01-149-2669			
			
				Structural Component Air Fitting			
			
				Fitting assembly, cowl latch 			
		 
			
			
			
				01-149-2679			
			
				Structural Aircraft Plate			
			
				Used on b-52 aircraft. material-cres steel aisi 321 or 347 annealed per mil-s-6721; stock size-.032 x 1.50 x 11.2"; location-sta 270.000, tail fairing installation, right hand inboard strut 			
		 
			
			
			
				01-149-2680			
			
				Structural Aircraft Plate			
			
				Location-closure rib assembly, function-web; matl 6al-4v 			
		 
			
			
			
				01-149-2681			
			
				Structural Aircraft Plate			
			
				Location-closure rib assembly; function-bearing strip; matl 6al-4v 			
		 
			
			
			
				01-149-2682			
			
				Structural Aircraft Plate			
			
				Location-closure rib assembly, function-bearing strip; matl 6al-4v 			
		 
			
			
			
				01-149-2683			
			
				Structural Aircraft Plate			
			
				Location-closure rib assembly, function-web 16; matl 6al-4v 			
		 
			
			
			
				01-149-2684			
			
				Structural Aircraft Plate			
			
				Location-closure rib assembly, function-doubler 16; matl 6al-4v 			
		 
			
			
			
				01-149-2685			
			
				Structural Aircraft Plate			
			
				Location-closure rib assembly, function-bearing strip; matl 6al-4v 			
		 
			
			
			
				01-149-2686			
			
				Structural Aircraft Plate			
			
				40.500" overall length 2.600" overall width 0.020" material thickness location-closure rib assembly; function-angle 16 			
		 
			
			
			
				01-149-2687			
			
				Structural Aircraft Plate			
			
				25.300" overall length 13.000" overall width 0.063" material thickness location-closure rib assembly, function-web 18; matl 6al-4v 			
		 
			
			
			
				01-149-2693			
			
				Aircraft Former			
			
				Used on B-52. function-chord assembly 			
		 
			
			
			
				01-149-2694			
			
				Aircraft Former			
			
				Used on B-52. function stiffener 			
		 
			
			
			
				01-149-2695			
			
				Aircraft Former			
			
				Used on B-52. function-chord assembly 			
		 
			
			
			
				01-149-2698			
			
				Aircraft Former			
			
				13.000" overall length 0.600" overall width 0.040" material thickness 			
		 
			
			
			
				01-149-2699			
			
				Aircraft Former			
			
				16.000" overall length 2.500" overall width 0.025" material thickness 			
		 
			
			
			
				01-149-2701			
			
				Aircraft Skin			
			
				Used on b-52 bomber airplane.... material;  cres sheet,  aisi 302,  comp 302 annealed,  surf cond 2n 			
		 
			
			
			
				01-149-2746			
			
				Radome			
			
				Used on c-5a aircraft. 			
		 
			
			
			
				01-149-3140			
			
				Structural Aircraft Plate			
			
				10.500" overall length 6.100" overall width 0.063" material thickness stainless steel sheet aisi 17-7 ph per bms 7-12a;  heat treat to 180, 000 to 200, 000 psi;  finish f-8.05 			
		 
			
			
			
				01-149-3141			
			
				Structural Aircraft Plate			
			
				11.000" overall length 11.000" overall width 0.080" material thickness used as doubler on installation rib number 5 			
		 
			
			
			
				01-149-3143			
			
				Structural Component Air Support			
			
				Used on uh-1f helicopter. function-support tail rotor drive 			
		 
			
			
			
				01-149-3144			
			
				Structural Component Air Bracket			
			
				1.400" overall length 2.100" overall width 0.063" material thickness clip 			
		 
			
			
			
				01-149-3145			
			
				Aircraft Frame			
			
				50.000" overall length 3.000" overall width 0.050" material thickness 			
		 
			
			
			
				01-149-3146			
			
				Structural Component Air Support			
			
				1.300" overall length 3.000" overall width 0.080" material thickness 			
		 
			
			
			
				01-149-3147			
			
				Structural Component Air Support			
			
				2.400" overall length 1.500" overall width 0.063" material thickness 			
		 
			
			
			
				01-149-3148			
			
				Structural Component Air Support			
			
							
		 
			
			
			
				01-149-3149			
			
				Structural Component Air Support			
			
				2.000" overall length 1.000" overall width 0.180" material thickness 			
		 
			
			
