01-207-5476
Thermal Insulation Pipe Covering
Acft c-5
01-207-6034
Fuselage Aircraft Fairing
Used on 1520-00-859-2670. 39.500" overall length
01-207-6035
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, to; 0.040 in. matl thk by 3.000 in. w by 28.000 in. lg; l cross section; prebent; left appl; w/o rivet holes
01-207-6036
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, T3; 0.025 in. matl thk by 1.500 in. w by 28.000 in. lg; l cross section; w/o rivet holes
01-207-6037
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-200/11; 2.560 in. lg; 1.100 in. w; 1.050 in. h; w/o holes; lower right position
01-207-6038
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-367 T6; primer surface treatment; 1.250 in. thk by 3.000 in. w by 3.500 in lg forging; design a alternate mfg method dwg note 3; w/o holes; right hand design
01-207-6039
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-367, T6; primer surface treatment; 1.250 in. thk by 3.000 in. w by 3.500 in. lg forging; design a alternate mfg method dwg note 4; left hand design; w/o holes
01-207-6047
Structural Aircraft Panel
01-207-6048
Structural Aircraft Panel
01-207-6049
Structural Aircraft Panel
01-207-6050
Structural Aircraft Panel
01-207-6055
Aircraft Skin
01-207-7102
Structural Component Air Support
Used on 1520-00-859-2670. aluminum alloy bell std 40-27-3; 24.800 in. lg; t cross section; w/o holes
01-207-7109
Aircraft Former
01-207-7110
Boom Stringer
Used on 1520-00-859-2670. 20.500" overall length 1.500" overall width t cross section; w/o holes; left appl
01-207-7111
Boom Stringer
Used on 1520-00-859-2670. 20.500" overall length 1.500" overall width t cross section; right appl; w/o holes
01-207-7477
Structural Aircraft Plate
01-207-7478
Structural Aircraft Plate
Used on uh-60a helicopter. matl, aluminum alloy, qq-a-250-13, comp 7075-0
01-207-7485
Aircraft Windshield Panel
01-207-8645
Access Aircraft Cover
Used on acft model b-1b. consist of 1 door, 6 coil insert, misc hardware; opposite p/n -001; nha L4302600; used on lower wing panel scavenge pump mount door assy
01-207-8735
Structural Component Air Support
Used on f-16c/d usaf aircraft. made from -7 forging, matl per qq-a-367-T73; location-duct seal-engine to inlet; eff on-178, 180, 182, 188, 190, 192, 194, 202, 204, 206, 208, 212, 220, 222, 224, 226, 228, 230, 233-9999; nha-16P3180-1
01-207-8755
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.032 in. matl thk by 4.000 in. w by 33.000 in. lg, l cross section; w/o rivet holes
01-207-8757
Structural Component Air Support
Used on f-16c/d usaf aircraft. c/o--9 support, -15 sealant (ar) , rivet (ar) ; -9 made from -7 casting, matl per ams-4218-T6; used on-rack, engine control; eff on-0178, 180, 182, 188, 190, 192, 194, 202, 204, 206, 208, 212, 214, 216, 218, 220, 222, 224, 226; nha-16P3130-1
01-207-8758
Structural Component Air Support
Used on c-130 acft. p/o flap track rib, rear beam; outer wing station 18.000
01-207-8761
Structural Aircraft Panel
01-207-8763
Aircraft Skin
01-207-8764
Boom Stringer
Used on 1520-00-859-2670. 42.000" overall length 2.300" overall width 0.050" material thickness bow shape; l cross section; left appl; w/o rivet holes
01-207-8765
Boom Stringer
Used on 1520-00-859-2670. 42.000" overall length 2.300" overall width 0.050" material thickness bow shape; l cross section; right appl; w/o rivet holes
01-208-0135
Structural Aircraft Plate
01-208-0136
Structural Aircraft Plate
01-208-0137
Structural Aircraft Plate
01-208-0138
Structural Component Air Support
Used on f-15 acft.
01-208-0139
Structural Component Air Support
Used on f-15 acft.
01-208-0140
Structural Component Air Support
Used on f-15 acft.
01-208-0141
Structural Component Air Support
Used on f-15 acft.
01-208-0142
Structural Component Air Support
Used on f-15 acft.
01-208-0143
Structural Component Air Support
Used on f-15 acft.
01-208-0144
Structural Component Air Support
Used on f-15 acft.
01-208-0145
Structural Component Air Support
Used on f-15 acft.
01-208-0146
Structural Component Air Support
Used on f-15 acft.
01-208-0147
Structural Component Air Support
Used on f-15 acft.
01-208-0153
Structural Aircraft Panel
Used on c-5a aircraft. matl - laminate-glass cloth per stm 22-302; size .030X22.0XX21.0in; part of -101a & -103a trim instl-cargo compt, fs 884.00 to 1004.00
01-208-0155
Structural Aircraft Panel
Used on c-5a aircraft. matl/size - LS34584-1X7; part of -141a
01-208-0156
Structural Aircraft Panel
01-208-0158
Longeron
Used on F-15.
01-208-0159
Longeron
Used on F-15.
01-208-0160
Longeron
Used on F-15.
01-208-0161
Longeron
Used on F-15.
01-208-0171
Aircraft Door
01-208-0456
Aircraft Floor
Used on aircraft model ca-53.
