01-162-9898
Aircraft Former
15.300" overall length 3.100" overall width 0.063" material thickness heat treat T4; finish f-2.115
01-162-9899
Aircraft Former
14.700" overall length 3.100" overall width 0.063" material thickness heat treat T4; finish f-2.115
01-162-9900
Aircraft Former
14.300" overall length 3.100" overall width 0.063" material thickness heat treat T4; finish f-2.115
01-162-9901
Aircraft Former
14.300" overall length 3.100" overall width 0.063" material thickness heat treat T4; finish f-2.115
01-162-9902
Aircraft Former
14.600" overall length 3.100" overall width 0.063" material thickness heat treat T4; finish 2.115
01-162-9904
Aircraft Skin
Used on B-52. 88.000" overall length 50.000" overall width
01-162-9905
Aircraft Skin
Used on B-52. 73.000" overall length 24.000" overall width
01-162-9906
Aircraft Skin
Used on B-52. 73.000" overall length 24.000" overall width
01-162-9908
Aircraft Skin
Used on B-52. 73.000" overall length 24.000" overall width opposite -8
01-162-9909
Aircraft Skin
Used on B-52. 73.000" overall length 24.000" overall width
01-162-9910
Fuel Aircraft Tank
Used on 700 gallon
01-163-0218
Structural Aircraft Panel
01-163-0286
Aircraft Pylon
C/o hardware, 2 skin, 1 le skin, 1 cover, 2 intercostal, 1 channel, 2 skin, 1channel, 1 closure, 1 rib assy, 1 bracketnha 16S500-895; eff on 67 2543, 2557, 2578, 2600, 2621, 2640, 2669, 2681, 2715, 2723, 2759, 2764, 2799, 2804
01-163-1576
Airframe Modification Kit
Used on f-5f aircraft.
01-163-1577
Airframe Modification Kit
Used on f-5f aircraft.
01-163-1601
Structural Aircraft Panel
Used on B-52. 88.000" overall length 50.000" overall width opposite p/n 35-8286-6; al honeycomb core perforated 3/16 hex, .0015 foil thickness type 3-15d
01-163-1602
Structural Aircraft Panel
Used on B-52. 88.000" overall length 50.000" overall width opposite p/n 35-8286-5; al honeycomb core perforated 3/16 hex, .0015 noinal foil thk type 3-15
01-163-1609
Structural Aircraft Panel
Used on KC-135. consist of one outer skin; one inner skin; one core; six doublers; four zee members; opposite p/n -626; nha 65C18229-603
01-163-1678
Structural Aircraft Panel
Used on B-52. 88.000" overall length 43.000" overall width al honeycomb core perforated 0.1875 in.hex
01-163-1679
Structural Aircraft Panel
Used on B-52. 88.000" overall length 43.000" overall width al honeycomb core perforated 0.1875 in.hex
01-163-1680
Structural Aircraft Panel
Used on f-5f aircraft. consist of one marking; six washers; three stud assembly; one aft panel
01-163-1681
Structural Aircraft Plate
1.625" overall length 0.625" overall width 0.050" material thickness used on aircraft
01-163-1683
Structural Aircraft Plate
88.000" overall length 45.000" overall width 0.020" material thickness used as doubler; opposite p/n 25-2371-13
01-163-1685
Structural Aircraft Plate
Used on acft model kc-135. al alloy clad sheet 2024-0 per qq-a-250/5; finish f-2.59; heat treated to cond T42; 7.600 in. lg, 5.500 in. w, 0.071 in. thk; nha 35-35420
01-163-1687
Structural Aircraft Plate
14.500" overall length 5.500" overall width 0.063" material thickness
01-163-1688
Structural Aircraft Plate
14.500" overall length 5.500" overall width 0.063" material thickness
01-163-1689
Structural Aircraft Plate
51 components
01-163-1690
Structural Aircraft Plate
Used on acft model b52. al clad 2024-0 per qq-a-362, 0.020 in.thk, 43.000 in.w, 88.000 in.lg, left hand, used on trailing edge, outboard strut panel assy
01-163-1691
Structural Aircraft Plate
Used on acft model b52. al clad 2024-0 per qq-a-362, 0.020 in.thk, 43.000 in.w, 88.000 in.lg, right hand, used on trailing edge, outboard strut, panel assy
01-163-1694
Structural Component Air Support
C/o: pan 35-10747-3, pad 35-10747-4, stiffener 35-10747-5, stiffener 35-10747-7, web 35-10747-803
01-163-1695
Structural Component Air Support
Used on acft model kc-135.
01-163-1696
Structural Component Air Support
Used on acft model kc-135.
01-163-1701
Structural Component Air Support
Used on acft model kc-135.
01-163-1704
Structural Component Air Support
Used on acft model kc-135.
01-163-1705
Structural Component Air Support
Used on acft model kc-135.
01-163-1708
Structural Component Air Support
Used on acft model kc-135.
01-163-1709
Structural Component Air Support
Used on acft model kc-135.
01-163-1710
Structural Component Air Support
Used on acft model kc-135.
01-163-1720
Structural Component Air Support
Used on acft model kc-135.
01-163-1721
Structural Component Air Support
Used on f-5 acft. function-support ALR46 antenna; right hand side
01-163-1722
Structural Component Air Support
01-163-1723
Structural Component Air Support
Used on f-5 acft.
01-163-1724
Structural Component Air Support
Nha 65C18500; nuclear critcl
01-163-1725
Structural Component Air Support
Nuclear critial; nha 65C18500
01-163-1726
Structural Component Air Support
Used on acft model kc-135. cfunctional description:used as fuse pin on outboard diagonal brace of nacelle strut; tolerance critical item; steel 4330m per BMS7-122, subcritical annealed to RC33 max; heat treated to hardness of RC34 plus/minus 1.5rc; 4.260-4.268 in. lg, 1.2785-1.2790 in.o.d. before plating, 1.2873-1.2885 in.o.d. after plating, .821-.823 in.i.d. before plating; counterbored ea end to .870-.880 in.i.d., .330 in.depth; chamfer 0.080 by 15 deg both ends; nha 65C18500;
01-163-1727
Structural Component Air Support
Nha 65C18500; nuclear critical
01-163-1728
Structural Component Air Support
Used on f-15 acft. function-support beam; location-pylon inboard, lower
01-163-1733
Movable Canopy
Haz class 1.4; warning label 1.4s; un sern 0349; dot regis 8808502; net explosive weight transportation/storage 0.023 lbs
01-163-1734
Aircraft Former
Used as an angle
01-163-1735
Aircraft Former
16.300" overall length 3.100" overall width 0.063" material thickness heat treat T4; finish f-2.115
