01-154-8963
Structural Aircraft Plate
01-154-8964
Structural Aircraft Plate
4.000" overall length 3.500" overall width 0.040" material thickness
01-154-8965
Structural Aircraft Plate
01-154-8966
Structural Component Air Support
3.600" overall length 1.800" overall width 0.063" material thickness opp 35-8682-21; used as clip on longeron no.1, nose cowl
01-154-8967
Structural Component Air Support
01-154-8968
Structural Aircraft Plate
01-154-8969
Structural Component Air Support
01-154-8970
Structural Component Air Support
Frame assy opposite p/n -2205
01-154-8971
Structural Component Air Support
Frame assembly used as frame assy on lh upper cowl panel assy; opp -2210
01-154-8972
Structural Component Air Support
Frame assembly used as frame assy on rh upper cowl panel assy; opp -2209
01-154-8973
Structural Component Air Support
Frame assembly used as frame assy on lh upper cowl panel assy; opp -2212
01-154-8974
Structural Component Air Support
Frame assembly used as frame assy on rh upper cowl panel assy; opp -2211
01-154-8975
Structural Component Air Support
Frame assembly used as frame assy on lh upper cowl panel assy; opp -2214
01-154-8976
Structural Component Air Support
Used as frame assy on rh upper cowl panel assy; opp -2213
01-154-8989
Aircraft Former
Used on B-52. opposite pn 35-8682-509
01-154-8990
Aircraft Former
10.300" overall length 5.100" overall width 0.071" material thickness opposite pn 35-8682-7
01-154-8991
Aircraft Former
32.000" overall length 2.200" overall width 0.025" material thickness function-angle
01-154-8992
Aircraft Former
32.000" overall length 2.200" overall width 0.025" material thickness function-angle; opposite 35-8227-831
01-154-8993
Aircraft Former
4.900" overall length 1.200" overall width 0.025" material thickness function-angle
01-154-8994
Aircraft Former
4.900" overall length 1.500" overall width 0.025" material thickness function-angle; opp 35-8227-833
01-154-8995
Aircraft Former
10.200" overall length 2.800" overall width 0.050" material thickness function-frame
01-154-8996
Aircraft Former
Used on B-52.
01-154-8997
Aircraft Former
16.000" overall length 5.500" overall width 0.063" material thickness opposite pn 39-14698-502
01-154-8998
Aircraft Former
16.000" overall length 5.500" overall width 0.063" material thickness opposite pn 39-1498-501
01-154-8999
Aircraft Former
7.500" overall length 4.500" overall width 0.063" material thickness opposite pn 39-14698-802
01-154-9000
Aircraft Former
7.500" overall length 4.500" overall width 0.063" material thickness opposite pn 39-14698-801
01-154-9002
Aircraft Former
58.000" overall length 5.000" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2216
01-154-9003
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, annealed, ht tr 180, 000-200, 000 psi
01-154-9004
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-9005
Aircraft Former
58.000" overall length 5.000" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2218
01-154-9006
Aircraft Former
58.000" overall length 3.500" overall width 0.025" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite on -2220
01-154-9007
Aircraft Former
30.000" overall length 1.500" overall width 0.063" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -103
01-154-9008
Aircraft Former
58.000" overall length 3.500" overall width 0.025" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite -2219
01-154-9009
Aircraft Former
58.000" overall length 4.000" overall width 0.025" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite -2222
01-154-9010
Aircraft Former
58.000" overall length 4.000" overall width 0.025" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite -2221
01-154-9011
Aircraft Former
58.000" overall length 3.200" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2224
01-154-9012
Aircraft Former
58.000" overall length 3.200" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2223
01-154-9013
Aircraft Former
58.000" overall length 4.500" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; oppsite pn -2226
01-154-9014
Aircraft Former
58.000" overall length 4.500" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2225
01-154-9015
Aircraft Former
58.000" overall length 3.500" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2228
01-154-9019
Aircraft Skin
Used on B-52.
01-154-9164
Fluid Aircraft Manifold
32.690" overall length
01-154-9368
Structural Aircraft Panel
Used on A-10.
01-155-0855
Bell Crank
0.2500" bore diameter retainer aluminum alloy, qq-a-25015 comp 2024 temper T3, 0.063 in. thk, 0.500 in.w, 1.940 in.working lg locatedon bb arm
01-155-2031
Access Aircraft Door
01-155-2082
Aircraft Frame
01-155-2083
Aircraft Frame
01-155-2084
Aircraft Frame
01-155-2085
Aircraft Frame
