01-162-0986
Structural Component Air Support
1.400" overall length 1.300" overall width 0.050" material thickness
01-162-0987
Structural Component Air Support
2.300" overall length 2.400" overall width 0.050" material thickness
01-162-0988
Structural Component Air Support
C/o: clip (1 ea) 26-5310-3, nutplate (2 ea) MK1000-1032
01-162-0989
Structural Component Air Support
C/o: clip (1 ea) 26-5310-804, nutplate (2 ea) MK2000-1032; used on rib no.3
01-162-0990
Structural Component Air Support
8.600" overall length 7.100" overall width 0.032" material thickness used as segment of shroud, insulation blanket, exhaust duct
01-162-0991
Structural Component Air Support
8.800" overall length 3.100" overall width 0.032" material thickness used as segment on shroud insulation blanket, exhaust duct
01-162-0992
Structural Component Air Support
8.600" overall length 7.100" overall width 0.032" material thickness used as flange on shroud insulation blanket, exhaust duct
01-162-0993
Structural Component Air Support
Used on b-52 acft. matl size 4.810 in. lg; opposite to p/n 35-19795-3; includes bushing; used as fitting, longeron assy
01-162-1006
Aircraft Former
8.000" overall length 2.500" overall width 0.063" material thickness opp 39-18421-9
01-162-1007
Aircraft Former
8.000" overall length 2.500" overall width 0.063" material thickness opp 39-18421-10
01-162-1010
Aircraft Former
10.200" overall length 2.700" overall width 0.063" material thickness
01-162-1016
Aircraft Skin
Used on B-52. 10.500" overall length 3.800" overall width
01-162-1018
Aircraft Skin
Used on B-52. 14.000" overall length 5.000" overall width
01-162-1020
Aircraft Skin
Used on B-52. 13.500" overall length 4.000" overall width
01-162-3169
Aircraft Channel
U/o: frame-canted, body cowl panel; opp 35-8220-23
01-162-3170
Structural Component Air Bracket
1.600" overall length 1.200" overall width 0.032" material thickness opp 35-8220-31
01-162-3173
Structural Aircraft Panel
C/o 1 honeycomb panel, 1 angle, 1 bonded skin, 1 shim, 1 clip, 1 fire seal, 1 airscoop, 1 fitting, 2 hook, 1 junction box, 1 fitting assy; opposite -508; nha 458-58024
01-162-3225
Structural Aircraft Panel
Used on B-52.
01-162-3226
Structural Aircraft Panel
Used on B-52. 10.500" overall length 5.500" overall width opposite p/n 39-9917-8
01-162-3227
Structural Aircraft Panel
Used on B-52. 10.500" overall length 5.500" overall width opposite p/n 39-9917-7
01-162-3228
Structural Aircraft Panel
Used on B-52/. 14.500" overall length 5.500" overall width opposite p/n 39-9917-10
01-162-3232
Structural Aircraft Plate
5.600" overall length 2.200" overall width 0.020" material thickness
01-162-3233
Structural Aircraft Plate
7.000" overall length 3.200" overall width 0.020" material thickness
01-162-3234
Structural Aircraft Plate
8.000" overall length 4.300" overall width 0.071" material thickness
01-162-3235
Structural Aircraft Plate
6.900" overall length 5.200" overall width 0.050" material thickness
01-162-3236
Structural Aircraft Plate
3.700" overall length opposite pn 35-8648-24; used as angle
01-162-3237
Structural Aircraft Plate
4.000" overall length used as angle; opposite pn 35-8648-26; extrusion
01-162-3238
Structural Aircraft Plate
9.000" overall length used as angle, opposite pn 35-8648-8
01-162-3239
Structural Aircraft Plate
9.750" overall length 7.500" overall width 0.050" material thickness used as gusset; opposite pn 35-8648-804
01-162-3240
Structural Aircraft Plate
8.250" overall length 7.500" overall width 0.050" material thickness used as gusset; opposite pn 35-8648-806
01-162-3241
Structural Aircraft Plate
10.500" overall length 5.500" overall width 0.063" material thickness opposite to p/n 39-9916-12; used as web
01-162-3242
Structural Aircraft Plate
10.500" overall length 5.500" overall width 0.063" material thickness opposite to p/n 39-9916-11; used as web
01-162-3243
Structural Aircraft Plate
17.000" overall length 5.500" overall width 0.063" material thickness used as web
01-162-3244
Structural Aircraft Plate
2.700" overall length 1.600" overall width 0.025" material thickness
01-162-3245
Structural Aircraft Plate
14.500" overall length 5.500" overall width 0.063" material thickness opposite to p/n 39-9917-9; used as web
01-162-3246
Structural Aircraft Plate
6.000" overall length 5.500" overall width 0.063" material thickness opposite pn 39-9917-16; used as doubler
01-162-3247
Structural Aircraft Plate
6.000" overall length 5.500" overall width 0.063" material thickness opposite pn 39-9917-15; used as doubler
01-162-3249
Structural Aircraft Plate
Used on acft model b-1b. al clad 2024-T3 per qq-a-250/5, 0.150 in.thk, 0.830 in.w, 2.200 in.lg, right hand
01-162-3250
Structural Component Air Support
2.300" overall length 2.300" overall width 0.063" material thickness
01-162-3252
Structural Component Air Support
3.800" overall length 1.000" overall width 0.070" material thickness
01-162-3253
Structural Component Air Support
3.750" overall length
01-162-3254
Structural Component Air Support
0.750" overall length
01-162-3256
Structural Component Air Support
Used on acft model f-16a/b usaf. to be used when -47 exhausted; part of support assy, upper-inlet duct strut; superseded p/n 16B4411-47 ow per ecn 2E892; nha 16B4411-821; eff on 61-0007-9999
01-162-3272
Aircraft Former
7.600" overall length opp 35-8648-14
01-162-3273
Aircraft Former
3.300" overall length 2.200" overall width 0.040" material thickness
01-162-3274
Aircraft Former
11.500" overall length 3.000" overall width 0.036" material thickness
01-162-3275
Aircraft Former
4.700" overall length 2.700" overall width 0.032" material thickness opp 35-8220-33
01-162-3276
Aircraft Former
1.900" overall length 1.000" overall width 0.063" material thickness
01-162-4186
Structural Aircraft Panel
Used on f-5 acft. function-firewall panel; location-firewall installation, inboard, fuselage station 460.0 to 545.0
01-162-4207
Structural Aircraft Panel
Used on f-5 acft. location-fuselage station 359.494 to 395.640; function-dorsal cover
