-5966
Bleed Air Duct Assembly
01-498-5971
Structural Component Air Fitting
Used on f-22 raptor. 5.000" overall length 4.000" overall width fitting assembly fracture/durability critical item; c/o: -115 fitting, 4065-088 bushing (4) , 4065-089 bushing (2) ; dim. are stock material; m/o 6-222 sta titanium plate
01-498-5972
Structural Aircraft Plate
Used on f/a-22 raptor. 14.513" overall length 2.500" overall width splice-fairing, aileron
01-498-5974
Bleed Air Duct Assembly
01-498-5975
Structural Component Air Fitting
Used on f/a-22 raptor. fitting assy
01-498-5995
Movable Canopy
Used on f-22 raptor.
01-498-6141
Structural Aircraft Plate
27.250" overall length 12.000" overall width 0.310" material thickness composite laminate repair
01-498-6142
Fuselage Parts Kit
Used on C-5. manf suggested name-heat exchanger kit
01-498-6143
Structural Aircraft Plate
36.250" overall length caul plate used to repair tf-39 outboard skin; at-092552 rh opp side; arch lth 38.630
01-498-6145
Structural Aircraft Plate
5.120" overall length 1.500" overall width 0.620" material thickness dim. are stock material; nha L3326421; m/o PH13-8M0 cres bar; u/o b-1b 1&subq; nuclear hardness critical item
01-498-6146
Structural Aircraft Plate
36.250" overall length 0.0375" material thickness caul plate used to repair tf-39 outboard skin; at-092667 lh opp side; arch lth 38.630
01-498-6147
Structural Aircraft Plate
4.880" overall length 1.500" overall width 0.062" material thickness next higher assy, L3326421, u/o b-1b 1
01-498-6148
Structural Aircraft Plate
5.120" overall length 1.500" overall width 0.062" material thickness 2next higher assy, L3326421, u/o b-1b 1
01-498-6150
Structural Aircraft Plate
5.120" overall length 1.500" overall width 0.620" material thickness 2next higher assy, L3326421, u/o b-1b 1
01-498-6151
Structural Aircraft Plate
5.120" overall length 1.500" overall width 0.062" material thickness next higher assy, L3326421, u/o b-1b 1
01-498-6152
Structural Aircraft Plate
5.120" overall length 1.500" overall width 0.620" material thickness dim. are stock material; u/o b-1b 1&subq; nha L3316421; nuclear hardnesscritical item
01-498-6153
Structural Aircraft Plate
5.120" overall length 1.500" overall width 0.062" material thickness ball attach plates next higher assy, L3326421 u/o b-1b 1
01-498-6154
Structural Aircraft Plate
5.120" overall length 1.500" overall width 0.620" material thickness dim. are stock material; nha L3326421; m/o PH13-8M0 cres bar; u/o b-1b 1&subq; nuclear hardness critical item
01-498-6155
Structural Aircraft Plate
5.120" overall length 1.500" overall width 0.062" material thickness 2next higher assy, L3326421, u/o b-1b 1
01-498-6156
Structural Aircraft Plate
4.880" overall length 1.500" overall width 0.062" material thickness next higher assy, L3326421 u/o b-1b 1
01-498-6157
Structural Aircraft Plate
4.880" overall length 1.500" overall width 0.620" material thickness dim. are stock material; m/o PH13-8M0 cres bar; nuclear hardness critical item; nha L3326421; u/o b-1b 1&subq
01-498-6158
Structural Aircraft Plate
5.120" overall length 1.500" overall width 0.062" material thickness next higher assy, L3326421, u/o b-1b 1
01-498-6159
Structural Aircraft Plate
4.880" overall length 1.500" overall width 0.062" material thickness next higher assy, L3326421, u/o b-1b, 1
01-498-6160
Aircraft Skin
Used on pacer special. skin assy, inbd elevon low observable critical
01-498-6161
Aircraft Skin
Used on pacer special. skin assy, inbd elevon low observable critical
