01-155-2207
Structural Component Air Support
5.600" overall length 3.800" overall width 0.250" material thickness opposite -1
01-155-2208
Structural Component Air Support
Used on acft model f-111. stock size K51A2T3511X2.2
01-155-2219
Aircraft Former
Used on B-52.
01-155-2220
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, annealed, ht tr 180, 000-200, 000 psi
01-155-2221
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, annealed, heat treated 180, 000-200, 000 psi
01-155-2222
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, annealed, heat treated 180, 000-200, 000 psi
01-155-2223
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-155-2224
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, anealed, ht tr 180, 000-200, 000 psi; opposite 39-14686-5
01-155-2225
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, annealed, ht tr 180, 000 to 200, 000 psi
01-155-2228
Aircraft Former
01-155-2230
Aircraft Former
Used on B-52. splice angle
01-155-2239
Airfoil Rib
Used on F-111. 8.000" overall length 6.000" overall width 3.000" material thickness
01-155-2327
Radome
Used on f-4g aircraft. part of chin pod, used on an/apr-38
01-155-2924
Access Aircraft Door
Used on acft model f-18.
01-155-3004
Fuselage Aircraft Fairing
Used on aircraft model f-18. cognizant service:navy;
01-155-4681
Access Aircraft Door
01-155-4706
Aircraft Fairing
01-155-4707
Aircraft Frame
01-155-4721
Structural Aircraft Plate
4.500" overall length 3.000" overall width 0.063" material thickness ht treated to 180000-200000 psi; finish f-8.05; opposite pn -2052; used as bearing plate
01-155-4722
Structural Aircraft Plate
58.000" overall length 1.000" overall width 0.032" material thickness htt treated to 180000-200000 psi; finish f-8.05; opposite pn -832; used as 16 deg longeron splice doubler
01-155-4723
Structural Aircraft Plate
58.000" overall length 1.000" overall width 0.032" material thickness ht tr 180, 000-200, 000 psi; finish f-2.05; opposite pn -831; used as 16 deg longeron splice-doubler
01-155-4726
Structural Aircraft Plate
2.100" overall length 1.600" overall width 0.040" material thickness
01-155-4729
Structural Aircraft Plate
1.400" overall length 1.400" overall width 0.040" material thickness
01-155-4730
Structural Aircraft Plate
1.400" overall length 1.400" overall width 0.040" material thickness
01-155-4731
Structural Aircraft Plate
2.100" overall length 1.400" overall width 0.040" material thickness
01-155-4732
Structural Aircraft Plate
Used on B-1B. 0.175" material thickness ht tr per ST0111LA0009, temper T62
01-155-4733
Structural Aircraft Plate
Used on acft model b-1b. matl 2024-0, 0.175 in.thk, located from zvs 184.762 to zvs 199.762
01-155-4734
Structural Component Air Support
18.000" overall length 2.500" overall width 0.080" material thickness opp 39-7648-501; used as seal lower nacelle
01-155-4735
Structural Component Air Support
Used on acft model b-52. aluminum alloy clad per 2024-T3 qq-a-362, 8.000 in. lg, 2.400 in. w, 0.050 in. thk
01-155-4736
Structural Component Air Support
Used on acft model b-52. made from BAC1518-302X45, aluminum alloy per 2024-0 qq-a-267
01-155-4739
Aircraft Former
58.000" overall length 3.500" overall width 0.040" material thickness heat treated 180, 000-200, 000 psi; finish f-8.05; opposite pn -2227
01-155-4740
Structural Component Air Support
55.000" overall length 3.500" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2230; dim. are stock material
01-155-4741
Aircraft Former
51.000" overall length 3.500" overall width 0.040" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2232
01-155-4742
Aircraft Former
48.000" overall length 3.500" overall width 0.025" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2234
01-155-4743
Aircraft Former
48.000" overall length 3.500" overall width 0.025" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2233
01-155-4744
Aircraft Former
0.850" overall length 0.700" overall width 0.050" material thickness finish f-2.115
01-155-4745
Aircraft Former
2.000" overall length 0.700" overall width 0.063" material thickness finish f-2.115
01-155-4746
Aircraft Former
2.000" overall length 0.700" overall width 0.063" material thickness finish f-2.115
01-155-4748
Longeron
Used on B-52. ht tr 180, 000-200, 000 psi; finish f-8.05; c/o 1 fwd
01-155-4751
Aircraft Skin
Used on B-52. 18.000" overall length 10.000" overall width opposite pn -830; finish f 2.10
01-155-4752
Aircraft Skin
Used on B-52. 18.000" overall length 10.000" overall width finish f 2.10; opposite pn -829
01-155-4753
Aircraft Skin
Used on F-111. 11.6000" overall length 5.800" overall width
01-155-4898
Access Aircraft Door
Used on b-52 aircraft. used on -44
01-155-4971
Aircraft Former
15.000" overall length 2.000" overall width 0.050" material thickness
01-155-4972
Aircraft Former
12.600" overall length 1.600" overall width 0.040" material thickness function-angle
01-155-5646
Structural Aircraft Plate
Used on B-52. used as doubler
01-155-5647
Structural Aircraft Plate
14.000" overall length 11.700" overall width 0.050" material thickness used as doubler
01-155-5648
Structural Aircraft Plate
Used on B-52. used as clip
01-155-5650
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-362, 2024-0; matl size 0.050 by 6.000 by 60.000 in. lg; vused as filler on doubler installation, nose cowl
01-155-5659
Aircraft Former
6.500" overall length 5.500" overall width 0.063" material thickness
