01-151-6659
Structural Component Air Support
4.700" overall length 3.900" overall width 0.040" material thickness
01-151-6660
Structural Component Air Support
2.600" overall length 1.600" overall width 0.040" material thickness
01-151-6661
Structural Component Air Support
4.000" overall length 3.000" overall width 1.200" material thickness
01-151-6662
Structural Component Air Support
9.210" overall length 4.880" overall width
01-151-6663
Structural Component Air Support
4.400" overall length 2.550" overall width 0.040" material thickness
01-151-6664
Structural Component Air Support
4.400" overall length 2.550" overall width 0.040" material thickness
01-151-6665
Structural Component Air Support
2.480" overall length 2.150" overall width 2.300" material thickness used on remote trimmer adapter, turbo-fan engines
01-151-6666
Structural Component Air Support
2.700" overall length 2.400" overall width 2.400" material thickness used on remote trimmer adapter turbo-engines
01-151-6667
Structural Component Air Support
01-151-6668
Structural Component Air Support
01-151-6669
Structural Component Air Support
01-151-6670
Structural Component Air Support
01-151-6671
Structural Component Air Support
01-151-6672
Structural Component Air Support
Titanium; opposite 35-8226-165
01-151-6673
Structural Component Air Support
6.300" overall length 2.200" overall width 0.032" material thickness pure titanium mil-t-9046c; finish f-10.10; opposite -864
01-151-6674
Structural Component Air Support
6.300" overall length 2.200" overall width 0.032" material thickness pure titanium mil-t-9046c, class c; finish f-10.10; opposite -863
01-151-6675
Structural Component Air Support
5.700" overall length 2.800" overall width 0.032" material thickness pure titanium mil-t-9046c, class c; finish f-10.10; opposite -866
01-151-6676
Structural Component Air Support
5.700" overall length 2.800" overall width 0.032" material thickness pure titanium mil-t-9046c, class c; finish f-10.10; opposite -865
01-151-6677
Structural Component Air Support
01-151-6678
Structural Component Air Support
Used on c-141a/c acft. matl al alloy, qq-a-362, 2024-0; matl size 0.071 by 6.000 by 8.000 in. lg; opposite to p/n 3F20294-103; used as intercostal, jack pad on fuselage station 351.40
01-151-6683
Aircraft Former
Used on b-52 acft.
01-151-6684
Aircraft Former
Used on b-52 acft.
01-151-6685
Aircraft Former
Used on b-52 acft.
01-151-6686
Aircraft Former
Used on b-52 acft.
01-151-6687
Aircraft Former
Used on b-52 acft.
01-151-6688
Aircraft Former
Used on b-52 acft. opposite 35-8226-105
01-151-6689
Aircraft Former
Used on b-52 acft. opposite 35-8226-108
01-151-6690
Aircraft Former
Used on b-52 acft. opp 35-8226-107
01-151-6691
Aircraft Former
Used on b-52 acft. opposite 35-8226-110
01-151-6692
Aircraft Former
Used on b-52 acft. opposite 35-8226-109
01-151-6693
Aircraft Former
Used on b-52 acft.
01-151-6694
Aircraft Former
Used on b-52 acft.
01-151-6695
Aircraft Former
Used on b-52 acft.
01-151-6696
Aircraft Former
1.400" overall length 0.600" overall width 0.050" material thickness
01-151-6697
Aircraft Former
Used on b-52 acft. heat treat T4
01-151-6698
Aircraft Former
Used on b-52 acft. opposite 35-8226-170
01-151-6699
Aircraft Former
Used on b-52 acft. opposite 35-8226-169
01-151-6700
Aircraft Former
17.000" overall length 4.500" overall width 0.063" material thickness finishf-10.10; used as channel
01-151-6701
Aircraft Former
17.000" overall length 4.500" overall width 0.063" material thickness
01-151-6702
Aircraft Former
Used on acft model b-52. 21.500" overall length made from bac-1490-2668
01-151-6703
Aircraft Former
4.700" overall length 1.500" overall width 0.032" material thickness opposite -63
01-151-6704
Aircraft Former
6.000" overall length 3.300" overall width 0.032" material thickness opposite -867
01-151-6705
Aircraft Former
6.000" overall length 3.300" overall width 0.032" material thickness opposite -862
01-151-6706
Aircraft Former
18.000" overall length 4.500" overall width 0.063" material thickness heat treat 180, 000-200, 000; opposite -870
01-151-6707
Aircraft Former
18.000" overall length 4.500" overall width 0.063" material thickness heat treat 180, 000-200, 000; opposite -869
01-151-6708
Aircraft Former
3.600" overall length 3.400" overall width 0.032" material thickness opposite -872
01-151-6709
Aircraft Former
0.700" overall length 0.600" overall width 0.040" material thickness finish f-2.115
01-151-6710
Aircraft Former
0.600" overall length 0.600" overall width 0.025" material thickness finish f-12.209
01-151-6711
Aircraft Former
10.000" overall length 3.200" overall width 0.032" material thickness finish f-10.00; opp -877
01-151-6712
Aircraft Former
10.000" overall length 3.200" overall width 0.032" material thickness finish f-10.00; opp -876
