01-149-3934
Structural Component Air Support
2.500" overall length 2.300" overall width 0.050" material thickness opposite to p/n 29-2517-6; used tosupport tube; includes nut plate, self-locking
01-149-3935
Structural Component Air Support
Channel 1 ea p/n 26-5306-1, guardstrip 1 ea p/n 26-5306-2
01-149-3936
Structural Component Air Support
16.000" overall length from nac wl 124.640 to nac wl 141.319, nac bl 0.00, nac sta 287.467
01-149-3937
Structural Component Air Support
16.000" overall length nac wl 124.640 to nac wl 141.319, nac BL0.00, nac sta 287.467
01-149-3944
Aircraft Former
Used on B-52. function-chord assy
01-149-3945
Aircraft Former
Used on B-52. function stiffener assembly
01-149-3947
Aircraft Former
4.600" overall length 3.600" overall width 0.032" material thickness
01-149-3949
Aircraft Former
4.600" overall length 3.600" overall width 0.036" material thickness
01-149-3950
Aircraft Former
1.500" overall length 0.500" overall width 0.028" material thickness
01-149-3951
Aircraft Former
6.000" overall length 5.000" overall width 0.062" material thickness
01-149-3953
Aircraft Former
3.000" overall length 2.000" overall width 0.036" material thickness
01-149-3954
Aircraft Former
6.700" overall length 1.800" overall width 0.050" material thickness
01-149-3956
Aircraft Former
1.800" overall length 1.100" overall width 0.050" material thickness
01-149-3958
Aircraft Former
3.000" overall length 0.800" overall width 0.050" material thickness opposite to 35-7495-531
01-149-3959
Aircraft Former
Used on B-52.
01-149-3960
Aircraft Former
5.700" overall length 2.100" overall width 0.040" material thickness commericially pure, do not use cadmium plated tools on this item
01-149-3961
Aircraft Former
9.300" overall length 1.400" overall width 0.040" material thickness do not use cadmium plated tools on this item; commercially pure
01-149-3962
Aircraft Former
3.800" overall length 1.600" overall width 0.040" material thickness commercially pure; do not use cadmium plated tools on this item
01-149-3963
Aircraft Former
3.800" overall length 1.600" overall width 0.040" material thickness commercially pure; do not use cadmium tools on this item
01-149-3965
Aircraft Skin
Used on b-52 bomber airplane....
01-149-3966
Aircraft Skin
Used on b-52 aircraft. amaterial-cres sheet aisi 302 per mil-s-5059 comp 302 annealed, surf cond 2d; stock size..025 x 15 x 35"; location-bl 0.00 on -509
01-149-4691
Structural Component Aircraf Web
14.000" overall length 13.000" overall width 0.050" material thickness
01-149-4697
Structural Aircraft Plate
Used on b-52 aircraft. material-cres sheet aisi 302 per mil-s-5059 comp 302 annealed, surf cond 2d; stock size-.040 x 1.3 x 2.3"; location-pp sta 236.25, tail fairing installation, right hand inboard strut
01-149-4698
Structural Aircraft Plate
Used on b-52 aircraft. material-cres sheet aisi 302 per mil-s-5059, comp 302 annealed, surf cond 2d; stock size .040 x 1.32 x 4.5"; location-sta 236.25, tail fairing installation, right hand inboard strut
01-149-4699
Structural Aircraft Plate
Used on b-52 aircraft. material-cres sheet aisi 302 per mil-s-5059, comp 302 annealed, surf cond 2d; stock size-.040 x 1.32 x 3.4"; location-tail fairing installation-right hand inboard strut
01-149-4702
Structural Aircraft Plate
4.500" overall length 2.300" overall width 0.080" material thickness location-rib number 2 installation
01-149-4703
Structural Aircraft Plate
26.000" overall length 3.000" overall width 0.063" material thickness used as doubler on installation rib number 5
01-149-4705
Structural Component Air Support
01-149-4706
Structural Component Air Support
01-149-4707
Structural Component Air Support
01-149-4708
Structural Component Air Support
01-149-4709
Structural Component Air Support
01-149-4710
Structural Component Air Support
01-149-4711
Structural Component Air Support
3.500" overall length 2.300" overall width 0.050" material thickness soft steel sheet 17-7ph BMS7-12
01-149-4712
Structural Component Air Support
10.000" overall length 3.200" overall width 0.032" material thickness commercially pure sheet; class 6; opposite p/n -144
01-149-4713
Structural Component Air Support
10.000" overall length 3.200" overall width 0.032" material thickness rh inboard/outboard sturt fairings; opp. p/n -143; class 6; fin.f-10.10
01-149-4714
Structural Component Air Support
10.000" overall length 3.600" overall width 0.032" material thickness opposite p/n -146; class 6; finish f-10.10
01-149-4715
Structural Component Air Support
10.000" overall length 3.600" overall width 0.032" material thickness class 6; finish f-10.10; opposite p/n -145
01-149-4716
Aircraft Fairing
10.000" overall length 17.300" overall width 0.050" material thickness
01-149-4726
Structural Component Air Bracket
Clip finish f-2.30; make from AND10136-2407 spec material; opp -12
01-149-4727
Aircraft Former
Used on B-52.
01-149-4731
Aircraft Former
12.100" overall length 0.600" overall width 0.016" material thickness finish f-2.115
01-149-4732
Aircraft Former
3.800" overall length 3.000" overall width 0.080" material thickness function-clip
01-149-4733
Aircraft Former
Opposite -560
01-149-4734
Aircraft Skin
Used on b-52 aircraft. opposite -533; material-cres sheet aisi 302 per mil-s-5059, comp 302 annealed, surf cond 2d; used on--1, -509
01-149-4735
Aircraft Skin
Used on acft model b-52. commercially pure titanium sheet per mil-t-9046 class 7; finish f-10.10; 80.000 in. lg, 13.000 in. w, 0.025 in. thk; opposite p/n -140
01-149-4736
Aircraft Skin
Used on acft model b-52. commercially pure titanium sheet per mil-t-9046 class 7; finish f-10.10; 80.000 in. lg, 13.000 in. w, 0.025 in. thk; opposite p/n -139
01-149-6376
Access Aircraft Cover
Used on b-52 aircraft. 0.218" hole diameter on torque bulkhead installation- inboard strut
01-149-6406
Structural Component Air Fitting
Forge per mil-f-7190
01-149-6412
Structural Aircraft Plate
10.100" overall length 4.000" overall width 0.050" material thickness opposite -9; used as longeron splice
