01-204-7548
Structural Aircraft Panel
Used on acft model b-1b. epoxy glass sheet, type iv grade g-11 per l-p-509; 71.00 in. long, 29.88 in. wide, 0.062 in. thick
01-204-7551
Aircraft Former
5.000" overall length
01-204-7552
Aircraft Former
01-204-7553
Aircraft Former
01-204-7554
Aircraft Former
01-204-7555
Aircraft Former
01-204-7556
Aircraft Former
01-204-7557
Aircraft Former
01-204-7559
Aircraft Former
01-204-7560
Aircraft Former
01-204-7561
Aircraft Former
01-204-7562
Aircraft Former
Fairing assy-missile launcher
01-204-7563
Aircraft Former
Fairing assy-missile launcher
01-204-7566
Longeron
Used on F-15.
01-204-7568
Longeron
Used on F-15.
01-204-7569
Longeron
Used on F-15.
01-204-7574
Aircraft Skin
Used on F-15.
01-204-7575
Aircraft Stringer
66.000" overall length
01-204-7580
Thermal Special Purpo Insulation
Hc/o 385 facesheet, inner, qq-s-766, cres foil, alloy 321, cond a, 10.000 in.l by 0.002 in.thk by 9 in.w; 387 facesheet, outer, same matl, 10.000 in.l by 0.002 thk by 9.000 w; 389 retainer, ribbon, same matl, 22.000 in.l by 0.0005 in.thk by 1.000 in.w; 393 batt crf-800 blanket, 8 lb/FT3, 10.000 in.l by 0.125 in.thk by 9.000 in.w; 395 ident plate, 2.750 in.l by 0.008 in.thk by 1.000 in.w; location nac, apu compt, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-7581
Thermal Special Purpo Insulation
C/o 253 facesheet, inner, qq-s-766, cres foil, alloy 321, cond a, 22.000 in.l by 0.002 in.by 11.000 in.w; 255 facesheet, outer, same matl, 22.000 in.l by 0.002 in.thk by 11.000 in.w; 257 retainer, ribbon, same matl, 68.000 in.l by 0.0005 in.thk by 1.000 in.w; 259 batt crf-800 blanket, 8 lb/FT3, 22.000 in.l by 0.125 in.thk by 11.000 in.w; 263 ident plate, grommet (8) ; location nac, apu compt, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-7583
Thermal Special Purpo Insulation
Gc/o 083 facesheet, inner, qq-s-766 cres foil, alloy 321, cond a, 23.000 in.l by 0.002 in.thk by 20.000 in.w; 085 facesheet, outer, same matl, 23.000 in.l by 23.000 in.l by 0.002 in.thk by 20.000 in.w; 087 retainer, ribbon, same matl, 100.000 in.l by 0.0005 in.thk by 1.000 in.w; 089 batt crf-800 blanket, 8 lb/ft, 23.000 in.l by 0.125 in.thk by 20.000 in.w; 093 ident plate, grommet (16) ; location nac, apu compt, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-7584
Thermal Special Purpo Insulation
C/o 213 facesheet, inner, qq-s-766 cres foil, alloy 321, cond a; 20.000 in.l by 0.002 in.by 12.000 in.w; 215 facesheet, outer, same matl; 80.000 in.l by 0.0005 by 1.000 in.w; 219 batt crf-800 blanket, 8 lb/FT3, 12.000 in.l by 0.125 in.thk by 11.000 in.w; 223 ident plate, grommet (3) ; location nac, apu compt, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-7585
Thermal Special Purpo Insulation
C/o 214 facesheet, inner, qq-s-766 cres foil, alloy 321, cond a, 20.000 in.l by 0.002 in.thk by 12.000 in.w; 216 facesheet, outer, same matl, 20.000 in.l by 0.002 in.thk, by 12.000 in.w; 218 retainer ribbon same matl, 80.000 in.l by 0.0005 in.thk by 1.000 in.w; 220 batt crf-800 blanket, 8 lb/FT3, 12.000 in.l by 0.125 in.by 11.000 in.w; 225 ident plate, grommet 3; location nac, apu compt, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-7586
Thermal Special Purpo Insulation
C/o 239 facesheet, inner, qq-s-766 cres foil, alloy 321, cond a, 26.000 in.l by 0.002 in.thk by 11.000 in.w; facesheet, outer, same matl, 26.000 in.l by 0.002 in.thk by 11.000 in.w; 245 retainer, ribbon, same matl, 63.000 in.l by 0.0005 in.thk by 1.000 in.w; 247 batt crf-800 blanket, 8 lb/FT3, 26.000 in.l by 0.125 in.thk by 11.000 in.w; 249 ident plate, grommet (10) ; location nac, apu compt, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-7587
Thermal Special Purpo Insulation
C/o 254 facesheet, inner, qq-s-766, cres foil, alloy 321, cond a, 22.000 in.l by 0.002 in.thk by 11.000 in.w; 256 facesheet, outer, same matl, 22.000 in.l by 0.002 in thk by 11.000 in.w; 258 retainer, ribbon, same matl, 68.000 in.l by 0.0005 by 1.000 in.w; 260 batt crf-800 blanket, 8 lb/FT3, 22.000 in.l by 0.125 in.thk by 11.000 in.w; 263 ident plate, grommet (8) ; location nac, apu compt, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-9278
Aircraft Fairing
01-204-9647
Structural Aircraft Plate
Used on acft model kc-135. 2024-0 sheet per qq-a-250/4; heat treat T4; 9.00 in lg, 3.35 in wd, 0.071 in thk; finish srf -2.30
01-204-9648
Structural Aircraft Plate
Used on acft model kc-135.
01-204-9649
Structural Aircraft Plate
Used on acft model kc-135.
01-204-9650
Structural Aircraft Plate
Used on acft model kc-135.
01-204-9651
Structural Aircraft Plate
Used on acft model kc-135.
01-204-9652
Structural Aircraft Plate
01-204-9653
Structural Component Air Support
Used on acft model b-1b. corrosion resistant steel PH13-8M0 per AMS5629; 2.750 in. lg, 1.750 in. w, 0.275 in. thk at base; 4 0.281 in. dia holes in base also 0.871 in. dia projection bottom of base 0.26 in. thk; 2 holes upper mount 0.2610 in. dia, csk 120 deg by 0.29 in. dia, tap special thread .2500-28; nha L8700201-101
01-204-9654
Structural Component Air Support
Used on f-15 acft. closure, lower-forward box, vertical stabilizer
01-204-9655
Structural Component Air Support
Used on f-15 acft. closure, lower-forward box, vertical stabilizer
01-204-9656
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9657
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9658
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9659
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9660
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9661
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9662
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9663
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9664
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9665
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9666
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9667
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-9668
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