			
				01-149-3150			
			
				Structural Component Air Support			
			
				2.500" overall length 1.000" overall width 0.180" material thickness 			
		 
			
			
			
				01-149-3151			
			
				Structural Component Air Support			
			
				2.500" overall length 1.500" overall width 0.180" material thickness 			
		 
			
			
			
				01-149-3152			
			
				Structural Component Air Support			
			
				3.200" overall length 1.500" overall width 0.125" material thickness 			
		 
			
			
			
				01-149-3153			
			
				Structural Component Air Support			
			
							
		 
			
			
			
				01-149-3154			
			
				Structural Component Air Support			
			
				4.000" overall length 1.000" overall width 0.130" material thickness 			
		 
			
			
			
				01-149-3156			
			
				Aircraft Former			
			
				50.000" overall length 5.000" overall width 0.063" material thickness 			
		 
			
			
			
				01-149-3157			
			
				Aircraft Former			
			
				Used on B-52. 12.000" overall length 5.000" overall width 0.080" material thickness 			
		 
			
			
			
				01-149-3158			
			
				Aircraft Former			
			
				18.000" overall length 6.000" overall width 0.063" material thickness 			
		 
			
			
			
				01-149-3918			
			
				Structural Aircraft Plate			
			
				Used as filler on firewall installation 			
		 
			
			
			
				01-149-3919			
			
				Structural Aircraft Plate			
			
				5.000" overall length 1.190" overall width 0.071" material thickness 			
		 
			
			
			
				01-149-3920			
			
				Structural Aircraft Plate			
			
				5.000" overall length 1.190" overall width 0.071" material thickness 			
		 
			
			
			
				01-149-3921			
			
				Structural Aircraft Plate			
			
				3.000" overall length 0.600" overall width 0.040" material thickness used as filler on firewall installation 			
		 
			
			
			
				01-149-3922			
			
				Structural Aircraft Plate			
			
				10.000" overall length 0.500" overall width 0.032" material thickness used as doubler on firewall installation 			
		 
			
			
			
				01-149-3923			
			
				Structural Aircraft Plate			
			
				Used as doubler on firewall installation, forward nacelle;  opposite p/n 25-2308-827 			
		 
			
			
			
				01-149-3924			
			
				Structural Aircraft Plate			
			
				10.000" overall length 0.500" overall width 0.032" material thickness used as doubler on firewall installation 			
		 
			
			
			
				01-149-3925			
			
				Structural Aircraft Plate			
			
				Used as doubler on firewall installation, forward nacelle;  opposite p/n 25-2308-829 			
		 
			
			
			
				01-149-3926			
			
				Structural Aircraft Plate			
			
				Used on b-52 aircraft. material-cres sheet aisi 301 per mil-s-5059, comp d 1/4 hard-surf cond 2b; stock size .025 x 5.0 x 8.2; location-sta 236.25, tail fairing installation, right hand inboard strut 			
		 
			
			
			
				01-149-3927			
			
				Structural Aircraft Plate			
			
				5.000" overall length 3.000" overall width 2.000" material thickness 10 holes along lg w/3/16 in. dia equally spaced; opposite to p/n 3F21107-103; used as fitting-tee, frame 			
		 
			
			
			
				01-149-3928			
			
				Structural Component Air Support			
			
				Used on f-4 aircraft. used on camera beam, left hand, forward station vertical or oblique still picture camera installation 			
		 
			
			
			
				01-149-3929			
			
				Structural Component Air Support			
			
				Used on f-4 aircraft. used on camera beam, right hand, forward station vertical or oblique still picture camera installation 			
		 
			
			
			
				01-149-3930			
			
				Structural Component Air Support			
			
				2.700" overall length 2.100" overall width 0.050" material thickness opposite to p/n 29-2517-2;  used T0 support tube 			
		 
			
			
			
				01-149-3931			
			
				Structural Component Air Support			
			
				2.700" overall length 2.100" overall width 0.050" material thickness opposite to p/n 29-2517-1; used tosupport tube;  incl. nut plate 			
		 
			
			
			
				01-149-3932			
			
				Structural Component Air Support			
			
				2.600" overall length 2.200" overall width 0.050" material thickness opposite to p/n 29-2517-4;  includes nut plate, self-locking;  used to support tube 			
		 
			
			
			
				01-149-3933			
			
				Structural Component Air Support			
			
				2.600" overall length 2.200" overall width 0.050" material thickness opposite to p/n 29-2517-3; includes nut plate, self-locking; used to suppoort tube