01-163-1736
Aircraft Former
16.100" overall length 3.100" overall width 0.063" material thickness heat treat T4; finish 2.115
01-163-1737
Aircraft Former
16.400" overall length 3.100" overall width 0.063" material thickness heat treat T4; finish 2.115
01-163-1738
Aircraft Former
10.500" overall length 3.500" overall width 0.065" material thickness
01-163-1739
Aircraft Former
2.700" overall length 1.300" overall width 0.063" material thickness
01-163-1742
Aircraft Skin
Used on B-52. 88.000" overall length 50.000" overall width opposite p/n 35-8286-7
01-163-1745
Aircraft Skin
Used on B-52. 88.000" overall length 43.000" overall width
01-163-1746
Aircraft Skin
Used on B-52. 88.000" overall length 43.000" overall width
01-163-1748
Aircraft Skin
Used on B-52. 99.000" overall length 43.000" overall width
01-163-1749
Aircraft Skin
Used on F-15. functions as sideplate
01-163-1751
Aircraft Window Panel
Used on acft model kc-135. heat resistant plastic sheet per mil-p-5425a, finish a; finish f-6.10; 4.700 in. lg, 4.700 in. w, 0.250 in. thk; nha 65C18229-603
01-163-1752
Aircraft Windshield Panel
Used on f-5f aircraft. used on forward aircraft, components-panel, ramp, filler-side 2, filler forward 1, facing 6, filler 1
01-163-4415
Structural Component Air Support
Used on b-52 aircraft. on hinge, base line 12, sta 138.25, upper body cowl; material-4340 steel per mil-s-5000, heat treated 180, 000 to 200, 000 psi ult; nickle plated
01-163-4416
Structural Component Air Support
Used on acft model b-52. steel forging per 4340 mil-s-5000
01-163-4422
Aircraft Former
7.600" overall length 3.900" overall width 0.063" material thickness heat treat T4; finish f-2.22
01-163-4423
Aircraft Former
7.700" overall length 4.100" overall width 0.063" material thickness heat treat T4; finish 2.22
01-163-4424
Aircraft Former
7.500" overall length 4.100" overall width 0.063" material thickness heat treat T4; finish f-2.22
01-163-4425
Aircraft Former
7.600" overall length 3.900" overall width 0.063" material thickness heat treat T4; finish f-2.22
01-163-4426
Aircraft Former
7.600" overall length 4.100" overall width 0.063" material thickness heat treat T4; finish 2.22
01-163-5182
Aircraft Windshield Panel
01-163-5209
Access Aircraft Door
Used on aircraft model f-18.
01-163-5388
Structural Component Air Fitting
Used on sh-60b helo.
01-163-5486
Fluid Aircraft Manifold
01-163-5487
Fluid Aircraft Manifold
01-163-6069
Aileron
Used on aircraft model f-18. cognizant service:navy;
01-163-6070
Aileron
Used on aircraft model f-18. cognizant service:navy;
01-163-6071
Aileron
Used on aircraft model f-18. cognizant service:navy;
01-163-6072
Aileron
Used on aircraft model f-18. cognizant service:navy;
01-163-6074
Horizontal Stabilizer
Used on aircraft model f-18. cognizant service:navy;
01-163-6075
Horizontal Stabilizer
Used on aircraft model f-18. cognizant service:navy;
01-163-6565
Access Aircraft Cover
Used on f-15 acft.
01-163-6703
Structural Component Air Support
Used on f-5f aircraft. 2.750" overall length 0.500" overall width 0.040" material thickness
01-163-6706
Structural Aircraft Plate
Used on c-5b aircraft. outboard, aft ramp; matl-15-5ph ams 5659; dimensions-11.870 in. lg, 2.250 in. w, 0.500 in. w
01-163-6707
Structural Aircraft Plate
Used on c-5b aircraft. outboard, aft ramp; matl-15-5 ph ams 5659; dimensions-11.370 in. lg, 2.250 in. w, 0.500 in. thk
01-163-6743
Aircraft Skin
Used on F-16. kit for all dash numbers this drawing, all layers
01-163-6744
Aircraft Skin
Used on F-16. kit for all dash numbers this drawing, all layers
01-163-6745
Aircraft Skin
Used on F-16. kit for all dash numbers this drawing, all layers
01-163-6746
Aircraft Skin
Used on F-16. kit for all dash numbers this drawing, all layers
01-163-6747
Aircraft Skin
Used on F-16. kit for all dash numbers this drawing, all layers
01-163-6750
Structural Aircraft Panel
Used on B-52. 74.000" overall length 26.000" overall width honeycomb core-perforated 3/16 he .0015 foil thickness, type 3-15d 5052 H38 or H39 per bms 4-4 type iic per mil-c-7438b; opposite -17
01-163-6764
Structural Aircraft Panel
Used on B-52. 74.000" overall length 26.000" overall width aluminum honeycomb core perforated 3/16 hex, type ii c; per mil-c-7438 b
01-163-6765
Structural Aircraft Panel
Used on B-52. 74.000" overall length 26.000" overall width aluminum honeycomb core perforated 3/16 hex, type ii c per mil-c-7438 b; opposite -819
01-163-6766
Structural Aircraft Panel
Used on B-52. 65.000" overall length 28.000" overall width aluminum honeycomb core perforated 3/16 hex, type ii c per mil-c-7438 b
01-163-6767
Structural Aircraft Panel
Used on B-52. 65.000" overall length 28.000" overall width aluminum honeycomb core perforated 3/16 hex, type ii c per mil-c-7438 b, opposite -833
01-163-6768
Structural Aircraft Panel
Used on B-52. 66.000" overall length 30.000" overall width aluminum honeycomb core perforated 3/16 hex, type ii c per mil-c-7438 b, ABNMJAA0.526
01-163-6769
Structural Aircraft Panel
66.000" overall length 30.000" overall width opp -835; alum honeycomb core
01-163-6796
Structural Aircraft Panel
Used on B-52. 88.000" overall length 45.000" overall width honeycomb core
01-163-6797
Structural Aircraft Panel
Used on B-52. 88.000" overall length 45.000" overall width honeycomb core
01-163-6798
Structural Aircraft Plate
2.900" overall length 1.000" overall width 0.190" material thickness 4335 mod steel; used as pad on fitting
