01-147-0524
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-283, 7075-0 bare; matl size 0.050 by 2.000 by 6.000 in. lg; opposite to p/n 3F20235-113; used as support on lower center, fuselage station 428.50
01-147-0525
Structural Component Air Support
Used on c-141 acft. matl size 6.000 in. lg; used as support on frame installation, lower center
01-147-0526
Structural Component Air Support
Used on c-141 acft. used as support on frame installation-lower center, fuselage station 379.55
01-147-0527
Structural Component Air Support
Used on acft model c141a/c. al alloy 7075-0 per qq-a-283, 0.050 in.thk, 2.000 in.w, 6.000 in.lg, right hand, located from wl 120.0 to wl 195.0 at fuselage station 404.00
01-147-0528
Structural Component Air Support
Used on c-141 acft. matl size 4.000 in. lg; used as support on frame installation-lower center buttock line 18.00; opposite to p/n 3F202341-141
01-147-0529
Structural Component Air Support
Used on c-141 acft. matl size 4.000 in. lg; used as stiffener on frame installation-lower center buttock line 18.00; opposite to p/n 3F20234-142
01-147-0530
Structural Component Air Support
Used on c-141 acft. matl size 4.000 in. lg; opposite to p/n 3F20234-135; used as clip on frame installation-lower center waterline 12500
01-147-0531
Structural Component Air Support
Used on c-141 acft. matl size 1.000 by 60.000 in. lg; used as seal on frame installation-lower center
01-147-0532
Structural Component Air Support
Used on c-141 acft. matl size 4.000 in. lg; opposite to p/n 3F20234-136; used as clip on frame installation-lower center waterline 125.00
01-147-0537
Aircraft Former
Used on C-141. 93.000" overall length 18.000" overall width 0.056" material thickness
01-147-0538
Aircraft Former
8.000" overall length 4.000" overall width 0.050" material thickness
01-147-0539
Aircraft Former
10.000" overall length 0.680" overall width 0.063" material thickness
01-147-0541
Aircraft Former
Used on C-141. 56.000" overall length 9.000" overall width 0.050" material thickness
01-147-0546
Aircraft Former
8.000" overall length 4.000" overall width 0.050" material thickness
01-147-0548
Aircraft Stringer
56.000" overall length 10.000" overall width 0.050" material thickness
01-147-0553
Aircraft Window Panel
Used on acft model b52g. hcellulose acetate butyrate sheet tenite 2 fabricate per bac 5038, 0.040 in.thk, 5.100 in.w, 8.600 in.lg, located at station 298.25, from rbl 5.00 to lbl 5.00, used on cover installation refueling receptacle
01-147-0649
Attachment Molded Tank Flange
01-147-0650
Attachment Molded Tank Flange
0.280" hole diameter
01-147-0651
Attachment Molded Tank Flange
01-147-1526
Movable Canopy
Haz class 1.4; warning label 1.4s; un sern 0349; dot regis 8808500; net explosive weight for transportation/storage 0.025 lbs
01-147-1527
Movable Canopy
Haz class 1.4; warning label 1.4s; un sern 0349; dot regis 8808501; net explosive weight transportation/storage 0.023 lbs
01-147-1529
Canopy Forward Transparency
Transparency, canopy, fwd
01-147-1530
Canopy Aft Transparency
Transparency, canopy, aft
01-147-1596
Aircraft Pylon
01-147-1805
Structural Aircraft Plate
16.000" overall length 14.000" overall width 0.063" material thickness lid-box dim. are stock material
01-147-1806
Aircraft Beam
70.000" overall length 3.000" overall width 0.063" material thickness opp 3P61515-116
01-147-1809
Structural Aircraft Plate
3.000" overall length 2.000" overall width 0.063" material thickness filler dim. are stock material
01-147-1810
Structural Component Air Bracket
01-147-1811
Structural Component Air Support
4.000" overall length 2.000" overall width 0.050" material thickness
01-147-1812
Structural Component Air Support
4.000" overall length 2.000" overall width 0.050" material thickness
01-147-1813
Aircraft Stiffener
01-147-1835
Structural Aircraft Plate
7.000" overall length 4.000" overall width 0.050" material thickness opposite to p/n 3F20236-109
01-147-1836
Structural Aircraft Plate
7.000" overall length 4.000" overall width 0.050" material thickness opposite to p/n 3F20236-110
01-147-1837
Structural Aircraft Plate
7.000" overall length 4.000" overall width 0.050" material thickness
01-147-1838
Structural Aircraft Plate
78.000" overall length 3.000" overall width 0.063" material thickness opposite to p/n 3P61515-114; used as doubler on panel, side box structure
01-147-1839
Structural Aircraft Plate
10.000" overall length 82.25 radius; used as splice bottom
01-147-1840
Structural Aircraft Plate
10.000" overall length 83.93 radius; used as splice, bottom
01-147-1846
Structural Component Air Support
Used on acft model f-111. material per K10A128-T8511 or may be made from 2025-T851 plate but must be dimensionally identical to extrusion, 2.620 in. lg o/a
01-147-1847
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-283, 7075-0 bare; matl size 0.050 by 2.000 by 6.000 in. lg; opposite to p/n 3F20236-113; used on frame installation-lower center, fuselage station 436.50
01-147-1848
Structural Component Air Support
Used on c-141 acft. matl size 58.000 in. lg; used as cap on frame installation-lower center, fuselage
01-147-1849
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-362, 2024-0 clad; matl size 0.062 by 2.000 by 60.000 in. lg; used as retainer on frame installation, lower center, fuselage statiion 379.55
01-147-1850
Structural Component Air Support
Used on c-141 acft. matl size 69.000 in. lg; used as stiffener on frame installation, lower center forward fuselage
01-147-1851
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-287, 7075-0 clad; matl size 6.000 in. lg; used as stiffener on frame installation-lower center, forward fuselage
01-147-1878
Aircraft Former
0.050" material thickness
01-147-1879
Aircraft Former
0.050" material thickness
01-147-1880
Aircraft Former
0.050" material thickness opposite -510
01-147-1881
Aircraft Former
0.050" material thickness opposite -509
01-147-1882
Aircraft Former
Opposite -7
01-147-1883
Aircraft Former
Used on c/kc-135. 0.050" material thickness heat treated to condition T6; finish f 2.47; c/o 4 assorted stiffeners, 1 gap filler; opposite assembly p/n -508
01-147-1885
Aircraft Former
Used on A-10.
