01-162-7492
Structural Component Air Support
Used on acft model kc-135.
01-162-7493
Structural Component Air Support
Used on acft model kc-135.
01-162-7494
Structural Component Air Support
Used on acft model kc-135.
01-162-7495
Structural Component Air Support
Used on acft model kc-135. inconel 625 sheet per AMS5599, annealed; finish f-25.01; 0.063 in. thk; contains 2 0.285 in. dia. mounting holes in base; 4 0.140 in. dia holes for connector attachment; nha 39-28100-1
01-162-7498
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-362, 2024-T3; 5.000 in. w; includes tab, 2; miscellaneous hardware used as fitting on jack pad adapter on fuselage station 1058
01-162-7512
Aircraft Former
7.000" overall length 5.400" overall width 0.063" material thickness
01-162-7513
Aircraft Former
5.500" overall length 4.800" overall width 0.063" material thickness
01-162-7514
Aircraft Former
5.500" overall length 4.800" overall width 0.063" material thickness
01-162-7515
Aircraft Former
80.000" overall length 45.000" overall width 0.040" material thickness opp -28; temper T3
01-162-7516
Aircraft Former
80.000" overall length 45.000" overall width 0.040" material thickness opp -27; tempered T3
01-162-7522
Airfoil Rib
25.500" overall length 19.000" overall width 0.080" material thickness
01-162-7523
Airfoil Rib
22.500" overall length 3.500" overall width 0.040" material thickness
01-162-7524
Airfoil Rib
22.500" overall length 3.500" overall width 0.040" material thickness
01-162-7526
Aircraft Skin
Used on B-52. 8.000" overall length 48.000" overall width
01-162-7529
Aircraft Skin
Used on B-52. 88.000" overall length 48.000" overall width opposite p/n 35-8236-19
01-162-7532
Aircraft Skin
Used on B-52. 64.000" overall length 28.000" overall width
01-162-7533
Aircraft Skin
Used on B-52. 64.000" overall length 28.000" overall width opposite -29
01-162-7534
Aircraft Skin
Used on B-52. 65.000" overall length 29.000" overall width opposite -32
01-162-7535
Aircraft Skin
Used on B-52. 65.000" overall length 29.000" overall width opposite -31
01-162-7536
Aircraft Window Panel
01-162-7537
Aircraft Window Panel
01-162-8130
Airframe Modification Kit
Used on uh-60 series helicopters.
01-162-9866
Structural Aircraft Panel
Used on B-52. 74.000" overall length 26.000" overall width al honeycomb core
01-162-9867
Structural Aircraft Panel
Used on B-52. 74.000" overall length 26.000" overall width
01-162-9868
Structural Aircraft Plate
2.500" overall length 2.000" overall width 0.050" material thickness opposite pn 35-8648-802; used as angle
01-162-9869
Structural Aircraft Plate
6.000" overall length 11.000" overall width 0.080" material thickness opposite to p/n 39-9920-14; used as web, forward
01-162-9870
Structural Aircraft Plate
6.000" overall length 11.000" overall width 0.080" material thickness opposite to p/n 39-9920-13; used as web, forward
01-162-9871
Structural Aircraft Plate
6.000" overall length 16.000" overall width 0.063" material thickness opposite to p/n 39-9920-16; used as web, aft inboard
01-162-9872
Structural Aircraft Plate
6.000" overall length 16.000" overall width 0.063" material thickness opposite to p/n 39-9920-15; used as web, aft inboard
01-162-9873
Structural Aircraft Plate
10.200" overall length 6.000" overall width 0.080" material thickness opposite to p/n 39-9921-09; used as web, fwd
01-162-9874
Structural Aircraft Plate
14.500" overall length 5.500" overall width 0.063" material thickness opposite 39-9921-12; used as web aft
01-162-9875
Structural Aircraft Plate
14.500" overall length 5.500" overall width 0.063" material thickness opposite to p/n 39-9921-11; used as web aft
01-162-9876
Structural Aircraft Plate
14.000" overall length 5.500" overall width 0.065" material thickness opposite to p/n 39-9921-14; used as web aft
01-162-9877
Structural Aircraft Plate
3.700" overall length 1.800" overall width 0.063" material thickness opposite pn 39-9921-28; used as clip aft
01-162-9878
Structural Aircraft Plate
3.700" overall length 1.800" overall width 0.063" material thickness opposite pn 39-9921-27; used as clip aft
01-162-9879
Structural Aircraft Plate
10.200" overall length 6.000" overall width 0.080" material thickness opposite 39-9921-8
01-162-9880
Structural Aircraft Plate
10.200" overall length 6.000" overall width 0.080" material thickness opposite to p/n 39-9921-7; used as web fwd
01-162-9881
Structural Aircraft Plate
10.200" overall length 6.000" overall width 0.080" material thickness opposite to p/n 39-9921-10; used as web fwd
01-162-9884
Structural Aircraft Plate
10.500" overall length 5.500" overall width 0.080" material thickness
01-162-9885
Structural Aircraft Plate
10.500" overall length 5.500" overall width 0.080" material thickness
01-162-9886
Structural Aircraft Plate
3.600" overall length 1.800" overall width 0.063" material thickness opposite to p/n 39-9921-30; used as clip
01-162-9887
Structural Aircraft Plate
3.600" overall length 1.800" overall width 0.063" material thickness opposite to p/n 39-9921-29; used as clip
01-162-9889
Structural Component Air Support
1.625" overall length 1.750" overall width 0.063" material thickness
01-162-9890
Structural Component Air Support
2.000" overall length 3.500" overall width 0.063" material thickness
01-162-9891
Structural Component Air Support
1.500" overall length opposite 39-9921-802
01-162-9892
Structural Component Air Support
1.500" overall length opposite 39-9921-801
01-162-9893
Structural Component Air Support
Used on acft model b-1b. used on avionics recirc system, located at station yf 512.125, rh
01-162-9895
Aircraft Former
41.000" overall length
01-162-9896
Aircraft Former
10.500" overall length 3.500" overall width 0.063" material thickness
01-162-9897
Aircraft Former
15.900" overall length 3.100" overall width 0.063" material thickness heat treat T4; finish f-2.115
