01-154-4965
Structural Aircraft Plate
5.000" overall length 1.400" overall width 0.032" material thickness do not use cadmium plated tools on this item
01-154-4966
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 -2051; used as bearing plate
01-154-4968
Structural Component Air Support
7.500" overall length 5.100" overall width 0.063" material thickness opp 35-15322-51; used as intercostal-45 deg skin splice, lower
01-154-4969
Structural Component Air Support
9.700" overall length 1.400" overall width 1.500" material thickness used as fitting-intercostal, rh lower body cowl
01-154-4970
Structural Component Air Support
Forge per mil-F07190 grade a
01-154-4971
Structural Component Air Support
5.900" overall length 2.400" overall width forged billet 4340
01-154-4972
Structural Component Air Support
5.900" overall length 2.400" overall width forged billet
01-154-4973
Structural Component Air Support
Bl 0.000; lefthand
01-154-4974
Structural Component Air Support
13.000" overall length 6.000" overall width 0.032" material thickness matl: al aly clad sht; 0 temp, ht T4; fin: f-2.115; opp -804
01-154-4975
Structural Component Air Bracket
1.800" overall length 1.400" overall width 0.040" material thickness part of: nose cowl anti-icing duct support; matl: cres st sht, aisi 17-7ph; ht: 150, 000 to 170, 000psi; fin: srf-12.206 opt to f-1.1929; dimensions listed are stock size
01-154-4976
Structural Component Air Support
Used on acft model b52. steel 4340 per mil-s-5000, forge per mil-f-7190 grade a, left hand, located at station 138.25, used on upper body cowl
01-154-4977
Structural Component Air Support
Forge per mil-f-7190 grade a, tensile test not required
01-154-4978
Structural Component Air Support
Forge per mil-f-7190 grade a, tensile test not req., right hand
01-154-4979
Structural Component Air Support
Forge per mil-f-7190 grade a, tensile test not required
01-154-4980
Structural Component Air Support
1.700" overall length 1.400" overall width 0.040" material thickness
01-154-4981
Structural Component Air Support
1.700" overall length 1.400" overall width 0.040" material thickness
01-154-4982
Structural Component Air Support
3.000" overall length 2.500" overall width 0.063" material thickness
01-154-4983
Structural Component Air Support
3.000" overall length 2.500" overall width 0.063" material thickness
01-154-4984
Structural Component Air Support
1.800" overall length 1.500" overall width 0.063" material thickness
01-154-4985
Structural Component Air Support
3.000" overall length 0.700" overall width 0.063" material thickness
01-154-4986
Structural Component Air Support
3.000" overall length 0.700" overall width 0.063" material thickness
01-154-4987
Structural Component Air Support
6.500" overall length 2.500" overall width forge per 7190 grade a excpt tensile test not required; at bl 12
01-154-4993
Aircraft Former
Used on B-52. opposite pn 35-8642-59
01-154-4994
Aircraft Former
3.500" overall length opp pn 35-8682-18; extrusion
01-154-4995
Aircraft Former
3.500" overall length opp pn 35-8682-17; extrusion
01-154-4996
Aircraft Former
Used on B-52. opposite pn 35-8682-4
01-154-4997
Aircraft Former
58.000" overall length 4.000" overall width 0.040" material thickness heat treated 180, 000 to 200, 000 psi; opposite pn -2030
01-154-4998
Aircraft Former
58.000" overall length 4.000" overall width 0.040" material thickness heat treated 180, 000 to 200, 000 psi; opposite pn -2029
01-154-4999
Aircraft Former
58.000" overall length 5.000" overall width 0.040" material thickness heat treated 180, 000 to 200, 000 psi; oppposite pn -2031
01-154-5001
Aircraft Former
58.000" overall length 3.500" overall width 0.040" material thickness heat treated 180, 000 to 200, 000 psi; opposite pn -2033
01-154-5002
Aircraft Former
58.000" overall length 5.000" overall width 0.040" material thickness heat treated 180, 000 to 200, 000 psi; opposite pn -2040
01-154-5003
Aircraft Former
7.000" overall length 6.000" overall width 0.040" material thickness heat treated T4; finish f-2.10
01-154-5004
Aircraft Former
58.000" overall length 5.000" overall width 0.040" material thickness finish f-8.05; heat treated 180, 000-200, 000 psi; opposite pn -2039
01-154-5005
Aircraft Former
55.000" overall length 3.500" overall width 0.040" material thickness finish f-8.05; heat treated 180, 000-200, 000 psi; opposite pn -2041
01-154-5006
Aircraft Former
53.000" overall length 2.000" overall width 0.080" material thickness
01-154-5007
Aircraft Former
89.000" overall length 2.100" overall width 0.080" material thickness
01-154-5008
Aircraft Former
89.000" overall length 2.100" overall width 0.080" material thickness
01-154-5009
Aircraft Former
01-154-5010
Aircraft Former
Used on B-52. AND10135-1002 x 39.5
01-154-5011
Aircraft Former
Used on B-52. 0.063" material thickness 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-5014
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-5015
Aircraft Former
Used on B-52. 0.040" material thickness 17-7ph, annealed, heat treated 180, 000 to 200, 000 psi
01-154-5016
Aircraft Former
10.700" overall length 1.600" overall width 0.040" material thickness function-angle
01-154-5017
Aircraft Former
10.700" overall length 1.600" overall width 0.040" material thickness function-angle
01-154-5018
Aircraft Former
12.600" overall length 1.600" overall width 0.040" material thickness function-angle
01-154-5019
Aircraft Former
12.600" overall length 1.600" overall width 0.040" material thickness function-angle
01-154-5020
Aircraft Former
12.600" overall length 1.600" overall width 0.040" material thickness function-angle
01-154-5021
Aircraft Former
14.800" overall length 1.200" overall width 0.020" material thickness function-angle
01-154-5022
Aircraft Former
2.200" overall length 1.600" overall width 0.032" material thickness function-angle
01-154-5023
Aircraft Former
4.100" overall length 1.400" overall width 0.025" material thickness function-angle
